United States                            cnnn
               Environmental Protection                     EPA-600/7-82-015
               Agency                             APRIL 1982
&EPA        Research  and
               Development
               A COMPENDIUM


               OF SYNFUEL END-USE


               TESTING PROGRAMS
               Prepared for




               EPA Program Offices

               EPA Regional Offices
               Prepared by

               Industrial Environmental Research
               Laboratory
               Research Triangle Park NC 27711

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                 RESEARCH REPORTING SERIES


Research reports of the Office of Research and Development, U.S. Environmental
Protection Agency, have been grouped into nine series. These nine broad cate-
gories were established to facilitate further development and application of en-
vironmental technology. Elimination  of traditional  grouping  was consciously
planned to foster technology transfer and a maximum interface in related fields.
The nine series are:

    1. Environmental Health Effects Research

    2. Environmental Protection Technology

    3. Ecological Research

    4. Environmental Monitoring

    5. Socioeconomic Environmental  Studies

    6. Scientific and Technical Assessment Reports  (STAR)

    7. Interagency Energy-Environment Research and Development

    8. "Special" Reports

    9. Miscellaneous Reports

This report has been assigned to the INTERAGENCY ENERGY-ENVIRONMENT
RESEARCH AND  DEVELOPMENT series. Reports in this series result from the
effort funded  under the 17-agency Federal  Energy/Environment Research  and
Development Program. These studies relate to EPA's mission to protect the public
health and welfare from  adverse effects of pollutants associated with energy sys-
tems. The goal of the Program  is to assure the rapid development of domestic
energy supplies in an environmentally-compatible manner by providing the nec-
essary environmental data and control technology. Investigations include analy-
ses of the transport of energy-related pollutants and their health and ecological
effects;  assessments  of, and development of, control technologies for energy
systems; and integrated assessments of a wide range of energy-related environ-
mental issues.
                       EPA REVIEW NOTICE
This report has been reviewed by the participating Federal Agencies, and approved
for  publication. Approval does not signify that the contents necessarily reflect
the  views and policies of the Government, nor does mention of trade names or
commercial products constitute endorsement or recommendation for use.

This document is available to the public through the National Technical Informa-
tion Service, Springfield, Virginia 22161.

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                       600782035
                                              EPA-600/7-82-015
                                              APRIL 1982
            A COMPENDIUM OF
   SYNFUEL END USE TESTING PROGRAMS
                   by

     M. Ghassemi, S. Quinlivan and M. Haro
                 TRW
        ENVIRONMENTAL DIVISION
           Redondo Beach, CA 90278
         EPA Contract No. 68-02-3174
           Work Assignment No. 18
         Project Officer: J. McSorley

   Industrial Environmental Research Laboratory
Office of Environmental Engineering and Technology
       Research Triangle Park, N.C. 27711
               Prepared for:

 U.S. ENVIRONMENTAL PROTECTION AGENCY
      Office of Research and Development
           Washington, D.C. 20460

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                                  ABSTRACT


      This  "Compendium  of Synfuel End Use Testing Programs" provides informa-
 tion on major  recently-completed, current and planned synfuel end use testing
 projects.   The compendium  is  intended to promote flow of information among
 various synfuel  testing programs, thereby reducing chances for duplication  of
 effort and enabling  design and implementation of cost-effective and systematic
 approaches to  the  collection  of appropriate environmental data in conjunction
 with on-going  and  planned  performance testing projects.   It is EPA's intention
 to update  this compendium  to  include results from current and future testing
 programs.

      Projects  described in the compendium involve testing of shale-derived
 fuels,  SRC-II .middle distillates, EDS fuel oils, H-coal  liquids and methanol-
 indolene mixtures  in various  equipment such as utility boilers, steam genera-
 tors,  diesel engines (lab-scale and full-scale), auto engines, and various
 other  combustors.

     A  separate  "data  sheet"  is devoted to each of the major projects covered.
 In  general, each data  sheet provides the following information on a project:
 type of fuel tested  (both synfuel and the reference fuel), test equipment used,
 test site,  test  objectives, sponsoring agency, contractor, test conditions,
 environmental  monitoring,  project status, summary of results, and references.
 A table summarizing the information in the data sheets and an overview of the
 synfuel testing programs are also included.

     Based  on  the data  presented in this compendium, the thrust of the synfuel
 testing program which has  been carried out to date has been to assess equip-
 ment performance and fuel  handling characteristics.  Where some emissions
 monitoring  has been conducted, such efforts have been limited in scope and
 have primarily emphasized  measurement of criteria pollutants (NOX, SOX, par-
 ticulates,  etc.).  Essentially no data have been collected on emissions of
 non-criteria/non-regulated  pollutants.

     Published reports  on  various testing efforts and discussions with test
sponsors/contractors are the sources of data for the compendium.  Agencies/
organizations providing input include DOD, DOE, NASA, EPRI, private synfuel
developers, and engine  manufacturers.

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                                  CONTENTS

Abstract	      ii
Tables 	       v
Acknowledgments	      vi
    1.0  Introduction and Objectives of the Document 	       1
    2.0  Data Base Used and Data Presentation	       2
    3.0  Overview of Synfuel Testing Programs	      15
Appendix - Data Sheets on Individual Projects	    A-l
    Test 1.  Combustion Demonstration of SRC-II Fuel Oil in a
    Tangentially-Fired Boiler	    A-l
    Test 2.  Combustion and Emission Characteristics of Coal-Derived
    Liquid Fuels 	    A-6
    Test 3.  Characterization and Combustion of SRC-II Fuel Oil.  .  .  .    A-10
    Test 4.  Catalytic Combustion of Coal-Derived Liquid Fuels ....    A-14
    Test 5.  Gas Turbine Combustor Performance on Synthetic Fuels.  .  .    A-17
    Test 6.  Solvent Refined Coal Burn Test	    A-24
    Test 7.  Test and Evaluation of Methanol in a Gas Turbine System .    A-27
    Test 8.  Effect of Fuel Bound Nitrogen on Oxides of Nitrogen
    Emissions From a Gas Turbine Engine	    A-30
    Test 9.  Shale-Derived Fuel Oil Engine Suitability Investigation .    A-34
    Test 10.   Fuel  Property Effects on Combustion Performance	    A-37
    Test 11.   Shale Oil Fuel Particulate Emissions Measurement ....    A-42
    Test 12.   Diesel Engine Test	    A-44
    Test 13.   Navy CVA-60 Boiler Test	    A-48
    Test 14.   Navy DDG-15 Boiler Test	    A-53
    Test 15.   Navy FF-1040 Boiler Test	    A-61
    Test 16.   Evaluation of Shale-Derived JP-5 Type Fuel in an
    Allison T63-A-5A Engine	    A-67
    Test 17.   Development of Alternate Sources of JP-5 Fuel, Endurance
    and Emission Tests of a T63-A-5A Engine Using a Tar Sands Derived
    JP-5	    A-73
    Test 18.   U.S.  Army's Energy and Synthetic Fuels Program .....    A-80
                                     i i i

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                         CONTENTS  (Continued)


 Test  19.   Evaluation  of  Military  Fuels  Refined  From  Paraho-II
 Shale Oil	A'83
 Test  20.   Evaluation  of  Fuel  Character  Effects  on  F101  Engine
 Combustion System	A~94
 Test  21.   Evaluation  of  Fuel  Character  Effects  on  J79 Smokeless
 Combustor	A"97
 Test  22.   Evaluation  of  Fuel  Character  Effects  on  J79 Engine
 Combustion System	A-100
 Test  23.   Fuel  Character Effects  on Current, High  Pressure  Ratio,
 Can-Type  Turbine  Combustion Systems	A-103

 Test  24.   Low  NO   Heavy  Fuel  Combustor  Concept	A-106
                X
 Test  25.   Low  NOV Heavy  Fuel  Combustor  Concept	A-110
                /\
 Test  26.   Low  NO   Heavy  Fuel  Combustor  Concept	A-117
                X
 Test  27.   Low  NO   Heavy  Fuel  Combustor  Concept	A-123
                X
 Test  28.   Low  NO   Heavy  Fuel  Combustor  Concept	A-127
                X
 Test  29.   Small Scale Combustion  Testing of Synthetic Fuels. .  .  .   A-135

 Test  30.   Evaporative Emissions From Vehicles Operating on
 Methanol/Gasoline Blends  	   A-144
 Test  31.   Experimental Results Using Methanol and  Methanol/
 Gasoline  Blends as Automotive Engine Fuel. . 	   A-146

 Test  32.   Fleet Trials Using  Methanol/fiasoline  Blends	A-151

 Test  33.   Gasohol  Fleet  Operations  	   A-155

 Test  34.   Evaporative Emissions From Methanol/Gasoline  Blends.  .  .   A-157

 Test  35.   Performance Evaluation  of Alcohol-Gasoline Blends in
 Late  Model Automobiles 	   A-159

 Test  36.   Determination of Individual Aldehyde  Concentrations in
 The Exhaust of a  Spark Ignited Engine Fueled by Alcohol/Gasoline
 Blends	A-162

 Test  37.  Methanol As a Boiler Fuel	A-164

 Test  38.  Characterization of Emissions From Methanol and
 Methanol/Gasoline Blended Fuels	A-167

Test  39.  Comparative Mutagenicity of Combustion Emissions  of a
 High  Quality No.  2 Diesel Fuel Derived  From Shale  Oil and a
 Petroleum-Derived No.  2 Diesel Fuel	A-173

Test  40.  Report  on the Methanol-Powered Bank of America Vehicle
 Fleet in San Francisco and Los Angeles	A-176

Test  41.  Advanced Combustion Systems for Stationary Gas Turbine
Engines	A-178

                                  iv

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                            CONTENTS (Continued)
    Test 42.   Advanced Combustion Systems for Stationary Gas Turbine
    Engines	A-186
    Test 43.   Evaluation of NOX Emission Characteristics of Alcohol
    Fuels for Use in Stationary Combustion Systems	A-197
    Test 44.   The Control of Nitrogen Oxide Emissions From Package
    Boilers	A-204
    Test 45.   Impact of Gasohol  on Automobile Evaporative and Tail-
    pipe Emissions	A-209
                                   TABLES
Number
  1.      List of Organizations/Individuals Providing Information Used
         in the Development of the Compendium	
  2.      Synfuels-Combustion System Combinations Tested and Emissions
         Monitored 	       4
  3.      On-Going Synfuel  Testing Programs 	      11
  4.      Tentative Synfuel  Testing Programs	      14

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                               ACKNOWLEDGMENTS


     Gratitude Is expressed to the EPA Project Officer, Mr.  Joe McSorley, for
suggesting the subject study and for his advice and guidance during the course
of the effort.

     This compendium is based on information and documents provided to the
study by individuals/organizations engaged in synfuel  characterization and end
use testing; those on the project staff wish to express their gratitude to the
supporting individuals/organizations,  particularly to  those  listed in Table 1,
to whom the project is deeply indebted.

     Special thanks are due to Mrs.  Monique Tholke for typing the manuscript
and for her invaluable secretarial  support to the project.   Mr.  Robert Scofield
and Mrs.  Anne Takata assisted in the preparation of data sheets  on the projects
covered.
                                     VI

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               .0  INTRODUCTION AND OBJECTIVES OF THE DOCUMENT
     A recently-completed synfuel utilization background study  identified a
great need for better coordination among various agencies involved in synfuel
end use testing programs so as to promote more systematic approaches to the
collection of environmental data in connection with such programs and to
reduce chances for duplication of effort.  This compendium of synfuel end use
testing programs, which has been developed per recommendation of the back-
ground study, is intended as an information source on major recently-completed,
on-going, and planned synfuel  end use testing programs.   The dissemination of
the document among agencies/organizations engaged in various aspects of synfuel
production, testing, utilization, and regulation, coupled with holding regular
symposia/workshops on synfuel  utilization and end use testing, should greatly
enhance coordination and flow of information among various programs and, in
the long run, contribute to the goal  of more rapid establishment of an environ-
mentally acceptable commercial synfuel  industry in the U.S.  It is EPA's inten-
tion to periodically update this document to include the results from current
and future testing programs.
 M.  Ghassemi  and R.  Iyer, "Environmental  Aspects of Synfuel  Utilization", EPA
 Report No.  EPA-600/7-81-025, March 1981.

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                 2.0   DATA BASE USED AND DATA PRESENTATION


      Information  presented in this document on the recently-completed, on-going
 and  planned  synfuel  testing programs has been obtained from published documents
 and  via  telephone calls and/or interviews with organizations involved in the
 testing  programs.  The key individuals/agencies providing most of the reports
 and  data used  in  this document are listed in Table 1.

      A separate  "data sheet" has been devoted to each project covered in this
 compendium to  permit  periodic updating of the document to include additional
 projects and incorporation of further results from on-going studies.  The data
 sheets are grouped into four categories, covering projects for which the key
 sponsors/participants are Electric Power Research Institute (EPRI), Department
 of Defense (DOD), Department of Energy (DOE), and Miscellaneous agencies (e.g.,
 EPA).  Data sheets are presented for a total of 45 projects, of which 7 are in
 the  EPRI-sponsored category, 16 in the DOD category, 13 in the DOE category,
 and  9 in  the Miscellaneous category.

     Where data have been available,  each data sheet provides the following
 information on a test project:   type  of fuel tested (both synfuel and the re-
 ference  petrofuel, where indicated),  test equipment used, test site, test
 objectives, sponsoring agency,  contractor, test conditions, environmental
 monitoring, project status,  summary of results, and references (where a report
 or reports have been published  on a project).

     A summary of the data contained  in the data sheets is presented in Table
2.   Tables 3  and 4 present brief descriptions of some of the recently initiated
and tentatively planned  synfuel  testing programs.

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                TABLE 1.   LIST OF  ORGANIZATIONS/INDIVIDUALS  PROVIDING  INFORMATION
                              USED IN  THE DEVELOPMENT  OF  THE  COMPENDIUM
 Electric Power Research Institute
 3412 Hillview Drive
 Palo Alto, CA  94303
  Mr. Al Dolbec

 Air Force Wright Aeronautical
 Laboratory, Aero Propulsion Laboratory
 Wright-Patterson AFB/POSF
 Dayton, OH  45433
  Mr. Charles Delaney

 Navy Air Propulsion Center
 P. 0. Box 7176
 Trenton, NJ  08628
  Mr. C. J. Nowack

 David W. Taylor Naval Ship R&D Center
 Code 2705
 Annapolis, MD  21402
  Mr. Carl A. Hershner

 Army Mobility Equipment Research and
 Command Center - Attn:  DRDME-GL
 Ft. Belvoir, VA  22060
  Mr. F. Schaekel

 U.S. Air Force HQ AFESC/RDV
 Tyndall AFB
 Tyndall, FL  32403
  Major J. Tom Slankas

 DOE, Bartlesvllle Energy
 Technology Center
 P. 0. Box 1398
 Bartlesville, OK  74003
  Mr. Dan Gurney

 DOE, Conservation and Solar Energy  Div.
'Washington, D.C.  20585
  Mr. Gene Ecklund

 DOE, Office of Coal Utilization
 Fossil Energy Research Center
 Washington, D.C.  20454
  Mr. John Fairbanks
DOE, Laramie  Energy Technology Center
P.  0. Box 3395
Laramie,  WY  82071
  Dr. R.  Poulson

DOE, Pittsburgh Energy Technology
Center, Analytical Chemistry Division
Pittsburgh, PA  15236
  Mr. Curt White

National  Aeronautics and Space
Administration
Lewis Research Center
21000 Brook Park  Drive
Cleveland, OH 44135
  Mr. Rick Niedzwiecki

EPA, Special  Studies Branch
Industrial Environmental Research Lab.
Research  Triangle Park, NC  27711
  Mr. G.  Blair Martin

EPA, Motor Vehicle Emission Laboratory
2625 Plymouth Road
Ann Arbor, MI 48105
  Mr. Robert  Garbe

EPA, Combustion Research Branch
Industrial Environmental Research Lab.
Research  Triangle Park, NC  27711
  Mr. G.  Blair Martin

EPA, Office of Environmental
Engineering and Technology
Industrial Environmental Research Lab.
Research  Triangle Park, NC  27711
  Mr. W.  S. Lanler

EPA, Mobile Sources Laboratory
Research  Triangle Park, NC  27711
  Mr. Frank Black
Southwest Research  Institute
Automotive Research Division
6220 Culebra  Road
San Antonio,  TX  78284
  Mr.  Charles T. Hare

Southwest Research  Institute
Mobile Energy Division
6220 Culebra  Road
San Antonio,  TX  78284
  Mr.  John A. Russell

U.S. Department  of Transportation
Systems Center
Kendall Square
Cambridge, MA  02142
  Mr.  Joe Sturm

U.S. Department  of Energy and
Coordinating  Research Council
Atlanta,  GA  30309
  Mr.  Al  Zingle

Carson Associates for
Bank of America
4117 Robertson Boulevard
Alexandria, VA  22309
  Mr.  Gavin McGurdy

Energy and Environmental Research
Corporation
8001 Irvine Boulevard
Santa  Ana, CA  92705
  Mr.  Dave Pershing

Ford Motor Company
Scientific Research Laboratory
Dearborn, MI   48121
                                               Vulcan Cincinnati, Inc.
                                               2900 Vernon Place
                                               Cincinnati, OH  45219
                                                Mr. R. W. Duhl

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TABLE 2.   SYNFUELS-COMBUSTION SYSTEM  COMBINATIONS TESTED AND  EMISSIONS  MONITORED
Test No. Agency Synfuel
1 EPRI SRC-II fusl oil
2 EPRI SRC-II fuel oil
H-Coal
EDS oil
3 EPRI SRC-II fuel oil
4 EPRI SRC-II, H-Coal
Reference Fuel
No. 6 fuel oil
No. 6 and No. 2
fuel oils
No. 2 and No. 5
fuel oil
No. 2 diesel
fuel
Combustion System
Tangentially-fired
utility boiler
Scaled-down
utility boiler
Babcock & Wilcox
package boiler
Three catalytic
reactors
Emissions Monitored
NOX, CO, THC, S03,
POM, particulates,
particle size, par-
ticulate composition
NO, C02, CO, S02,
S03, THC, smoke,
particulates, par-
ticle size
NOX, CO, C02, S02,
hydrocarbons, 02,
and dust
NO and CO
General Conclusions
• No adverse boiler performance effects
with SRC-II fuel.
• NOX emissions nominally 70% higher than
No. 6 fuel.
t Higher fuel nitrogen content of SRC-II
fuels produced higher NO emissions than
reference fuels.
• NO emissions from H-Coal and EDS liquids
were lower than SRC-II.
• No unique differences in combustion or
emission characteristics of SRC-II fuel
blends.
t NOX emissions consistent with fuel nitro-
gen content.
• Combustion performance of SRC-II fuel oil
was similar to No. 2 and No. 5 fuel oils.
• Coal-derived liquids can be burned cata-
tytically but SRC-II, and to a lesser
dearee H-Coal , appeared to degrade reactc
EPRI
 EPRI
Hydrogenated
shale oil and
various liquid
fuels for SRC-I,
H-Coal, EDS,
and SRC-II
Solvent refined
coal
No.  2 distillate
fuel
Full-scale and
sub-scale turbine
combustors
NOX,  CO, UHC, par-
ticulates, and
smoke
                             Bituminous  coal     Utility boiler
 EPRI
                     Jet-A  fuel,
                     natural gas,
                     metHanoi
                    Two utility gas
                    turbines
                                        NOX, S02. C02,  par-
                                        ticulates, particu-
                                        late composition
                      NOX,  CO, S02, THC,
                      POM,  sulfates, par-
                      ticulates, aldehydes,
                      opacity
  performance significantly as evidenced by
  higher CO emissions.
i  NOX emissions were consistent with  fuel
  nitrogen content.

•  A selected number of  coal liquids and
  shale oil fuels can  be  used in current
  turbines.
• Emission levels of CO,  UHC, and particu-
   lates for  synfuels were about the same as
   for No.  2  fuel - not.significant.
•  Significant  quantities of FBN are con-
   verted  to  NOX causing emissions  higher
   than EPA limits.

•  The boiler stayed much cleaner  with SRC
    than with coal,  producing an equivalent
    boiler efficiency as coal at full  load.
•   The quantity of SRC  flyash was 10 to  15S
    of that of coal  flyash with no bottom ash
    accumulation from SRC.
 •   Particulates,S02 and NOv emissions from
    SRC were all under EPA limits.

 •  Methanol  is  a suitable fuel  for gas  tur-
    bines;  turbine performance and  NOX and
    particulate emissions are improved over
    the other fuels.
                                                                                                                             (Continued)

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                                                                  TABLE 2.    (Continued)
             Test No.  Agency
    Synfuel
                     Reference  Fuel
                    Combustion  System
                                          Emissions Monitored
                                                                                                General Conclusions
                        DOD
                        DOD
                10      DOD
(Ji
                11       DOD
                12      DOD
              13-15     DOD
                16      OOD
                                 Shale-derived
                                 JP-5  and  blends
                                 with  petroleum
                                 JP-5
                                 Shale-derived DFM
                                                     Petroleum JP-5
                                 JP-5  from  oil
                                 shale,  coal, and
                                 tar  sands
                                 Shale  fuel  oil
Shale-derived
diesel fuel
                                 Shale-derived  DFM
Oil shale-derived
JP-5 fuel
                                                      Petroleum diesel
                                                      fuel
                                                      (MIL-F-16884G)
                     Jet-A,  JP-5,
                     diesel  marine
                     fuel ,  leaded
                     gasoline,  and
                     blends  of  the
                     above
                     Petroleum diesel
                     fuel  marine
                     (DFM)
Petroleum
distillate
                                                      Petroleum DFM
Petroleum-
derived JP-5
fuel
                                         DOD  helicopter
                                         engine:   Allison
                                         T63-A-5A  turbo-
                                         shaft
                                         U.S.  Navy  LM2500
                                         turbine  engine
                    Two high tempera-
                    ture/pressure
                    research combustors
                    Steam generator
                    diesel  engine
Lab-scale diesel
engine
                                                                         3 different types
                                                                         of prototype steam
                                                                         generators
DOD helicopter
engine:  Allison
T62-A-5A turbo-
shaft
                                          NOX,  CO, C02, and
                                          THC
                                          NOX,  CO, THC, and
                                          smoke
                      NOX,  CO,  UHC,  and
                      smoke
                      Particulates  and
                      particulate  compo-
                      sition
NOX, THC,  and smoke
                                                              NOX, S02, CO, C02,
                                                              THC, 02, and smoke
NOX> CO,  and THC
t  NOX emissions increased with increasing
   fuel  nitrogen content;  conversion effi-
   ciency was about 45%.
•  No significant effects  were noted on en-
   gine  performance or CO, C02, and THC
   emissions due to the presence of high
   levels of fuel bound nitrogen.

•  Combustor and engine operating  character-
   istics were identical  when using marine
   diesel or DFM shale oil; thus,  DFM shale
   oil would be suitable  for use in LM2500
   engines.
9  NOX emissions followed  fuel nitrogen con-
   tent; CO and THC levels were essentially
   the same for both fuels.

»  In all performance areas, the synfuels
   correlated in the same  manner as petro-
   leum-derived fuels except for NOX emis-
   sions from the shale oil fuel.
9  Smoke formation was dependent on hydrogen
   content;  combustion efficiency, CO,  and
   UHC depend more on higher boiling point
   components than fuel viscosity.

«  No significant differences between parti-
   culate emission products measured in the
   study from the combustion of DFM or  shale
   fuel  oil.

c  There was no significant difference  in
   performance or emissions with the shale-
   derived fuel.

•  There were no significant differences in
   measured pollutant emissions resulting
   from the combustion of petroleum DFM or
   shale-derived DFM on the CVA-60, DDG-15,
   and the FF-1040 boilers.  In each case,
   S02,  NOX, and smoke were below levels set
   by EPA.

«  Performance, CO, and THC emissions were
   equivalent for both fuels.
(  NOX emissions followed  fuel nitrogen con-
   tent.
                                                                                                                                                        (Continued)

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                                                            TABLE  2.    (Continued)
Test No. Agency
17 DOD
18 DOD

19 DOD
Synfuel
Uniflned kerosene
derived from tar
sands
Distillate, avia-
tion, turbine, and
diesel fuels de-
rived from coal , tar
sands and oil shale
Shale-dHved JP-5,
JP-8, and DFM
Reference Fuel
Petroleum-
derived JP-5
fuel
Various petro-
leum-derived
fuels

JP-5, diesel
fuel No. 2, and
Jet A
Combustion System
DOD helicopter
engine: Allison
T63-A-5A turbo-
shaft
Wide variety of
Army power-plant
systems

DOD helicopter
engines : Allison
T-63 gas turbine,
Emissions Monitored
NOX, CO, and IJHC
Various pollutants

CO, NOX, unburned
hydrocarbons , and
smoke
General Conclusions
• Uni fined kerosene was a satisfactory sub-
stitute for petroleum JP-5 fuel.
• NOX emissions were slightly higher when
using unifined kerosene than with JP-5.
• Product quality of manv svnfuels tested
and other results are described in indivi-
dual abstracts.

• The carbon monoxide emissions followed the
same trend as combustion efficiency. At the
lower power points, DFM showed slightly
20-22
          DOD
                                       13 petroleum de-
                                       rived fuels: JP-4,
                                       JP-8, diesel No.
                                       2 & various blends
                                                           Detroit Diesel  6V-
                                                           53T. LDT-465-1C
                                                           diesel engine,
                                                           Teledyne-Continenta1!
                                                           AVDS-1790 diesel
                                                           engine, and Detroit
                                                           Diesel 3-53
General Electric
F101 turbofan, J79-
17C turbojet, and
J79 turbojet engines
NOX, CO, UHC, and
smoke
   higher  CO  than JP-5 and Jet A.  There were
   no fuel  property effects on the emissions of
   unburned hydrocarbons and NOX.  The flame
   radiation  and exhaust smoke levels for the
   synfuels were higher than those of Jet A and
   are attributed  to  differences  in hydrogen
   content.
•  The shale JP-5  in  the DD6V-53T engine showed
   a 6% average loss  1n maximum  power output
   when compared  to  the reference diesel fuel
   which approximates the  6.5% oower loss obser-
   ved in the same engine  with petroleum-derived
   JP-5.  The shale-derived JP-5 and DFM per-
   formed in the CUE-1790  engine like  similar
   petroleum-derived fuels.  Evaluation of  DFM
   from shale in the LDT-465-1C  engine resulted
   in no difference between the  maximum power
   produced by this fuel  and that of a oetroleum
   No. 2 diesel fuel.
•  The results from the 210-hour test  in  the DD
   3-53 engine are indistinguishable from those
   that may  result from tests with conventional
   petroleum-derived diesel fuel with similar
   properties.
»  Shale-derived fuels met virtually every mili-
   tary specification with the  exception of the
   failure of  JP-5 to meet copper corrosion re-
   quirement and DFM to meet maximum pour point
   limit.

e   In all  three engines,  fuel hydrogen content
    strongly  affected smoke and  NOX emissions.
    NOX emissions  were also highly dependent
    upon combustor  operating  conditions.
                                                                                                                                              (Continued)

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TABLE  2.   (Continued)
Test No. Agency Synfuel Reference Fuel
23 DOE * 12 petroleum-
derived fuels:
JP-4, JP-8, and
various blends

24 DOE SRC-II middle Low quality resi-
distillate dual oil, and
petroleum refe-
rence distillate
fuel
25 DOE SRC-II middle Petroleum
distillate distillate



26 DOE SRC-II middle Low quality
distillate residual oil and
distillate fuel



27 DOE SRC-II middle Low quality
distillate residual oil,
petroleum refe-
rence distillate
oil , and natural
gas



28 DOE SRC-II middle Low quality
distillate residual oil,
petroleum refe-
rence distillate
oil







Combustion System Emissions Monitored
TF41 turbofan com- NOX, CO, UHC, and
bustor smoke



Combustor sized NOX, CO, C02, THC,
for use with in- and smoke
dustrial gas
turbine

Various combustor NOX, smoke
concepts



Seven combustors NOX> smoke, CO, un-
of varying designs burned HC
for use in utility
gas turbine engines


Combustors for use NOX, CO, THC, smoke
in utility gas
turbine engines






Experimental com- NOX, CO, UHC, smoke
bustor for use
with utility gas
turbine engines








General Conclusions
• All pollutant emissions measured were
highly dependent upon ooerating conditions.
CO and smoke levels were also strongly
affected by hydrogen and aromatic content
of fuels.
a The combustor was able to achieve low NOX
with all fuels.
• CO and smoke varied directly with rich
zone equivalence ratio and inversely with
lean zone equivalence ratio.
» Values of NOX were reduced for the smaller
diameter quench zone and increased for
larger diameter quench zone.
c Rich-lean burn stage combustion system can
meet EPA emission standards.
» A lean-lean combustor has potential for
achieving ultra-low NOX emissions with
distillate, residual or other fuels con-
taining up to 0.25% (wt.) fuel nitrogen.
CO and smoke met program goals from this
combustor also.
• Lean-lean combustor NOX emission levels
were higher than emission goals using SRC-
II fuel. CO emissions remained low using
SRC-II fuel, while no smoke was detectable
and UHC levels were negligible throughout
these tests.
• Rich-lean combustor NOX emissions appeared
to reach a minimum below the NOX emission
goal for rich primary zone condition.
a Five combustors have been found adequate
for further development: rich-lean diffu-
sion flame venturi quench, burner ceramic
lined pipe lean burner, multiannular swirl
burner, Rolls-Royce combustor, and lean
catalytic combustor. These meet NOX emis-
sion limits set by EPA with petroleum
distillate and/or residual oils.
s SRC-II fuel NOx emissions were close to
meeting EPA limits in only two combustors:
rich-lean diffusion and ceramic lined pipe
lean burners.
                                                            (Continued)

-------
                                                              TABLE  2.   (Continued)
CO
- - — • — — — — 	
Test No. Agency Synfuel
29 DOE SRC-II middle and
heavy distillate,
fuel oils & three
blends of the
above








30 DOE *


31 DOE *




32 DOE *



33-35 DOE *




36 DOE *





37 Vulcan *
Cincinnati

Reference Fuel
No. 2 and No. 6
petroleum- based
fuel oils










Indolene and 10%
methanol/90%
indolene
Unleaded gasoline
and methanol/
indolene mixtures


10% methanol/90%
gasoline blends


Ethanol ,
methanol, and
gasoline blends


Indolene, indo-
lene/methanol
blends and
ethanol/indolene
blends

No. 6 residual
oil, natural gas,
and methanol
Combustion System
A 20-hp Johnston,
fire-tube boiler











Two light duty
vehicles

Auto engines (10)




Auto engines (7)



Fleet vehicles




Pontiac 4-cylinder
modified engine




Small scale boiler
test stand and a
49 HW utility
Emissions Monitored
NOX, S02, CO, HC
and polynuclear
aromatic hydro-
carbons









Evaporative emissions
(hydrocarbons and
methanol )
NOX> CO, THC. alde-
hydes, and methanol



NOX, CO, and eva-
porative emissions
(HC and methanol)

Evaporative and
tailpipe hydrocarbon
emissions


Total aldehydes and
specific organics




NO,,, CO, and
aldehydes

General Conclusions
« The levels of NOX and 503 produced were pro-
portional to the amount of nitrogen and
sulfur in the fuel.
• There appear to be two sources of trace or-
ganics in the exhaust gases: small amounts
of the fuel Itself not burned during combus-
tion, and the products of combustion. For
the petroleum fuels, n-alkanes and polynuclear
aromatic hydrocarbons are seen in the exhaust
gas; for the SRC-II fuels, the alkanes are
absent or present at very low levels, and
polynuclear aromatic hydrocarbons not seen in
the petroleum exhaust gases are present.
• Using methanol 10% blend increased evapo-
rative emissions by 130% for short term
use and 220% for long term use.
• Aldehyde, methanol, and hydrocarbon emis-
sions increased with higher concentration
of methanol 1n the fuel.
• CO was reduced by the addition of methanol
to the base fuel .
B Data show consistent reduction in CO
emissions with use of methanol blends.
• Significant increases in evaporative
emissions with methanol blends.
• 75% increase in evaporative emissions with
methanol blends over a straight gasoline.
* Emissions were lower for vehicles fueled
with gasohol but data was inadequate to
conclude a significant difference.
t Total aldehydes increased 25% in going from
indolene to ethanol/indolene and methanol/
indolene blends.
» Formaldehyde is the largest component of
the total aldehydes (up to 90 mole percent
of the total).
• In the utility boiler, methanol NOX levels
were 7-14% of those measured during resi-
dual oil combustion.
                                                              boiler
CO emission levels of methanol were less
than 100 ppm and generally  less than those
observed for the residual oil.
Aldehyde emissions during methanol com-
bustion were generally less than 1 opra.
                                                                                                                                          (Continued)

-------
                                                           TABLE  2.    (Continued)
Test No.
38
39
Agency Synfuel
Ford *
Motor
Co.
DOT Shale-derived DFM
Reference Fuel
Methanol ,
indolene, and
blends\
No. 2 diesel
fuel
Combustion System
Ford 400 CID engine
and 1975 Ford LTD
with 400 Cin engine
VW Rabbit engine
Emissions Monitored
Total hydrocarbons
and specific
organics
NOX, CO, THC, parti-
culates, Ames test
 propane >
   isopropanol > alcohol  mixture > methanol.
   Although there was considerable scatter in
   the data, aldehyde concentrations  were
   around 10 ppm for methanol.
   NO emissions for all  fuels decreased with
   increasing fraction of flue gas recircula-
   tion.
   CO and hydrocarbon emissions were  always
   below 50 ppm and smoke was not observed
   for any fuel.
                                                                                                                                          (Continued)

-------
                                                           TABLE  2.    (Continued)
Test No.   Agency       Synfuel
Reference Fuel
                    Combustion System     Emissions Monitored
                                                                                                                    General Conclusions
   44       EPA
   45       EPA
No.  5 residual
oil, natural  gas,
and methanol
Indolene and
ethanol blends
Industrial  water-
tube and fire-tube
boilers
Two light duty
vehicles
                                                                                   NO,,
                                                                                   ethanol,  and  evapo-
                                                                                   rative emissions
Flue gas recirculation was capable of re-
ducing NOX emissions  during methanol com-
bustion.
Methanol NOX emissions were significantly
lower than during residual oil  combustion
and were also less than  during  natural
gas combustion.

The addition of ethanol  to indolene  re-
duced tailpipe emissions of THC and  CO,
but increased NOX.
Use of gasohol increased evaporative
emissions substantially.
  Because of the unavailability of synfuels, the fuels used in some of these programs were not "true" synfuels  (e.g.,  methanol-derived  from natural
  gas was used instead of coal-derived methanol).  These studies, however, are included in this report because  they were  conducted  to show what
  might  be expected from the combustion of actual synfuels in the indicated combustion systems.

-------
                                 TABLE  3.    ON-GOING  SYNFUEL  TESTING  PROGRAMS
 Sponsoring Agency
      Test Fuels
                               Schedule
                                 Project Description
EPA.  Motor Vehicle
Emission Laboratory
EPA, Combustion
Research Laboratory
Shale-derived dlesel  fuel
and SRC-II fuel  versus
National  Average Baseline
Diesel Fuel,  and Mobil-M
gasoline

EDS and H-coal  liquids
                           SRC-II  fuel
SRC-II middle and heavy
distillates, EDS middle
distillates, and shale-
derived No.  2 fuels
DOE, Bartlesville
Energy Technology Center;
Contractor/test site:

A.  General  Electric,
    Erie, PA
    Transamerica
    Delaval,
    Oakland,  CA
SRC-II middle distillate
and oil shale distillate
H-coal liquids


SRC-II middle distillate
    1981  to       Volkswagen  Rabbit diesel engine testing.  Emissions
   late 1982      monitored to  Include particulates, N0x, C0/C02> hydro-
                  carbons, and  aldehydes.
 Late 1981  to     Large  standing diesel engines and a GE research engine.
September 1982    Emissions monitoring includes collection of particulates.

     1982         Electronically controlled internal combustion engine at
                  Southwest Research  Institute, San Antonio, TX.

November 1981-    North  American package boiler and Caterpillar Model D334
  April  1982      stationary  diesel engine testing.  Package boiler repre-
                  sents  small-to-medium sized fire-tube boiler for indus-
                  trial  and commercial applications; boiler can be equipped
                  with low NOX  burner which may be tested with synfuels.
                  The stationary diesel represents medium-sized industrial
                  and commercial engine used for backup power generation,
                  pumping and other applications.  Emissions monitored in-
                  clude  particulates, NO , CO/CO,, SO,, and hydrocarbons.
    1981-         Testing  of  GE  EDI-8, 8-cylinder "V" configuration, 5344
  early 1982      cu.  in.  standing diesel engine for electric power, rail
                  and  marine  applications.  Parameters evaluated include:
                  starting ability,  injection timing, fuel rate variation
                  effects  and internal engine temperatures.  Emissions
                  monitored include  0,, CO/CO,, NO  , SO,, HC, H9SO., and
                  particulates.      i       *    x    '       ^  q

  January to      Limited  testing with single cylinder diesel engine.
  April 1982      Emissions monitored include 0,,, C0/C02> NO , SO,,, and HC.

    1981-         Testing  of  Delaval DSR 46, 6-cylinder in-line configura-
  early 1982      tion,  28,600 cu. in. standing diesel engine for electric
                  power, compressor  and marine aoplications.  Performance
                  parameters  being evaluated include starting ability,
                  precombustion  chamber effects, ignition delay, and other
                  engine parameters.  The engine has been operated at full
                  load using  a pre-mixed blend of 60% SRC-II liquid and
                  40%  diesel  oil which had been injected into the combus-
                  tion chamber with  no modification of the engine, followed
                  by  increasing  proportions of SRC-II liquid up to 100^.
                  Emissions monitored include 0,, CO/CO,, NO , SO,, THC,
                                                                        and smoke.
                                                                                                                  x'
                                                                                                                    (Continued)

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                                                                  TABLE  3.    (Continued)
                  Sponsoring Agency
      Test Fuels
                               Schedule
                                Project Description
                 C.  A. 0. Little,
                     Beloit, WI
SRC-II middle distillate
ro
                 D.  Energy  and  Envi-
                     ronmental Research,
                     Springfield, OH
                  E.  Acurex,
                     Shoreham-by-the-Sea,
                     England
                  DOE,  Conservation  and
                  Solar Energy Division
                  DOE, Office of Coal
                  Utilization
                                             Various  H-coal and  EDS
                                             liquids
Shale-derived distillate
oil
                                             Shale  oil  residuals
Various shale- and coal-
derived fuels

SRC-II distillates and
shale-derived JP-5 and
DFM mixed with powdered
carbon, sawdust, or other
cellulosic material
Coal-derived methanol
and gasohol

SRC-II and shale-derived
fuels
  1981-1982       Fairbank-Morse 38 to 8-1/8, 6-cylinder opposed  piston
                 design,  3108 cu. in. standing diesel engine for electric
                 power  and marine applications, compressors and  pumps
                 being  tested.  Parameters evaluated include effects of
                 load variations, combustion pressure vs.  time,  and engine
                 delay.   Emissions monitored include C0/C02, NO, N0?,  S02,
                 SO^, HC, PAH, particulates, and oxidants.
  March to       Testing  of  Fairbanks piston engine at NAVSSES test faci-
November 1982    lity,  Philadelphia, PA.  Emissions monitoring to include
                 gaseous  pollutants  and collection of sizable  (i.e.,  5 g)
                 quantities  of particulate matter.

    1981-        Testing  of  Superior 6-cylinder in-line configuration
  early 1982     turbo-charged 4120  cu. in.  standing diesel engine for
                 use in compressors, pumping and electrical power genera-
                 tion.   The  purpose  of  the  tests is  to comoare  engine
                 performance parameters during synfuel and  conventional
                 fuel  combustion.  Tests  with  shale-derived distillate
                 oil and a  baseline  No. 2 diesel  fuel  include SASS train
                 sampling for PAH and  particulates.   Other emissions
                 monitored  include  CO,  HC,  N0x, and  smoket.

    1981-        Testing of A.f'.E.  Allen  BSC 128  6-cylinder,  in-line
  early 1982     configuration,  5101 cu.  in. standing diesel  engine for
                 marine, pumping, compressor and  electric power applica-
                 tions.  Tests include injection,  starting, combustion
                 duration and steadiness.  Emissions monitored  include
                 C0/C02, NO , N02,  THC, and smoket.

  1978-1984      Auto engine dynamometer testing  being conducted at
                 SwRI.   Particulates,  NOX, CO/C02, hydrocarbons, and
                 aldehydes being monitored.
  1981  to  ---     Slurry/fuel project involving diesel engine testing.
                 Particulates, NO , and other emissions being monitored.
  1981 to  ---     Testing in 1,000 fleet vehicles; program currently
                 constrained for lack of fuel samples.

  1980 to  ---     Medium speed  diesel engine  testing  conducted  by  SEMT-
                 Pielstich, Paris;  Baumester Wain, Copenhagen;  rirandi
                 Motori  Trieste, Trieste;  and Selzer of Switzerland.
                                                                                                                                       (Continued)

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                                               TABLE  3.    (Continued)
 Sponsoring Agency
      Test Fuels
                               Schedule
                Project Description
DOE, Office of Coal
Utilization
  (Continued)
DOE, Pittsburgh Energy
Technology Center
Air Force/Navy/FAA
(under the direction of
Capt.  H. Cewell. USAF
Civil  Engineering and
Services Center, Tyndall
AFB)

Department of
Transportation and
Rutgers University

Sandia Laboratories
Bank of America
SRC-II middle distillates,    1980 to ---
a 2.9 to 1  blend of SRC-II
middle and heavy distillate,
and shale-derived fuels
SRC-II middle distillate      1981 to ---
Biomass fuel, H-coal,           1981  to
Exxon Donor Solvent,          October 1982
and shale fuel oils
Shale-derived JP-4 and         1982-1984
JP-8
Coal- and shale-derived       1981 to 1982
dlesel fuel
Petroleum-derived synfuel     1981 to —
simulation fuels, with
higher hydrocarbon/aroma-
tic content than conven-
tional fuels

Methanol/gasollne blends      1980 to ---
Program conducted at Norwegian  Technical  Institute  in
various ships.
Continuation of low NOX fuel  combustor concept  program
(see Tests 24-28).   Several  combustors to be  tested  by
Westinghouse; staged combustor to be tested at  several
operating loads at  Detroit Diesel  Allison;  testing of  5
combustors planned  at GE.

Continuation of small scale combustion of synthetic  fuels
program (see Test 29).   A 20-hp firetube boiler is to  be
tested with the above synfuels using No.  2  and  No. 6 fuel
oils as a baseline.  The purpose of the program is to
assess the possible environmental  impact of substituting
synfuels for petroleum in utility and industrial  boilers.

Testing of CF-6 and CFM-56 turbine engines.   Emissions
monitoring to include NOX, SOX, CO/CO?, hydrocarbons,  and
particulates.  Limited Ames mutagenicity testing  to  be
performed on particulate samples, as well as  photochemi-
cal reactivity testing on exhaust gases.
Testing of a recently-designed and constructed one cylin-
der diesel engine, including collection of particulates
and other combustion products.

Testing being conducted in single cylinder diesel  systems
and auto/truck engines from Cumins Engine Co.  Emphasis
on measurement of flame fronts and other engine/burn
parameters.  Limited emissions monitoring performed.
Testing being conducted in blends ranging from 2 to 18%
methanol in fleet vehicles, with emphasis on blends of 2
and 4%.  CO, NO, and unburned hydrocarbons being moni-
tored.
 The schedules and some of the activities listed under the  Project  Description  are  somewhat tentative and subject to modification.

fTest results obtained to date have Indicated that  the performance  of  the  shale-derived fuel was comparable to the No. 2 diesel
 fuel, although easier atomization and lower fuel  consumption  were  observed  with  the  shale-derived fuel.

'The test engine satisfactorily burned residual  shale oil when heated  above  the wax melting point and with agitation; emissions
 were comparable to a No.  2 diesel fuel  except for  an Increase of cylinder deposits of fine carbon.

-------
                              TABLE 4.  TENTATIVE SYNFUEL  TESTING  PROGRAMS
Sponsoring Agency
Fuels to be Tested
                Time  Period
          Project Description
Army, MERADCOM,
Ft. Belvoir, VA
Navy Air Propulsion
Test Center,
Trenton, NJ

AF Wright Aeronautical
Lab, Aero Propulsion
Laboratory, Wright-
Patterson AFB,
Cincinnati, OH

EPRI
Diesel fuels and
other synfuels (high
aromatic content
fuels, low lubricity
fuels)

Various shale-derived
fuels
                1982  to  - —
                1982 to - —
Various
fuels
shale-derived   1982 to  1983
Various liquid and
solid synfuels, in-
cluding shale-derived
heavy and middle
residuals, and
methanol
                Fall  1982
                   1986
Development of accelerated fuel  quali-
fication test procedures, including
matrix of specific Army equipment com-
ponents and candidate fuels; project is
part of Army Alternative Fuels Program.

Testing of synfuels in various test
burners and aviation equipment.
Engine augmenter tests and whole engine
tests on 3 engines; emissions monitor-
ing for NO , C0/C09, and hydrocarbons.
Testing of synfuels in
engines, turbines, and
various diesel
boilers; limited
                                                                 emissions  monitoring for SOX, NO
                                                                 C0/C09,  09 and/or particulates.
 Tests pending receipt of synfuel  samples.

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                  3.0  OVERVIEW OF SYNFUEL TESTING PROGRAMS
     Based on the data presented in the test program data sheets and summarized
in Table 2, and on the discussions which have been held with a number of syn-
fuel developers, trade associations and potential major users of synfuels, the
following are some general observations on the status, nature, and thrust of
the synfuel testing programs:

     •  Since the primary use of synfuel products is expected to be as combus-
        tion fuels, nearly all synfuel end use testing programs have involved
        evaluation of fuel suitability for use in existing combustion systems
        (auto engines, industrial/utility boilers, turbines, etc.).

     •  Reflecting the developmental status of the synfuel technologies, the
        thrust of the synfuel testing programs which have been carried out to
        date has been to assess equipment performance and fuel handling charac-
        teristics.  Where some emissions monitoring has been conducted, such
        monitoring efforts have been limited in scope and have primarily em-
        phasized measurements of gross parameters such as particulates, NOX,
        SOX, etc., emissions.  The limited scope of the monitoring programs
        has also been in part due to:  (a) an absence of a clear definition of
        the specific environmental data which would be required on synfuel
        products by regulatory agencies (e.g., by EPA's Office of Pesticides
        and Toxic Substances in connection with the Premanufacturing Notifica-
        tion Section of the Toxic Substances Control Act); and (b) lack of a
        standard protocol for testing for environmental data acquisition.

     •  Most of the synfuel end use testing programs have been, or are being,
        conducted/funded by DOD, EPRI, and DOE.  The programs of these organi-
        zations have, respectively, emphasized use of shale oil products  in
        military aviation and ship equipment;  use of coal liquids  in  boilers;
        and testing of methanol and methanol-gasoline blends  in auto  engines
        and use of coal and shale-derived fuels  in  stationary  diesel  engines.

     •  Many synfuel developers appear to have in-house synfuel testing pro-
        grams; the emphasis of these programs  is primarily on synfuel charac-
        terization and not on end use testing.  The data generated in these
        programs are generally considered company proprietary and are not
        published.

     •  Nearly all the refined shale oil products which have been used in com-
        bustion testing to date have been from the refining of the 100,000
        barrels of Paraho shale oil at Sohio's Toledo (Ohio) refinery.  Since
                                      15

-------
this refining operation apparently did not involve the use of typical
unit operations which would be employed in commercial refining of
shale oil, the refined products from this operation are not considered
to be representative of products from any future commercial refining
of the shale oil.

To date the synfuel  testing effort has been severely curtailed by
lack of adequate quantities of fuel  for testing.  Some of the planned
testing programs will utilize shale  oil products from the forthcoming
refining of 50,000 barrels of shale  oil by Union Oil for the Defense
Fuels Supply Center.

Synfuel products (specially the shale-derived materials) which will
be marketed in the future will most  likely be blends and not 100 per-
cent pure products.   The use of 100  percent pure products in the
initial synfuel testing programs has been justified on grounds that
it would simulate a possible "extreme/worst" case condition (at least)
from the standpoint of emissions and their environmental implications).

Although the performance testing is  continuing, the limited data which
have been gathered to date indicate  that the tested synfuels are
generally comparable to petrofuels and do not present any unique pro-
blems from the standpoint of fuel  handling and combustion characteris-
tics.  Potential problems with long-term fuel storage stability
(observed with certain shale- and petroleum-derived middle distillates)
and durability and material compatibility problems (e.g., possible
increase in the engine wear with methanol  use) are under investigation.

The very limited data which have been collected on the emission of
criteria pollutants (particulates, NOX, SOX, etc.) indicate that,
except for a higher emission of NOX  with synfuels having a higher con-
tent of fuel-bound nitrogen, the emissions of such criteria pollutants
are similar for both synfuel and their petrofuel counterparts.   For
most synfuels, however, no data have been collected on emissions of
non-criteria pollutants such as polycyclic organic matter (ROM's),
primary aromatic amines, nitropyrenes and other organics.  There is
also very limited data on overall  trace element composition of emis-
sions.
                             16

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                                  APPENDIX

                   DATA  SHEETS  ON  INDIVIDUAL  PROJECTS


                                   TEST  1

 COMBUSTION DEMONSTRATION OF SRC-II FUEL OIL  IN  A TANGENTIALLY-FIRED BOILER


1.   FUELS TESTED (see Table A-l)

    Synfuel:  SRC-II distillate fuel oil

    Reference fuel:  No. 6 fuel oil

2.   TEST EQUIPMENT (See Figure A-l)

    Combustion Engineering, Inc.,  tangentially-fired boiler with a rated

    steam flow of 450,000 Ib/hr.

3.   TEST SITE

    74th Street Generating Station of the Consolidated Edison Company of New

    York.

4.  TEST OBJECTIVES

    t  Demonstrate the  use of  SRC-II fuel oil in a utility boiler system of
       a design typical of a large  fraction of utility generation capacity,
       yet consistent with the limited availability of the synthetic liquid
       fuel;

    •  Compare the boiler performance with that obtained firing conventional
       petroleum fuel oil;

    •  Assess the potential for minimizing NOX emissions from high nitrogen,
       coal-derived liquids through choice of operating conditions;

    •  Obtain comparative information on the quantity and composition of
       particulates and organic compounds present in the combustion products
       of SRC-II fuel oil and  No.  6 petroleum fuel oil under comparable boiler
       operations.

5.   SPONSORING AGENCIES

    Electric Power Research Institute         New York State ERDA
    3412 Hillview Avenue                                   '
    Palo Alto, CA  94304                      U'S- Department of Energy

    EPRI Project Manager:  W.C. Rovesti        Consolidated Edison Comoany
    Telephone No'.   415-855-2519             of New York


                                     A-l

-------
                   TABLE A-l.   AVERAGE  FUEL PROPERTIES
:=rz:
API Gravity at 60°F
H20 % by Volume
Sulfur % by Weight
Carbon % by Weight
Hydrogen % by Weight
Nitrogen % by Weight
Oxygen % by Weight
Heating Value (Btu/lb)
Ash % by Weight
Viscosity (sec.)
No. 6 Fuel Oil
25.0
0.20
0.24
87.02
12.49
0.23
--
19,200
0.02

SRC II Fuel Oil
11.0
0.28
0.22
85.50
8.86
1.02
4.38
17,081
0.02

 Saybolt Universal  at 100°F                                   40

Viscosity (sec.)
 Saybolt Universal  at 122°F         300  -  700

Pour Point (°F)                        95                     -30

Flash Point (°F)                      >200                     150


Note:  Because of sulfur content  limitations in  New York  City, the No.  6 oil
       utilized  by Con Edison  exhibits properties  close to  a  No. 5 residual
       oil.
    CONTRACTOR

    KVB Incorporated
    246 North  Central Avenue
    Hartsdale,  New  York  10530

    Principal  Investigators:  B.F. Piper
                             S. Hersh
                             W. Nazimowitz

    TEST CONDITIONS

    Tests conducted at full load (^450 klb/hr steam flow rate), half  load,

    and three-quarter load.  Tests also included variations designed  to

    reduce NOX emissions, including reducing the number of burners used and
    redistributing admitted air (see Table A-2).
                                    A-2

-------
                              ECONOMIZER
                              SAMPLE POSITION
         BOILER, N«_J 22
    74th STREET  STATION

Figure A-l.   Boiler 122 Cross Section
                A-3

-------
                            TABLE A-2.   SRC  II  FUEL OIL -  EMISSIONS TEST  SUMMARY
TEST
NO.
II-l
II-2
II-3
II-4
II-5
II-6
II-7
II-8
II-9
11-10
11-11
11-12
11-13
11-14
11-15
11-16
11-17
DATE
9/11/78
9/11/78
9/11/78
9/12/78
9/12/78
9/12/78
9/13/78
9/13/78
9/13/78
9/13/78
9/14/78
9/14/78
9/14/78
9/J4/78
9/15/78
9/15/78
9/15/78

Full
Full
Full
Full
Full
Full
Half
Half
Half
Half
Full
Full
TEST CONDITIONS
Load/Baseline
Load/Low NOx/6 Burner
Load/Low NOx/6 Burner
Load/Baseline
Load/Lou NOx/8 Burner
Load/Low NOx/8 Burner
Load/Baseline
Load/3 Burners
Load/4 Burners
Load/Baseline
Load/Baseline*
Load/Low NOx/6 Burner
3/4 Load/Low NOx/6 Burner
3/4 Load/Low NOx/J-14
Half
Half
Full
Load/Low N0x/N30
Load/Upper/Lower Pattern
Load/Low NOx/6 Burner
BOILER PERFORMANCE GASEOUS EMISSIONS
STM FLOW SH TEMP BOILER SO NO, NO NOx
EFF.
(klb/hr) (°F) (%) (ppm) (ppm (ppm (Ibs
Dry @ Dry @ N02/
3% 02) 3% 02) lOSBti
435
430
425
430
440
436
251
246
240
230
477
472
340
305
243
245
492
955
925
955
962
938
930
935
939
948
905
955
943
900
890
870
865
935
0.3,0.9 2
85.7 1
1
-
-
86.3
2
87.8 1
1
2
86.0 0
0
2
-
87.1 0
0
86.2 0
258
212
236
298
228
232
261
287
279
301
239
194
159
186
188
188
175
.341
.280
.311
.391
.299
.305
.345
.378
.368
.397
.313
.255
.211
.244
.247
.247
.230
02 CO
(%) (ppm)
j
3.6
3.7
3.4
3.9
2.5
2.7
4.7
4.1
5.0
4.8
2.7
3.5
3.9
3.1
4.1
4.0
2.7
6
9
9
9
17
24
5
15
19
6
25
65
12
16
6
5
22
PARTICULATE EMISSIONS
THC
(ppm) (lb/106 Btu)
2
1
1
2
2
2 .017. .016. .016, (.021)**
1
0
1
0 . 007 , . 006
1 .018, .019
0
0
-
1 .009,. 010
2
2 .024,. 026
* Boiler setup not typical of usual baseline operation - refer to Section 7
** (Value) from ASME in-stack thimble

-------
8.  ENVIRONMENTAL MONITORING

    Nitric oxides, oxygen, carbon monoxide, polycyclic organic matter, total

    unburned hydrocarbons, sulfur trioxide, particulate mass and particle

    size distribution.

9.  PROJECT STATUS

    This effort is an element of EPRI's ongoing R&D program directed at gain-

    ing operating experience in utility boilers firing various liquid and

    solid coal-derived synthetic fuels.  Additional tests are planned in

    various-scale equipment using fuels from the solvent refined coal (SRC-t

    and SRC-II), H-Coal, Exxon EDS and other advanced liquefaction processes
    as adequate fuels from these processes become available for testing.

10. RESULTS

    The results of the test program are highlighted below and summarized in
    Table A-2.

    •  No major operational problems or adverse boiler performance effects
       encountered with SRC-II fuel oil.  Nitrogen oxide emissions nominally
       70 percent higher than with the No. 6 fuel oil currently used by
       Consolidated Edison.  Reductions in NOX levels on the order of 35 per-
       cent demonstrated through combustion modifications with both fuels.

    •  Particulate mass emissions were lower for the SRC-II fuel  oil than
       for the No. 6 fuel oil.  At full load, the SRC II fuel oil  particulate
       emissions exhibit a bi-modal size distribution; many were <0.05 microns
       and others were >0.1 microns.  Particulate mass composition is also
       reported.

    t  Total hydrocarbon emissions were <3ppm under all  operating consitions
       with both fuels.

    »  Total POM for both fuels were low, <6xlO~6 lb/106 Btu.

11. REFERENCE

    B.P.  Piper, et al., "Combustion Demonstration of SRC-II Fuel  Oil in a
    Tangentially Fired Boiler", Final Report, May 1979,  EPRI Projects 1235-5
    and 1412-2, prepared by KVB, Incorporated, Hartsdale, New York.
                                    A-5

-------
                                  TEST 2

    COMBUSTION  AND  EMISSION CHARACTERISTICS OF  COAL-DERIVED LIQUID FUELS


1.   FUELS TESTED

    Synfuels:   SRC-11  fuel  (5  ratios  of medium  and  heavy  boiling range com-

    ponents);  H-Coal  (syncrude mode of operation, full-range distillate); EDS

    (full-range distillate).

    Reference  fuel:  No.  6  and No. 2  petroleum-derived  fuels.

2.   TEST EQUIPMENT

    An 80-HP firetube boiler  system extensively modified  to simulate a utility

    boiler including an indirectly fired  air  preheater, a scaled-down utility

    boiler burner,  radiation  shields  to increase the  thermal  environment in

    the combustion  chamber, and  capabilities  to implement staged combustion.

3.   TEST SITE

    KVB Combustion  Research Laboratory, Tustin, California.

4.   TEST OBJECTIVES

    •  Develop an understanding  of the effect of compositional  variations of
       a particular coal  liquid  and the resulting effects on the implementa-
       tion of combustion modifications for pollutant emission  reductions;
    •  Establish an understanding of  the  difference in  the combustion and
       emission characteristics  of coal liquids produced  from various pro-
       cesses—specifically the  SRC-11 Process, the Exxon Donor Solvent
       Process, and the H-Coal Process;

    •  Establish a  standard test method,  using  a small-scale facility, to
       predict the  response to changes in operation of  smoking  tendency,
       CO, and NOX.  This will be used to differentiate various fuel pro-
       perties and  the performance of each fuel in  a  large variety of com-
       mercial  boilers.

5.   SPONSORING AGENCY

    Electric Power  Research Institute (EPRI)
    Power Generation  Program
    Advanced Power  Systems  Division
    Palo Alto,  California


                                     A-6

-------
    EPRI Project Manager:  W.C. Rovesti
    Telephone No:  415- 855-2519

6.  CONTRACTOR

    KVB Inc.
    Irvine, California

    Principal investigators:  L.J. Muzio, J.K.  Arand
    Telephone No. 714-641-6200

7.  TEST CONDITIONS

    A systematic set of experiments was conducted which investigated the

    following variables:   excess air with single stage combustion, burner

    stoichiometry with two-staged combustion, firing rate, air preheat tem-

    perature, fuel temperature (viscosity), and atomizer (mechanical, steam),

8.  ENVIRONMENTAL MONITORING

    Oj' CO^, CO, NO, SOp, S0~, unburned hydrocarbons, smoke number, parti -
    culate size distribution.

9.  PROJECT STATUS

    Completed.

10. RESULTS

    Emissions from the various synfuels combustion tests in this program are

    summarized in Table A-3.  A brief description of other emission test
    results are shown below.

    SRC II

        Particle size data indicate that SRC-II fuel blends produced finer-
    size-distribution particulate than No.  6 oil, the exception being SRC-II
    heavy distillate component under single-stage combustion.   Measured SO?
    emissions were consistent with the fuel  sulfur content, with nearly all
    fuel sulfur emitted as S02-  An $03 concentration of 2 ppm for heavy
    distillate component  was the only SRC-II test detecting this pollutant.
    Reference fuel  No.  6  oil burn test also emitted 2ppm $03.   Unburned
    hydrocarbon concentrations measured for SRC-II combustion  tests ranged
    from 1  to 14 ppm.

    H-Coal
        Average particle size of particulate matter proved to be less than
    0.4 microns.   Measured S0£ emissions were consistent with fuel  sulfur
    content in that the S02 emissions were the lowest of all  synfuels tested.


                                    A-7

-------
                                         TABLE A-3.  SUMMARY OF EMISSIONS
I
CO
Fuel Type
No. 6 oil
*
SRC-II 5.75/1
SRC-II Medium
Distillate
*
SRC-II 2.9/1
*
SRC-II 0.4/1
SRC-II Heavy
Distillate
SRC-II Heavy
Distillate (210°F
Fuel Temperature)
H-Coal
EDS Fuel
Fuel Ash
Content
lb/106 Btu
0.

0.

0.

0.

0.
0.


0.

0.
0.
0045

0017

0012

0041

018
034


034

0095
0045
Single-Stage
°2
3.7

3.8

4.0

3.3

3.4
3.3
3.8

—

2.8
2.8
Part.
lb/106
Btu
0.024

0.014

0.011

0.012

0.031
0.029
0.037

—

0.022
0.022
NO
ppm @
3% 02
270

400

476

361

509
381
392

—

247
259
Two-Stage (Low 02)
°2
3.6

3.2

3.1

2.9

3.3
3.5


3.2

3.1
3.2
Part.
lb/106
Btu
0.037

0.022

0.017

0.015

0.039
0.184


0.065

0.037
0.0184
NO
ppm @
3% 02
199

303

307

308

279
249


339

226
270
Two-Stage (High 0?)
°2
...

4.9

4.2

4.5

4.7
4.6


—

4.95
5.15
Part.
lb/106
Btu
...

0.020

0.012

0.017

0.039
0.090


—

0.034
0.0154
NO
ppm @
3% 02
— «= —

382

342

371

375
269


—

202
216

     *
      Middle  to  heavy distillate ratio.

-------
    SOs was not detected,
    4 ppm.

    EDS
Unburned hydrocarbon emissions ranged from 1  to
        Two particle sizing tests showed the average particle size to be less
    than 0.4 microns.  Measured S02 emissions were consistent with the fuel
    sulfur content.  EDS flue gas samples showed no detectable levels of 563.
    Measured unburned hydrocarbon emissions were 1 and 2 ppm.

11- REFERENCE

    Muzio, L.J.  and J.K Arand.  Combustion and Emission Characteristics of
    Coal-Derived Liquid Fuels.  EPRI AP-1878, Electric Power Research Insti-
    tute, Palo Alto, Calif., 1981.
                                     A-9

-------
                                  TEST  3
              CHARACTERIZATION AND COMBUSTION OF  SRC-II  FUEL  OIL

1.    FUELS TESTED
     Synfuel:   SRC-II  fuel  oil,  5.75/1 blend of medium/heavy  distillate with
     nominal  boiling  range  of 350-850°F.
     Reference fuels:   No.  2 fuel oil, No.  5 fuel  oil.
2.    TEST EQUIPMENT
     Babcock  & Wilcox  FM  boiler  (Model FM  1070) designed to the following
     specifications:
                      Steam Capacity        50,000 Ibs/hr
                      Design Pressure       1050  psig
                      Operating  Pressure    150 to 1000  psig
                      Heating Surface       4410  Ft2
                      Furnace Volume        1065  Ft^
                      Furnace Dimensions    20' x 6'-4"  x 8'-6*'
                      Fuel                  Nat.  gas/No.  6 fuel oil/
                                             No.  2 fuel  oil.
     Modifications  to  the boiler facility  included:
     •    Connection of an existing air heater to  supply  combustion air
         at 400°F.
     •    Revamping of  the boiler controls  to permit biasing of the fuel/
         air ratio.
     •    Installation of a  high pressure mechanical return flow pumping &
         atomization system.
     •    Various piping and pump modifications.
     •    Installation of various gas and particulate analysis  instrumentation.
3.   TEST SITE
    Alliance Research Center of
     Babcock and Wilcox Co.
    Alliance, Ohio

                                    A-10

-------
4.  TEST  OBJECTIVES

    •   To obtain  a  detailed  analysis  and  characterization  of a  portion
        of the  same SRC  II distillate fuel  oil  product scheduled  for
        subsequent  field testing  in a utility  boiler.

    •   To carry  out  combustion  tests in  a  modified  water  tube  package
        boiler  using  a conventional circular burner  (to provide data
        for comparing emissions  and combustion  performance of the test
        fuels).

    •   To determine  the effectiveness of using a  dual  register burner
        in order  to control  NOX  emissions from  the combustion of  SRC II
        fuel  oil  in the  test boiler.

5.  SPONSORING AGENCY

    Electric Power Research Institute
    Fossil  Fuel  and  Advanced Systems Division
    Palo  Alto, California

    Project Manager: W.C.  Rovesti
    Telephone  No:      (415) 855-2519

6.  CONTRACTOR

    The Babcock  &  Wilcox Company
    Alliance Research Center
    Research and Development Division
    Alliance,  Ohio

    Principal  Investigators: W.  Downs and  A.J.  Kubasco

7.  TEST  CONDITIONS

    The test program was conducted in three phases.   The  first involved  de-

    tailed fuel  analyses of SRC  fuel  oil,  No.  2 fuel  oil, and  No.  5 fuel  oil

    The second involved combustion tests on the FM  boiler using  a  conven-

    tional  circular  burner.  Operating variables  included excess air, load,

    and burner register settings.  Four  fuel  atomizers were tested: Y-jet,

    Racer,  T-jet,  and Return flow mechanical  atomizer.  The third  test  in-

    volved combustion studies with a Babcock  & Wilcox dual  register burner

    on  the FM  package boiler.

8.  ENVIRONMENTAL  MONITORING
     NOX, CO,  C02,  S02>  HxCy,  02,  and stack capacity.   Dust loadings were
     taken  by EPA's  Method  5.
                                     A-11

-------
9.  PROJECT STATUS
    Project completed;  final  report dated June,  1979.
10. RESULTS
    NOX emissions and combustion  performance were the  principal  variables
    studied.   The quantifiable  aspects  of combustion performance are stack
    opacity and CO measurements.   The  interactions between minimum excess
    air, flame appearance,  flame  impingement, burner stability,  and furn-
    ace rumble played a role  in assessing combustion performance.   In this
    context,  the influence  of the various operating parameters upon NOX
    sions and combustion performance are  listed  as follows:
    «  N0xemissions increased moderately  with increases  in 02-
    •  Oxidation of fuel-bound  nitrogen in the SRC fuel  oil was
       the predominant  factor attributing to NOX emissions.
    •  Combustion performance for SRC  fuel  oil was similar to No.  2
       and No. 5 fuel  oils.
    e  At full boiler load, the type of fuel  atomizer  had  a substan-
       tial  affect upon NOX emissions and combustion performance.   At
       reduced loads,  the type  of fuel  atomizer  had a  lesser impact
       on either variable.
    e  Combustion performance improved  slightly  at reduced loads.
    •  Burner register  settings had little affect on NOX emissions.
    •  Burner register  settings had a substantial  impact upon combus-
       tion  performance at minimum excess air conditions.
    e  Combustion and boiler  efficiency were similar for both SRC
       fuel  oil  and No.  5 fuel  oi.
    Several  conclusions were  drawn regarding emissions and combustion of SRC
    fuel  oil:
    •  Although  the capability  to. burn  SRC fuel  oil in such a way  as
       to limit  NOX emissions to  less than  EPA's proposed  New Source
       Performance  Standard of  0.5 pound  N02/million Btu was not demon-
       strated,  it  appears that this new  limit could be  met on the
       typical wall-fired utility  boiler  by the  use of two stage com-
       bustion and  by the proper matching of burner and  atomizer designs.
    •  The ineffectiveness of the  dual  register  oil burner to control
       NOX resulted from a design  error which prevented  controllability
       over fuel-air mixing.  Schedule  restraints  negated  the opportunity
       to correct that  problem.
                                   A-12

-------
    •  The fuel  nitrogen in SRC fuel  oil  appears to oxidize more readily
       than does the fuel  nitrogen in other fuels.

    9  The interaction between fuel and air mixing appears to have a pre-
       dominating influence upon NCL  formation and emissions.  Most of
       the potential for reducing NDX emissions lies in the control of fuel
       nitrogen  oxidation with a lesser potential  existing for reducing
       thermally derived NCL.  Therefore, the influence of air preheat
       temperature and the flame temperature parameter Ha/Sc should have
       only a minor impact upon NOX emissions.  Boiler load may have some
       influence upon NOX emissions and control.

    •  SRC fuel  oil produced no significant smoking tendencies.  Flame
       Appearance, as well as stack opacity, with SRC fuel oil was slightly
       better than with No. 5 fuel oil.

    §  Neither combustion efficiency  nor boiler efficiency were affected
       by conversion from No. 5 fuel  oil  to SRC fuel oil.

    §  Particulate emissions limits in compliance with EPA's proposed
       New Source Performance Standards of 0.03 pound/million Btu can be
       easily attained with SRC fuel  oil.

11.  REFERENCE
    Downs, W. and A.J. Kubasco.  Characterization and Combustion of SRC II
    Fuel Oil.  EPRI FP-1028, Projects 1235-3,-4, 1412-1.  Prepared for the
    Electric Power Research Institute, Palo Alto, California, June, 1979.
                                    A-13

-------
                                  TEST 4
               CATALYTIC COMBUSTION OF COAL-DERIVED LIQUID FUELS

 1.  FUELS TESTED
    Synfuels:  SRC-II fuel oil blend (a blend of middle and heavy distillates
    in a 5:1 ratio with a nominal boiling range of 360-700°F); H-coal  fuel
    oil (from distillation of atmospheric overhead products, nominal boiling
    range was 300-500°F).
    Reference fuel:  No. 2 petroleum-derived diesel fuel.
 2.  TEST EQUIPMENT
    Three different catalytic reactors were combustion-tested with  the three
    fuels:   (1) a high dispersion washcoated precious metal catalyst made  by
    UOP, (2) a high platinum loading catalyst made by Acurex, and (3)  a  pro-
    prietary monolith with platinum applied by Acurex.
 3.  TEST SITE
    Acurex Combustion Laboratory
 4.  TEST OBJECTIVES
    •  Determine the combustion characteristics of coal-derived liquids  in
       catalytic reactors.
    •  Evaluate the potential  poisoning effects of coal-derived liquids  on
       state-of-the-art catalytic reactors.
5.  SPONSORING AGENCY
    Electric Power Research Institute
    Power  Generation Program
    Advanced Power Systems Division
    Palo Alto,  California
    Project  Manager:   L.C.  Angello
    Telephone No.:   415-855-2873
                                    A-14

-------
6.  CONTRACTOR
    Acurex Corporation
    Energy and Environment Division
    Mountain View, California
7.  TEST CONDITIONS
    This test program included a series of screening tests and a durability
    test.  Screening tests were run with all three catalytic reactors at a
    pressure of one atmosphere and over a range of equivalence ratios nomin-
    ally between 0.3 (fuel-lean) and 1.35 (fuel-rich).  Nominal operating
    conditions were for an air preheat of 800°F, reactor temperature of 2100°F,
    and reference face velocities between 20 and 80 fps at the measured pre-
    heat temperature and chamber pressure.
    A durability test series was also run using the UOP and H-Coal fuel oil.
    Durability tests were conducted at a pressure of three atmospheres.  The
    combustor inlet face velocity was decreased by a factor of three, but the
    residence time was increased by a factor of three.  Nominal reactor temp-
    eratures ranged from 2100-2370°F.
8.  ENVIRONMENTAL MONITORING
    CO and NOX
9.  PROJECT STATUS
    This effort was conducted during the period November 1978 to February 1980.
10. RESULTS
    The results of the screening tests are summarized in Table A-4.  In the
    durability test with H-Coal, catalyst deactivation became substantially
    evident after about 26 hours; CO emissions increased from a baseline of
    about 10 ppm to about 24 ppm.  After 40 hours on H-Coal, the combination
    was unstable and the reactor fractured.   At this point, combustion test-
    ing was terminated.
11. REFERENCE
    Chu, E.K., G.C. Snow, H. Tong.  Catalytic Combustion of Coal-Derived
    Liquid Fuels.  EPRI AP-1666, Electric Power Research Institute,  Palo
    Alto, January 1981.

                                     A-15

-------
TABLE A-4.  SUMMARY OF SCREENING TEST RESULTS


Reactor
UOP
Acurex Pt
Ac u rex Pt
on proprie-
tary mono-
lith


Reactor
UOP
Acurex Pt
Acurex Pt
on proprie-
tary mono-
lith

SRC II
100-200
250-800
Not
active

SRC
Combustion
Stable
Inactive
--

Lean
CO (ppmv)
H-Coal
50-100
50-100
80-200
Rich
II
FN
Conversion
17%
--
—

Combustion
Diesel
25-50
40-60

NO (ppmv) 15%
SRC-IIX H-Coal
390-440 140
450-590 140
Not 140-167
active
EO
Diesel
4-9
2-10

Combustion
H-Coal
Combustion
Stable
Inactive
Inactive

Diesel
FN FN
Conversion Combustion Conversion
30% Stable
__
—

—
—
—


-------
                                   TEST 5

            GAS TURBINE COMBUSTOR PERFORMANCE ON SYNTHETIC FUELS


1.    FUELS TESTED


     Synfuels:  the 18 synfuels tested are described in Table A-5 below.

                       TABLE A-5.  FUEL DESCRIPTION

Fuel #
1
2
2A
3
4
5
5A
6
7
8
9
9A
10
10A
10B
11
12
13
Name
SRC-I Light Organic Liquid
H-Coal (210-480°F)
H-Coal (300-500°F)
H-Coal (450-650°F)
H-Coal, ATM. Bottoms
EDS-Hydrogenated Recycle Solvent
Reprocessed EDS (W/0 650° + Fraction)
SRC-I Wash Solvent
SRC-I Recycle Solvent
SRC-II Middle Distillates
SRC-II Heavy Distillates
SRC-II Heavy Distillates (Second Batch)
SRC-II Blend (Medium)
3:1 Mixture - #2 Dist. & SRC-II Blend
1:1 Mixture - #2 Dist. & SRC-II Blend
Shale Oil - Paraho (Hydrogenated)
Shale Oil - Deashed
Shale Oil - Desulfurized
%N
0.29
0.15
0.16
0.33
0.61
0.08
0.04
0.35
0.69
0.91
0.98
0.94
0.91
0.23 Est
0.45 Est
0.33
1.82
1.63
%Ca
28
34
29
43
57
48
47
61
76
63
77
71
63
--
--
14
--
--
%H
12.18
11.32
11.19
10.03
9.27
9.95
10.16
9.23
7.74
8.83
7.13
7.22
8.70
11.6 Est
10.6 Est
12.80
11.4
12.2

 %H - Percent Bound Nitrogen
 %Ca- Percent Aromatic Carbon
 %\\ - Percent Hydrogen
                                    A-17

-------
     Reference fuel:  No. 2 petroleum distillate oil.

 2.   TEST EQUIPMENT

     Two combustors were used, including a full-scale Westinghouse  commercial

     unit (0.3 m diameter) typical of those used in Westinghouse  W-251  and

     W-501 combustion turbine engines and a half-diameter  (0.14 m)  version.

 3.   TEST SITES

     Full scale:  Westinghouse Combustion Turbine System Division Laboratory,

     Lester, Pennsylvania.

     Subscale tests:  Westinghouse Research and Development Center,  Pittsburgh,

     Pennsylvania.

 4.   TEST OBJECTIVES

     t   Identify problems that will arise in using these synfuels on  current
         engines.
     •   Determine fuel properties that lead to a fuel suitable for  current
         engines.
     «   Determine which synthetic fuels now available are  suitable  for  use.
     •   Determine combustor/engine improvements needed to  use the synthetic
         fuels that do not meet these specifications.

 5.   SPONSORING AGENCIES

     Electric Power Research Institute
     Power Generation Program
     Advanced Power Systems Division
     Palo Alto, California
     Project Manager:  A. Cohn
     Telephone No:   415-855-2519

6.   CONTRACTOR

     Westinghouse Electric Corporation
     Combustion Turbine Systems Division
     Long-range Development Department
     Concordville, Pennsylvania

     Subcontract support for fuel analysis was provided by Mobil  Research  and
     Development Corporation.

7.   TEST CONDITIONS

     Typical  combustor test conditions were as follows:


                                    A-18

-------
                                Full-scale Combustor      Subscale Combustor

     Inlet air temperature           600°F                    600°F

     Pressure Level                  8 ATM                    4 ATM

     Air Flow                        33 Ib/sec                1.5 Ib/sec

     Fuel/test                       2,000 gal                100 gal

8.   ENVIRONMENTAL MONITORING

     NOX, CO, C02, smoke, unburned hydrocarbons (UHC), particulates.

9.   PROJECT STATUS

     Testing was completed July 1980, and the final report is dated November
     1980.

10.  RESULTS

     NOv
     •  Figures A-2 and A-3 show NOX vs. burner outlet temperature curves de-
        rived  from subscale and full-scale tests.  Because of their high fuel-
        bound-nitrogen (FBN) content, the synfuels produced higher NOX emissions
        than No. 2 baseline fuel.  Each curve indicates the fuel type and
        number, and the percent weight FBN.  Detailed graphs of NOX response
        to each fuel under all test conditions are documented in the referenced
        report.

     0  Synfuels with hydrogen content greater than 10% (by wt.) and nitrogen
        content less than 0.2% should be satisfactory for engines of current
        design.

     Smoke

     •  Smoke  increased with increasing combustor burner outlet temperature.
        Level  of smoke was dependent on fuel quality; fuels of better quality
        (higher % HZ, lower aromaticity) tended to smoke less.  Smoke emissions
        may be a problem with some of the poorer fuels, especially at idle
        conditions.

     Other Emissions

     •  Particulates were measured during full-scale tests on H-Coal (fuel
        No. 2) and baseline fuel No. 2.  All measured concentrations were
        below  0.5 lb/106 ft.3, which is quite low.  It was concluded that
        particulate emissions are no different for coal derived and petroleum
        derived fuels.

     t  In all cases, CO emissions were below 100 ppm; measured results are
        shown  in Figure A-4.
                                     A-19

-------
o
     4UU
     360
     320
     280
     240
     200
     160
     120
     80
     40
NO 20IL (BASELINE FUEL!
H COAL PROCESS FUELS
SRC I PROCESS PRODUCTS
SRC II PROCESS FUELS
EDS PROCESS FUEL
HYDROGENATED SHALE OILS
                       //A\
      •JOO
                        SUBSCALE COMBUSTOR
                        INLET AIR TEMP. ~ 620°F
                        AIR FLOW 1.4-1.5 LBM/SEC
                        FUEL TEMP. 77°F
                        PRESSURE ~4 ATM
                _L
                                 _L
                   _L
                                                    _L
_L
               1100      UOO      1500      1700      1900      2100

                     AVERAGE OUTLET COMBUSTOR TEMPERATURE (°FI
                                              2300
Figure A-2.   NOX  Emissions  for Synthetic Fuels  and No.  2 Oil,
               Subscale  Combustor Tests
                                   A-20

-------
 X
O
z
      400
      360
      320
      280
      240
      200
      160
      120
       80
       40
          NO. 2 OIL (BASELINE FUEL)
          H-COAL PROCESS FUEL
          SRC-II PROCESS FUEL
          HYDROGENATED SHALE OIL
   % WT. FBN
-  FUEL NO.
        0
        900
                             I
                        FULLSCALE COMBUSTOR
                        INLET AIR TEMP. ~ 635°F
                        AIR FLOW ~ 30.5 LBM/SEC -
                        FUEL TEMP. 64-77°F
                        PRESSURE- 8 ATM
                           I	I	|	
     1100    1300   1500   1700    1900   2100   2300

  AVERAGE OUTLET COMSUSTOR TEMPERATURE (°F)
  Figure A-3.  NOX Emissions  for Synthetic  Fuels  and  No.  2  Oil,
              Full-Scale Combustor Tests
                               A-21

-------
8
    60
    50
    40
    30
    20
    10
-    D
           D  Coal Liquid Tests

           °  Surrogate Tests
        1100       1300      1500      1700      1900
                    Av. Outlet Combustor Temp, °F
                                                                2100
2300
          Figure A-4.   Baseline  CO Emissions With  No.  2 Fuel  Oil
                                       A-22

-------
     •  In general, unburned  hydrocarbon levels were found to be < 10 ppm.

     t  C02 data are  displayed in Figure A-5 for combustion  Information  only,


11.  REFERENCE

     DeCorso, S.M., P.W.  Pillsburn,  G.  Bauserman, P.R. Mulik, and T.R. Stein.
     Gas Turbine Combustor  Performance  on Synthetic Fuels, Volumes I and  II.
     EPRI AP-1623.  Prepared  for the Electric Power Research Institute,  Palo
     Alto, California,  November 1980.
    CXJ
   8
                                         ° Coal Liquid Tests

                                         0 Surrogate Tests
                                              I
1
         900       1100      1300      1500      1700      1900
                             Av. Outlet Combustor Temp, °F
        2100
2300
             Figure A-5.   Baseline C02 Emissions With No. 2 Fuel Oil
                                      A-23

-------
                                   TEST 6
                       SOLVENT REFINED COAL BURN TEST

1.   FUELS TESTED
     Synfuel:  Solvent Refined Coal (SRC) fuel.
     Reference fuel:  Bituminous coal.
2.   TEST EQUIPMENT
     Babcock & Wilcox F-type 22.5 MW power plant boiler using a specially
     designed dual register, water-cooled burner.
3.   TEST SITE
     Georgia Power Company's Plant Mitchell near Albany, Georgia.
4.   TEST OBJECTIVES
     9  To evaluate the shipping, handling, boiler-performance, and combustion-
        emission characteristics of SRC.
5.   SPONSORING AGENCY
     U.S. Department of Energy
     DOE project support:   Nueworth, M.G.
6.   CONTRACTOR
     Southern Company Services, Inc.
     Research and Development Department
     Birmingham, Alabama
     Project Managers:  Dr.  W.B. Harrison and Mr. S.R. Hart, Jr.
     Telephone No:  (205)  870-6011
     Many other organizations also provided technical support.
7.   TEST CONDITIONS
     Tests were run in three phases.  Phase I was to operate and test the
     boiler under normal  conditions firing coal.  For Phase II, new burners
     and pulverizer feeders  were installed, and the boiler was tested against

                                    A-24

-------
     firing coal.   During Phase III,  when SRC was fired,  hot air to pulverizers
     was closed off,  pulverizer spring pressure was reduced, and the boiler
     was tested for a third time.   For each phase, tests  were run at unit loads
     of approximately 7,  14, and 21  MWe.   Usually two tests, each of 4-hours
     duration,  were run at each load  in each phase (see Table A-6).
 8.   ENVIRONMENTAL MONITORING
     Particulates, S09, and NO  were  monitored using EPA  and ASME procedures.
                     £        X
     Also,  continuous monitors analyzed flue gas for opacity, SO^, NO ,  CO-,
     and 02-
 9.   PROJECT STATUS
     Project completed; final report  dated July 1979.
10.   RESULTS
     Boiler efficiency measurements  performed throughout  all phases of the
     burn test indicated that efficiency at full load was essentially the same
     when either SRC or coal was burned.   The boiler stayed much cleaner with
     SRC than with coal,  eliminating  the need for deslagging the burner  front
     or the use of soot blowers during the entire 18-day burn test.   Typical
     SRC em
     below.
SRC emissions and current EPA requirements (in lb/10  Btu)  are shown
                                         EPA
                                     Requirements     SRC
                    S02                  1.2          1.00
                    NOV                  0.7          0.45
                      J\
                    Particulates         0.1          0.04
     The quantity of fly ash generated while burning SRC was nominally 10 to
     15 percent of that generated when firing coal,  and bottom ash was vir-
     tually nonexistent.  Boiler conditions and emissions are summarized in
     Table A-6.
11.   REFERENCE
     Southern Services Company.   Solvent Refined Coal  Burn Test, Final Report.
     Prepared for the U.S. Department of Energy.  The Research and Development
     Department of Southern Services, Inc., Birmingham, Alabama, July 1979.
     214 pp.
                                     A-25

-------
                                    TABLE  A-6.  OPERATION AND EMISSIONS DATA
                                  Phase I
                                Phase  II
                                       Phase  III
3>
cr>
      Load,  MW
      Fuel Rate,  Ib/hour
      Excess  023  %
      Participate
      Loading In,
      lb/106  Btu
      Particulate
      Loading Out,
      lb/106  Btu
22.5   15      7.5
23,880 16,143  9,010
 4.7    6.0   11.0

 9.90  10.84   9.81

 2.30   0.46   0.11
21     14      7,5   21
20,676 14,784  9,510 20.065
 4.4    6.2   11.6    4.6

 7.39   9.09   8.96   4.72

 1.66   0.81   0.32   0.07
21      14      7.5   21
17,714 12,178  7,311 17,678
 6.0    7.5   11.3    6.2

 1.04   1.91   1.77   0.96

 0.90   1.42   0.93   0.04
Carbon in Ash, %
Carbon Efficiency, %
S02, lb/106 Btu
NOV, lb/106 Btu
X
Average Opacity, %
kWh/106 Btu
Average COo, %
13.9
97.70
1.94
1.01
41
78.05

14.5
97.47
2.15
0.46
18
78.67
8.88
19.5
97.07
2.44
0.89
7
67.85

22.33
98.00
1.20
0.49
30
79.30

20.6
97,18
1.57
0.47
22
75.81
8.
16.9
97.18
1.80
0.49
12
64.97
27
28.1
97.87
0.94
0.47
66
80.22

77.4
98.51
0.95
0.43
32
78.98

88.7
96.98
0.98
0.45
29
76.18
8.
89.4
97.07
1.06
0.42
15
65.77
76
74.8
98.60
0.93
0.46
40
78.88


       Secondary precipitator tests.

-------
                                   TEST 7

           TEST AND EVALUATION OF METHANOL IN A GAS TURBINE SYSTEM


1.    FUELS TESTED*

     Reference fuels:   distillate fuel  (Jet-A); natural  gas; and chemical  grade

     methanol derived from natural gas.

2.    TEST EQUIPMENT

     Two Turbo Power and Marine Systems, Inc. (TPM) gas  turbines combined  with

     an electric generator in a TP-4 Twin Pac configuration.

3.    TEST SITE

     SCE's Ellwood Energy Support Facility at Goleta, California.

4.    TEST OBJECTIVES

     •  Compare gas turbine emissions and performance characteristics operating
        on distillate, methanol, and natural  gas fuel.

     •  Evaluate the handling and storage of methanol.

     •  Compare maintenance requirements operating the  gas turbines on methanol
        or distillate fuel.

     •  Determine emissions operating the gas turbines  on distillate fuel  with
        and without water injection.

     •  Determine the performance and emissions operating the methanol fueled
        gas turbine with water injection.

     t  Determine the necessity of a lubricant additive  to the methanol fuel
        system.

5.    SPONSORING AGENCY

     Electric Power Research Institute
     Power Generation Program
     Advanced Power Systems Division
 Because of the unavailability of synfuels, the fuels used in some of these
 programs were not "true" synfuels (e.g., methanol-derived from natural  gas was
 used instead of coal-derived methanol).   These studies, however, are included
 in this report because they were conducted to show what might be expected from
 the combustion of actual synfuels in the indicated combustion systems.

                                    A-27

-------
     Project Managers:  R.L. Duncan and H. Schreiber
     Telephone No:  415-455-2502

 6.  CONTRACTOR

     Southern California Edison Company (SCE)
     Research and Development
     Rosemead, California
     Principal Investigators:  A.  Weir, Jr., W.H. Von Kleinsmid,  and E.A.  Danko,
     Emissions testing was performed by KVB, Inc., Irvine, California

 7-  TEST CONDITIONS

     Emissions were measured at base load (25 MW), 75 percent load  (18 MW),
     and 50 percent load (13 MW).

     The effects on gaseous emissions of using water injection for NO  control
                                                                     /\
     were also investigated.

 8.  ENVIRONMENTAL MONITORING

     NOX, NO, CO, C02, S02, total  hydrocarbons, particulates (including sul-
     fates and POM), aldehydes, and opacity.

 9.  PROJECT STATUS

     The methanol program was begun on 6/25/79 and was completed in 12/79.
     Report is dated 2/81.

10.  RESULTS

     The major emissions and performance results  are summarized  in Table A-7
     for baseload conditions.

11.  REFERENCE

     Weir, A.,  W.H.  VonKleinsmid,  and E.A.  Danko.   Test and Evaluation of
     Methanol in a Gas Turbine System.   EPRI AP-1712, Research Project 988-1.
     Prepared for the Electric Power Research Institute, Palo Alto, California,
     February 1981.
                                    A-28

-------
              TABLE A-7.  EMISSIONS AND PERFORMANCE RESULTS


N0xt
N02t
cot
Hydrocarbonst
Aldehydest
so2t
Particulates, lb/106 Btu
Solid
Condensible
Total POM, yg/SCM
Opacity, %
Heat rate, Btu/kW-hr
Fuel consumption @ 24 MW
Liquid (GPM)
Gas (SCFM)
Methanol
(dry*)
45
10
70
10
1.8
0

0.003
0.011
1.22
0
11,722

82.4
—
Jet
(dry*)
207
10
50
5
—
13

—
—
—
0
11,863

37.4
—
A
(wet*)
56
10
60
5-6
0.05
13

0.008
0.017
1.07
0
12,014

38.0
— -
Natural
(dry*)
124
50
175
216
10.6
0

—
—
—
0
11,863

—
4,860
Gas
(wet*)
65
40
220
280
12.1
0

—
—
—
0
—

—
---

 "Dry"  and "wet"  refer to water injected  and  nonwater injected.
Measured at 15 percent 02,  dry,  ppm.
                                    A-29

-------
                                   TEST 8

        EFFECT OF FUEL BOUND NITROGEN ON OXIDES OF NITROGEN EMISSIONS

                          FROM A GAS TURBINE ENGINE


1.   FUELS TESTED

     Synfuel:   JP-5 type fuel  derived from crude shale oil.

     Reference fuel:  JP-5 derived from petroleum.

2.   TEST EQUIPMENT

     Allison T63-A-5A turboshaft engine (free turbine type used in Army OH-58A

     and Navy TF-57A helicopters).

3.   TEST SITE

     Naval Air Propulsion Test Center
     Trenton,  New Jersey

4.   TEST OBJECTIVES

     0  Confirm the presence of high levels of NO  in engine exhaust;
                                                 A
     9  Obtain information on  conversion efficiency of fuel bound nitrogen
        into NO ;
               X
     0  Assess the impacts of  high nitrogen fuel on meeting pollution control
        regulations.

5.   SPONSORING AGENCY

     Deputy Chief of Naval Material  (Development)
     Department of the Navy
     Washington, D.C.   20361

     Project Officer:   L. Maggitti
     Telephone No:   202-545-6700

6.   CONTRACTOR

     Naval Air Propulsion Center
     Fuels and Fluid Systems  Division,  PE71
     Trenton,  New Jersey  08628

     Authors:   A.  F. Klarman,  A.  J.  Rollo
     Telephone No:   609- 896-5841
                                     A-30

-------
 7.   TEST  CONDITIONS
     The T63-A-5A engine was installed in a sea level  test cell  using a three-
     point mounting  system.   A flywheel  and an Industrial  Engineering Water
     Brake, Type  400,  were connected to  the engine gearbox assembly at the
     forward power output pad to absorb  the engine power.   The brake reaction
     was measured by a Baldwin load cell.  All parameters  to determine the
     engine starting and steady-state performance with the fuels were measured
     using standard  test cell instrumentation.  Engine performance data is
     contained in the  reference report.
     Fuels of varying  nitrogen content were tested in  a T63-A-5A engine to
     measure their effects on exhaust gas emissions.   Five test  fuels varying
     in fuel bound nitrogen content from 3 yg (nitrogen)/g (fuel) to 902 yg
     (nitrogen)/g (fuel) were evaluated.   The nitrogen content in the fuel was
     adjusted by  mixing a JP-5 type fuel  derived from  shale oil  (902 yg (ni-
     trogen)/g (fuel)) and regular petroleum JP-5 fuel (3  yg/ (nitrogen)/g
     (fuel)).
 8.   ENVIRONMENTAL MONITORING
     Hydrocarbons, carbon dioxide, carbon monoxide, and nitrogen oxides.
 9.   PROJECT STATUS
     Project report  completed November 1977.  This is  part of an on-going Naval
     program to evaluate fuel products derived from alternate sources.
10.   RESULTS
     Table A-8 shows the results of the  exhaust gas measurements performed
     during the test program.  Additional results include  the following:
     •  NOX emissions  for the same engine power rating increased with in-
        creasing  fuel  nitrogen content.
     •  The conversion efficiency of fuel bound nitrogen to NO and NOX was
        approximately  45 percent for the test data in  which the  NO and NOX
        values could be accurately measured.
     •  No significant effects were noted on engine performance  or carbon
        monoxide  (CO)  and unburned hydrocarbons (HC) emissions due to the
        presence  of  high levels of fuel  bound nitrogen.
                                    A-31

-------
                                          TABLE  A-8.   EMISSION DATA SUMMARY
CO
ro
Witrogen
^g/g fuel

3


47


267


SIS


9O2

Engine
Power
Rate
IDLE
60* 8R
MIL
IDtS
60* Ht:
Mil,
IDLE
60* NR
MIL
IDLE
6O* HR
MIL
IDLE
60* MR
MIL
COj
1.98
-
3.03
2.03
2.43
3.03
2.03
2.43
3.03
2.10
2.43
3.03
2.1O
2.43
3.03

Pf»»
103S
-
140
985
430
130
S.005
380
140
950
445
110
992
460
135
CO
g/s
0.714
-
0.327
O.692
O.482
0.207
0.69S
0.438
O.224
0.688
0.482
0.210
0.710
0.500
0.210

fl/kg fu«l
99.2
-
9. 25
90. S
35.0
8.60
92.3
31.0
9.26
86.7
36.2
8.60
90.4
37.4
8.93

HO
HQg (as B3O2)
_r>pa g/s g/kg fual pp*a
6.7
-
23.9
7.7
12.7
24.3
9.1
16.5
27.6
11.6
17.8
31.6
14.9
22.1
35.9
0.00495
-
0.0416
0.00579
O.O1S2
0.0415
O.OO677
0.0204
0.0473
O.OO9OO
0.0206
0.0547
0.0114
0.02S7
0.0621
0.688
-
1.69
0.758
1.11
1.72
0.895
1.44
1.96
1.13
1.55
2.24
1.45
1.92
2.SS
6.7
-
23.9
7.3
13.1
34.3
9.4
16.7
27.6
12.3
18.4
31.6
16.0
22. S
36.3
g/s c
O.OO690
-
0.0637
0.00937
0.0241
0.0635
0.0108
0.0315
O.0726
0.0146
0.0327
0.0938
0.0188
O.O4O1
0.0962
j/kg fuel
1.06
-
2.59
1.16
1.75
2.64
1.42
2.24
3.00
1.85
2.47
J.*4
2.39
3.01
3.95
ppra
157
-
S.6
131
18.3
8.4
134
14.5
11.1
109.6
18.6
8.7
116
18.2
8.4
HC
g/s «y
O.OS03
-
0.00422
O.O427
0.00952
0.00621
0.002
0.00775
0.00825
0.0368
O.OO935
O.OO652
O.O385
0.00918
O.O0629

fctft fuel
6.99
-
0.172
5. 59
0.692
0.258
S.71
O.S49
0.341
«.6S
0.702
0.287
4.91
0.697
0.-2S8
F/A
{calculated )
O.O097S
-
0.0146
0.0105
0.0119
0.0146
0.0105
0.0119
0.0146
O.C10€
0.0119
0.014S
0.0106
0.0119
0.0146

-------
     •  The use of shale derived JP-5 fuel  with a high nitrogen content
        will make it more difficult to meet the EPA NOX standards for
        aircraft gas turbine engines.

11.   REFERENCE

     Klarman, A.F. and A.J. Rollo.   "Effect of Fuel Bound Nitrogen on Oxides
     of Nitrogen Emission From a Gas Turbine Engine", Naval  Air Propulsion
     Center, Trenton, New Jersey, NAPC-PE-1, November 1977,  32 pp.
                                     A-33

-------
                                   TEST 9

         SHALE-DERIVED FUEL OIL ENGINE SUITABILITY INVESTIGATION


1.   FUELS TESTED

     Synfuel:   Shale-derived diesel  fuel marine (MIL-F-16884G).

     Reference fuel:  Petroleum-derived diesel fuel marine  (MIL-F-16884G).

2.   TEST EQUIPMENT

     U.S. Navy LM2500 gas turbine engine configured as a gas generator
     with a fixed conical nozzle replacing the standard power  turbine.

3.   TEST SITE

     General Electric, Evendale, Ohio

4.   TEST OBJECTIVES

     e  To determine the suitability of using shale-derived DFM in  the
        LM2500 engine.
     o  Compare performance, exhaust emissions, smoke level, and combustion
        liner temperatures of the two fuels.

5.   SPONSORING AGENCY

     U.S. Navy
     David W.  Taylor Naval Ship Research and
       Development Center, Code 2705, Annapolis Laboratory
     Annapolis, MD  21402
     Contract Technical  Monitors:
     Mr.  Robert M. Giannini
     Mr.  Carlton H.  Hershner
     Telephone No: (301) 267-2674

6.   CONTRACTOR

     General Electric Company
     Aircraft Engine Group
     Evendale, Ohio

     Program Manager:  Mr. A.F.  Pyatt
     Telephone No:  513-243-2000
                                    A-34

-------
7.   TEST CONDITIONS
     Both fuels were tested in a one atmosphere annular combustor test rig.
     Determinations were made of pattern factor, temperature profiles, light
     off characteristics, lean blow out characteristics, and low power effi-
     ciencies.  Following the one atmosphere testing, back-to-back engine
     testing throughout the power rating of the engine was conducted using
     both fuels.  Engine performance, outer combustor liner temperatures and
     exhaust emissions were measured.  All testing was done under essentially
     identical ambient conditions.
8.   ENVIRONMENTAL MONITORING
     NO , CO, hydrocarbons, and smoke.
       A
9.   PROJECT STATUS
     This program was conducted November-December, 1979.  Final report is
     dated January 22, 1980.
10.  RESULTS
     All testing indicated that the combustor and engine operating character-
     istics were identical when using petroleum-derived or shale-derived DFM.
     From exhaust emissions analysis it was determined that shale-derived
     DFM gave consistently lower NO  levels (which could only be due to
                                   A
     nitrogen content in the fuel) throughout the engine operating range.
     CO, hydrocarbon, and smoke emission levels are summarized in Table A-9.
     Shale-derived DFM yielded slightly higher CO and HC levels at the lower
     power settings, but within current acceptable limits.  At higher power,
     CO and HC levels were essentially the same for both fuels.
11.  REFERENCE
     General Electric Company, Marine and Industrial Projects Division.
     Shale-Derived Fuel Oil Engine Suitability Investigation.  Document
     No.: NSRDC-02, Naval Ship Research and Development Center, Annapolis
     Laboratory, Annapolis, Maryland, January 22, 1980. 91 pp.
                                    A-35

-------
TABLE A-9.   TEST DATA  SUMMARY  LM2500,  NOV.  1979
NG*
Date/Run Fuel RPM
11/17/79 Petroleum- 5015
Deppjfd 5550






6000
7016
7500
7964
8466
8710
11/19/79 Shale- 4980
Derived ccnn
DFM
6018




1
7023
7529
8016
8510
8752
*
Gas generator speed.
NO emissions corrected to
F/A
Ratio
FAR 39
.01385
.01365
.01259
.01208
.01236
.01557
.02152
.02363
.01268
.01364
.01238
.01203
.01216
.01557
.02152
.02357
humidity =
Emi s
si on
CO HC
(LB/1000 LB
102.2
86.0
77.7
58.8
47.3
15.9
2.3
1.6
102.9
94.5
78.7
60.4
45.2
13.0
1.8
1.5
44 GR/LB
52.3
41.0
33.3
21.7
13.3
2.7
0.9
0.6
63.8
54.0
38.9
22.9
11.8
1.9
0.5
0.4

Index
4-
NOY
Fuel)
1.88
2.16
2.42
3.29
4.38
7.81
15.11
17.9
1.524
1.7
2.0
2.9
4.35
8.45
14.58
17.9

Smoke
No.
5.54
1.43
4.86
5.54
4.84
1.80
1.95
4.56
2.72
1.97
3.37
11.42
3.10
1.25
9.89
9.06

                   A-36

-------
                                  TEST 10

               FUEL PROPERTY EFFECTS ON COMBUSTOR PERFORMANCE


1.   FUELS TESTED

     Synfuels:  JP-5 from oil shale, coal, and tar sands.

     Reference fuels:  Fifteen (15) fuels (see Table A-10).

2.   TEST EQUIPMENT

     Two 2-inch-diameter, high-temperature/pressure research combustors of

     varying designs.  Figure A-6 shows design of the Phillips Combustor,  and

     Figure A-7 shows the design of the T-63 Combustor.

3.   TEST SITE

     U.S. Army Fuels and Lubricants Research Laboratory
     Southwest Research Institute
     San Antonio, Texas

4.   TEST OBJECTIVES

     •  Study the sensitivity of combustor performance to the physical  and
        chemical  properties of fuels.

     •  Determine the impact of broadening fuel specifications and of using
        nonspecification fuels in emergencies.

5.   SPONSORING AGENCIES

     U.S. Naval Air Propulsion Center
     Trenton, New Jersey

     Project Manager:  Mr.  Larry Maggitti
     Contract Number:  N00140-77-C-1345
     Telephone No:    609 -896-5841

6.   CONTRACTOR

     Mobile Energy Division
     Southwest Research Institute
     P.  0.  Drawer 28510
     San Antonio, Texas  78284
                                    A-37

-------
                  TABLE A-10.  FUEL BLEND CHARACTERISTICS
Fuel  No.                               Description
    1         Jet A -  Used for adjusting  combustor operating conditions.

    2         Base Fuel  - JP-5 with 1  to  2  percent olefins,  2 to 3 percent
             naphthalenes and 10-15 percent aromatics.   Fuels 3 to 7 are de-
             rived by adding materials to  this  fuel.

    3         16-mm smoke point obtained  by adding dicyclic  polynuclear aroma-
             tics to  base fuel.

    4         16-mm smoke point obtained  by increasing  naphthalene to 4 percent
             and adding monocyclic aromatics as necessary to JP-5 base fuel.

    5         Addition of 40 percent aromatics typical  of petroleum distillates
             in JP-5  distillation  range  (smoke  point must be less than  19
             mm).

    6.        Specification maximum for aromatics (25 percent) and olefins (5
             percent) typical  of petroleum distillates  in the JP-5 distilla-
             tion range (smoke  point  below 19 mm permissible).

    7.        Distillation end point of 580°F, achieved  by adding compounds
             typical  of petroleum  distillates in the required range (varia-
             tions in other specification  limits permissible -  except aromatic
             content).

    8.        Synthetic  JP-5 from Oil  Shale.

    9.        Synthetic  JP-5 from Coal.

   10.        Synthetic  JP-5 from Tar  Sands.

   11.        JP-5 Base  Fuel  for blending Fuels  12-14.

   12.        JP-5 plus  10 percent  diesel marine fuel (1).

   13.        JP-5 plus  20 percent.

   14.        JP-5 plus  40 percent.

   15.        Diesel marine fuel (1).

   16.        Leaded gasoline.

   17.        Diesel marine fuel (2).

   18.        Diesel marine fuel (1) plus 30 percent leaded  gasoline.


                                   A-38

-------
CO
UD
                                       TOTAL RADIATION
                                       PYMOMETCf
                                                                                                     Exhaust Gas
                                                                                                     Sampling Probe
                                                     -.\\-tkV.II.\l ' I\\1I AM KM i IXVtNVil.-sXl •  NN.XM I
                                                                           EXHAUST GAS
                                                                           THERMOCOUPLES
WATER IN
              INLET
              THERMOCOUPLES
                                                                     Mirror
                                                 FUEL IN
                                            Figure A-6.  Phillips  2-inch  Combustor

-------
3>


O
                             RADIATION
                              SENSOR
                       FUEL-
                              LINER
                         THERMOCOUPLES
                I
       BURNER CAN
COMBUSTOR HOUSING
                                     Figure A-7. T-63 Combustor

-------
     Authors:   C.  A.  Moses,  D.  W.  Naegeli
     Telephone No:    512 -684-5111

 7-   TEST CONDITIONS

     Both two-inch research  combustors were operated at various air flow and

     heat input conditions as described in the referenced report.

 8.   ENVIRONMENTAL MONITORING

     Exhaust smoke, CO,  NO , and UHC.
                          A
 9.   PROJECT STATUS

     This document is the  final  project report dated March 1980.   The first

     phase of this program was reported in Interim Report AFLRL No.  101, AD

     No.  A054229,  entitled "Effect of High Availability Fuels  on  Combustor

     Properties",  was performed under Contract No.  DAAK70-78-C-0001  and  was

     monitored by  U.S.  Army Mobility Equipment Research and Development  Command,

     DRDME-6L, Fort Belvoir, VA.

10.   RESULTS

     •  Gaseous emissions  and combustion efficiency were not significantly
        affected by fuel properties although some sensitivity  to  boiling point
        distribution  was evident.

     •  In all performance areas,  the syncrude fuels correlated in the same
        ways as the petroleum-derived fuels except for the NOX emissions from
        the nitrogen-containing shale oil  fuel.

     •  Flame radiation and smoke  were best correlated by hydrogen content
        rather than hydrocarbon structure; the soot formation  was  due to gas-
        phase reactions.
     •  Lean-blowout conditions were about the same for all fuels  except that
        gasoline could be  burned leaner at idle conditions.

     •  Ignition limits were more  sensitive to volatility than viscosity.

11.   REFERENCE

     Moses, C.A. and D.W.  Naegeli.   "Fuel  Property Effects on  Combustor  Per-
     formance", Mobile Energy Division, Southwest Research Institute, San
     Antonio, TX,  AD A084017, March 1980,  52 pp.
                                    A-41

-------
                                   TEST 11
             SHALE-DERIVED DFM PARTICIPATE EMISSIONS MEASUREMENT


1.   FUELS TESTED

     Synfuel:  shale-derived diesel  fuel  marine (MIL-F-16884G).

     Reference fuel:  petroleum-derived diesel fuel marine (MIL-F-16884G).

2.   TEST EQUIPMENT

     U.S. Navy DDG-15 Class ship's propulsion steam generator.

3.   TEST SITE

     Navy Ship Systems Engineering Station, Philadelphis, Pennsylvania.

4.   TEST OBJECTIVE

     0  To make comparative particulate emissions measurements between petro-
        leum-derived and shale-derived diesel fuel marine (DFM).

5.   SPONSORING AGENCY

     U.S. Navy
     David W. Taylor Naval Ship Research and
       Development Center, Code 2705, Annapolis Laboratory
     Annapolis, MD  21402
     Contract Technical  Monitors:
     Mr.  Robert M. Giannini
     Mr.  Carl ton H. Hershner
     Telephoned:   301-267-2674

6.   CONTRACTOR

     NAVSSES (Materials  Branch 053).

7.   TEST CONDITIONS

     All  test runs were  conducted in  triplicate at nominal 100 percent,  35
     percent, and  20 percent of full  power with both fuels.
                                    A-42

-------
 8.   ENVIRONMENTAL MONITORING
     Participates and participate matter composition.
 9.   PROJECT STATUS
     The study was conducted in January 1981.
10.   RESULTS
     There were no significant differences between the particulate emission
     products described and measured in this study resulting from the combus-
     tion of petroleum-derived or shale-derived DFM on the DDG-15 boiler
     (utilizing steam-atomized burners).  Particulate  emissions from both
     petroleum-derived and shale-derived DFM were below the EPA limit of 0.1
     lbs/106 Btu.
     Results of emission spectroscopy (qualitative analysis) of particulate
     matter retained on filter paper are given as follows:
                                              Trace Element
Zinc
major
major
Lead
trace
trace
Iron
trace
not
detected
Tin
trace
not
detected
Copper
trace
not
detected
     Shale-derived DFM
     Petroleum-derived DFM   major

11.  REFERENCE
     E.A. Dixon.  Memorandum for File.  Shale Oil Fuel, Particulate Emissions
     Measurement; DDG-15 Boiler.  U.S. Navy, NAVSSES (Materials Branch 053)
     053C:ED:amt, 6240(A2797), Ser. 3151, undated, 7 pp.
                                    A-43

-------
                                   TEST 12

                             DIESEL ENGINE TEST


1.   FUELS TESTED (See Table A-ll)

     Synfuel:   shale-derived diesel fuel marine  (MIL-F-168846).

     Reference fuel:  petroleum-derived distillate fuel No. 2.

2.   TEST EQUIPMENT

     A single cylinder, turbocharged, prechambered, four stroke  cycle,  labora^

     tory diesel engine (supplied by a Navy diesel engine manufacturer).

3.   TEST SITE

     Diesel engine manufacturer's facility.

4.   TEST OBJECTIVE

     •  To compare the performance and emissions of the shale-derived diesel
        fuel marine (DFM) with those of the petroleum-derived No. 2 fuel.

5.   SPONSORING AGENCY

     David W.  Taylor Naval Ship R&D Center
     Annapolis Laboratory, Code 2705
     Annapolis, MD  21402

     Project Officers:  Carl H. Hershner and Robert M. Giannini
     Telephone No:  301-267-2674

6.   CONTRACTOR

     Same as sponsoring agency (see above).

7.   TEST CONDITIONS

     See Table A-12 for Test Plan.

8.   ENVIRONMENTAL MONITORING

     Nitrogen  oxides,  hydrocarbons, and smoke.
                                    A-44

-------
TABLE A-ll. COMPARISON OF FUEL CHARACTERISTICS


Gravity
API
Specific gravity
Ib/gal
Cetane Index
Low Heat Value
Btu/lb
Btu/gal
Btu increase by wt.
Btu increase by vol .
Viscosity @ 100°F (SUS)
Aniline Pt.
Pour Point
Cloud Point
Flash Point
Distillation
IBP (°F)
90% (°F)
EP (°F)
Water and Sediment, %
Sulphur
Ash %
C %t wt.
H %, wt.
Ca, ppm
Na, ppm
Ni , opm
V, ppm
Pb, pom
Corrosion, Copper Strip
(3 hr 
-------
                          TABLE A-12.  TEST PLAN
  I.    Baseline performance with petroleum fuel.

        A.  Engine break-in.
        B.  Run engine to determine mechanical  and pumping losses
            for correlation of data.
        C.  Collect part load and emissions data at:

            1.  2200 RPM - rated speed
            2.  1400 RPM - peak torque

        Data taken at load points equivalent to the 0,  50%,  and 100% BMEP
        points.

  II.   Performance with shale-derived DFM  -  repeat  step I-C.

        A.  With same timing and rack setting.
        B.  With rack and timing adjusted  to the same power  as  in step 1-3.

  III.   "OBSERVED" shale-derived DFM  comparison -  steps  I-C and II  repeated
        for personnel  from Naval  Ship Research  and  Development  Center.
 9.  PROJECT STATUS

     Testing conducted in April 1980; results documented on 12 May 1980.

10.  RESULTS

     Performance and emissions for both fuels were compared and found to be

     the same with the exception of 2.5 to 4.0 percent lower thermal  efficien-

     cy with the shale-derived DFM.   Results are presented in Table A-13.

     Additional  part load performance tests and advanced timing performance

     tests also  showed no significant differences in either performance or
     emissions  for both fuels.

11.   REFERENCES

     "Diesel  Engine  Test,  12  May 1980",  supplied by C.  H.   Hershner,  David W.
     Taylor Naval  Ship R&D Center, Annapolis Laboratory (Code 2705).  Annapolis,
     nU 9  I L. pp«

     Telephone communication  to C. H.   Hershner, U.S.  Department of the Navy,

     ?7 March      °"          P R&°  Center*  AnnaP°lis>  MD>  to s-  Quinlivan,
                                    A-46

-------
                    TABLE A-13.   SUMMARY OF TEST RESULTS
                                                 Petroleum        Shale
I.






II.


III.






IV.


2200 rpm - max load (fixed rack @ .440)
BMEP* (psi)
BSFCt (lb/bhp-hr)
BSEC? (btu/bhp-hr)
Smoke
HC (gr/bhp-hr)
NOV (gr/bhp-hr)
A
2200 rpm - idle
HC (gr/bhp-hr)
NOY (gr/bhp-hr)
A
1400 rpm - max load (fixed rack @ .440)
BMEP* (psi)
BSFCt (lb/bhp-hr)
BSECf (btu/bhp-hr)
Smoke
HC (gr/bhp-hr)
NOY (gr/bhp-hr)
A
1400 rpm - idle
HC (gr/bhp-hr)
NOV (gr/bhp-hr)
X

125
.447
8,194
.03
.09
1.17

.09
.22

142
.411
7,534
.08
.12
.57

.05
.12

126
.448
8c n "3 f o Q°/-^ \
, D(J6 ( o . o/o> )
.03
.03
1.25

.15
.16

142
.406
7,706 (2.3%>)
.11
.12
.51

.06
.11

 BMEP = brake mean effective pressure.
fBSFC = brake specific fuel consumption.
^BSEC = brake specific energy consumption.
                                     A-47

-------
                                   TEST 13
                NAVY CV-60 CLASS BOILER EMISSION MEASUREMENTS


1.   FUELS TESTED

     Synfuel:  shale-derived diesel  fuel  marine (MIL-F-16884G).

     Reference fuel:  petroleum-derived diesel  fuel  marine (DFM).

2.   TEST EQUIPMENT

     U.S. Navy CV-60 Class ship's propulsion steam generator (see Table A-14

     for description).


           TABLE A-14.  CV-60 STEAM GENERATOR-OPERATIONAL PARAMETERS


             Number                                      1
             Class                                    CV-60


     Boiler Manufacturer                         Babcock & Wilcox (B&W)
     Operating Pressure                          1200 psig
     Superheated Steam Temperature               950°F
     Steam Generated @ Full  Power                261,450 Ib/hr
     Oil Burner @ Full  Power                     20,000 Ib/hr
     Combustion Gas Pressure                     2 psig
     Boiler Type                                 Natural Circulation
     Water Cooled Furnace                        Yes
     Furnace Frontwall  and Floor Materials       Refractory
     Superheater Type                            Horizontal
     Number of oil  Burners                       7
     Burner Type                                 *

     Automatic Combustion Control                Yes
     *
      B&W Iowa Registers with mechanical  vented plunger atomizers.
3.    TEST SITE

     Naval  Ship Systems  Engineering Station, Philadelphia, Pennsylvania.


                                    A-48

-------
 4.   TEST  OBJECTIVE

     §   To perform comparative emissions measurements between petroleum-
        derived diesel  fuel  marine (DFM) and shale-derived DFM for comparison
        with EPA stationary  source steam generator standards.

 5.   SPONSORING AGENCY

     David W.  Taylor Naval  Ship R&D Center
     Annapolis Laboratory,  Code 2705
     Annapolis, MD  21402

     Project Officers:   Carl  H. Hershner and Robert M.  Giannini
     Telephone No:  301-267-2674

 6.   CONTRACTOR

     NAVSSES,  Philadelphia,  Pennsylvania.

 7.   TEST  CONDITIONS

     Boiler operating conditions presented in Table A-15.   It was  originally

     intended  to conduct the emissions testing at boiler  loading conditions of

     10, 25, 50, 75, 100, and 120 percent of full  power.   However,  due  to  lack

     of a  full complement of forced draft blowers,  rates  of 63 percent  or

     lower were obtained (see Table A-15).

 8.   ENVIRONMENTAL MONITORING (See Figure A-8)

     S02,  N0x, CO, HC,  C02,  02, and smoke.

 9.   PROJECT STATUS

     Project began in March  1980 and completed in September 1980.

10.   RESULTS

     Pollutant emission results summarized in Table A-15.   No significant  dif-

     ferences  observed  between emissions resulting  from use of petroleum-

     derived DFM or shale-derived DFM for any boiler load  condition.   It  is

     noteworthy that:

     •   Shale-derived DFM sulfur oxide emissions  were generally somewhat  lower
        than petroleum-derived DFM at the same operating  rates,  due to  the
        lower  initial sulfur content of the shale DFM vs.  petroleum DFM (0.02
        v  0.16 percent).
     •   Petroleum-derived DFM oxides of nitrogen  exceeded  those of shale-
        derived DFM.


                                    A-49

-------
            TABLE  A-15.  CV-60,  PETROLEUM-DERIVED/SHALE-DERIVED DFM  EMISSIONS COMPARISON
Operating Rate,
Sulfur Dioxide,
PPM, Measured
Theoretical
Sulfur, PPM
EPA - Units,
lb; Per 106
BTU
Oxides of Ni-
trogen, PPM,
teasured
EPA - Units,
rbs Per 106
BTU
Carbon Mono-
xide, PFM
Hydrocarbons,
•J" PPM, as
tji Methane
O
Carbon Dio-
xide, *
Smoke, Kingel-
mann Number
Oxygen. 1,
Excess Air
OFG
Ibs Fuel Oil
Pressure
Fuel Oil Rate,
HR
% of Ful 1 Power
Time/Date

Coiment


11
DFM

2

-

-


9


_


1500

140



1.2

<1
14.2
-
-

65

2137
11
1030
5/16/80
White
Smoke

DFM

3

93.5

0.005


10


0.012


800

30



1.2

*'
11.6
112
207

65

2137
11
1100
5/16/80
Trace
Stack

Shale

0

11.7

0


9


0.011


200

15



3.5

•O
11.4
109
206

64

2400
12
1200
5/29/80
Normal
Opera-
tion
12
Shale

0

12.01

0


50


0.060


200

20



4.5

cl
10.2
83
201

65

2400
12
1430
5/29/80
Normal
Opera-
tion
25
Shale

0

11.80

0


15


0.018


350

15



3.6

*'
11.1
100
205

64

2400
12
1500
5/29/30
Normal
Opera-
tion
DFM

10

99

0.016


60


0.071


30

-



-

«!
7.1
48
195

120

5150
25
1110-
5/9/80
Normal
Opera-
tion
DFM

1

99

0.002


.


_


0

3



0


-------
        ECONOMIZER
I
tn
                                  TRANSMISSOMETER
                                  (OPACITY SMOKE METER)
I  ^HEAT EXCHANGER

           CHEMICAL DRTER

               ZERO
                                                                                                   GAS ANALYZERS
                                              BACK FLUSH AIR
                                               PRE FILTER

                                               (GLASS VOOL)
                      CVA-60

                STEAM GENERATOR
                                    (HAVSSES! TRAILER
                               Figure A-8.  Source  Emissions Instrumentation Schematic Diagram

-------
     Pollutant levels (i.e.,  sulfur oxides, nitrogen oxides, and smoke) were

    .all  found to be below EPA stationary source standards.

11.   REFERENCES

     "Shale Fuel  Oil  Emissions Measurement:  Interim Report", Memorandum Series
     3242,  24 August 1980,  supplied by C.  H.  Hershner, David W. Taylor Naval
     Ship R&D Center, Annapolis Laboratory (Code 2705), Annapolis, Maryland,
     12 pp..

     Telephone communication  of C.  H.  Hershner,  U.S.  Department of Navy, David
     W. Taylor Naval  Ship  R&D Center,  Annapolis,  Maryland,  to S. Quinlivan,
     TRW,  17  March  1981.
                                   A-52

-------
                                   TEST 14

            U.S.  NAVY DDG-15 CLASS BOILER EMISSIONS MEASUREMENTS


1.    FUEL TESTED

     Synfuel:   shale-derived diesel fuel marine (DFM), MIL-F-16884G.

     Reference fuel:   petroleum-derived diesel fuel marine (DFM), MIL-F-16884G

2.    TEST EQUIPMENT

     U.S. Navy DDG-15 Class propulsion steam generator (see Table A-16 for
     description).

3.    TEST SITE

     Naval Ship Systems Engineering Station, Philadelphia, Pennsylvania.

4.    TEST OBJECTIVE

     •  To perform comparative emissions measurements between petroleum-
        derived diesel fuel marine and shale-derived DFM for comparison with
        EPA stationary source steam generator standards.

5.    SPONSORING AGENCY

     David W.  Taylor Naval Ship R&D Center
     Annapolis Laboratory, Code 2705
     Annapolis, MD  21402
     Project Officers:  Carl H. Hershner and Robert M. Giannini
     Telephone No:   301-267-2674

6.    CONTRACTOR

     NAVSSES,  Philadelphia, Pennsylvania.

7.    TEST CONDITIONS

     Comparative  emissions data on petroleum-derived and shale-derived DFM
     obtained  over an operating range of 12 to 106 percent of full  power.

     Other boiler operating conditions presented in Table A-17.
                                    A-53

-------
           TABLE A-16.   GENERAL DDG-15 BOILER DESCRIPTION
   Class
                                               DDG-15
Boiler Manufacturer
Operating Pressure
Superheated Steam Temperature
Steam Generated @ Full  Power
Oil Burner @ Full Power
Combustion Gas Pressure
Boiler Type
Water Cooled Furnace
Furnace Frontwall and
Floor Materials
Superheater Type
Number of Oil  Burners
Burner Type

Automatic Combustion Control
Combustion Engineering
1200 psig
950°F
137,500 Ib/hr
10,980 Ib/hr
2 psig
Natural Circulation
Yes

Refractory
Vertical
4
C.E./Wallsend
Steam Assist Burner
Yes
                              A-54

-------
                    TABLE A-17.  DDG-15, PETROLEUM-DERIVED/SHALE-DERIVED DFM EMISSIONS COMPARISON
cn
tn
Kal«j I UH1 ' l>m SHAM! IIFM
Sulfur
II Ion Me,
Tlioor 1 I Icnl
Siilfni ',_ ffm
KI'A-lliilts,
Ihs I'or
III'1 P.11I
Oxlih-s of
HI ir.T.i'".
r.l'A-lliilts.
Ilia IV r
10 ' inn
Carbon
llydror-nrhitna ,
IHi.xlilG.X
Siw.kn, Klnp.iH-
M.IIIII Number
Km OSM Air
ID 10 9
58 58 57
0.027 0.027 0.026
25 25 28
0.051 0.0ril 0.057
200 200 200
55-
8.0 8.0
Clear Clo.ir Clc.ir
9.8 	 10.0 10.1
HO 81 m
31ft 118 141
6 6 6 66
6.5 6 6.5 6.5 -
0.018 0.019 0.018 0.019 -
27 27 25 10 36
0.060 0.061 0.060 0.06? -
00000
55622

Clenr Clcnr Clenr Clenr Clr;
_L> .- .1 __1JL_L_ .11- ?__ J.2.- .P__r ..
9/ 102 97 100
If.H 178 UH 171

5J 52 52 50
0.028 0.029 0.029 0.028
40 40 10 43
O.OU'I 0.092 0.092 0,10
7500 15(10 1500 10
35 35 30
ft. 4 -
r Snick
_1 K 7 	 1 2_10 	 12.0 42.7
911 101 101 110
1/0 179 179 392

6666
0.015 0.016 0.016 0.016
35 36 42 42
11.0110 0.090 0.090 0.09C
0 0 100 100
1 1 I 1
5.0 5.0 5.8 5.8
Clenr Clear Clenr Clear
mo no no 110
171 192 192 19?
10 11 10 10
51 61 59 57
0.027 0.032 0.028 0.0
23 28 28
0.047 0.056 0.0
100 ncg ncK nei;
*5 5 5 ' 10
9.0 9.6 9.6 7.'i
Trace Trace
Clenr Stack Stack Cle
9_. 2 	 10. 1 	 9J 	 _1_0_.
71 H3 77 83
119 142 J10 341
SIIAI.K
J 5 55
- 7 - 7
29 - 0.014 - 0.015
38 37 32 33
i6 - 0.076 - 0.071
neg nog neg neg
1 121
4.0 4.0 4.0 4.0
ir Clear Clear Clenr
1 	 :_ 	 10 J_^_iP_..6 	
	 ^ 	 83 - 88 	
142 - J51
                                                                                                 (Continued)

-------
                                               TABLE A-17.  (Continued)
en

-------
                                              TABLE A-17.  (Continued)
I
cn
—i

Kale. Z
Kul fur
Dloxl tie
jipar wnouri.'*)
lln-iirfl li:nl
Sn 1 f ur j I'J"*
KI'A-UnUn,,
Ilis IV r 10 '
irm
OxI.K-s of
N 1 1 i nr.cn ,
IH'W, BM>,-isurCMl
KJ'A-llnlls,
11,9 IV i 10
imi
C.i r l,c. II
Mom, .Me,
[>!•»
Ityilrorflflioiia ,
|>|,l>, .IB
nvllumn
C.-ii him
Dioxide, Z
r.nnkr. Rhi|(,-|-
HIJIIII NiialuT
.. .
Ilicyi;'1"! I

IIKH
5228
55 57 55 51
0.0)5 0.006 0.006 U.025
50 18 52 55
0.110 O.OHO 0.110 o.no
200 - 310 TiO
5 10 , 20 10
i
I.I 8.B | , 0.4 9,1
Trace ClPnr Clpnr (Me/ir
<1 <1 '1
10.9 10. 2 10.9 12.0

SIIAI.K
f. 5.5 5.5
6 6
0.020 (1.020
15 1U 35
0.1199 • 0.091
000
1 1 0
, V
5.0 4.8 4.9
Clenr L'lonr (llenr
<1 
-------
                                                           TABLE  A-17. (Continued)
O|N»rnt InR
H.itf, Z
Kxn-nn Air
lift:
llm Fuel
Ul 1 I'rensiire
Z of Kull
1'iiWRr
Tine/
li.ile
1 of
Itiirner*
ruMHttlt
m :
IIFN
91 81
•J'ifl l/i 1
7071 7073
70 70
0950 Kimi
6/J3/00 ^
4 'i
Trace
SI nrk

*"
92 100
15H 3/1
7073 7071
70 70
1015 1100
4 4


SIIAI.K i
112 112
414 414
7451 7453 7451
68 68 6H
1045 1055 1105
9/IO/HO
444

KXI
om
KM 98 107
174 370 387
10810 10810 10830
1OO 100 100
1110 1330 1400
6/25/80
4 44

106
SIIAI.K
112 132
434 434
11790 11790
106 106
1435 1445
9/3/80
4 4
1.1 nht
Trace
Stuck
i
cn
CO
                        NOTK:  - • InetniMpnt not In o|>nr*it1iHi

                            n.c.* not rtfleuIntPd

-------
 8.   ENVIRONMENTAL MONITORING

     S02>  CO,  C0£, NOX,  HC,  Q^*  ancl smoke emission levels were monitored by
     the NAVSSES Mobile  Source Emissions Unit (see Figure A-9 for schematic)
     which was positioned adjacent to the DDG-15 boiler.

 9.   PROJECT STATUS

     Testing performed intermittently between June and September 1980.

10.   RESULTS

     Pollutant emission  results  summarized in Table A-17.  No significant

     differences observed between emission resulting from use of petroleum-
     derived DFM or shale-derived DFM for any boiler load condition.   However:

     •  Shale-derived DFM, sulfur oxides emissions were generally lower than
        those of petroleum-derived DFM at the same operating rates due  to
        lower initial sulfur content of shale fuel versus petroleum (0.02 per-
        cent vs. 0.16 percent).   In addition, shale DFM excess air values
        tended to be higher-than those of petroleum DFM,  consequently diluting
        stack sulfur dioxide emissions further.
     •  Petroleum-derived DFM oxides of nitrogen emissions were slightly higher
        than those of shale-derived DFM, at the  same rate of combustion.

     t  Hydrocarbon emissions were generally low.   Carbon dioxide emissions
        from petroleum-derived DFM tended to be  unusually higher than those
        of shale-derived DFM at 12, 50, and 70 percent of full power, due in
        part to incomplete setting of boiler operating condition and  the ad-
        justment of excess air settings after the  onset of data taking.   Carbon
        monoxide emissions from the petroleum fuel were also higher than those
        from shale fuel  which were in most cases negligible.

     Pollutant levels all found to be below EPA  stationary source standard.

11.   REFERENCES

     "Shale Oil Fuel Measurement, DDG-15 Boiler  Interim Report", 18 February
     1981, supplied by C. H. Hershner, David W.  Taylor Naval Ship R&D Center,
     Annapolis Laboratory (Code 2705), Annapolis,  MD.   7  pp.
     Telephone communication of C. H. Hershner,  David  W.  Taylor Naval Ship R&D
     Center, Annapolis,  MD,  to S. Quinlivan, 17  March  1981.
                                     A-59

-------
      ECONOMIZER
i
CT>
O
                                 TRAKSUISSOKETER
                                 (OPACITT SMOKE METER)
HEAT EXCHANGER

       CHEMICAL

            ZERO CAS
                                                                                                 CAS ANALYZERS
                                              PRE  FILTER
                                             (CLASS WOOL)
                   CVA-60

              STEAM GENERATOR
                                  (HAYSSES) TRAILER
                              Figure A-9.   Source  Emissions Instrumentation Schematic  Diagram

-------
                                   TEST 15
                       U.S.  NAVY FF-1040 CLASS BOILER
                PRESSURE-FIRED EXHAUST EMISSIONS MEASUREMENTS

1.    FUELS TESTED
     Synfuel:   shale-derived diesel fuel marine (DFM), MIL-F-16884G.
     Reference fuel:   petroleum-derived fuel  marine (DFM), MIL-F-16884G.
2.    TEST EQUIPMENT
     U.S. Navy FF-1040 Class pressure-fired steam generator (see Table A-18
     for description).
3.    TEST SITE
     Naval Ship Systems Engineering Station,  Philadelphia, Pennsylvania.
4.    TEST OBJECTIVE
     •  To perform comparative emissions measurements between petroleum-
        derived and shale-derived DFM for comparison with EPA stationary
        source steam generator standards.
5.    SPONSORING AGENCY
     David W.  Taylor Naval  Ship R&D Center
     Annapolis Laboratory,  Code 2705
     Annapolis, MD  21402
6.    CONTRACTOR
     NAVSSES,  Philadelphia,  Pennsylvania.
7.    TEST CONDITIONS
     Boiler conditions are  presented in Table A-19.   It was originally in-
     tended to conduct the  emissions testing  over the full operating  range of
     the FF-1040; due to mechanical problems, data acquisition was limited to
     the operating condition 20 to 60 percent of full power.
                                    A-61

-------
                                          TABLE A-18. GENERAL BOILER DATA
                              Class
                                                     FF-1040
en
ro
Boiler Manufacturer

Operating Pressure

Superheated Steam Temp.

Steam Generated @ Full Power

Oil Burner @ Full Power

Combustion Gas Pressure

Boiler Type

Water Cooled Furnace

Furnace Frontwall and
Floor Materials

Superheater Type

Number of Oil Burners

Burner Type
                          Automatic  Combustion
                          Control
                                                                            Foster-Wheeler
                                                                            1200  pslg
                                                                            950°F
126,000 Ib/hr

  9,740 Ib/t.r

up to 60 pslg

Pressure Fired

Yes

Can type - refractory
No Frontwall

Horizontal - Ring Tube Type

   3

TODD triplex mechanical
pressure atomizer



Yes

-------
                 TABLE A-19.  FF-1040,  PETROLEUM-DERIVED/SHALE-DERIVED DFM EMISSIONS COMPARISON
cr>
u>

Rate. Z
Sulfur
DIo«Ue,
PP«. ncasured
Tlienrctlcol
Sulfur, rP»
EPA- Units.
Ibn p«r 10
BTV
Oxides of
Nitrogen, rpm
ETA-Ilnit..,
Ibs per 10
BTU
Carbon
Monoxide, pjin
Hydrocarbon*,
ppuit an
>e thane
Carl'on
Dioxide, Z
Smoke, Rlnnel
•ann Number
Oxygen ,Z
Excess Air

19.5 20
2 0
57

21 62
0.090
200 10
5 1
5.4 7.2
Trace
White Clear
13.3 10.1
83
^
19 19 20 20
0010
8787
0.027
66 65 64 61
1 t
0.120 0.133 0.125 0.125
0000
8 7 - 10
10.0 B.8
Clear Clear Clear Clear
8.9 9.8 9.2 9.7
68 81 71 79

25
0
61

60
0.110
10
0
9.0
Clear
9.0
70

26
0
7

67
0.130
200
125
8.8
Clear
9.0
70

33
2.5
64
0.068
6)
0.110
0
0
8.7
Clenr
8.7
63

33
0.5
6
0.015
72
0.156
0
45
14.0
Clear
10.9
92

'.5
2
61
O.OS'i
65
0.125
0
0
10.0
Clear
9.2
71

48
2
7
0.05ft
77
0.160
100
285
8.6
Clenr
10.3
85

56 56
3 4
64 64
1
0.076 0.102
92 92
0.170 0.170
0 0
0 0
10.5
Clt'.ir Clear
8.7 8.7
63 63

58
2
8
0.052
120
0.227
50
200
9.2
Clear
8.9
68
                                                                                                (Continued)

-------
                                                          TABLE A-19.  (Continued)
en
Ope rut Ing
Rntc. Z
UKC
F.K-1 Oil
Rate. Hr
1-St.iR*
Burner
firman
I of full
Power
Tl«c/
Date
19. S 20 19 19 20 20 25 26 33 33 45 48 56
341
1906 19C4
550/55 550/50
19.5 20
1455 1440
9/17/80 9/17/B(
114 318 319 334
IBftO 1880 2000 2000
550/40 550/40 550/50 550/5(
19 19 20 20
1245 1145 1200 1215
) 9/23/BO 9/23/80 9/23/80 9/23/1
318
2448
) 545/9f
25
1400
W 9/17/(
318
252;
54B/TO
26
1245
10 9/18/8
104
1232
'> 552/1
11
1126
0 9/17/
159
1136
»5 54': /H
11
1200
BO 9/IB/fl
119
4391
5 575/K
45
1250
0 9/l//f
346
4681
5 562/440
48
1130
10 9/1K/JO
104
5315
Sf.0/545
135
.SIIALK
56 58
104
5515
560/545
135
56 • 56
1135 : 1200
9/17/80 9/17/80
314
5617
555/545
115
18
1045
9/18/80
                      Tf»c«
                      Uliltr
                      Saokr
                      Frui
                      Stuck
{-) " Instrument Inopcriitlvc

-------
 8.   ENVIRONMENTAL MONITORING (See Figure A-10)

     S02,  NOX,  CO, HC,  and smoke.

 9.   PROJECT STATUS

     Data  acquired on three operating days (17, 18, and 23 September 1980).

10.   RESULTS

     Pollutant  emissions summarized in Table A-19.   No significant differences
     observed between emissions resulting from use  of petroleum-derived or

     shale-derived DFM for any boiler load condition.  It is noteworthy that:

     •  Petroleum-derived DFM sulfur emissions slightly exceeded shale fuel
        emissions under the same operating conditions.
     •  Shale fuel nitrogen oxide emissions slightly exceeded petroleum-
        derived emissions under the same operating  conditions.

     Pollutant  levels (i.e., Sulfur oxides, nitrogen oxides, and smoke) all
     found to be below EPA stationary source standards.
                              !
11.   REFERENCES

     "Shale Fuel Oil Emissions Measurement, FF-1040 Boiler, Interim Report",
     18 February 1981,  Memorandum Series 3037, supplied by C. H. Hershner,
     David W. Taylor Naval Ship R&D Center, Annapolis Laboratory (Code 2705),
     Annapolis, MD.  6 pp.
     Telephone  communication of C. H. Hershner, U.S. Department of Navy, David
     W. Taylor  Naval Ship R&D Center, Annapolis, MD, to S. Quinlivan,  17 March
     1981.
                                    A-65

-------
       ECONOMIZER
CT>
CT>
                                  TRAKSWISSOMETER
                                  (OPACITY SMOXEMETER1
LIGHT SOURCE
       Mt
                                               I  •«-HEAT EXCHANGER
                                                          CHEMICAL DRIER

                                                               ZERO CAS
                                                                                                     GAS ANALYZERS
                                              IACK FLUSH AIR
                                                                                                    CO  CO,  CO,  .0,  0,
                                                                                                    xoit  ion  rut CHU Utci
                                                PRE  FILTER
                                               (GLASS WOOD
                                                                                 PART ICIII AT ES
                                                                                 FILTER
                                                                        8ACX FLOSH
                                                                        AIR
                                                                                                  HEATED flO
                                                                                              HYDROCARBON ANALYZER
                    CVA-60

               STEAM GENERATOR
                                    (X/tVSSES) TRAILER
                          Figure  A-10.   Source Emissions  Instrumentation Schematic Diagram

-------
                                   TEST 16

                 EVALUATION OF SHALE-DERIVED JP-5 TYPE FUEL

                        IN AN ALLISON T63-A-5A ENGINE


1.   FUELS TESTED

     Synfuel:   JP-5 fuel derived from shale oil (see Table A-20).

     Reference fuel:  JP-5 petroleum-derived fuel (see Table A-21).

2.   TEST EQUIPMENT

     Allison  T63-A-5A turboshaft engine used in Army OH-58A and Navy TH-57A

     helicopters.  Consists of a combination six-stage axial flow,  one-stage

     centrifugal  flow compressor directly coupled to a two-stage free turbine

     which is coupled to a gas producer turbine.

3.   TEST SITE

     Naval Air Propulsion Test Center, Trenton, New Jersey.

4.   TEST OBJECTIVE

     •  To evaluate the performance and emissions of JP-5 type fuel  derived
        from  shale oil compared to petroleum-derived JP-5 in the sea level
        operation of a T63-A-5A helicopter engine.

5.   SPONSORING AGENCY

     U.S. Navy
     Naval Air Systems Command
     Washington,  D.C.

6.   CONTRACTOR

     Naval Air Propulsion Test Center
     Fuels and Fluid Systems Division
     Trenton,  N.J.

     Project  Officer:  J. Solash
     Telephone No:   609-896-5841

7.   TEST CONDITIONS

     Emissions test cycle parameters are presented in Table A-22.  This sequence


                                     A-67

-------
TABLE A-20. LABORATORY ANALYSIS OF  SHALE  OIL DERIVED JP-5
: 	 	 	
Gravity, Specific 15.5/15. S'C
(60/60'F)
Gravity. "API. 15.5/15. S'C
(60/60'F)
DlatllUtlon. IBP, *C CF)
5Z Over *C CF)
10Z Over 'C CF)
20Z Over 'C CF)
30Z Over 'C CF)
40Z Over 'C CF)
50Z Over 'C CF)
60Z Over *C CF)
70Z Over *C CF)
801 Over 'C CF)
90Z Over 'C CF)
95Z Over 'C CF)
End Point, *F
Recovery Z Vol.
Reeldue Z Vol.
Loee, Z Vol.
CUB, Exl*tent. «J/100 «1
Sulfur, Z Wt.
F.I. A Saturates, Z Vol.
Olafins. Z Vol.
Aruiutlcs, Z Vol.
Aniline Point, *C
Aniline Crevlty, Conetant
Hut of Coabuetlon. MJ K*"1
(STU/lb)
Corroelon, Copper Strip
Saoke Point, en
Freeie Point, *C CF)
Flaeh Point, *C CF)
Vlecoeltv, «2a"1 X 10~* (eke).
.-34. S'C (-30'F)
Contaalnatlon, agl~
Thertul Stability t 260. 0'C
(SOO'F) (JFTOT)
Water Separonecer Teat, Modified
Oil Shale
0.8058

44.1

171.1 (340)
185.5 (366)
191.0 (376)
199.0 (390)
205.5 (402)
212.0 (414)
219.0 (426)
225.5 (438)
2)3.5 (452)
242.0 (468)
254.5 (490)
265.5 (510)
282.0 (540)
97.8
1.0
1.2
81.7
0.05
71.76
2.29
25.95
61.8
6,315
43.105
(18,532)
1-a
22
-22.5 (-28)
65.5 (150)
Froien

164.20
Fall

76
MIL-T-5624J
Requirement*
Average
JP-5 (a) Nintanni Naxlvuai
0.8170 0.788 0.845

41.7 M.O *8.0

_ -
_ -
197.0 (387) - 204.5 (400)
-
-
-
216.5 (422)
-
-
.
243.0 (469)
-
263.5 (506) - 288.0 (550)
_
1.5
1.5
1.3 - -7
0.096 - 0.4
-
0.8 - 5.0
16.0 - 25.0
62.5
6.059 4.500
43.091 42.565
(18,526) (18.300)
1-b
22.2 19
-49.0 (-56) - -46.0 (-51)
60.0 (140)
10.5 - 16.5

. - 1.0
Paaa - Paea

94 85
   (n) Mlnerel Indue try Survey•, Avlntlon Turbine Fueli,  1973 Reference.
                                A-68

-------
TABLE A-21.  LABORATORY ANALYSIS OF  PETROLEUM-DERIVED JP-5
              FOR T63-A-5A ENGINE TEST

Gravity, Specific 15.5/13.5'C
(60/60'F)
Gravity. 'API. 15.5/15.5*C
(60/60'F)
Distillation. IBP. *C CD
5Z Ov«r 'C CF)
10X Over 'C CD
201 Over *C (*P)
301 Over 'C CF)
401 Over *C CF)
501 Over 'C CF)
601 Over 'C CF)
701 Over 'C CF)
801 Over 'C CF)
901 Over "C CF)
951 Over *C CF)
End Point, *F
Recovery Z Vol.
Residue Z Vol.
Lots. Z Vol.
CUB, Existent, mg/100 ml
Sulfur, Z Ut.
F.I.A Saturates, Z Vol.
Oleflns. Z Vol.
Aromatics, Z Vol.
Aniline Pol.it, *C
Aniline Gravity, Constant
Heat of Conbuatton, HJ Kg"1
(BTTJ/lb)
Corroalon, Copper Strip
Saoke Point, "m
Freete Point. *C CF)
Flaah Point, *C CF)
Vlacoslty, B2a'1 X 10"6 (cU).
38.0'C (100'F)
Viscosity, mV1 X 10"6 (cks).
-34.5*C (-30°F)
Contaaloat loo, mgf1
The raj 1 Stability 9 260. O'C
(500'F) OFTOT)
Water Scparoneter Test, Modified
Average
JP-5 Used JP-5 (it)
0.811* 0.1170
42.9 41.7
176. S (350)
188.0 (370)
192.0 (378) 197.0 (387)
198.0 (388)
202.0 (396)
208.0 (406)
213.5 (416) 216.5 (422)
216.5 (422)
223.5 (434)
229.0 (444)
238.0 (460) 243.0 (469)
245.5 (474)
258.0 (496) 263.5 (50t)
98.5
1.0
0.5
0 l.J
0.06 0.096
80.86
0.95 0.8
18.10 16.0
61.7 62.5
6,139 6.059
43.170 43.091
(18,560) (18,526)
1-a ,
28 22.2
-50.0 (-58) -49.0 (-56)
63.5 (146)
1.55
9.40 10.5
1.80
Pass Pass
98 94
M1L-T-5624J
Requirements
Minimi* Haxlmua
0.788 0.845
36.0 48.0
-
-
204.5 (400)
-
-
-
-
-
-
-
-
-
288.0 (550)
-
1.5
1.5
- . 7
0.4
-
5.0
25.0
-
4,500
42.565
(18,300)
1-b
19
-46.0 (-51)
60.0 (140)
16.5
1.0
Pass
85
   (A) Min«r«l Industry Surveys, Aviation Turbin* Fuel*, 1973 Reference.
                                 A-69

-------
                       TABLE A-22. EMISSIONS TEST CYCLE
      Engine Power Rating

       Cold  Start

       Maximum  Power  (nil)

       Normal Rated Power  (NR)

       902 NR

       60% m

       402 NR

       Flight Idle

       Ground Idle
Tine (Minutes^


     10

     10

     10

     10

     10

     10

     10
                                              TOTAL  TIME
     70
     was repeated to  provide  duplicate data.  Throughout  the  test  program,  the
     power turbine was  kept at  538  RPS  (35,000  RPM) except  at ground  idle.
 8.   ENVIRONMENTAL MONITORING
     CO, C02,  NO, N02,  and total  hydrocarbons (THC).
 9.   PROJECT STATUS
     The study was completed  in May 1976.   It was  recommended that other labo-
     ratory tests should  be initiated to measure other  performance factors  of
     the shale derived  JP-5 (e.g.,  material  compatibility,  cleanliness,  addi-
     tive requirements, flammability, etc.).
10.   RESULTS
     f  The performance of the  JP-5 type fuel derived from  oil  shale  was
        equivalent to that of petroleum-derived JP-5.   Although the shale oil
                                    A-70

-------
       JP-5 was highly contaminated with solid particles, no effect on engine
       performance was observed.  Most of the solid matter was collected by
       two in-line filters and a filter upstream of the engine fuel pump.

    •  The CO and THC emissions were equivalent for both fuels.  NOX emission
       levels were higher for the oil shale derived JP-5, due to the higher
       levels of organic nitrogen compounds present in the oil shale derived
       JP-5  (see Figure A-11).

    •  The shale oil JP-5 was not recommended for  use in flight operations,
       due to failure to meet standard specifications.

12.   REFERENCES

     Solash,  J.,  C.J.  Nowack,  and  R.J.  Delfosse.   "Evaluation  of a  JP-5 Type
     Fuel  Derived  from Oil  Shale",  Navy  Air  Propulsion Test  Center, Trenton,
     NJ.   NAPTC-PE-82,  May  1976,  44  pp.

     Telephone communication of  C.J.  Nowack,  Navy  Air  Propulsiton  Center,
     with S.  Quinlivan,  TRW, 3 March 1981.
                                     A-71

-------
    70
    60
    50
    AO
 §
 o
 55
 O
 o

  X
 o
     30
     20
     10
        0.010
                                            O  JP-5


                                            D  SHALE OIL JP-5
                                      I
0.015
                                 FUEL/AIR RATIO
0.020
Figure A-ll. Exhaust Emissions of Oxides  of Nitrogen (NO ) for T63-A-5A  ENGINE.
                                       A-72

-------
                                   TEST 17

        DEVELOPMENT OF ALTERNATE SOURCES OF JP-5 FUEL,  ENDURANCE AND

     EMISSION TESTS OF A T63-A-5A ENGINE USING A TAR SANDS DERIVED JP-5


1.    FUELS TESTED (see Table  A-23)

     Synfuel:   unifined kerosene-derived from Athabascan Tar Sands.

     Reference fuel:   petroleum-derived JP-5 fuel.

2.    TEST EQUIPMENT

     An Allison T63-A-5A turboshaft engine.  Free turbine type  used  in  the

     Army OH-58A and Navy TH-57A helicopters.

3.    TEST SITE

     Naval Air Propulsion Test Center,
     Trenton, New Jersey

4.    TEST OBJECTIVES

     •  Investigation of the  suitability of JP-5 fuel  derived from alternate
        sources for Navy use.

5.    SPONSORING AGENCY

     Department of the Navy
     Naval Air Propulsion Test Center
     Trenton, New Jersey

     Prepared by:  C. J. Nowack
     Telephone No:   609 -896-5841

6.    CONTRACTOR

    -Department of the Navy
     Naval Air Propulsion Test Center
     Trenton, New Jersey

     Author:   C. J. Nowack
     Telephone No:   609-896-5841

7.    TEST CONDITIONS

     The T63-A-5A engine was  installed in a sea level  test cell  using a three-

     point mounting system.  Engine inlet air and fuel  temperatures  during  the

                                     A-73

-------
TABLE A-23.  PROPERTIES OF UNIFINED KEROSENE, AVERAGE JP-5 AND NAPTC  JP-5
            (T63  ENGINE CALIBRATION FUEL)

Gravity, Specific, 60/60 °F
Gravity, °API, 60/60 °F
Reid Vapor Pressure, Ib/in^
Distillation, I.E. P. °F
5% over °F
10% over °F
20% over °F
30% over °F
40% over °F
50% over °F
60% over °F
70% over °F
80% over °F
90% over °F
95% over °F
End poing °F
Recovery % vol .
Residue % vol .
Loss % vol.
Gum, Existent, mg/100 ml
Sulfur, % wt.
F.I, A. Saturates, % vol.
Olefins, % vol.
Aromatics, % vol .
Aniline Point, °C
Aniline - Gravity Constant
Heat of Combustion, Btu/lb
Corrosion, Copper Strip
Smoke Point, mm
Freeze Point, °F
Flash Point, °F
Water Tolerance
Viscosity, cks. , 100°F
0°F
-30°F
Contamination, mg/ liter
Thermal Stability (JFTOT)
Total Acid Number
Doctor Test
Water Separometer Test, Modified
Uni fined
Kerosene
0.8328
38.4
0.00
366
380
388
398
408
418
428
436
448
462
480
500
546
98.1
1.4
0.5
1.2
0.01
77.06
3.67
19.27
59.8
5,361
18,436
la
20.0
-64
154
#1 (1.0)
1.74
6.38
12.85
0.11
Pass
0.007
Sweet
95
NAPTC JP-5
0.8142
42,3
--
356
374
380
386
394
400
410
418
430
442
460
480
508
99.0
1.0
0.0
--
0.05
75.98
3.65
20.37
61.5
6,036
18,551
la
21
-58
154
--
--
--
9.34
0.33
Pass
—
—
--
MIL-T-5624J
Requirements
Min Max
0.788 0.845
36.0 48.0
"~ "" — ~
"* ~ "• •"
— — — —
400
-— __
— . _
--
— —
—
--
--
--
--
550
—
1.5
1.5
7
0.4
-_
5.0
25.0
__
4,500
18,300
Ib
19
-51
140
__
—
__
16.5
1.0
Pass
0.15
Sweet
85
                                    A-74

-------
                 between 70 and 90°F.   The studies were conducted according to
     the  following  test sequences:
       Fuel                      Test Sequence                      Time/Hours
     JP-5                 Pre-test  Engine Calibration                   3
     Unifined  Kerosene    Engine Performance/Endurance Studies         54
     JP-5                 Post-test Engine Calibration/Exhaust          1
                          Emissions
     Unifined  Kerosene    Post-test Engine Exhaust Emissions            1

     Throughout the test program, the power turbine was kept at a constant
     speed  of  35,000 RPM except at  ground idle.   The engine power ratings
     designated for the emission survey were selected as being representative
     of a typical  Army helicopter duty cycle.  (Performance ratings are de-
     tailed in the  reference report.)
 8.   ENVIRONMENTAL  MONITORING
     Carbon monoxide, nitrogen oxide and unburned hydrocarbon emissions.
 9.   PROJECT STATUS
     The  Naval Air  Propulsion Test  Center investigation of the suitability for
     Navy use  of JP-5 derived from  alternate sources was originally authorized
     on June 1974 under NAVAIR AIRTASK No.  A330-33-C/052B/5F571-571-301.   It
     was  recommended that various laboratory tests be continued on a low
     priority  basis and that further engine testing be delayed.
10.   RESULTS
     •  Unifined Kerosene as derived from Athabascan Tar Sands by GCOS  is a
        satisfactory substitute for petroleum derived JP-5 in the sea  level
        operation of the T63-A-5A engine under the environmental  conditions
        tested.   There was no visual degradation  of fuel system materials or
        hot end components after 55 hours of engine performance.
     •  The carbon  monoxide (CO) and total  unburned hydrocarbon (THC)  emis-
        sions  were  higher at low engine fuel-air  ratios (lower power)  for JP-5
        than were obtained with Unifined Kerosene (see Figures A-12 and A-13).
     •  The nitrogen oxide (NO,,,) emission was slightly higher at all fuel-air
        ratios when using Unifined  Kerosene than  with JP-5 (see Figure  A-14).
                                     A-75

-------
       1000  .
  CO

(ppm)
        800 -
        600 -
        400 •
        200 •
                      I
                    .01
     .015

Fuel/Air Ratio
  i
.02
               D - Unif ined Kerosene
               O - JP-5
               Figure A-12, Carbon  Monoxide  Emissions,  ppm
                            T63-A-5A Engine  (S/N 401331)
                                      A-76

-------
      500 -,
      400 -
      300 -
 THC
(ppm)
      200
      100 -
                                       	i	
                                           .015

                                        Fuel/Air  Ratio
—!	
 .01
            D - Unifined Kerosene
            O - JP-5
              Figure A-13. Total  Unburned  Hydrocarbon  Emissions
                           T63-A-5A  Engine (S/N  401331)
—r-
 .02
                                     A-77

-------
       60
        50-
        40-
(ppm)   30 |
        20-
        10-
         0«7
                     i
                   .01
.015
.02
                                       Fuel/Aiif Ratio
            D  - Unifined Kerosene
            O  - JP-5
                       Figure A-14. Nitrogen Oxide Emissions
                                   T63-A-5A Engine (S/N 401331)
                                      A-78

-------
11.   REFERENCE

     Memo No.  PE71:CJN:er, 10340,  Ser F1002,  "NAVAIR Work Unit  Plan  No.  NAPTC-
     812, Development of Alternate Sources of JP-5 Fuel,  Report on  Endurance
     and Emission Tests of a T63-A-5A Engine  Using a Tar  Sands  Derived  JP-5",
     26 June 1975, 18 pp.
                                     A-79

-------
                                  TEST  18
               U.S. ARMY'S  ENERGY AND SYNTHETIC  FUELS  PROGRAMS
1.  FUELS TESTED
    Previously tested fuels are shown  in Table A-24.   Future testing is
    scheduled to focus on fuels from oil shale,  direct coal  liquefaction,
    and biomass.
2.  TEST EQUIPMENT
    A wide variety of powerplant systems must be satisfied if synfuels are
    to be adopted.  These range from 2-cycle spark-ignition  engines to large
    2-cycle and 4-cycle compression  ignition engines  found in self-propelled
    guns and tactical support equipment.
3.  TEST OBJECTIVES
    The Army Energy Plan establishes the basis for reducing  energy consump-
    tion, reducing dependency on conventional  hydrocarbon fuels, and tasks
    the Army to obtain a position of energy leadership.   One of the major
    programs of the plan is the alternative fuels program, which is directed
    towards minimizing potential loss  of military effectiveness from a dis-
    ruption of energy supplied under foreigh control.
4.  SPONSORING AGENCY
    U.S. Army
5.  CONTRACTOR                \
                                 This  information for many individual
                                 tests are described in separate
                                 abstracts.
6.  TEST SITE
7-  TEST CONDITIONS
8.  ENVIRONMENTAL MONITORING
9.  PROJECT STATUS            /
    The Army has evaluated the suitability of several synfuels for use in
    Army equipment (Table A-24).

                                   A-80

-------
    The current thrusts within the U.S.  Army's Alternative and Synthetic
    Fuels Program encompasses the following efforts:  Develop Capability
    for Using Synthetic and Alternative Fuels; Develop New, Accelerated
    Fuel-Engine Qualification Procedure Methodology; and Conduct Gasohol
    Evaluation in Tactical  Equipment.
          TABLE A-24.  PREVIOUSLY EVALUATED SYNTHETIC FUELS
Syncrude
Source:
Coal

Tar Sands


Shale




Shale



Process :
C.O.E.D.(Pyrolysis)

Steam Extraction
(Gulf Canada)

Paraho (Above-
Ground Retort)



Paraho (Above-
Ground Retort)


Fuels:
Gasoline
Distillate
Aviation
Turbine
(JP-5)
Gasoline
Diesel
Aviation
Turbine
(JP-5/JET-A)
Aviation
Turbine
(JP-5 & JP-8)
Diesel
When
Tested:
1973-74

1975


1976-77




1979-80



Product
Quality:
Marginal
Marginal
Excellent


Marginal
Poor
Marginal


Satisfac-
tory


10.  RESULTS
    The product quality of fuels tested so far are shown in Table A-24.   Test
    results from individual  tests are described in separate abstracts.
11.  MISCELLANEOUS
    The file described in this abstract contains four documents:  (1)  Army
    Energy R&D Plan 1981, (2) a magazine article describing the Army's  syn-
    fuel  program, (3) a photocopies set of overhead-projector transparencies
    describing the Army Mobility Fuels Program, and (4)  a progress report on
    fuels and lubricants research during 1980.
                                    A-81

-------
12.   REFERENCES

     Le Pera,  Maurice  E.   The  U.S.  Army's  Alternative and Synthetic Fuels
     Program.   Army Research,  Development,  and  Acquisition Magazine.  Septem-
     ber-October 1980.   pp.  18-20.

     Department of  the  Army.   Progress  of  Fuels and  Lubricants Research During
     FY 80.  U.S. Army  Mobility  Equipment  Research and Development Command
     (MERADCOM),  Fort Belvoir, Virginia.   January 1981.   22 pp.

     Department of  the  Army.  Army  Energy  R&D Plan -  1981.   U.S.  Army Mobility
     Equipment Research and  Development Command, Fort Belvoir, Virginia.
     March  12,  1981.
                                   A-82

-------
                                   TEST 19
        EVALUATION OF MILITARY FUELS REFINED FROM PARAHO-II SHALE OIL

1.    FUELS TESTED
     Synfuels:  shale-derived JP-5, JP-8, and marine diesel fuel (DFM) (see
     Table A-25.
     Reference fuels:  JP-5, diesel fuel No. 2, and Jet A fuel derived from
     petroleum.
2.    TEST EQUIPMENT
     In the gas  turbine combustion performance test, the combustor used is
     based on hardware from the Allison T-63 gas turbine engine used in several
     Army helicopters.
     In the diesel engine performance test, the four diesel engines used re-
     present critical and widespread engines in the military tactical  fleet:
     the militarized version of the Detroit Diesel  6V-53T;  the military-
     developed LDT-465-1C; a single cylinder from the Teledyne-Continental
     AVDS-1790 air-cooled diesel  mounted on a CUE crankcase; and a commercially
     configured  Detroit Diesel 3-53 diesel engine (see Table A-26 for test
     engine characteristics).
3.    TEST SITE
     U.S. Army Fuels and Lubricants Research Laboratory
     Southwest Research Institute
     San Antonio, Texas
4.    TEST OBJECTIVES
     •  To evaluate JP-5, JP-8, and DFM produced from Paraho-II shale oil  for
        specification requirements and other properties, and to ascertain  their
        performance in Army engine systems as a part of the overall program to
        develop  a capability for  consuming multisource fuels within the Depart-
        ment of  Defense.
                                     A-83

-------
TABLE A-25.   PROPERTIES OF FUELS  DERIVED FROM SHALE OIL
	 Properties
Specific Gravity, 15.6/15.6"C
Gravity, 'API
Distillation, *C
IBP
10Z Recovered
20! Recovered
501 Recovered
90Z Recovered
End Point
Z Recovered
Z Residue
Z Loss
Flash Point, 'C
Viscosity at 37.B*C,cSc
Viscosity at -20*C,cSt
Aniline Point, 'C
Cloud Point, *C
Pour Point, *C
Freezing Point, *C
Existent Gum, mg/100«l
Total Acid Number, mg KOH/g
Neutrality
Aromatics, volZ (FIA)
Olefins, volZ (FIX)
Carbon, vtZ
Hydrogen, vtZ
Nitrogen, ppm
Oxygen, vtZ
'Sulfur, vtZ
Thermal Oxidation Stability (JFTOT)
at 260°C
tf, mm Hg
Tube rating, visual
TDR-spun
TDR-spot
Net Heat of Combustion, HJ/kg
Smoke Point , mm
Aniline-Gravity Product
Visual Appearance
Color, ASTM Rating
Accelerated Stability, mg/100 •!
Particulate Matter, ag/1
Ash, wtZ
Cetane Number
Carbon Residue on
10Z bottoms, wtZ
Demulsif ication, minutes
Ring Carbon
Mono-aromatlcs, wtZ
Di-aromatics, wtZ
Trl-aromatics, wtZ
GC Distillation, 'C
0.1 wtZ off
1 wtZ off
10 wtZ off
20 wtZ off
50 wtZ off
90 wtZ off
95 wtZ off
99 wtZ off
99.5 wtZ off
HPLC Aromatics, WtZ
HPLC Saturates, wtZ
JP-8 	
0.8044
44.4
178
187
189
201
227
257
98.5
1.0
0.5
57
1.30
4.19
62.4
	
	
-52
0.4
0.01
	
21
2
66.05
13.70
0.31
0.40
0.002


0
2
10.0
12.0
1A
42.82
20.2
6,407
Straw, clear
0.5
0.29
0.3
	
45

	
	

13.84
1.19
0.003

120.1
153.6
170.4
176.6
203.1
241.0
252.2
274.6
285.7
23.5
76.5
JP-8
0.775-0.840
37-51
	
205 max
	
300 max
	
1.5 max
1.5 max
38 Bin
	
8.0 mix
	
	
-50 max
7 max
0.015 max
	
25 max
5 max
	
13.5 mln
	
	
0,30 max


25 max
<3
	
IB max
42.8 mln
19 mln
	
	
	
	
1 max
	
	

	
	

	
	
	

	
	
186 max
	
	
— .-
	
	
330 max
	
	
JP-5
0.8081
43.6
179
189
192
202
228
248
98.5
1.5
0
62
1.38
4.68
60.4
	
	
-51
0
0
	
22
2
85.92
13.66
<1
0.38
0.005


0
1
2.0
8.0
2C
42.68
17.5
6,134
White, clear
<0.5
0.14
0.1
	
45

	
	

13.54
1.36
0.002

136.5
159.7
174.5
185.3
208.9
245.9
255.0
278.8
291.6
24.9
75.1
JP-5
Requirements
36-48
	
205 max
-——
290 max
	
1.5 max
1.5 nax
60 mln
	
8.5 max
	
	
-46 max
7 max
0.015 max
	
25 max
5 max
	
13.5 min
	
	
0.40 max


25 max
<3
	
~
42.6 min
19 mtn
4,500 mln
	
	
	
1 max
	
	

	
	

	
	
	

	
	
185 max
	
	
	
	
	
320 max
	
	
DFM
37.9
206
233
243
264
295
312
99
1
0
80
2.71
67.0
10
-18
	
0
0.001
Neutral
30
1
86.54
.3.36
<1
0.37
0.004


0
3
11.5
19
1A
42.50
16.5
	
White, clear
<0.5
0.20
0.5
0
49

0.04
5

11.58
4.03
0.045

103.4
152.3
214.0
236.2
271.8
316.5
323.3
336.1
342.1
27.8
72.2
DFH
Requirements
Record
	
	
— —
357 max
385 max
™
3 max

60 aln
1.8-4.5
Record
-1 max
-7 max
	
	
0.3 max
Neutral
	
— -
	
	
	
	
1.00 max


	
	
	
	
	
	
	
Clear, bright
3 max
2.5 max
8 max
0.005 max
45 mln

0.2 max
10 max

	
	
	

—
	 	
—
	
	
.»—
	
	 .
_
	
	
                         A-84

-------
                               TABLE A-26.  TEST ENGINE CHARACTERISTICS
Manufacturer

Designation

Induction System


Combustion System


Strokes/Cycle

Number of Cylinders

Arrangement

Displacement


Bore and Stroke
Rated Power at Speed
  kW(Hp) at rpra

Max Torque at Speed
 Nm(lb-ft) at rpm
Compression Ratio

Fuel System
Detroit Diesel

6V-53T

turbocharged


direct
injection

2

6

60° V

5.21L
(318 in. )

9.84 x 11.43 cm
(3-7/8x4-l/2in.)
Detroit Diesel   Teledyne Continental
3-53

normally
aspirated

direct
injection

2

3

in-line

2.61L
(159 in. )
                                                              LDT-465-1C

                                                              turbocharged


                                                              M.A.N.


                                                              4

                                                              6

                                                              in-line

                                                              7.83L
                                                              (478 in. )
9.84 x 11.43 cm   18.0 x 19.2
(3-7/8x4-l/2in.)  (4.56x4.87 in.)
                         244(300) at 2800   67.1(90) at 2800  104(140) at 2600


                         834(615) at 2200   278(205) at 1800  556(410) at 1600

                         17                 21                22
Teledyne Continental*

CUE-1790

simulated
turbocharge

direct injection


4

1



2.44L
(149.1 in. )


(5.75x5.75 in.)
                         N70 unit
                         injector
                   N50 unit
                   injector
                  Bosch PSB6A-90EH-
                  5337A3 with
                  ABD-355-124-7 nozzles
*Single cylinder from Teledyne-Continental AVDS-1790-2D engine adapted to a CUE crankcase by others.

-------
    •  Fuels were analyzed to determine their specification requirements,
       storage stability, additive response, compatibility with petroleum-
       based fuels, combustion performance, diesel engine performance,  and
       microbiological growth susceptibility.

5.  SPONSORING AGENCIES

    U.S. Army Mobility Equipment Research and Development Command
    Ft. Belvoir, Virginia  22060
    Contract Monitor:  F.H.  Schaekel
    Telephone No:  703-664-6071

    U.S. Department of Energy
    Bartlesville Energy Technology Center
    Bartlesville, Oklahoma  74003
    Project Officer:   Dr. D.W. Brinkman
    Telephone No:  918-336-2400

6.  CONTRACTOR

    Southwest Research Institute
    Energy Systems Research  Division
    San Antonio, Texas  78284
    Principal Investigator:   John N.  Bowden
    Telephone No:  512-684-5111

7.  TEST CONDITIONS

    Table A-27 presents the  operating conditions which represent the air flow

    rates in the actual engine for the six different power points (idle to
    full power)  investigated.  Emission data were recorded at each power point
    for each fuel.

    Three diesel engines were used during maximum power output and specific

    fuel consumption  testing:  the 6V-53T, the LDT-465-K, and the AVDS-1790.
    The engines  were  mounted on dynamometer test stands and alternately

    operated on  the shale-derived JP-5 and DFM and the petroleum-derived re-
    ference fuel - diesel fuel No. 2.

    The 3-53 diesel engine was operated for 210 hours with shale-derived DFM
    according to the  Army/CRC wheeled-vehicle endurance cycle to evaluate the
    wear and deposit  formation tendencies of this fuel.

8.  ENVIRONMENTAL MONITORING

    CO, NO , unburned hydrocarbons, and smoke.
          A

                                   A-86

-------
TABLE A-27.  T-63 COMBIJSTOR RIG OPERATING CONDITIONS

Mode
Ground Idle
—
Descent
Crui se
Cl imb/Hover
i>
5 Takeoff
Percent
Power
10
25
40
55
75
100
Burner
Inlet Air
Pressure,
kpa
230
283
329
369
418
477
Burner
Inlet Air
Temperature,
°K
422
452
478
294
518
547
Air Flow
Rate,
kg/s
0.64
0.75
0.86
0.93
1.02
1.10
Fuel Flow
Rate,
kg/m
0.42
0.54
0.68
0.93
1.01
1.30
Fuel /Air
Ratio
0.0109
0.0121
0.0131
0.0145
0.0166
0.0198

-------
 9.   PROJECT  STATUS

     Work was conducted  from  June  1979  through  November  1980.   Interim report

     dated March  1981.   Additional  tests  planned  for  FY  82  usino other types

     of army  equipment.

10.   RESULTS

     Specification Analysis

     t  The shale-derived  fuels met virtually all  the  military specifications
        with  the  exception of the  failure of JP-5  to meet copper corrosion  re-
        quirement and  DFM  to  meet  maximum limit for pour point as seen in
        Table A-25.

     Storage  Stability Tests

     •  Storage  stability  of  the shale-derived  fuels was equivalent to that of
        petroleum products at 43°C for  32 weeks.   Accelerated  stability at  80°
        and 150°C indicated instability at  the  lower temperature, but none  at
        150°C.

     Compatibility,  Additive  Response,  and  Microbiological  Growth Tests

     •  Compatibility  tests with JP-5 and DFM petroleum- and shale-derived
        fuels indicated  that  the fuels  are  compatible  with  each other.   JP-5
        and DFM  synfuels responded to the addition of  a  centane improver
        additive  in  a  manner  similar to that of a  petroleum-based fuel.  The
        addition  of  a  corrosion inhibitor incrementally  improved the corrosion
        tendencies of  JP-5 and DFM but  did  not  affect  the JP-8.   Microbiolo-
        gical growth susceptibility tests showed  that  growth of C1 adosporiurn
        resinae  was  supported by shale-derived  JP-5 and  OFM.

     Gas Turbine  Combustion Performance

     t  In general,  the  combustion properties of  synthetic  JP-5 and DFM are
        not significantly  different from  the respective  petroleum-derived
        fuel  (see Table  A-28).

     •  Combustion inefficiency is determined by  CO and  UHC in the exhaust.
        Figure A-15  shows  that DFM gives  slightly  higher CO emissions than
        JP-5  and  Jet A.  Contrary  to its  fuel properties, DFM  gave somewhat
        lower UHC emissions than the other  fuels  as seen in Figure A-16.

     •  NOX emissions  shown in Figure A-17  were essentially the same for both
        shale fuels  and  Jet A at all operating  conditions.

     t  Exhaust  smoke  indices for  the shale-derived fuels were higher than
        the respective Jet A  fuel.
                                    A-88

-------
TABLE A-28.  SUMMARY OF GAS TURBINE COMBUSTION RESULTS
Power
Point
100
100
100
75
75
75
55
55
55
40
40
40
25
25
25
10
10
10
Fuel
No.
0
1
2
0
1
2
0
1
2
0
1
2
0
1
2
0
1
2
Fuel Flame
Type Radia.
Jet A
JP-5
DFM
Jet A
JP-5
DFM
Jet A
JP-5
DFM
Jet A
JP-5
DFM
Jet A
JP-5
DFM
Jet A
JP-5
DFM
42.8
59.7
60.1
37.0
48.9
50.7
31.9
43.7
48.1
26.7
37.4
43.2
23.3
30.0
39.2
17.8
26.2
31.9
Smoke
No.
28.9
48.7
45.2
32.1
38.1
41.0
15.8
19.7
22.6
12.0
25.2
27.9
11.7
21.2
29.9
7.9
17.7
23.2
Smoke
mg/M
4.3
13.2
10.8
5.1
7.1
8.46
1.8
2.4
2.9
1.3
3.4
4.0
1.27
2.6
4.5
0.84
2.06
3.0
NO
X
E.I.
7.2
7.2
6.7
5.5
5.7
4.7
4.7
4.6
4.3
4.7
4.7
4.7
3.1
3.6
3.3
1.3
3.3
3.1
CO
E.I.
9.5
9.1
13.8
30.3
30.8
34.3
48.3
47.7
50.1
59.6
59.9
65.4
82.3
75.8
102.3
113.6
107.9
118.0
UBH
E.I.
0.2
0.4
0.4
2.0
1.9
2.9
7.1
7.3
7.0
11.7
13.3
12.5
35.9
30.7
33.7
71.5
82.9
69.0
Combustion
Efficiency
99.79
99.78
99.67
99.31
99.28
99.13
98.64
98.59
98.54
98.14
97.97
97.91
95.57
96.13
95.35
92.37
91.52
92.42
                         A-89

-------
                120
   100
 o>
 x"
 iu
 Q
 Z
' Z
 o
 w
 5
 LU
 8
                 80
                 60
                 40
                 20
                                    1 JP-5 (SHALE)
                                    2 DFM (SHALE)
                                    0 JET A (PETROLEUM)
                         20     40      60     80
                         PERCENT OF FULL POWER
                                                    100
   Figure A-15.   Effect of  Fuel  on Carbon Monoxide Emissions
                100

                90

               , 80
               l
                70

                60
              * 50
              Q
              Z
              Z
              o
   30

   20

   10

    0
                   1 JP-5 (SHALE)
                   2 DFM (SHALE)
                   0 JET A (PETROLEUM)
                                                    0,1.2
                         20     40     60     80
                          PERCENT OF FULL POWER
                                      100
Figure A-16.   Effect of Fuel  on Unburned Hydrocarbon Emissions
                                A-90

-------
                     10
                    LLJ
                    D
                    u.
                    u.
                    O
                    0>

                    X~
                    Q
                    2
                    §
                    to
                    e/2
                    I
                    UJ
                                               +2
JP-5 (SHALE)

DFM (SHALE)
                                      0 JET A (PETROLEUM)
                             20     40     60     80

                              PERCEMT OF FULL POWER
              100
                 Figure A-17.   Effect  of Fuel  on NO  Emissions
                                                   A
     Diesel  Engine Performance

     •  In the power output and specific fuel consumption tests of  the three
        diesel engines using shale-derived JP-5 and DFM and  petroleum-derived
        diesel fuel, the only observable difference between  the fuels were
        those attributed to differences in heat of combustion.  The  percent
        change in observed horsepower and volumetric fuel consumption for the
        three test engines are summarized in Tables A-29, A-30, and  A-31.
     0  Results of the 210-hour endurance test showed no power loss  during the
        test nor evidence of distress or component failure;  and piston deposits
        and  component wear were acceptable.  The results of  the shale-derived
        DFM  in this test were indistinguishable from those obtained  using a
        petroleum-derived diesel fuel.

11.   REFERENCE

     Bowden, J.N., et al.  Military Fuels Refined From Paraho-II  Shale Oil.
     Prepared by Southwest Research Institute for U.S. Army  (MERADCOM),  Interim
     Report  AFLRL No.  131.  March 1981.
                                     A-91

-------
     TABLE A-29   PERCENT CHANGE IN OBSERVED HORSEPOWER AND VOLUMETRIC
                  FUEL CONSUMPTION IN DETROIT DIESEL 6V-53T
Engine Speed
1800
2000
2200
2400
2600
2800
Average
From DF-2
Power
-0.8
-1.4
-1.8
-1.8
-1.5
-2.4
-1.7 ± 0.5
to DFM
Fuel*
1.5
1.5
1.1
1.1
1.2
0.9
1.2 ± 1.0
From DF-2
Power
-3.4
-5.1
-5.3
-6.2
-7.3
-8.4
-6.0 ± 0.5
to JP-5
Fuel*
5.8
4.2
3.8
5.5
5.5
6.6
5.2 ± 1.0

Brake specific volumetric  consumption  (Gal/BHP-hr).
       TABLE A-30.   PERCENT CHANGE  IN  OBSERVED POWER AND VOLUMETRIC
                    FUEL CONSUMPTION  IN  CUE-1790

Engine Speed,
rpm
1800
2000
2200
2400
Average
Std Dev
From DF-2
Power
+2.7
+1.4
+3.7
+1.8
+2.4
1.0
to DFM
Fuel*
-1.1
-1.4
-3.0
-2.9
-2.1
1.0
From DF-2
Power
-2.9
-4.6
-1.1
-2.3
-2.7
1.5
to JP-5
Fuel*
7.0
0.3
1.8
3.8
3.2
2.9
Brake specific volumetric consumption  (Gal/BHP-hr).
                                   A-92

-------
            TABLE A-31.   PERCENT  CHANGE  IN  OBSERVED  POWER AND
                          FUEL  CONSUMPTION  IN  LDT-465-1C
                          (From Diesel  Fuel  to DFM)

Engine Speed,
rpm
1600
2100
2600
Average
Change in
Max Power, %
-1.9
-0.6
+0.4
-0.7
Change
Full Power
+1.3
-0.1
+ 1.0
+1
in Fuel*, %
3/4 of Full Power
+0.8
+1.8
+2.7
.3

Brake specific volumetric consumption (Gal/BHP-hr).
                                    A-93

-------
                                   TEST 20
                   EVALUATION OF FUEL CHARACTER EFFECTS ON
                        FT01  ENGINE COMBUSTION SYSTEM

1.   FUELS TESTED
     Reference fuels:   thirteen non-synfuels were tested; i.e., a typical
     JP-4; five blends of JP-4 with a single ring aromatic concentrate; a
     double ring aromatic concentrate, and a light oil; a typical JP-8; five
     blends of JP-8 with the  same three compounds used for the JP-4 blends;
     and a Number 2 diesel  fuel.   The thirteen fuels incorporated systematic
     variations in hydrogen content (12.0 to 14.0 weight percent), aromatic
     type (monocyclic  or bicyclic), initial  boiling point (285 to 393 K by
     gas chromatograph), final boiling point (532 to 679 K also by gas chroma-
     tograph), and viscosity  (0.83 to 3.25 cSt at 300 K).
2.   TEST EQUIPMENT
     General  Electric  F101  turbofan engine main combustion system elements.
     A sector rig and  a full-annular rig were used to generate the combustion
     data.  Separate rigs were used to obtain carboning and nozzle fouling
     data on  the fuels.
3.   TEST SITE
     General  Electric  test  facility, Evendale, Ohio.
4.   TEST OBJECTIVES
     •  To determine the effects  of broad variations in fuel  properties on
        the performance, emissions, and durability of the F101 combustion
        system.
     •  The rationale  for selection of the test fuels was to span systematical
        ly the possible future variations in key properties that might be
        dictated by availability, cost, the use of nonpetroleum sources for
        jet fuel production,  and  the possible change from JP-4 to JP-8 as the
        prime USAF aviation turbine fuel.
                                    A-94

-------
5.    SPONSORING AGENCIES
     Air Force Aero Propulsion Laboratory (SFF)
     Air Force Wright Aeronautical Laboratories
     Wright-Patterson AFB, Ohio  45433
     Government Project Engineer:  T.A. Jackson
     Telephone Number:  513-255-2008
     Additional funding and technical guidance was provided by the Environ-
     mental  Sciences Branch of the Environics Division in the Research and
     Development Directorate of HQ Air Force Engineering and Services Center
     located at Tyndall Air Force Base, Florida.
6.    CONTRACTOR
     General Electric Company
     Aircraft Engine Group
     Cincinnati, Ohio  45215
     Project Officer:  C.C. Gleason (and T.L. Oiler)
     Telephone Number:  513-243-3207
7.    TEST CONDITIONS
     Test fuels were evaluated in:  (a) 13 high pressure/temperature full-
     annular combustor performance/emissions/durability tests; (b) 13 atmos-
     pheric pressure/high temperature full-annular combustor pattern factor
     performance tests; (c) 13 high pressure/temperature single fuel nozzle/
     swirl  cup carbon deposition tests; (d)  14 low pressure/temperature 54-
     degree sector combustor cold day ground start/altitude relight tests;
     (e) 15 high temperature short duration  fuel nozzle fouling tests; and
     (f) 0 high temperature longer cyclic fuel nozzle valve gumming tests.
8.    ENVIRONMENTAL MONITORING
     NO , CO, smoke, and unburned hydrocarbons.
       A
9.    PROJECT STATUS
     Testing and analytic activity occurred  from August 1977 through September
     1978.   Final  report submitted June 1979.
10.   RESULTS
     •  As  expected, gaseous emissions and smoke levels were strongly depen-
        dent upon  operating conditions for all fuels tested.

                                    A-95

-------
     •  Low power emissions of CO and UHC were only significant at idle, and
        decreased sharply with increasing power level.  Levels of CO were
        readily correlated with power level; UHC exhibited more variability
        while following a similar trend.

     •  Oxides of nitrogen were primarily a high power emission and, for fuels
        with negligible amounts of fuel-bound nitrogen, correlated readily
        with power level.
     •  At high power conditions, fuel  hydrogen content was found to have a
        very significant effect on annular liner temperature, smoke, and NOX
        levels.   While smoke levels decreased with increasing hydrogen content,
        the levels were very low with all  the fuels (i.e., smoke levels of 0.4
        to 3.2,  which are on the threshold of smoke measurement system accu-
        racy).

     t  At low power operation, CO and  UHC correlated  with the 10 percent dis-
        tillation recovery temperature  and with relative spray droplet size
        (a function of fuel  viscosity,  surface tension, and density).

     •  Cold day ground start and altitude relight correlated with fuel atomi-
        zation/volatility parameters.

     t  Combustor liner life analyses  yielded relative life predictions of
        1.00,  0.72, 0.52, and 0.47 for" fuel  hydrogen contents of 14.5, 14.0,
        13.0,  and 12.0 percent, respectively.   At  the  present state of turbine
        stator development,  no fuel  effect on life is  predicted.

     •  Extended cyclic fuel  nozzle valve  gumming  tests revealed significant
        effects  of fuel  type and temperature on nozzle life.   The results cor-
        related  with laboratory thermal stability  ratings  of the fuels based
        on tube  deposits  alone.

11.   REFERENCE

     Gleason,  C.C., T.L.  Oiler,  M.W.  Shayeson,  and D.W.  Bahr.   Evaluation of
     Fuel  Character Effects  on the F101 Engine  Combustion  System.   AFAPL-TR-
     79-2018,  CEEDO-TR-79-07,  U.S.  Air  Force,  Wright-Patterson AFB,  Ohio,
     June  1979.   199 pp.
                                    A-96

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                                   TEST 21
                   EVALUATION OF FUEL CHARACTER EFFECTS ON
                           J79 SMOKELESS COMBUSTOR
     FUELS TESTED
     Reference fuels:   thirteen refined and blended non-synfuel  fuels were
     tested;  i.e.,  a current JP-4, five blends of the JP-4,  a current JP-8,
     five blends of the JP-8, and a No. 2 diesel fuel.   These fuels incorpo-
     rated systematic variations in hydrogen content (11.9 to 14.5 weight
     percent), aromatic type (monocyclic or dicyclic),  initial  boiling point
     (298 to  409 K by gas chromatograph), final  boiling point (554 to 646 K,
                                                                     p
     also by  gas chromatograph), kinematic viscosity (0.90 to 3.27 mm /s  as
     294.3 K), and thermal  stability breakpoint (518 to 598  K by JFTOT)  for
     evaluation.
2.    TEST EQUIPMENT
     The J79-17C turbojet engine main burner as represented  by  two single can
     combustor rigs and a fuel  nozzle rig.
3.    TEST SITE
     General  Electric test facility, Evendale, Ohio.
4.    TEST OBJECTIVES
     •  To determine the effects of broad variations in fuel  properties  on
        the performance, emissions, and durability of the combustion system
        identified above.
     •  Compare results to those previously obtained in similar tests of  the
        J79-17A and F101 combustion systems.
     •  Test  fuels were selected to represent variations in  properties that
        can be expected to affect the combustion system; ranges of property
        variations were set to  represent broad limits that may  be anticipated
        in using fuels refined  from an expanded portion of the  petroleum  re-
        source and from non-oetroleum hydrocarbon sources.
     •  The combustion system was selected because it represented a redesign
        of a  system in wide usage by the USAF (as well  as one which was  tested
        under a preceeding fuels program, the J79 standard configuration).

                                    A-97

-------
        This provided an opportunity to compare two different combustion
        systems designed for the same engine.
5.   SPONSORING AGENCY
     Aero Propulsion Laboratory (AFWAL/POSF)
     Air Force Wright Aeronautical Laboratories (AFSC)
     Wright-Patterson AFB, Ohio  45433
     Government Project Engineer:   Jeffrey S. Stutrud
     Telephone No:  513-255-2008
     Partial funding and technical support in the area of the measurement and
     analysis of gaseous emissions and smoke data were provided by the Envi-
     ronmental Sciences Branch of the Environics Division in the Research and
     Development Directorate of HQ Air Force Engineering and Services Center.
6.   CONTRACTOR
     General Electric Company
     Aircraft  Engine Business Group
     Technology Programs and Performance Technology Dept.
     Cincinnati, Ohio  45215
     Principal Investigator:  C.C. Gleason (and T.L. Oiler)
     Telephone No:  513-243-3207
7.   TEST CONDITIONS
     The fuels were evaluated in:   (a) 14 high pressure/temperature combustor
     cold-day ground start/altitude relight tests; (b) 14 low pressure/temper-
     ature combustor cold-day ground start/altitude relight tests; and (c) 7
     high temperature cyclic fuel  nozzle fueling tests.
8.   ENVIRONMENTAL MONITORING
     NO , CO, smoke, and unburned  hydrocarbons.
       A
9.   PROJECT STATUS
     The period of performance for this effort,  including testing and analysis,
     was July 1, 1979 through June 1, 1980.  Final report is dated November
     1980.
10.   RESULTS
     •   As expected, gaseous emissions and smoke levels  were strongly depen-
        dent upon  operating conditions for all fuels tested.
                                    A-98

-------
    •  Low power emissions of CO and UHC were only significant at idle, de-
       creasing sharply with increasing power level.  Levels of CO were readi-
       ly correlated with power level; UHC exhibited more variability while
       following similar trends.

    •  Oxides of nitrogen were primarily a high power emission and, for fuels
       with negligible amounts of fuel-bound nitrogen, correlated readily
       with power level.

    •  Smoke increased with power level but for the system tested (a low smoke
       combustor) the emission was below 20 Smoke Number.  This is below
       visible and also in a range where the accuracy of the measurement sys-
       tem is suspect.
       At
       be
high power operating conditions, fuel hydrogen content was found to
a very significant fuel property with
        flame  radiation,  smoke,  and  NO   emission
respect
levels.
to liner temperature,
     0  At  idle and  cruise  operating  conditions, CO and HC emission levels
       were  found  to  be  dependent  on
       spray droplet  size.
                           both fuel hydrogen content and relative
     0   At  cold-day  ground  start  conditions,  lightoff correlated with the
        relative  fuel  droplet  size.
     0   Altitude  relight  limits at  low  flight  Mach  numbers were fuel dependent
        and also  correlated with  the  relative  fuel  droplet size.
     0   Combustor liner life analyses,  based  on  the test data, yielded relative
        life predictions  of 1.00, 0.93,  0.83,  and 0.73  for fuel hydrogen con-
        tents of  14.5,  14.0, 13.0,  and  12.0 percent, respectively.
     0   High temperature  cyclic fuel  nozzle fouling tests revealed  significant
        effects of fuel quality and operating  temperature on nozzle life.  The
        results correlated  with laboratory thermal  stability rating of the
        fuels.
11.   REFERENCE

     Gleason, C.C.,  T.L.  Oiler,  M.W.  Shayeson,  and  M.J.  Kenworthy.   Evaluation
     of Fuel  Character Effects  on  J79 Smokeless Combustor.  AFWAL-TR-80-2092,
     ESL-TR-80-46,  U.S.  Air  Force,  Wright-Patterson AFB,  Ohio,  1980.   178 pp.
                                    A-99

-------
                                   TEST 22
                   EVALUATION OF FUEL CHARACTER EFFECTS ON
                        J79 ENGINE COMBUSTION SYSTEM
     FUELS TESTED
     Reference fuels:   thirteen non-synfuels were tested; i.e., a typical JP-
     4; five blends of JP-4 with a single ring aromatic concentrate, a double
     ring aromatic concentrate, and a light oil;  a typical  JP-8; five blends
     of JP-8 with the  same three compounds used for the JP-4 blends; and a
     Number 2 Diesel  fuel.  The thirteen fuels incorporated systematic varia-
     tions in hydrogen content (12.0 to 14.5 weight percent), aromatic type
     (monocyclic or bicyclic), initial  boiling point (285 to 393 K by gas
     chromatograph),  final boiling point (532 to  679 K also by gas chromato-
     graph), and viscosity (0.83 to 3.25 cSt at 300 K).
2.   TEST EQUIPMENT
     J79 turbojet engine main combustion system elements.  Two single can test
     rigs were used to generate combustion data at high and low pressure points
     A fuel nozzle rig was used to obtain nozzle  fouling data on the test
     fuels.
3.   TEST SITE
     General Electric  test facility, Evendale, Ohio.
4.   TEST OBJECTIVES
     t  To determine  the effects of broad variations in fuel properties on the
        performance,  emissions, and durability of the J79 combustion system.
     •  The rationale  for selection of  the test fuels was to span systematical-
        ly the possible future variations in key  properties that might be
        dictated by availability,  cost, the use of nonpetroleum sources for
        jet fuel production,  and the possible change from JP-4 to JP-8 as the
        prime USAF aviation turbine fuel.
                                   A-100

-------
5.    SPONSORING AGENCIES

     Air  Force Aero  Propulsion  Laboratory (AFWAL/POSF)
     Air  Force Wright  Aeronautical  Laboratories
     Wright-Patterson  AFB,  Ohio  45433

     Government Project  Engineer:   T.A.  Jackson
     Telephone No:   513-255-2008

     Additional funding  and technical  guidance was  provided by the Environ-

     mental  Sciences Branch of  the  Environics Division  in the  Research and

     Development  Directorate of HQ  Air Force Engineering and Services  Center
     located at Tyndall  Air Force Base,  Florida.

6.    CONTRACTOR

     General  Electric  Company
     Aircraft Engine Group
     Cincinnati,  Ohio  45215

     Project Officer:  C.C. Gleason (or  T.L.  Oiler)
     Telephone No:   513-243-3207

7.    TEST CONDITIONS

     Test fuels were evaluated  in:   (a)  14 high pressure/temperature combustor

     performance/emissions/durability  tests;  (b)  14  low pressure/temperature

     combustor cold-day  ground  start/altitude relight tests; and  (c) 18 high

     temperature  fuel  nozzle fouling  tests.

8.    ENVIRONMENTAL MONITORING

     NO , CO, smoke, and  unburned hydrocarbons.

9.    PROJECT STATUS

     Testing and  analytical activity  occurred from  June 1977 through August

     1978.   Final report  is dated June 1979.

10    RESULTS

     •   Fuel  hydrogen  content strongly affected smoke,  carbon  deposition, liner
        temperature, flame  radiation  and moderately  affected NOX  emissions.
        Hydrogen  content  is, therefore,  probably  the single most  important fuel
        property, particularly  with respect  to high  power performance  and
        emission  characteristics and  combustor durability (life).
     t
Fuel volatility (as indicated by initial boiling range) and viscosity
effects became evident at low power operating conditions.  Cold day
                                   A-101

-------
        starting and altitude relight capability are highly dependent upon
        these properties.

     •  Within the range tested,  neither aromatic type (monocyclic or bicyclic)
        nor final  boiling  range  produced any direct effect on emissions or
        combustor performance.

     •  None of the fuel  properties  produced any measurable effect on combus-
        tor exit temperature  distribution (profile and pattern factor), idle
        stability, fuel  nozzle fouling  tendency, or turbine life.

     t  The fuel  nozzle  fouling  tests were  indeterminate.   More sophisticated
        long-term tests  are needed to determine  the effects of fuel  thermal
        stability on fuel  supply/injection  system components.

11.   REFERENCE

     Gleason,  C.C.,  T.L. Oiler, M.W.  Shayeson, and  D.W. Bahr.   Evaluation  of
     Fuel  Character Effects on 079 Engine Combustion System.   AFAPL-TR-79-
     2015,  CEEDO-TR-79-06, U.S. Air  Force,  Wright-Patterson AFB, Ohio,  June
     1979,  197 pp.
                                   A-102

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                                   TEST 23
           FUEL CHARACTER EFFECTS ON CURRENT, HIGH PRESSURE RATIO,
                     CAN-TYPE TURBINE COMBUSTION SYSTEMS

1.    FUELS TESTED
     Reference fuels:   twelve fuels were tested including a baseline JP-4, a
     baseline JP-8,  and five blends of each baseline fuel.   Hydrogen content,
     aromatic type,  distillation range, and viscosity were  varied by blending
     JP-4 and JP-8 fuels with a mineral seal  oil and two types of aromatic
     solvents.   The  fuel matrix incorporated  systematic variations in hydrogen
     content (12.0 to 14.4 percent wt.), aromatic type (single or multi-ring),
     10 percent distillation point (353 to 464 K by gas chromatograph),  final
     boiling point (541 to 612 K by gas chromatograph), and viscosity (0.888
     to 2.305 centi-stokes at 298 K).
2.    TEST EQUIPMENT
     A single can combustor rig, simulating a 36° segment of the mainburner
     of the TF41  turbofan engine, was used to generate high and low pressure
     data.   A special  fuel nozzle rig was used to generate  combustor carboning
     and nozzle fouling data.
3.    TEST SITE
     Detroit Diesel  Allison, Indianapolis, Indiana.
4.    TEST OBJECTIVES
     •  The purpose  of this program was to determine the effects of fuel  pro-
        perty variations on the performance,  exhaust emission, and durability
        characteristics of the TF41  turbofan  engine combustion system.   The
        system  was selected because it is one of two high pressure ratio,
        connular  system in use by the Air Force.
     •  The rationale  for selection and testing of test fuels  was to study the
        operational  and performance characteristics that might occur with  the
        ultimate  use of non-petroleum-derived fuels in the  TF41  turbofan
        engine.
                                   A-103

-------
5.   SPONSORING AGENCY
     Air Force Aero Propulsion Laboratory
     Air Force Wright Aeronautical Laboratory
     Air Force Systems Command
     Wright-Patterson AFB, Ohio  45433
     Government Project Engineer:  T.A. Jackson
     Telephone No:  515-255-2008
     Partial funding and technical support in the area of the measurement and
     analysis of gaseous emissions and smoke data were provided by the Envi-
     ronmental Sciences Branch of the Environics Division in the Research and
     Development Directorate of HQ Air Force Engineering and Services Center
     (HQ AFESC/RDVC).
6.   CONTRACTOR
     Detroit Diesel Allison (DDA)
     Division of General Motors Corporation
     Indianapolis, Indiana  46206
     Project Officer:  Dennis Troth
     Telephone No:  317-242-5000
7.   TEST CONDITIONS
     Performance tests were accomplished at idle, altitude cruise,  dash,  and
     takeoff conditions.  Sea level  and altitude ignition tests were also
     completed.  Carboning and fuel  nozzle fouling tests were conducted under
     accelerated failure conditions.
8.   ENVIRONMENTAL MONITORING
     NO ,  CO, smoke,  and unburned hydrocarbons.
       A
9.   PROJECT STATUS
     Test and analytical activity were conducted from June 15,  1978 through
     June 15, 1979.   Final  report is  dated April 1980.
10.   RESULTS
     •   Fuel fouling  and carboning characteristics were established.   Combustor
        operating  parameters such as  liner temperature, pattern factor, igni-
        tion fuel/air ratio, lean blowout fuel/air ratio, and exhaust emissions
        were correlated to fuel  properties.
                                   A-104

-------
    •  This program did have a problem with fuel-to-fuel contamination.  As a
       result, two fuel data files were created:  one file for high pressure
       tests, the other for low pressure tests.  High pressure combustor data
       such as performance, exhaust emissions and durability were correlated
       with fuel information identified as high-pressure fuel data.  Altitude
       relight and stability measurements were correlated with low-pressure
       fuel data.

    •  Hydrogen content, total aromatic content, and multi-ring aromatic
       content were found to strongly affect CO and smoke emissions, combus-
       tion efficiency, and liner wall temperatures at  high power operation.

    •  None of the fuel property characteristics produced any measurable
       effect on combustor exit temperature distribution (pattern factor or
       radial profile), idle performance or emissions,  or hot section hardware
       life.
    •  Maximum achievable ignition altitude was most strongly influenced by
       total  aromatic  content  and hydrogen content.  Once ignition was
       achieved, combustor stability was controlled by  10 percent boiling
       point, viscosity, vapor pressure, and surface tension.

11.  REFERENCE

    Vogel,  R.E., D.L.  Troth, and A.J. Verdouw.  Fuel Character Effects on
    Current,  High  Pressure Tatio, Can-Type Turbine Combustion Systems.  AFAPL-
    TR-79-2072,  ESL-TR-79-29,  U.S. Air Force,  Wright-Patterson AFB, Ohio,
    1980.   148  pp.
                                    A-105

-------
                                   TEST 24
                    LOW NO  HEAVY FUEL COMBUSTORS CONCEPT
                          y\
1.    FUELS TESTED
     Synfuel:   middle distillate SRC-11  fuel.
     Reference fuels:  low quality petroleum residual, and petroleum reference
     distillate fuel  (see Table A-32).
                        TABLE A-32. FUEL PROPERTIES


Hydrogen, wt %
Carbon, wt %
Nitrogen (FBN)
wt%
10%. Dist.
6F (K)
End point
°F (K)
Pour point,
6F (K)
Petroleum
Distillate
(ERBS)*
12.88
87.05
0.013
375 (464)
645 (614)
-35 (236)
Petroleum
Residual
(RESID)
11.24
87.39
0.27
572 (573)
1026 plus
(825)
40 (278)
Synthetic-CDL
(SRC-II)
8.81
85.84
0.83
410 (483)
597 (587)
-50 (228)

    *Experimental  Referee Broad Specification
2.    TEST EQUIPMENT
     Air-staged combustor with rich burning zone followed by quench zone and
     a lean reaction and dilution zone;  sized for use with Detroit Diesel
     Allison Model  570-K industrial gas  turbine.
3.    TEST SITE
     Detroit Diesel Allison high pressure test facility, Indianapolis, Indiana.
                                   A-106

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4.    TEST  OBJECTIVES

     t   Assess  the capability of Model  570-K turbine to function in an environ'
        mentally acceptable fashion on  the three fuels described above.
     0   Emission and performance goals  are shown in Table A-33.

       TABLE  A-33.  EMISSIONS AND PERFORMANCE GOALS AND TEST RESULTS*
Emissions and Performance
Parameters
FBN content, wt %
Maximum EPA NO. ppm at 15% 09
X L.
Program NO goal, ppm at 15% 09
X C.
Minimum NO measured, ppm at 15% 09
X c.
Program smoke goal, SAE smoke number
Measured smoke, SAE smoke number
Program combustion efficiency goal, %
Demonstrated combustion efficiency, %

ERBS
0.013
180
90
49
20
5
99
99.9
Test Fuels
Residual
0.27
230
230
53
20
3
99
99.9

SRC-II
0.88
230
230
50
20
3
99
99.9
Rich-zone equivalence ratio at minimum
  measured NO,
 1.25
 1.40
 1.35
Measured CO,  ppm at 15% 02
Measured unburned hydrocarbons,  ppm at
  15% 00
22
24
25
25
Rich-zone  maximum metal  temperature,°K
 1,015
(1,366)
 1,170
(1,644)
 1,110
(1,541)
k
 Operating  conditions:   Rich/quench/lean  (RQL)  combustor
                        6% pressure  drop
                        0.60 lean-zone equivalence  ratio
                        Maximum continuous  power conditions
                                    A-107

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 5.   SPONSORING AGENCIES

     U.S.  Department of Energy
     Office of Coal  Utilization
     Heat  Engine and Heat  Recovery Division

     Project Officer:   Warren  Bunker
     Telephone No:   301-353-2816

     NASA-Lewis Research Center  (Technical Program Management)
     Cleveland, Ohio  44135

     Project Officer:   J.  Notardonato
     Telephone No:   216-433-4300,  Ext.  6132

 6.   CONTRACTOR

     Detroit Diesel  Allison
     Indianapolis,  Indiana
     Project Manager:   A.S.  Novick
     Telephone No:   317-242-5428

 7.   TEST  CONDITIONS

     Combustor inlet temperature:   300°F  and  575°F

     Lean  zone equivalence ratios:  0.45  to 0.50,  and  0.55 to 0.60

     Total  mass flow:   rated airflow and  125% rated airflow

     Combustor was  operated  at maximum  continuous  power,  as well  as idle power
     and 50% and 70% load  power.

 8.   ENVIRONMENTAL  MONITORING

     Carbon monoxide,  unburned hydrocarbons,  nitrogen  oxides, carbon dioxide,

     smoke.

 9.   PROJECT STATUS

     Project was begun in  1980 and completed  in  October 1981.

10.   RESULTS (See Table A-33)

     •   The combustor  was  able to  achieve low NOX  with significantly different
        fuels and levels of  fuel-bound  nitrogen  at 50% and 70% load" power and
        maximum continuous oower.

     t   High NOX levels (approximately  260 ppm at  15%  02) were obtained with
        SRC-II fuel  at idle  power  due to  burn-through  in  the combustor dome,
        which shifted  the  rich zone equivalent ratio below stoichiometric or
        to  full  lean conditions.
                                    A-108

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     •   Unburned  hydrocarbons  measured at all  power levels were all  below  25
        ppm.

     t   Both  CO and smoke varied directly with rich zone equivalence ratio and
        inversely with lean zone equivalence ratio.  Higher inlet temperatures
        reduced CO and smoke emissions.   Smoke levels were usually below 10
        smoke number.

11.   MISCELLANEOUS

     Project  is part of a multiple contract effort sponsored by DOE  to  develop

     low NO  combustor technology.  Other participating contractors  are:
           A
     Westinghouse, General  Electric, United Technologies Corporation, and

     Solar Turbine International.

12.   REFERENCE

     Novick,  A.S. and D.L.  Troth.  "Low NOX Heavy Fuel Combustor Concept Pro-
     gram".  Detroit Diesel Allison Division of General Motors. DOE-NASA-014B-1,
     NASA CR-165367, October 1981.
                                    A-109

-------
                                  TEST  25
                    LOW NO   HEAVY  FUEL COMBUSTOR CONCEPT
                         /\

1.    FUELS TESTED
     Synfuel:   SRC-11  fuel oil.
     Reference fuels:   low quality petroleum residual  and petroleum reference
     distillate fuel.    :
2.    TEST EQUIPMENT
     The combustion  configurations and their variations evaluated in this
     study are described below.
     A.  Rich Burn - Lean Burn Concept
     The baseline configuration is the rich-lean (rich burn-quick quench)
     staged combustion system.  This concept consists  of a metered primary
     zone airflow tube which provides the capability of varying the burner
     front end equivalence ratio within  a pre-mix pre-vaporized fuel prepara-
     tion system or  an airblast fuel nozzle centered in a 45-degree recessed
     air swirler fuel  preparation device, a rich burning combustion zone where
     fuel and air are burned at equivalence ratios greater than 1.3, and a
     quench zone where secondary air is  introduced and mixed for further oxida-
     tion in a lean  combustion zone.
     Variations to the rapid quench  section were made by replacing the baseline
     hardware (3-in. diam.)  with 2-inch  or 4-inch diameter sections.  A third
     variation addressed the feasibility of using uncooled non-metallic mate-
     rials for the rich zone combustor.   The material  chosen for this section
     was a cylinder  of carbon compound.   Another variation to the baseline
     concept was the use of  externally  controlled plungers to vary the pressure
     drop in the rapid quench zone of the baseline combustor.
     B.  Graduated Air^Addition Configuration
     This configuration contains two rich zones of combustion  (primary equi-
                                    A-110

-------
    valence ratios of  greater  than  2.0 and about 1.6)  followed  by the  lean
    burn zone.
    C.  Rich Product Recirculation
    This configuration utilizes  a large diameter mixing  chamber as  the  rich
    combustion  zone.   Secondary  air is then added by one of  two methods.  The
    first  utilizes the rapid quench zone of the  base rich burn-lean configura-
    tion.  The  second  method uses a quenching  tube where air is introduced
    into the center of the  large mixing chamber  through  a necked down region
    at  the chamber exit through  a 60°  swirler.
    D.  Pre-burner Fuel  Preparation
    The pre-burner configuration consists of a small chamber with an air
    boost  fuel  nozzle  upstream of the  primary  zone in  which  a small  amount of
    fuel is burned to  supply heat to vaporize  the remaining  fuel  injected in
    a necked down region of the  pre-burner exit.   The  vaporized fuel then
    travels into an aerodynamic  swirler where  vigorous mixing takes place.
    Operation downstream of this section is the  same as  in the  baseline rich
    burn-lean burn configuration.
    E.  Rich-Lean Annihilation Combustor
    This configuration consists  of  an  air boost  nozzle for fuel  atomization
    in  the front end of the combustor, a rich  burn module, a lean burn  module,
    an  annihilation module, a  rapid quench module, and a lean burn  module.
3.   TEST SITE
    Pratt  and Whitney  Aircraft,  West Palm Beach, Florida.
4.   TEST OBJECTIVE
    •  Computer evaluation  of  several  combustor  concepts for achieving  low
        NOX emissions with high-nitrogen fuels  (including SRC-II) in utility
        gas turbine engines  application without the use of water injection.
5.   SPONSORING  AGENCIES
    U.S. Department of Energy
    Office of Coal Utilization
    Heat Engine and Heat Recovery Division
                                   A-lll

-------
     Project Officer:  Warren Bunker
     Telephone No:   301-353-2816
     NASA-Lewis Research Center (Technical Program Management)
     Cleveland, Ohio  44135
     Project Officer:  D. Schultz
     Telephone No:   216-433-4000
 6.  CONTRACTOR
     Power Systems Division
     United Technologies Corporation at
     Pratt and Whitney Aircraft
     Government Products Division
     West Palm Beach, Florida
     Project Manager:  G. W.  Beal
     Telephone No:   305-840-2000
 7.  TEST CONDITIONS
     Conditions of the tests  run are shown in Table A-34.
 8.  ENVIRONMENTAL MONITORING
     NO , CO, and smoke.
       /\
 9.  PROJECT STATUS
     Modeling of individual configurations has been completed and performance
     characteristics with respect to combustor flow fields and emission cha-
     racteristics predicted.   Preliminary test results for some configurations
     are available and are described in Table A-34.  These only include tests
     with the baseline configuration and variations to the fuel preparation,
     primary rich zone length and quench zone diameter.
10.  RESULTS
     The results of tests completed as of this paper's publication date are
     shown in Table A-34. As  predicted, the values of NO  were reduced for the
     smaller diameter quench  zone and increased for the larger diameter quench
     zone.  The results indicate the rich burn-lean burn staged combustion
     system can meet the emissions goals of the EPA standard.
11.  MISCELLANEOUS
     Project is part of a multiple contract effort sponsored by DOE to develop

                                    A-112

-------
TABLE A-34.   TEST SUMMARY
Configuration Description
1. •

•

t
1A. •
t

•
IB. 0
•

•
•
1C. •
«

•
•
2A. •
»


*
Rich-Lean Burn
(Rich Burn Quick Quench)
18-in. (45.7 cm) Rich Zone
Length
Premix Tube
Rich-Lean Burn
18-in. (45.7 cm) Rich Zone
Length
Recessed Air Swirler
Rich-Lean Burn
18-in. (45.7 cm) Rich Zone
Length
Recessed Air Swirler
Copper Cooling Coil
Rich-Lean Burn
18-in (45.7 cm) Rich Zone
Length
Recessed Air Swirler
Thicker Liner Material
Rich-Lean Burn
12-in. (30.5 cm) Rich Zone
Length

Recessed Air Swirler
Win. N0x/Rich Approximate
Fuel Equiv. Ratio Run Hours Comments


ERBS 35/1.4 5 Burned hole in rich zone at
high pressure.


SRC-II 35/1.8 7.5 Burned hole in rich zone.
25/1.9


ERBS 20/1.7 1 Burned hole in rich zone.




ERBS ' 25/1.6 8 S.A.E. Smoke numbers 5.0 to 8.
Overheated Rich Zone
SRC-II 44/1.6
Resid. 78/1.7

SRC-11 52/1.6 13 S.A.E. Smoke numbers 2.0
74/1.6 3.0 on No. 2 & SRC-II.
50/1.7 Overheated rich zone.

                                                        (Continued)

-------
                                         TABLE A-34.   (Continued)
Configuration Description
         Min.  N0x/Rich     Approximate
Fuel     Equiv.  Ratio        Run Hours
                                           Comments
2B. •  Rich-Lean Burn
    •  12-in.  (30.5 cm) Rich Zone
       Length
    •  Recessed Air Swirler
    •  Improved Liner Cooling
2C. •  Rich-Lean Burn
    •  12-in (30.5 cm) Rich.Zone
       Length
    •  Recessed Air Swirler

    e  Improved Liner Cooling

3A. •  Rich-Lean Burn
    •  18-in. (45.7 cm) Rich Zone
       Length
    •  Recessed Air Swirler

    •  Improved Liner Cooling

    •  Small Dia.  Quench Zone
4A. •  Rich-Lean Burn
    9  18-in. (45.7 cm) Rich Zone
       Length
    t  Recessed Air Swirler
ERBS
42/1.5
ERBS        58/1.8
Resid.      95/2.0
(0.3% FBN)
Resid.      90/1.8
(0.4% FBN)
Resid.      100/1.9
(0.5% FBN)
Resid.       58/1.6
(0.3% FBN)
Resid.       70/1.6
(0.4% FBN)"
Resid.       85/1.6
(0.5% FBN)
Resid.       57/1.6
(0.3% FBN)
Resid.       49/1.6
(0.4% FBN)
                   10
                   15
                   15
Burned hole in rich zone at high
pressure due to loss of coolant
flow.
No cooling problems.
No cooling problems.
No cooling  problems.

Heavy coking at entrance  of rich
zone.
                                                                                                         (Continued)

-------
TABLE A-34.  (Continued)
Configuration Description
• Improved Liner Cooling
• Large Dia. Quench Zone
8A. 0 Rich-Lean Burn
• 18-in (45.7 cm) Primary
• Recessed Air Swirl er
• Improved Liner Cooling
t Variable Quench Zone
5A. • Rich-Lean Burn
• 18 Inch (45.7 cm) Primary
• Recessed Air Swirl er
• Non-Metallic Liner


r . Min. NCL/Rich
^uel Equiv. Ratio
Resid.
(0.5% FBN)
ERBS
Resid.
(0.3% FBN)
Resid.
(0.4% FBN)
Resid.
(0.5% FBN)
SRC- 1 1

ERBS
ERBS
ERBS
50/50
ERBS/Resid.
Resid.
(.3% FBN)
Resid.
(.5% FBN)
58/1.6
184/1.54
250/1.60
73/1.59
108/1.56
78/1.60

36/1.55
30/2.09
26/1.57
39/1.65
50/1.60
77/1.66
80/1.54
Approximate
Run Hours Comments


No cooling problems. Variable area
stuck at low temps.
12

Fuel Nozzle Tip Bent.

Smoke Number 13.8 @ 4> . = 2.0
13 No Cooling Problems (600°F Inlet)
(2 Hr. High (315°C).
Pressure)
180 PSIA (1290 kPa).
Smoke Number 21.9 A  - = 2.0
Non-Metallic Liner Ablated.
Started in Cone Exit ~6 Hrs. into
Testing After Blow Out Instability
at 300°F (150°C) Inlet Condition
with Residual Fuel .

-------
     low NO  combustor technology.   Other participating contractors are:
           A
     Westinghouse,  Detroit Diesel Allison Division of General  Motors, General

     Electric Company,  and Solar Turbine  International.

12.   REFERENCE

     Russell, P.L.,  G.W.  Beal,  R.A.  Sederquist,  and  D.  Schultz.   "Evaluation
     of Concepts  for Controlling Exhaust  Emissions from Minimally Processed
     Petroleum and  Synthetic  Fuels", ASME Paper  No.  81-GT-157.   Paper pre-
     sented at the  Gas  Turbine  Conference and  Products  Show, March 9-12, 1981,
     Houston, Texas.
                                  A-116

-------
                                   TEST 26
                    LOW N0v HEAVY FUEL COMBUSTOR CONCEPT
                          A

1.   FUELS TESTED
     Synfuel:   middle distillate SRC-11 fuel oil.
     Reference fuels:  low quality petroleum residual, and petroleum reference
     distillate fuel  (see Table A-35).

                       TABLE  A-35.  FUEL PROPERTIES


Spec. grav. @ 289/289 K
Hydrogen content,
percent
Sulfur content, percent
Net heat of combustion,
MJ/kg
Viscosity, m2/s @ 311 K
Nitrogen content,
percent
Surface tension, N/M
Surface tension, N/M
Pour point, K
Vanadium, ppm by wt
ERBS
0.8377
12.95
0.085
42.5
1.36xlO"6
0.0054
244
—
SRC II
0.9796
9.07
0.20
38.1
3.55xlO"6
0.87
255
—
Residual
0.9440
11.52
0.49
41.3
1. 345x1 O"3
0.23
3.29xlO"2 @ 339 K
3.06xlO"2 @ 366 K
294
26

 Experimental  Referee  Broad  Specification (ERBS)  petroleum distillate  fuel.

2.    TEST EQUIPMENT
     Seven 20-cm diameter experimental  combustors of varying designs (see
     Table A-36).
                                    A-117

-------
         TABLE  A-36.  DESCRIPTION OF TEST  COMBUSTORS
Combustor #
Type
                                                  Characteristics
             Rich-Lean Combustor
             with Premixing
             Rich-Lean Combustor
             with Multiple
             Nozzle
             Rich-Lean Combustor
             Series-Staged Lean-
             Lean  Combustor
             Series-Staged Lean-
             Lean  Combustor with
             Premixed Main Stage
             Parallel-Staged
             Lean  Combustor,
             Combustor 6
             Lean  Burning
             Catalytic  Com-
             bustor,  Combustor 7
                 3-part combustor consisting  of single-
                 fuel  nozzle  and  swirl  cup  in a premixing
                 tube  ahead of the rich stage to provide
                 uniform mixing of fuel  and air and  avoid
                 smoke production, a  necked-down quench
                 zone  where secondary air is  introduced,
                 and a. lean stage.

                 Consists of  eight fuel  nozzles and  swirl
                 cups  in the  head of  a  rich stage, followed
                 by a  quench  zone and lean  stage.  Differs
                 from  Combustor 1  in  multiple nozzle head
                 end.

                 Same  as Combustor 2  except for differen-
                 ces in design of the mixing  passages
                 between rich and lean  stages, where  secon-
                 dary  and dilution air  are  introduced  and
                 mixed with the products of combustion of
                 the rich stage in minimum  time to generate
                 minimum additional NOX.

                 Consists of  pilot stage with single-air
                 atomizing fuel injector and  two-stage
                 counter-rotating swirl  cups,  and main
                 stage which  employs  eight  single-stage
                 swirlers and air atomizing fuel  injectors.
                 Design minimizes long  gas  residence times
                 associated with  recirculating zones that
                 generate thermal  NOX.

                 Consists of  pilot stage having six  dual
                 counter-rotating swirlers  arranged  in an
                 annulus around a main  stage  premixing duct.
                 Main  stage fuel  is introduced into  the
                 forward end  of the duct and  mixed with air
                 prior to entering the  combustion zone
                 through twelve axial slots at the aft of
                 the premixing duct.

                 Has low velocity pilot stage with a single
                 swirl cup and air atomizing  fuel injector
                 at the dome  end.   Main stage has annular
                 high-velocity dome with six  swirl cups and
                 fuel  injector in a concentric arrangement
                 around the discharge end of  the pilot
                 stage.

                 Designed to  demonstrate ultra-low thermal
                 NOX performance.   Includes a fuel prepa-
                 ration section preceding the catalytic
                 reactor main stage containing seven fuel
                 nozzles. Main stage catalytic reactor con-
                 sists of an  MCB-12 Zironia-spinel substrate
                 coated with  a proprietary  VOP noble metal
                 catalyst. Reactor is  followed by a down-
                 stream pilot stage section for ignition,
                 acceleration and part-load operation  to
                 50 percent  load, at  which  point lightoff
                 occurs for  further load increase to full
                 power.
                                  A-118

-------
3.    TEST SITE

     General  Electric test facilities, Evendale, Ohio.

4.    TEST OBJECTIVES

     •  Evaluation of several  combustor concepts for achieving low NOX emis-
        sions with high-nitrogen fuels (including SRC-II fuels) in utility gas
        turbine engines application without the use of water injection.
     t  Emissions and performance goals presented in Table A-37.


                TABLE A-37.  EMISSIONS AND PERFORMANCE GOALS
          Pollutant
                                   Maximum
                                    Level
Operating
Condition
 (a)   Emissions  Goals

      Oxides  of  nitrogen

      Sulfur  dioxide
      Smoke

      Performance  Goals
(b)
      Combustion  efficiency
      Total  pressure  loss

      Outlet temperature
      pattern factor

      Combustor exit  radial
      temperature profile
                               75  ppm at  15%  0

                               150 ppm at 15% 0

                               S.A.E.  no.  = 20
   All

   All

   All
                                             99%  at  all  operating conditions
                                             6% at base  power  load
                                             0.25 at base  load and load
                                             power
                                             Equivalent  to  production comb.
                                             values
5.   SPONSORING AGENCIES

     U.S. Department of Energy
     Office of Coal Utilization
     Heat Engine and Heat Recovery Division

     Project Officer:  Warren Bunker
     Telephone No:   301 - 353-2816

     NASA-Lewis Research Center (Technical Program Management)
     Cleveland, Ohio  44135

     Project Officer:  J. Notardonato
     Telephone No:   216 -433-4000, Ext. 6132
                                    A-119

-------
 6.   CONTRACTOR
     General  Electric  Company
     Evendale,  OH   45215
     Project  Manager:   M.  B. Cutrone
     Telephone  No:   513-243-2000,  Ext.  3651
 7.   TEST CONDITIONS
     Engine conditions (ignition  to  peak  load):   fuel-air ratios (0.0054 to
     0.025),  combustor inlet pressures  (ambient  to 1.166 mPa), combustor inlet
     temperature  (ambient  to 609°K),  and  reference velocity (11.3 to 43.6
     m/sec).
 8.   ENVIRONMENTAL  MONITORING
     Carbon monoxide,  nitrogen  oxides,  and  unburned hydrocarbon (UHC) emis-
     sions.
 9.   PROJECT  STATUS
     Program  begun  in  May  1979.   To  date, results available for testing per-
     formed on  combustors  1, 2, 4, and  6  (see  Table A-38); additional  testing on
     combustors 1 and  2, as well  as  on  combustors 3 and  5 recently completed;
     results  will be published  in August  1981.   Combustor 7 currently being
     fabricated and tests  planned for summer  1981.   Program to be completed
     by November  1981.
10.   RESULTS
     Combustor  1  (only ERBS fuel  tested)
     9  The high  NOX emissions  (20.0 to 24.0  g/kg NOX fuel) experienced due to
        nozzle  misalignment; significant  NOX  reduction experienced after
        nozzle  correction  and  increased rich  stage equivalence ratio (12.0
        g/kg  NOX  fuel).
     •  Smoke emissions exceptionally low (approximately 0-5 SAE smoke number).
     •  Combustible emissions  (CO and UHC)  were  well  within program goals (see
        Table A-37).
     Combustor  2
     «  NOX emissions  with SRC-II and residual  fuels higher than program goals
        (see  Table  A-37)  (certain modifications  reduced NO  emissions consider-
        ably).                                             x
                                    A-120

-------
                          TABLE A-38.  TEST MATRIX
Combustor No.
4
6
i
1
2
ERBS RESID SRC II
x x+ x
A X X
vt
X
xf x x
  See Table  A-36 for description  of combustors.
  Fuel  doped with  pyridine  to  increase  fuel-bound  nitrogen.
     •   Excellent smoke performance with SRC-II fuel  (SAE smoke  number  was  18
        at an  air/fuel  ratio of 0.029).
     •   Combustible emissions (CO,  UHC)  within program goals (see  Table A-37)
        for SRC-II and residual fuels; CO emissions were approximately  20 ppm
        at baseload conditions.
     Combustor 4
     •   NOX emissions approximately 10 percent above program goals (see Table
        A-37)  at 4-1/2 percent pressure  drop with the ERBS and  residual  fuels.
     •   With SRC-II fuel,  NOX emissions  were well above program  goals.
     •   Smoke  levels well  below goals (see Table A-37) at base  and peak level
        conditions with all  three types  of fuel.
     Combustor 6
     •   NOX levels approximated program  goals (see Table A-37)  at  base  load
        conditions with ERBS fuel and residual fuel, but were 37 percent above
        the goal with SRC-II fuel.
     t   Low smoke levels observed for all fuels tested (*v20 SAE  smoke number).
11.   MISCELLANEOUS
     Project is part of a  multiple  contract effort sponsored by DOE to  develop
     low NOX combustor technology.   Other participating contractors are:
     Westinghouse, Detroit Diesel Allison Division of General Motors, United
     Technologies Corporation, and  Solar Turbine International.
                                    A-121

-------
12.   REFERENCES

     Cutrone,  M.G.,  M.B.  Hilt,  et  al.   "Evaluation  of  Advanced Combustors for
     Dry NOX  Suppression  with Nitrogen  Bearing  Fuels in  Utility and Industrial
     Gas Turbines",  ASME  Paper  No. 81-GT-125.   Presented at  26th International
     Gas Turbine  Conference, Houston, Texas, March  9-12,  1981.   10 pp.

     Telephone communication to J. Fairbanks, U.S.  DOE,  Washington,  D.C., with
     S.  Quinlivan, TRW, March 24,  1981.

     Telephone communication to J. Notardonato, NASA Lewis Research  Center,
     with S.  Quinlivan, TRW, May 20, 1981.
                                  A-122

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                                   TEST 27
                    LOW NOV HEAVY FUEL COMBUSTOR CONCEPT
                          /\

}.    FUELS TESTED
     Synfuel:   middle distillate SRC-11 fuel.
     Reference fuels:  low quality petroleum residual  and petroleum reference
                           *
     distillate fuel  (ERBS)  and natural gas.
2.    TEST EQUIPMENT
     Two basic combustor approaches were tested including a staged combustor
     with a rich primary zone and a lean secondary zone, and a lean-lean com-
     bustion system.   Three variations of the rich-lean combustor configuration
     were tested including a longer primary zone (Configuration 1), a shorter
     primary zone (Configuration 2), and a convectively cooled primary zone
     (Configuration 3).  Only one configuration of the lean-lean combustor
     system was tested.
3.    TEST SITE
     Solar Turbine International, San Diego, California.
4.    TEST OBJECTIVES
     •  Evaluation of several combustor concepts for achieving low NOX emis-
        sions  with high-nitrogen fuels (including SRC-II) in utility gas
        turbine engines application without the use of water injection.
     •  Emission goals and performance standards for this work are shown below
        in Table A-39.
5.    SPONSORING AGENCIES
     U.S. Department of Energy
     Office of Coal Utilization
     Heat Engine and Heat Recovery Division
*
 Experimental  Referee Broad Specification.
                                    A-123

-------
      TABLE A-39. COMBUSTOR EMISSION GOALS AND PERFORMANCE STANDARDS
     Goal/Standard                             Level
NO
  x
NO
  x                          ERBS* fuel.

Combustion efficiency        >99 percent.

Pressure drop                <6 percent.

Pattern factor               0.25.
                                  75 ppm corrected to 15 percent Q£ for
                                  FBN levels up to 1 percent (wt).

                                  37 ppm corrected to 15 percent 02 for
                                      *
     *
      Experimental  Referee Broad  Specification.


     Project Officer:   Warren Bunker
     Telephone No:    301 - 353-2816

     NASA-Lewis Research  Center (Technical  Program Management)
     Cleveland, Ohio  44135

     Project Officer:   H.G. Yacobucci
     Telephone No:    216-433-4000

6.   CONTRACTOR

     Solar Turbine  International
     San Diego, California

     Telephone No:    714-238-5500

7.   TEST CONDITIONS

     Lean-Lean
     ERBS Fuel:

        Inlet Air Temperature            260  &  371°C  (500 & 700°F)
        Inlet Air Pressure               586, 793 &  1200  kPa (85,  115 & 161
     SRC-II  Fuel:
        Inlet  Air  Temperature              260  &  371 °F  (500 &  700°F)
        Inlet  Air  Pressure                 308, 584  & 908  kPa  (45,  85 & 132

     Rich-Lean                                                         PS

     Configuration 1 with Natural Gas:

        Inlet  Air  Temperature              149, 177  & 204°C (300,  350 & 400°F)
        Inlet  Air  Pressure                 310  kPa  (45  psia)


                                   A-124

-------
    Configuration  2  with  ERBS Fuel:

        Inlet  Air Temperature                 143 & 260°C (290 & 500°F)
        Inlet  Air Pressure                    310 & 379 kPa (45 & 55 psia)
    Configuration  3  with  ERBS & SRC-II  Fuel

        Inlet  Air Temperature                 143 & 260°C (290 & 500°F)
        Inlet  Air Pressure                    586 to 910 kPa  (85 to  132  psia)

 8.  ENVIRONMENTAL  MONITORING

    NO  ,  CO,  unburned  hydrocarbons,  and smoke.
      /v

 9.  PROJECT STATUS

    The described  combustor concepts  were tested and recommendations  for
    further testing  were  made.   Report presented in March  1981.

10.  RESULTS

    Lean-Lean

    ERBS Fuel:
    •   The  high thermal  NOX is  attributed to pre-mixing of the fuel  and air.
        Higher inlet  temperatures increased the  NOX emissions  for a  given
        equivalence ratio, as did higher inlet pressure.
    •   The  CO emission levels were consistently low at all  conditions
        evaluated.
    •   Unburned hydrocarbons were negligible and no smoke  was detectable
        throughout  these  tests.
    SRC-II  Fuel:
    •   For  rich primary  zone conditions,  NOX emission levels  were higher than
        the  emission  goals.   Increasing  inlet pressure resulted in a decrease
        in NOX emissions.
    •   CO emissions  remained low using  the SRC-II middle distillate fuel.
    0   No smoke was  detectable  and unburned  hydrocarbons were negligible
        throughout  these  tests.

    Rich-Lean Combustor
    Configuration  1  with  Natural  Gas:
    •   NOX  emissions were below 60 ppm  and tended to decrease with  decreasing
        inlet  temperature.
    •   Low  CO and  negligible unburned hydrocarbon emissions were observed  at
        all  conditions  evaluated.
    Configuration  2  with  ERBS Fuel:
    •   For  rich primary  zone conditions,  NOX emissions dropped below 75 ppm


                                    A-125

-------
        (corrected to 15 percent 03)  and Increased sharply as stolchlometric
        primary zone conditions  were  approached.
     t  Low CO emissions were  observed  at all  conditions evaluated.
     Configuration 3 with ERBS Fuel:
     •  At each of four temperature and pressure  conditions, the NOX emissions
        appear to reach a minimum below the  most  stringent program goal, for
        rich primary zone conditions.
     •  CO emissions levels were consistently  low.
     t  No smoke was detectable  and unburned hydrocarbon emissions remained
        negligible throughout  the tests.
     Configuration 3 with SRC-11 Fuel:
     •  At each of four inlet  conditions  evaluated,  the NOX emissions appear
        to reach a minimum below the  lower (large engine) NOX emission limit,
        for rich primary zone  conditions.
     •  The CO emissions level was consistently low.
     0  No smoke was detectable  and unburned hydrocarbon emissions remained
        negligible throughout  these tests.
11.  MISCELLANEOUS
     Project is part of a multiple contract  effort sponsored by DOE to develop
     low NOX combustor technology.  Other participating contractors are:
     Westinghouse, Detroit Diesel  Allison Division of  General  Motors, United
     Technologies Corporation, and General Electric  Company.
12.  REFERENCE
     White, D.J., A.  Batakis,  R.T. LeCren, and H.G.  Yacobucci.   "Low NOX Com-
     bustion Systems for Burning Heavy  Residual Fuels  and High-Fuel-Bound
     Nitrogen Fuels", ASME Paper No.  81-GT-109.   Presented at the  Gas Turbine
     Conference and Products Show, March  9-12, 1981, Houston,  Texas.
                                   A-126

-------
                                 TEST 28



                  LOW NO  HEAVY FUEL COMBUSTOR CONCEPT
                        rt
   FUELS TESTED


   Synfuel:   middle distillate SRC-II fuel.


   Reference fuels:  low quality petroleum residual, and petroleum reference


   distillate fuel  (see Table A-40), and various blends of these fuels.



                      TABLE A-40. FUEL PROPERTIES

Gravity, °API (15.6°C)
Specific Gravity
Hydrogen, wt %
Nitrogen, wt %
Sulfur, wt %
Ash, wt %
Pour Point, °C (°F)
Viscosity, cst
@ 37.8°C(100°F)
Distillation Temp. °C (°F)
IBP
10%
50%
90%
FBP
Net Heat of Combustion
Btu/lb
ERBS*
38.2
.8338 @ 15.6°C
12.55
.008
.09
<.0002
-45.6(-50)
1.87

126 (259)
180 (356)
224 (435)
330 (620)
408 (766)
18,343
Petroleum SRC-II Middle
Residual Distillate
—
.9533 (@ 22°C)
11.43
.22
.48
.03
13.3
.9772
9.19
.79-. 8
.25
.0015
23.9(+75) -59.4(-75)
>835 (furol sec)

180 (356)
250 (482)
358 (676)
445 (833)
490 (914)
17,609
4.03

110 (230)
190 (374)
242 (486)
295 (563)
370 (698)
16,674
*Experimental Referee Broad Specification (ERBS) petroleum distillate fuel
                                  A-127

-------
2.   TEST EQUIPMENT

     Several different combustion configurations were built for this  test

     (Table A-41).  The combustion configurations selected for development and

     design involved staged combustion (rich-lean) utilizing diffusion flames

     and stated catalytic combustion.   Detailed descriptions and illustrations

     of each combustor are presented in the referenced report.

3.   TEST SITE

     Westinghouse Electric, Madison, PA.

4.   TEST OBJECTIVES

     •  Evaluation of several  combustor concepts for achieving low NOX emis-
        sions with high-nitrogen fuels (including SRC-II) in utility gas
        turbine engines application without the use of water injection.

     •  Emissions and performance goals presented in Table A-42.

5.   SPONSORING AGENCIES

     U.S. Department of Energy
     Office of Coal Utilization
     Heat Engine and Heat Recovery Division

     Project Officer:   Warren  Bunker
     Telephone No:   301 -353-2816

     NASA-Lewis Research Center (Technical  Program Management)
     Cleveland, Ohio  44135

     Project Officer:   J. Notardonato
     Telephone No:   216 -433-4300, Ext.  6132

6.   CONTRACTOR

     Westinghouse Electric Co.
     Synthetic Fuels Division
     P. 0.  Box 158, Waltz Mill  Site
     Madison,  PA  15665

     Telephone No:   412-722-5716

7.   TEST CONDITIONS

     The reported test conditions for  the configurations  tested are shown in
     Table  A-43.
                                   A-128

-------
     TABLE A-41. COMBUSTOR CONFIGURATION DESIGNED
                 AND BUILT FOR TESTING
Direct Injection - Rich-Lean

1.   Direct Injection, Venturi Quench

2.   Direct Injection, Vortex Quench

3.   Direct Injection, Vortex Quench, Perforated Plate

4.   Direct Injection, Vortex Quench, Catalyst

9.   Multiannular Swirl Burner

11. Rolls-Royce Combustor

Premix Rich-Lean

5.   Recirculating Counter Swirl, Venturi Quench

10. Perforated Plate, Venturi Quench

Rich Primary Catalytic - Lean Staged Combustion

7.   Catalyst A, Venturi Quench

8.   Catalyst B, Venturi Quench

Rich Hybrid Premix/Direct Injection

6.   Hybrid Piloted Rich Burner, Venturi Quench

Lean Catalytic

12. Catalytic

Lean Hybrid Premix/Direct Injection

13. Hybrid Piloted Lean Burner
                          A-129

-------
   TABLE A-42  LOW NOX HEAVY FUELS COMBUSTOR CONCEPT PROGRAM
              ' SUMMARY OF GOALS AND OBJECTIVES
A.  Emissions Limits (All  Operating Conditions)

    1.  Oxides of Nitrogen         -    75 ppm @ 15% 02

    2.  Sulfur Dioxide             -    105 ppm @ 15% 0

    3.  Smoke                      -    S.A.E. No.  = 20
B.  Performance Specifications

    1.  Combustion Efficiency

    2.  Total Pressure Loss

    3.  Outlet Temperature
        Pattern Factor

    4.  Combustor Exit
        Temperature Profits
>99%(@ all operating conditions)

<6% (@ base load power)

<0.25 (@ base load and load power)
-Equivalent to typical
 production engine
 combustor values
C.  General

    1.  Retrofitable to current production and field engines

    2.  Highly durable

    3.  Maintainable

    4.  Fuel Flexible - Capable of meeting emissions and performance
        specification on liquid fuels including petroleum distillates
        and residuals and synfuels from coal and shale
                                 A-130

-------
        TABLE A-43.  TEST  CONDITIONS  FOR BURNER  CONFIGURATIONS TESTED
Direct  Injection  -  Rich-Lean
  Venturi  Jet Quench/Lean Burner
     Burner outlet  pressure:       165 psia    (1.14  MPa)
     Burner inlet temperatures:    600°F      (316°C)
     Burner outlet  temperatures:  1950°F     (1066°C)
     Total  air flow:               4.1  Ib/sec  (1.86  kg/sec.)
  Vortex Mixer/Lean Burner
     Quench module  with vortex mixer was tested  under
     similar conditions to those described  above.
  Vortex Mixer/Catalytic Lean Burner (typical  expected operating conditions
     at full  pressure)
     Catalyst inlet temperature:    1480°F   (804°C)
     Catalyst outlet temperature:    2100°F   (1140°C)
Lean Catalytic Burner
     Combustor inlet pressure:
     Air inlet temperature:
180 psia (1.24 MPa)
720°F    (382°C)
Rolls Royce Combustor (peak conditions)
     Combustor inlet pressure:
     Air flow:

Multiannular Swirl  Burner
     Combustor inlet pressure:
     Combustor inlet temperature:
     Air flow:
163 psia    (1.13 MPa)
7.6 Ib/sec.  (3.45 kg/sec)
11.2 atmos  (1.19 MPa)
638°F       (338°C)
5.2 Ib/sec.  (2.36 kg/sec.)
                                    A-131

-------
 8.  ENVIRONMENTAL MONITORING

     Carbon monoxide, nitrogen oxides, unburned  hydrocarbons,  and smoke.

 9.  PROJECT STATUS

     The combustion configurations which have been  designed  and built are

     shown in Table A-41. Combustion emission sampling results available  so  far

     are for configurations 1, 2, 4, 9, 11, and  12  using  unblended fuels.

     The study results were presented in March 1981.

10.  RESULTS

     Direct Injection - Rich-Lean

     Ventori_ Jet_ Quenc_h/Lear[ Burnerj_
     •  Minimum NO  values of 68-70 ppmv were obtained  for the ERBS fuel.
                  X
     •  Minimum NO  values of about 140 ppmv were obtained with SRC-II fuel.
                  /\
     «  Smoke measurements for this configuration for the ERBS fuel  show SAE
        smoke numbers of 20 and 26 for the primary  equivalence ratio (1.6
        which resulted in minimum NO  emissions).
                                    J\
     •  Smoke numbers were higher for SRC-II fuel oil (29 at a primary equiva-
        lence ratio of 1.62).

     Vpjrte_x_Mj_xe_r/_Lean_ B_u_rne_rj_

     •  NOX emissions of approximately 195 ppmv  were obtained  with the SRC-II
        fuel.

     •  NOX emissions of approximately 120 ppmv  were obtained  with the ERBS
        fuel.

     j/o_rtex/Mj_xer/Caita, 1 y_tj_c_Lean_ J3u_rner:_

     t  NOX emission buds were about the same as described above for the vortex
        mixer without the catalytic element for  both fuels and did not appre-
        ciably change over the range of equivalence ratios considered.

     •  FBN  conversion in the SRC-II fuel was about 23 percent.

     Lean Catalytic Burner

     •  NOX emission for the ERBS fuel was 2 ppm.

     •  Approximate NOX emissions and FBN conversions for the  ERBS fuel with
        pyridine added are shown below:
*
 FBN - fuel bound nitrogen.
                                    A-132

-------
          FBN, Wt %    NO,,, ppmv*"% Conversion of FBN
                         A                  •  •   —•—•—• • "• -
             0.2           60                60

             0.5          100                47

             1.2          200                40
          *                     •  - - - -   •	.	—	
           Corrected to 15 percent oxygen.


•  NOX emissions from SRC-11 fuel were 190 and 200 ppmv.

•  Conversion efficiency of FBN from the SRC-II fuel in the lean catalytic
   combustor was about 50 percent.

Rolls-Royce Combustor
• Emissions for
as follows:
Emission
Constituent
NOX
CO
Unburned
Hydrocarbon
Smoke No.
ERBS and SRC-II fuel
Emission Level -
ERBS (ppm)
91
8
2
5 & 11
at the peak design
Emission Level-
SRC-II (ppm)
280
16-37
2
7
condition were
Emission Level -
Petroleum
Residual (ppm)
120


•  Conversion rates of FBN were about 40 percent for SRC-II fuel and 30-
   40 percent for petroleum residual fuel.

Multiannolar Swirl Burner
t Preliminary results from this burner are shown below:
Fuel
ERBS
SRC-II
Petroleum
Residual
Temperature, °F (°C)
2035 (1113)
1948 (1064)
1995 (1091)
NO., (ppmv) Remarks
X
26
165
127
Central nozzle only
Central & radial nozzles
Central & radial nozzles
•  FBN conversion for SRC-II fuel was 20 percent, which is lower than
   that of a conventional burner.
                               A-133

-------
11.   REFERENCE

     Lew,  H.G.,  S.M.  DeCorso,  G.  Vermes,  D.  Carl,  W.J.  Havener,  J.  Schwab, and
     J.  Notardonato.   "Low NOX and  Fuel  Flexible  Gas  Turbine Combustors", ASME
     Paper No.  81-GT-99.   Presented at  the  Gas  Turbine  Conference and Products
     Show, March 9-12,  1981, Houston, Texas.
                                   A-134

-------
                                   TEST 29

              SMALL SCALE COMBUSTION TESTING OF SYNTHETIC FUELS


1.    FUELS TESTED (See Table A-44)

     Synfuel:   SRC-II middle distillate, heavy distillate, and three blends
     of middle and heavy distillate fuel oils.

     Reference fuels:  No.  2 and No. 6 fuel oils.

2.    TEST EQUIPMENT

     A 20-hp,  Johnston, three-pass, firetube boiler designed to transfer
     roughly 670,000 Btu/hr.

3.    TEST SITE

     Combustion Technology Division, Pittsburgh Energy Technology Center,

     Pittsburgh, Pennsylvania.

4.    TEST OBJECTIVE

     •  To characterize exhaust emissions and boiler efficiencies from both
        synthetic fuels and petroleum-based fuels  burned under identical  com-
        bustion conditions, in  order to assess any change in the environmen-
        tal impact of industrial or utility boiler exhaust gases upon changing
        from petroleum-based fuels to synthetic fuels.

5.    SPONSORING AGENCY

     U.S. Department of Energy
     Pittsburgh Energy Technology Center
     Analytical Chemistry Division and
     Combustion Technology Division
     Pittsburgh, Pennsylvania

     Principal Investigator:  G. A. Gibbons
     Telephone No:  412-675-5804

6.    CONTRACTOR

     None.
                                    A-135

-------
                                            TABLE A-44.   FUEL ANALYSIS
I
GO

SRC-II "Blends"
Fuel,
%
Carbon
Hydrogen
Nitrogen
Sulfur
Ash
Oxygen (diff)
Heating Value
(Btu/lb)
No. 2
Fuelt
Oil
87.3
12.5
--
0.21
--
--
19,840
No. 6
Fuel
Oil
87.0
11.0
0.30
0.70
0.10
1.9
18,610
Middle
Distillate
(M)
85.9
9.0
0.9
0.3
0.10
3.8
17,260
Blend
No. 1
(3M:1H)
86.2
8.9
0.9
0.2
—
3.8
17,590
Blend
No. 2
(2M:1H)
87.5
8.5
0.9
0.4
0.60
2.1
17,140
Blend
No. 3
(1M:2H)
99.1
7.9
1.0
0.4
0.3
1.3
17,130
Heavy
Distillate
(H)
88.9
7.3
1.1
0.5
0.6
1.6
17,050

       Typical  analysis of No.  2 fuel  oil.
       Mixtures of middle and heavy distillate; blend No. 1 received already mixed.

-------
 7.  TEST  CONDITIONS
    To  date,  eight  runs  have been made with No.  6 oil:   five at about 23 per-
    cent  excess  air  and  three at about 11  percent excess air.   Two runs  have
    been  completed  on  No.  2 oil:   one at 11 percent excess air and one at 20
    percent  excess  air.   Five SRC-II  fuels have  been tested:   a heavy dis-
    tillate,  a middle  distillate, and three blends.   The initial  blend of
    SRC-II was approximately three parts middle  distillate to  one oart heavy
    distillate.   Six runs,  three at each of two  conditions,  were  made with
    this  blend.   Subsequently, separate supplies of middle and heavy  distil-
     late  were obtained,  and two blends were prepared:   one of  two parts  middle
    to  one part  heavy  distillate and  the second  of one  part  middle to two
    parts heavy  distillate.  Three tests were run on each blend.   Single tests
    were  run  on  the  middle  distillate and heavy  distillate alone  (see Table
    A-45).
 8.   ENVIRONMENTAL MONITORING
    NO  ,  S0?, CO, HC,  particulates, and polynuclear aromatic hydrocarbons
      }\.   (-
     (qualitative).
 9.   PROJECT  STATUS
    Tests with SRC-II  fuel  oils and baseline petroleum  fuel  oils  were con-
    ducted from  October  1979 through  October 1980.   The Progress  Report  is
    dated 1981.   Additional tests are planned with other synfuels - H-coal,
     Exxon Donor  Solvent  fuel, shale oil, and biomass fuel.   The program  will
     run until October  1982.
10.   RESULTS
    The results  of  the test program are highlighted below and  in  Tables  A-46
     through  A-49.
     •  In general,  combustion performance was good in all the  test runs.
        Total  particulate loadings in  the stack were small, and CO and total
        hydrocarbon  levels  were below  100 and 1 ppm,  respectively.
    t  The  levels of NOX and S02 produced were proportional  to the amount of
        nitrogen  and  sulfur  in the fuel.
    0  There  appear  to be  two sources of trace organics in the exhaust gases:
        small  amounts of  the fuel itself not burned during combustion, and the
                                    A-137

-------
        TABLE A-45.  TEST CONDITIONS FOR THE SYNFUELS TEST  PROGRAM
Run
No.
LSF-20
LSF-21
LSF-22
LSF-23
LSF-24
LSF-25
LSF-26
LSF-27
LSF-28
LSF-29
LSF-30
LSF-31
LSF-32
LSF-34
LSF-35
LSF-36
LSF-37
LSF-38
LSF-39
LSF-40
LSF-41
LSF-42
LSF-43
LSF-44
Fuel
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
SRC-II, Blend 1
SRC-II, Blend 1
SRC-II, Blend 1
SRC-II, Blend 1
SRC-II, Blend i
SRC-II, Blend 1
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 2 Fuel Oil
No. 2 Fuel Oil
SRC-II, Mid. Dist.
SRC-II, Blend 3
SRC-II, Blend 3
SRC-II, Blend 3
SRC-II, Blend 2
SRC-II, Blend 2
SRC-II, Blend 2
SRC-II, Heavy Dist.
Excess
% o2 *
3.9
2.1
4.1
4.4
3.9
2.2
3.9
2.3
4.5
1.9
2.3
4.0
2.1
4.1
4.6
2.2
4.4
2.5
4.2
2.2
2.5
3.9
2.6
2.9
Fuel
Ratet
(Gal/Hr. )
5.6
5.4
5.4
5.4
5.4
5.4
5.4
5.6
5.2
5.6
5.4
5.4
5.4
5.4
5.2
5.1
5.3
5.6
5.7
5.3
5.6
5.3
5.6
5.5
Steam Production/
Gal Fuelf
(Ibs. Steam/Gal.)
—
—
—
—
—
—
—
107.5
117.6
-__
111.2
103.7
108.3
110.5
106.1
106.7
111.7
115.7
114.0
115.7
109.8
108.7
109.4
114.7

"Percent oxygen was  set as  an  experimental  condition;  two levels were se-
 lected:  2.0-2.5 percent 0« and 4.0-4.5 percent CL.
f
 Fuel  rates were set at approximately 5.4 gal/hr and  adjusted slightly to
 maintain the same Btu/hr input for the fuel.
*Pounds of. steam produced per  gallon of fuel  fired.
                                   A-138

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      TABLE  A-46.   NO  EMISSIONS AS A FUNCTION OF FUEL NITROGEN CONTENT
Fuel
No. 2 Fuel Oil
No. 2 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
SRC-II, Blend #1
SRC-II, Blend #1
SRC-II, Blend #1
SRC-II, Blend #1
SRC-II, Blend #1
SRC-II, Blend #1
SRC-II, Blend #2
SRC-II, Blend #2
SRC-II, Blend #2
SRC-II, Mid. Dist.
SRC-II, Blend #3
SRC-II, Blend #3
SRC-II, Blend #3
SRC-II, Blend #5
Run %
LSF 35
LSF 36
LSF 20
LSF 21
LSF 22
LSF 23
LSF 30
LSF 31
LSF 32
LSF 34
LSF 24
LSF 25
LSF 26
LSF 27
LSF 28
LSF 29
LSF 41
LSF 42
LSF 43
LSF 37
LSF 38
LSF 39
LSF 40
LSF 44
% Excess Air
26.0
11.0
21.0
10.5
23.0
25.0
11.5
22.0
10.5
23.0
21.5
11.0
21.5
11.5
26.0
9.5
13.0
21.5
13.5
25.0
13.0
24.0
11.0
15.0
% N (Fuel)
0
0
0.3
0.3
0.3
0.3
0.3
0.3
0.3
0.3
0.9
0.9
0.9
0.9
0.9
0.9
0.9
0.9
0.9
0.9
1.0
1.0
1.0
1.1
N0x (ppm)*
193
178
329
261
364
353
292
350
312
331
599
456
493
517
548
434
480
604
528
590
557
576
549
622

*
 Adjusted to a dry,  0% Excess Air Basis.
                                    A-139

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       TABLE A-47.  S02 EMISSIONS AS A FUNCTION OF FUEL SULFUR  CONTENT

Fuel
No. 2 Fuel Oil
No. 2 Fuel Oil
SRC-II, Blend #1
SRC-II, Blend #1
SRC-II, Blend #1
SRC-II, Blend #1
SRC-II, Blend #1
SRC-II, Blend #1
SRC-II, Mid. Dist.
SRC-II, Blend #2
SRC-II, Blend #2
SRC-II, Blend #2
SRC-II, Blend #3
SRC-II, Blend #3
SRC-II, Blend #3
SRC-II, Heavy Dist.
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
No. 6 Fuel Oil
Run %
LSF 35
LSF 36
LSF 24
LSF 25
LSF 26
LSF 27
LSF 28
LSF 29
LSF 37
LSF 41
LSF 42
LSF 43
LSF 38
LSF 39
LSF 40
LSF 44
LSF 20
LSF 21
LSF 22
LSF 23
LSF 30
LSF 31
LSF 32
LSF 34
% Excess Air
26.0
11.0
21.5
11.0
21.5
11.5
26.0
9.5
25.0
13.0
21.5
13.5
13.0
24.0
11.0
15.0
21.0
10.5
23.0
25.0
11.5
22.0
10.5
23.0
% S (Fuel)
0.20
0.20
0.20
0.20
0.20
0.20
0.20
0.20
0.30
0.40
0.40
0.40
0.40
0.40
0.40
0.50
0.70
0.70
0.70
0.70
0.70
0.70
0.70
0.70
S02 (ppm)
272
194
233
204
221
203
200
—
213
301
312
310
372
381
376
463
—
—
369
446
434
421
448
364
*
 Adjusted to a dry,  0% Excess Air Basis.
                                    A-140

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TABLE A-48.  CALCULATED EFFICIENCIES FOR SELECTED TESTS

Run #
LSF-32
LSF-34
LSF-35
LSF-36
LSF-37
LSF-41
LSF-42
LSF-43
Fuel
No. 6
No. 6
No. 2
No. 2
SRC-II, Middle Distillate
SRC-II, Blend of 2 Parts
Middle Distillate to
1 Part Heavy Distillate
% (A Enthalpy
Balance)
+1.2
+1.5
-0.32
+5.0
+5.35
+2.4
+5.6
+5.8
Effi
% (Heat Loss)
83.1
78.7
74.8
80.0
83.8
78.4
80.7
82.5
ciency
% (Input-Output)
81.2
77.4
75.1
74.0
78.5
75.6
74.6
76.4

-------
            TABLE A-49.  SUMMARY OF GC-MS DATA OBTAINED FROM
                         A SYNFUEL AS WELL AS A PETROLEUM BURN
Compound
Naphthalene
2-Methyl naphthalene
1 -Methyl naphthalene
Biphenyl
2-Ethylnaphthalene
2,6- & 2,7-Dimethylnaphthalene
1,3- & 1 ,7-Dimethylnaphthalene
1 ,5-Dimethyl naphthalene
1 ,2-Dimethylnaphthalene
Acenaphthene
Dibenzofuran
Fluorene
9-Methylfluorene
2-Methyl fluorene
1 -Methyl fluorene
Dibenzothiophene
Phenanthrene
Anthracene
Carbazole
1-Phenyl naphthalene
3-Methyl phenanthrene
2-Methyl phenanthrene
9- & 4-Methyl phenanthrene
1 -Methyl phenanthrene
2- Phenyl naphthalene
Fluoranthene
Benzo(def )dibenzothiophene
Pyrene
Retene
Benzo(b)fluorene
4-Methyl pyrene
2-Methyl pyrene
Benzo(a)anthracene
Chrysene/Triphenylene
n-Alkanes
Detected
SRC- 1 1
L
L
L
L
L
L
L
L
L
L
L
M
M
M
M
M
H
L
L
L
M
M
M
M
L
M
L
H
L
M
L
L
L
L
L
in Combustion Emission
No. 2 Fuel Oil
M
H
L
L
L
L
L
L
L
L
L
L
ND
ND
ND
L
H
L
ND
ND
ND
ND
ND
ND
ND
L
ND
L
ND
ND
ND
ND
ND
ND
H
ND = Not Detected
H  = High
M  = Medium
L  = Low
Total Hydrocarbon = 1  ppm.
                                  A-142

-------
       products  of  combustion  (note  that  No.  2  and  No.  6  fuel  oil  are  essen-
       tially  aliphatic).   For the petroleum  fuels,  n-alkanes  and  polynuclear
       aromatic  hydrocarbons are  seen  in  the  exhaust gas;  for  the  SRC-11
       fuels,  the alkanes  are  absent or present at  very low levels,  and poly-
       nuclear aromatic  hydrocarbons not  seen in the petroleum exhaust  gases
       are  present.

11.   REFERENCE

     Gibbons,  G.A.,  et al.   Small  Scale Combustion Testing of Synthetic  Fuels.
     Progress  Report prepared  by Pittsburgh Energy Technology Center.   1981.
                                    A-143

-------
                                   TEST 30

                     EVAPORATIVE EMISSIONS FROM VEHICLES

                    OPERATING ON METHANOL/GASOLINE BLENDS
1.   FUELS TESTED*
     Non-synfuel:   10 percent methanol/90 percent gasoline (Indolene) blend.

2.   TEST EQUIPMENT

     Two light duty vehicles were tested.  Vehicle A was a 1977 Chevrolet

     Impala with a 305 CID engine and 2V carburetor; vehicle B was a 1977

     Buick Skylark with a 231 CID engine and 2V carburetor.   Both vehicles

     had activated carbon canisters for vapors from fuel tank only.

3.   TEST SITE

     Bartlesville Test Center, Bartlesville, Oklahoma.

4.   TEST OBJECTIVE

     *  To determine the influence of the addition of methanol to gasoline on
        evaporative emissions from light-duty vehicles.

5.   SPONSORING AGENCY

     U.S. Department of Energy
     Bartlesville Energy Technology Center
     Bartlesville, Oklahoma

     Project Manager:  Ken R. Stamper
     Telephone No:   918-336-2400

6.   CONTRACTOR

     None

7.   TEST CONDITIONS

     Tests were performed using EPA's Sealed Housing for Evaporative Determina-
~*
 Because of the unavailability of synfuels, the fuels  used in  some of these
 programs were not "true" synfuels (e.g., methanol-derived from natural  gas  was
 used instead of coal-derived methanol).  These studies, however,  are included
 in this report because they were conducted to show what might be  expected  from
 the combustion of actual synfuels in the indicated combustion systems.

                                    A-144

-------
     tions  (SHED)  test  procedure which focuses on the measurement of evapora-
     tive  losses generated  in  two operations:   diurnal  and hot soak.   The
     diurnal  portion  of the test simulates a condition  in which the temperature
     of  the  fuel is raised  from 60°F to 84°F (16°C to 29°C),  due to the  daily
     temperature cycle.   The hot-sock portion  of the test is  designed to simu-
     late  evaporative emissions resulting from the rise in temperature of  the
     fuel  in the carburetor bowl, typical of the temperature  rise which  occurs
     after  a fully warmed engine is turned off.
 8.   ENVIRONMENTAL MONITORING
     Hydrocarbons  (corrected for methanol) and methanol.
 9.   PROJECT STATUS
     Tests  completed, and paper presented October 20-23,  1980.
10.   RESULTS
     Results from  these tests  show that using  a 10 percent methanol/90 percent
     gasoline blend  increases  evaporative emissions by  130 percent for short-
     term  use and  220 percent  for long-term use, relative to  the evaporative
     emissions produced using  a reference gasoline.  The  evaporative  hydrocar-
     bon emissions produced when the vehicles  were operating  on the methanol
     blend  had a slightly higher photochemical reactivity than those  produced
     from  the reference gasoline.
11.   REFERENCE
     Stamper, K.R.  Evaporative Emissions from Vehicles Operating on  Methanol/
     Gasoline Blends.  SAE Technical Paper 801360, Presented  to Society  of
     Automotive Engineers,  Fuels and Lubricants Division, Baltimore,  Maryland,
     October 20-23,  1980.  12  pp.
                                    A-145

-------
                                 TEST  31
         EXPERIMENTAL  RESULTS  USING  METHANOL  AND METHANOL/GASOLINE
                     BLENDS  AS AUTOMOTIVE  ENGINE FUEL
    FUELS TESTED
    Non-synfuels:   two  unleaded  gasolines  (Indolene  and  a  commercial  fuel)
    were used as base  fuels.   Test  data  were  obtained  for  each base fuel  used
    alone and in a blend  with  5,  10,  and 15 percent  methanol  and for pure
    methanol.
    TEST EQUIPMENT
    The test  equipment  included  a fleet  of 10 cars of  varying size (Table
    A-50) and a stand-mounted  1975  350-CID engine.
     TABLE A-50. TEST  VEHICLES OPERATED  ON METHANOL/GASOLINE  FUEL BLENDS

Vehicle
Designation
A
B
C

D
E
F

G

H
I
J

K
Year and Make

1974 Chevelle
1974 Ford Torino
1975 Maverick
(non catalyst)
1975 Vega
1975 Chevelle
1975 Granada
(non catalyst)
1975 Dodge Dart
(non catalyst)
1975 Impala
1975 Monza
1975 Plymouth
(non catalyst)
1972 Buick
Engine
Size, CID
350
351
250

140
350
351

318

454
262
318

350
Transmission Carburetor

Automatic 2 bbl
2 bbl
1 bbl

1 bbl
2 bbl
2 bbl

2 bbl

4 bbl
2 bbl
2 bbl

4 bbl


Because of the unavailability of synfuels,  the fuels used in some of these
programs were not "true"  synfuels (e.g.,  methanol-derived from natural gas was
used instead of coal-derived methanol).   These studies, however, are included
in this report because they were conducted  to show what might be expected from
the combustion of actual  synfuels in the  indicated combustion systems.
                                  A-146

-------
3.   TEST SITE
    Bartlesville Energy Research Center, Bartlesville, Oklahoma.
4.   TEST OBJECTIVE
    •  To determine the emission and fuel-economy characteristics of methanol
       and methanol/gasoline blends as automotive fuels.
5.   SPONSORING AGENCY
    Energy Research and Development Administration
    Bartlesville Energy Research Center
    Bartlesville, Oklahoma
    The work was done, in part, in cooperation with the EPA.
    Project Leader:  J. R. Allsup
    Telephone No:   918- 336-2400
6.   CONTRACTOR
    None.
7.   TEST CONDITIONS
    On the stand-mounted engine, test variables and engine parametric adjust-
    ments included engine speed, exhaust gas recirculation rate, air-fuel
    ratio, ignition timing, and compression ratio for 5,  10,  15, and 100  per-
    cent methanol/gasoline blend fuels.  The test vehicles were tested on  a
    chassis dynamometer to determine the influence of ambient temperature
    (20°, 75°, and 100°F) using 5 and 10 percent methanol  fuels.  Five of  the
    test vehicles were also tested to determine the effects of sustained  use
    (5000-7500 miles) of gasoline/methanol  blends (10 percent methanol).
    These vehicles were repetitively driven over a controlled test route
    during both summer and winter seasonal  periods.
8.   ENVIRONMENTAL MONITORING
    Steady-state engine emissions of the following compounds  were measured:
    hydrocarbons, methanol, aldehyde, nitrogen oxides, and carbon monoxide.
9.   PROJECT STATUS
    Tests are completed, and report is dated January 1977.  A companion study
    involving the physical properties of the methanol/gasoline mixtures was
                                   A-147

-------
     conducted concurrently and will  be made available as a Report of Investi-

     gations entitled "Physical Properties of Gasoline/Methanol Mixtures" by

     B.H.  Eccleston and F.W.  Cox.

10.  RESULTS

     Emissions data are summarized in Tables A-51 and A-52.

     •  The data indicate that for both base fuels, at normal  ambient tempera-
        ture, the average HC  emissions were increased by addition of methanol
        and were further increased (up to 30 percent) at higher temperatures;
        the change in HC emissions due to methanol  may be the  result of methanol
        in leaning the air/fuel ratio or to its effect in increasing fuel vapor
        pressure.
     •  In general, aldehyde  emissions increased with higher concentration of
        methanol in the fuel.   Levels of NOX emissions were unaffected by the
        amount of methanol  in  the  fuel but were slightly reduced as the ambient
        test temperature was  increased and slightly increased  at cold ambient
        temperature.

     •  CO was substantially  reduced  by the addition of methanol to the base
        fuel at cold  and median ambient temperatures.  At high ambient tempera-
        ture, CO emission levels varied erratically.  In general, the fuels
        containing methanol  produced  higher CO levels than the base fuels.

     •  Results from  the dynamometer  tests suggest  that emissions a(re generally
        affected to the extent that methanol  addition affects  air-fuel  stoi-
        chiometry, fuel heat  content, and fuel vapor pressure.

     •  Results from  the road  tests indicate that vehicle emissions and fuel
        economy were  essentially unchanged during approximately 7,500 miles of
        road testing; no engine or fuel  system component failures were encoun-
        tered during  that testing.

     •  Results from  the bench-mounted engine suggest that operation with pure
        methanol may  allow use of  high-compression  engines to  realize improved
        fuel energy economy with relatively low oxides of nitrogen emission.

11.  REFERENCE

     Allsup, J.R.  Experimental Results Using Methanol and Methanol/Gasoline
     Blends as Automotive Engine Fuel.  BERC/RI-76/15, Bartlesville Energy
     Research Center, Energy  Research and Development Administration, Bartles-
     ville, Oklahoma, January  1977.   81  pp.
                                    A-148

-------
TABLE A-51. EXHAUST EMISSIONS AND FUEL RATE - VEHICLES A-E

Emissions, g/tnile:
CO 	
HC 	
NOX
Aldehydes
Methanol 	
Fuel economy, rr.i/10 btu:
Erni s s i on cy cle.....
Hifrhway cycle 	
Emissions, g/raiie:
CO 	
HC 	
NO 	 , 	
.-v
Aldehydes . . „ 	
Kethanol 	
Fuel economy, mi/ 10" btu:
Emission cvcle
Highway cycle 	

Ambient temperature, °F
20
Base
fuel
57.
Me OH
10%
MeOH
75
Base
fuel
5%
MeOH
10%
MeOH
100
Base
fuel
57.
MeOH
10%
MeOH
BASE FUEL -- INDOLENE
48.8
2.7
2.1
.09
.01
8.7
15.4
39.1
2.6
2.1
.11
.08
8.6
15.4
35.0
2.3
2.0
.13
.13
8.7
15.1
17.7
1.4
2.0
.10
.01
10.0
15.9
14.2
1.6
1.9
.12
.08
9.8
15.9
10.9
1.8
1.9
.13
.15
9.7
15.6
25.8
1.6
1.8
.09
.02
10.2
16.4
44.0
2.0
1.6
.10
.10
9.6
15.8
34.2
2.1
1.7
.09
.17
9.8
15.9
BASE FUEL -- COMMERCIAL GASOLINE
48.2
2.5
1.9
.10
.02
9.5
16.8
42.3
2.5
1.9
.11
.08
9.0
15.9
32.1
2.6
2.0
.16
.14
8.7
15.2
18.7
1.3
1.8
.10
.02
10.1
15.9
13.2
1.6
1.8
.10
.08
9,8
15.2
9.6
1.7
1.7
.12
.15
9.6
14.9
19.7
1.6
1.7
.10
.02
10.3
16.5
28.3
2.1
1.6
.11
.10
10.0
16.3
19.6
2.3
1.7
.13
.17
9.8
15.8

-------
                          TABLE A-52.  EXHAUST EMISSIONS AND FUEL RATE - VEHICLES A-J -
                                      COMMERCIAL GASOLINE BASE FUEL/METHANOL BLENDS
tn
o

Dni.ssions, g/:nile:
CO 	 - 	
HC . 	
NO 	 , 	
1 x

Fuel economy, mi/10" btu:


Ambient t o.npera ture^ °
2!"!
Clear
fuel.
40.3
2.5
1.9
.11
.01
9.3
15.8
57=
Mf.GH
35.7
2.6
2.1
.13
.08
9.1
15.3
10/:.
MoOH
29.?
2.8
2.0
.16
.15
8.9
14.8
-'cj
Clear
fuel
13.5
1 .1
2.1
.10
.02
10.0
15.9
5X.
Me OH
10.1
1.3
/.O
.11
.07
9.7
15.2
10/1
MeOlt
8.2
1.5
1.9
.12
.13
9.7
14.8

100
Clear
iuel
13.2
1.2
2.0
.09
.02
10.4
16.0
57-
MeOH
18.3
1.6
l.R
.10
.08
10.0
15.9
10%
MeOH
13.2
1.8
1.8
.12
.14
10.0
15.7

-------
                                   TEST 32

                 FLEET TRIALS USING METHANOL/GASOLINE BLENDS


1.    FUELS TESTED*

     Non-synfuels:  10 percent methanol/90 percent gasoline blends.

2.    TEST EQUIPMENT

     The seven automobiles used in this study are described below in Table

     A-53.  The fuel metering hardware of the vehicles was not changed,


                       TABLE A-53. FLEET DESCRIPTION

Vehicle
No.
161
162
163
164
176
175
190
Vehicle
Description
1977 Chevrolet Impala
1977 Buick Skylark
1977 Ford LTD II
1977 Plymouth Fury
1978 Volvo 242 DL*
1978 Ford Pinto*
1978 Ford Fairmont
Engine
Disp. , CID
305
231
302
225
130
140
200
Carb.
2V
2V
2V
2V
FI
2V
IV
Test
I.W., Ib.
4,000
3,500
4,500
4,000
3,000
2,750
3,000

      Vehicles are equipped with 3-way catalytic converters and closed-loop
      A/F control.
3.    TEST SITE

     Bartlesville Energy Technology Center, Bartlesville, Oklahoma.
*
 Because of the unavailability of synfuels, the fuels used in some of these
 programs were not "true" synfuels (e.g., methanol-derived from natural  gas was
 used instead of coal-derived methanol).  These studies, however, are included
 in this report because they were conducted to show what might be expected from
 the combustion of actual synfuels in the indicated combustion systems.

                                    A-151

-------
 4.   TEST OBJECTIVE

     0  To provide information on the fuel  economy, driveability, emissions,
        and the engine and fuel-handling component deterioration associated
        with extended use of methanol/gasoline blends in current-production
        automobiles.

 5.   SPONSORING AGENCY

     U.S. Department of Energy
     Bartlesville Energy Technology Center
     Bartlesville, Oklahoma

     Telephone No:   918-326-2400

 6.   CONTRACTOR

     Same as sponsoring agency.

 7.   TEST CONDITIONS

     The vehicles were operated  over a course designed to accumulate mileage

     at a rate and duty cycle similar to automobiles used by the private

     sector.  Vehicle tests were run at each 5,000-mile accumulation interval

     to determine the fuel economy and the  mass of pollutant emissions gene-
     rated.

 8.   ENVIRONMENTAL MONITORING

     CO, NO , unburned fuel, evaporative emissions of hydrocarbons and
           /\
     methanol.

 9.   PROJECT STATUS

     The tests described in this report have been completed, although further
     tests were recommended.

10.   RESULTS

     •  The data show consistent reduction  in CO emissions associated with the
        use of the 10 percent methanol blend (see Figure A-18).

     •  The influence of the methanol blend on NOX emissions did not show a
        consistent effect on the individual test vehicles.  However, the 1977
        model-year fleet showed  slightly increased NOX emissions relative to
        the emissions generated  while operating on indolene, and the 1978
        model-year fleet showed  slightly decreased NOX emissions compared to
        those from indolene-operating engines (see Figure A-19).
                                   A-152

-------
c
o

to
to


UJ
  r

                                          -O
                                           X
                                           o
  O)


  i


  en
                                           c
                                           o
o
                                                  1978  MY  Fleet
Indolene

Methanol Blend
                                              Mil
            10     20    30     40     SO

      eage Accumulation Level  (K  miles)
             Figure  A-18.
                           CO Emission Rates From  1977-MY  and  1978-MY
                           Vehicles Operated Over  the  FTP  Urban  Cycle
                           on Indolene and Methanol/Gasoline Blends
                   to
                   c
                   o
                   CO
                   to
                   UJ
                   O) •
                   C7>
                   o
                   i-
                   +J
                   1/1
                   O)
                   -a

                   X
                   o
                          1978  MY  Fleet
                                             0Indolene
                                             ^Methanol
                                                 Blend
                                                        30
                        0      10     20     30     40

                      Mileage Accumulation Level (K miles)
      Figure A-19.
                    NOX Emission  Rates  From Vehicles Operated Over the FTP
                    Urban Cycle on  Indolene and Methanol/Gasoline Blends
                                      A-153

-------
     •  The emission  rates  of unburned fuel  from the test fleet show slight
        increases associated with the use of 10 percent methanol blend over
        test results  from the fleet operating on indolene (see Figure A-20).

     •  The data showed a significant increase in evaporative emissions asso-
        ciated with short-term use of the methanol  blends and an even greater
        increase when the methanol  blend is  used for extended periods.

11.   REFERENCE

     Stamper, K.R.   Fleet Trials  Using Methanol/Gasoline Blends.  In:  Pro-
     ceedings of the  IV International  Symposium on  Alcohol  Fuels Technology,
     Sao Paulo, Brazil, October 5-8,  1980.   Vol.  II.   pp.  563-571.
                    1.30
                      0       10     20     30     40    90

                    Mileage Accumulation Level (K miles)
      Figure A-20.  UBF  Emission Rates  From Vehicles Operated  Over  the
                   FTP  Urban Cycle on  Indolene and Methanol/Gasoline
                   Blends
                                   A-154

-------
                                   TEST 33

                          GASOHOL FLEET OPERATIONS
1.   FUELS TESTED*
     Non-synfuel:   gasohol and gasoline.

2.   TEST EQUIPMENT

     110 Southwestern Bell Telephone fleet vehicles.

3.   TEST SITE

     Bartlesville Energy Technology Center, Bartlesville, Oklahoma.

4.   TEST OBJECTIVES

     •  To obtain comparative field experience and laboratory emission data
        with gasohol and gasoline in controlled tests with units of a commer-
        cial service fleet.

5.   SPONSORING AGENCY

     U.S. Department of Energy
     Bartlesville Energy Technology Center
     P. 0. Box 1398
     Bartlesville, Oklahoma  74003

     Project Manager:  Jerry All sup
     Telephone No:   918-336-2400

6.   CONTRACTOR

     Same as sponsoring agency.

7.   TEST CONDITIONS

     Operators of SWBT vehicles observed and recorded information from vehicles

     during use in normal  field service.  Service records provided information
*
 Because of the unavailability of synfuels, the fuels used in some of these
 programs were not "true" synfuels (e.g., methanol-derived from natural  gas was
 used instead of coal-derived methanol).  These studies, however, are included
 in this report because they were conducted to show what might be expected from
 the combustion of actual synfuels in the indicated combustion systems.

                                    A-155

-------
     on fuel economy and fuel system problems.  Emissions and fuel economy
     data were obtained from tests of the vehicles at BETC using a chassis
     dynamometer to run EPA-prescribed test routines.
 8.  ENVIRONMENTAL MONITORING
     Regulated pollutants.
 9.  PROJECT STATUS
     Project complete.
10.  RESULTS
     •  On the average, emissions  were lower for vehicles fueled with gasohol,
        but data is inadequate to  conclude real  differences.
     0  Fuel economy was found to  be unchanged between fuels, while driveabili-
        ty was somewhat poorer with gasohol.
11.  REFERENCE
     Allsup, J.   The BETC Fleet Test Program.   In:   Proceedings  of Conference
     on Fleet Use of Unique Automotive Fuels; Report No. MED117, August 13-14,
     1980.
                                   A-156

-------
                                   TEST 34

             EVAPORATIVE EMISSIONS FROM METHANOL/GASOLINE BLENDS


1.    FUEL TESTED*

     Non-synfuel:  unleaded low-octane indolene and a 10 percent methanol/90
     percent indonene blend.

2.    TEST EQUIPMENT

     Two automotive vehicles.

3.    TEST SITE

     Bartlesville Energy Technology Center, Bartlesville, Oklahoma.

4.    TEST OBJECTIVE

     •  To determine the effect of short-term and long-term canister service
        on evaporative emissions from vehicles using the above indicated  fuels.

5.    SPONSORING AGENCY

     U.S. Department of Energy
     Bartlesville Energy Technology Center
     P.  0. Box 1398
     Bartlesville, Oklahoma  74003

     Project Manager:  Jerry Allsup
     Telephone No:   918- 336-2400

6.    CONTRACTOR

     Same as sponsoring agency.

7.    TEST CONDITIONS

     The original canisters were aged by operating the vehicles on 10 percent

     methanol  blends over routine duty for an extended period.  Additional
*
 Because of the unavailability of synfuels, the fuels used in some of these
 programs were not "true" synfuels (e.g., methanol-derived from natural  gas was
 used instead of coal-derived methanol).  These studies, however, are included
 in this report because they were conducted to show what might be expected from
 the combustion of actual synfuels in the indicated combustion systems.

                                   A-157

-------
     tests were run on both test fuels using fresh canisters to determine

     effects of short-term service with methanol  blends.

 8.   ENVIRONMENTAL MONITORING

     Evaporative emissions (hydrocarbons),

 9.   PROJECT STATUS

     Project complete.

10.   RESULTS

     ®  Aged canisters resulted in a 90 percent increase in evaporative losses
        over fresh canisters with the vehicle operating on the methanol blend.

     t  Data from the short-term use of methanol  blends indicated that a 75
        percent increase in evaporative emissions would result with the blend
        over a straight gasoline.

     t  Effect of long-term canister service on evaporative emissions operating
        on methanol blends indicated that either  fuel  modifications or emission
        control design modification must be made  before emissions standards can
        be met with this type of fuel.

     «  There are indications that the "Sealed Housing for Evaporative Determi-
        nation" test procedure employed was not completely adequate to simulate
        in-use evaporative losses from light-duty vehicles.

11.   REFERENCE

     Allsup, J.  The BETC Fleet Test Program.   In:   Proceedings of Conference
     on Fleet Use of Unique Automotive Fuels Report No. MED117, August 13-14,
     1980.
                                   A-158

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                                   TEST 35

              PERFORMANCE EVALUATION OF ALCOHOL-GASOLINE BLENDS
                          IN LATE MODEL AUTOMOBILES


1.   FUELS TESTED*

     Non-synfuels:  ethanol/gasoline fuel  blends, and methanol/gasoline fuel
     blends.

2.   TEST EQUIPMENT

     Fourteen test vehicles as indicated in Table A-54.

3.   TEST SITE

     Anaheim, California.

4.   TEST OBJECTIVES

     •  Performance evaluation of alcohol-gasoline blends in late-model  auto-
        mobiles.

     •  Experimental evaluation of the effect of ethanol  and methanol  in
        gasoline on:  1) exhaust emissions; 2) evaporative emissions;  and
        3) vehicle driveability.

5.   SPONSORING AGENCIES

     U.S. Department of Energy and
     Coordinating Research Council (CRC)
     Atlanta, Georgia
     CRC Contract No. CM-125-1-79
     Project Officer:  Al Zingle
     Telephone No:   404-396-3400

6.   CONTRACTOR

     Systems Control, Inc.
     Environmental Engineering Division
     421  E.  Cerritos Avenue
     Anaheim, California  92805
*
 Because of the unavailability of synfuels, the fuels used in some of these
 programs were not "true" synfuels (e.g., methanol-derived from natural  gas was
 used instead of coal-derived methanol).  These studies, however, are included
 in this report because they were conducted to show what might be expected from
 the combustion of actual synfuels in the indicated combustion systems.

                                    A-159

-------
                                     TABLE  A-54.  TEST VEHICLE DESCRIPTION
CT>
O
VEHICLE
NUMBER
G-l
G-2
G-3
G-4
G-5
G-6
G-7
G-8
G-9
G-10
G-ll
G-12
G-13
G-14
MAKE
Plymouth
Plymouth
Dodge
Dodge
Volvo
Dodge
Buick
Buick
Chevrolet
Ford
Ford
Ford
Ford
Cadillac
MODEL
Horizon
Horizon
Omni
Omni
DL
Aspen
Century
Century
Impala
Pinto
Pinto
Pinto
Pinto
Eldorado
VEHICLE ID.
NUMBER
ML24AAD102722
ML24AAD186522
ZL24AAD230651
ZL24AAD230652
VC24245A1166691
NE41CAF150663
4L69AAZ116617
4L69AAZ1 16703
1L69HAC114146
OT10A149924
OT10A142387
OT10A152199
OT10A152198
6L57AE617086
ENGINE
SIZE
105
105
105
105
2.3L
225
231
231
305
2.3L
2.3L
2.3L
2.3L
3f.O
INERTIA
WEIGHT
2,625
2,625
2,625
2,625
3,000
4,000
3,500
3,500
4,000
3,000
3,000
3,000
3,000
4,250
ACTUAL
HORSEPOWER
6.8
6.8
6.8
6.8
12.5
11.6
11.3
11.3
10.3
9.7
9.7
9.7
9.7
11.8
CONTROL
SYSTEM
Open
Open
Closed
Closed
Closed
Open
Closed
Open
Open
Open
Open
Closed
Closed
Closed

-------
    Program  Manager:   Richard  Carlson
    Telephone  No:    714-956-5450
 7.  TEST  CONDITIONS
    This  program  is  divided  into a  program start-up  phase  and  two  testing
    phases  (Phase  I  for ethanol/gasoline fuel  blends and Phase II  for methanol/
    gasoline fuel  blends).
 8.  ENVIRONMENTAL  MONITORING
    Ethanol, aldehyde, methanol, hydrocarbon,  carbon monoxide, and nitrogen
    oxides.
 9.  PROJECT  STATUS
    Work  performed to date  includes the following:   1)  fuel  and vehicle
    acquisition;  2)  vehicle  preparation including 4,000 mile break-in; 3)
    demonstration  testing;  and 4) Phase I emissions, fuel  economy, and drive-
    ability  testing  was completed in April 1981.   Phase II of  the  program  is
    to be completed  in 1982.
10.  RESULTS
    None  reported  to date.   A  draft final report  is  currently  being prepared
    for Phase I  results and  should  be available by the  end of  1981.  A draft
    final report  for Phase  II  will  be prepared in 1982.
11.  REFERENCE
    Carlson, R.R.   "Performance Evaluation of Alcohol-Gasoline Blends in Late
    Model Automobiles".  In:  Proceedings of Conference on Fleet Use of  Unique
    Automotive Fuels Report  No. MED117, August 13-14, 1980.
                                    A-161

-------
                                   TEST  36

         DETERMINATION OF INDIVIDUAL ALDEHYDE CONCENTRATIONS IN THE

    EXHAUST OF A SPARK IGNITED ENGINE FUELED BY ALCOHOL/GASOLINE BLENDS


1.    FUEL TESTED*

     Non-synfuels:   100 percent Indolene;  20 percent ethanol/80 percent Indo-

     lene (20E); 20 percent methanol/80  percent Indolene (20M); and 30 percent

     methanol/70 percent Indolene (30M).

2.    TEST EQUIPMENT

     A 1963 four-cylinder Pontiac engine modified with a 1974 cylinder head

     and camshaft.   The compression ratio  was 8.1:1.

3.    TEST SITE

     Department of  Mechanical  Engineering, University of Miami, Coral  Gables,

     Florida.

4.    TEST OBJECTIVE

     §  To measure  and compare individual  aldehyde emissions from an alcohol/
        gasoline blend fueled  engine operated at various fuel-air equivalence
        ratios.

5.    SPONSORING AGENCY

     U.S. Department of Energy
     Heavy Duty Transport and  Fuels Utilization
     1000 Independence Avenue, S.W.
     Washington, D.C.   20585

     Project Officer:   Euqene  Ecklund
     Telephone No:    202 -252-8055
 Because of the unavailability of synfuels,  the fuels used in some of these
 programs were not "true"  synfuels (e.g.,  methanol-derived from natural gas was
 used instead of coal-derived methanol).   These studies, however, are included
 in this report because they were conducted  to show what might be expected from
 the combustion of actual  synfuels in the  indicated combustion systems.
                                   A-162

-------
 6.   CONTRACTOR

     Department of Mechanical Engineering
     University of Miami

     Project Manager:   Robert R.  Adt, Jr.
     Telephone No:   305-284-2571

 7.   TEST CONDITIONS

     Engine was operated at steady-state conditions,  2000 rpm and  minimum

     spark advance for maximum torque with fuel-air equivalence ratios  of
     0.96, 0.90, and 0.82.   During  operation at 0.82,  the engine experienced
     lean-limit misfiring.

 8.   ENVIRONMENTAL MONITORING

     Total aldehydes,  formaldehyde, acetaldehyde,  acetone,  propionaldehyde,
     and acrolein.

 9.   PROJECT STATUS

     Project complete; final  report presented in October 1979.

10.   RESULTS

     •  Total  aldehydes (including  acetone) increase  25 percent in going from
        Indolene to 20E, 10 percent to 20M, and 30 percent  to 30M.
     •  Aldehyde concentrations in  the engine exhaust  are generally a stronger
        function of fuel blend than equivalence ratio.
     •  Formaldehyde is the largest component of the  total  aldehydes; up to
        70-90 mole percent  of the total.
     •  The emissions  of formaldehyde and acetaldehyde are  strongly controlled
        by the content of methanol  and ethanol  in  the  fuel, respectively.
     t  Acetone concentration increases as the  lean misfire limit  is approached
        (* = 0.82).
     •  Acrolein concentration decreases slightly  with increasing  alcohol  blend
        level.
     t  Aldehydes are  partially destroyed in the exhaust system and virtually
        completely destroyed  in the catalyst.

11.   REFERENCE

     Harrenstien, M.S., K.T.  Rhee,  and R.R. Adt.  Determination of Individual
     Aldehyde Concentrations  in the Exhaust of  a Spark Ignited Engine  Fueled
     by Alcohol/Gasoline Blends.   SAE Paper No. 790 952.  1-4 October  1979.
                                   A-163

-------
                                   TEST 37
                          METHANOL AS A BOILER FUEL

1.   FUELS TESTED*
     Reference fuels:   methanol, natural  gas, and residual oil No. 6.
2.   TEST EQUIPMENT
     A small  scale boiler test stand and  a Babcock & Wilcox R-B95 utility
     boiler with a rated capacity of 425,000 Ib/hr steam and a net capability
     of 49 MW.
3.   TEST SITE
     Boiler test stand:   Coen Co., Burligame, California.
     Utility boiler:   A.B.  Patterson steam generating station, New Orleans,
     Louisiana.
4.   TEST OBJECTIVES
     •  Demonstrate the use of methanol in external combustion boiler systems.
     0  Compare boiler performance and emissions of methanol and conventional
        fuel  combustion.
5.   SPONSORING AGENCY
     Vulcan Cincinnati,  Inc.
     Cincinnati, Ohio
     Program Manager:   R.W. Duhl
     Telephone No:  513-281-2800
6.   CONTRACTOR
     None.
*
 Because of the unavailability of synfuels, the fuels used in some of these
 programs were not "true" synfuels (e.g., methanol-derived from natural gas was
 used instead of coal-derived methanol).  These studies, however, are included
 in this report because they were conducted to show what might be expected from
 the combustion of actual synfuels in the indicated combustion systems.

                                    A-164

-------
 7.   TEST  CONDITIONS

     All  fuels were tested at two excess air levels and at load levels  of 100,

     75,  and 50 percent.   Methanol  firing required a centrifugal  pump and

     Babcock & Wilcox 85° "Y" type burner tips;  no other changes  were made.

 8.   ENVIRONMENTAL MONITORING

     NOV,  CO,  and aldehydes.
       X

 9.   PROJECT STATUS

     Testing was conducted in 1972.   Final  report dated December  1972.

10.   RESULTS

     In the boiler stand test, combustion of methanol  produced NO  emissions
                                                                 A
     one-fourth and one-tenth of those produced  by natural gas and No.  6  resi-
     dual  oil, respectively.

     The  results of the utility boiler test program are highlighted below and
     in Figure A-21.

     •  No particulate or sulfur compounds  were  emitted during methanol com-
        bustion.
     t  NO/ emission levels of methanol  were 7-14 percent of those measured
        during residual oil combustion.
     •  CO emission levels of methanol were less than 100 ppm and generally
        less than those observed for the residual oil.
     o  Organic acids and aldehydes were generally less than 10 and 1 ppm,
        respectively.  These emissions,  as  well  as hydrocarbon emissions, were
        considered negligible.

11.   REFERENCES

     t  Hagen, D.L.  "Methanol as a Fuel:  A Review With Bibliography".   Paper
        No. 770792, Irr.  Passenger Car Meeting,  Detroit, Michigan, September
        1977.
     •  Vulcan Cincinnati, Inc.  "Methyl Fuel Combustion Test, Vol. I and II".
        Report of Test at A.B. Paterson  Plant, Restricted to the  Sponsors.
        December 15, 1972, 1000 pp.
     •  Duhl,  R.W. and T.O. Wentworth (Vulcan Cincinnati, Inc.).   "Methyl Fuel
        From Remote Gas Sources".  Am. Instit. Chem. Eng. Soc. Calif. Section
        llth Annual Mtg., April 16, 1974, Los Angeles,  CA.
                                    A-165

-------
Duhl,  R.W.  (Vulcan Cincinnati,  Inc.).  "Methanol,  A Boiler  Fuel Alter-
native".  Am.  Inst. Chem.  Eng.,  8th Annual Mtg., Boston,  Mass., Sept.
7-10,  1975.
Duhl,  R.W.   "Methanol as a Boiler  Fuel".  Submitted for  Publication,
Chem.  Eng.  Prog., February 1976.

Duhl,  R.W.  (Vulcan Cincinnati,  Inc.) and J.W. Boylan (A.M.  Kinney,
Inc.).   "Use of Methanol as a Boiler Fuel".   IV  A  - Symposium Swedish
Academy of  Engineering Sciences, Stockholm,  Sweden, March 23, 1976.
               31
               -
           3.30
          jg.^0
          CC
          IU
          °-.20
          ffi

          £.15


          a.to
             .05
METHANOL .
                 20    30    40     50    60

                    UNIT LOAD-MEGAWATTS
                      Figure A-21.
             NOX Emission  Levels of Methanol,
             Natural  Gas,  and Oil
                          A-166

-------
                                   TEST 38

               CHARACTERIZATION OF EMISSIONS FROM METHANOL AND

                       METHANOL/GASOLINE BLENDED FUELS


1.    FUELS TESTED*

     Non-synfuels:  M-20 fuel  (methanol/Indolene clear fuel  - 20/80 volume
     percent);  pure methanol,  and Indolene clear fuel.

2.    TEST EQUIPMENT

     Vehicle test:  1975 Ford  LTD with 400 CID engine; automatic  transmission
     and air conditioning operating during test.

     Engine test:   a 1975 Ford, 400 CID engine without EGR.

3.    TEST SITE

     Scientific Research Laboratory, Dearborn, Michigan.

4.    TEST OBJECTIVES

     •  To develop techniques  for the quantitative analysis of methanol  in
        vehicle exhaust.
     •  To compare the influence of fuel composition on the aliphatic,  aroma-
        tic, and oxygenated hydrocarbon emissions.

5.    SPONSORING AGENCY

     Ford Motor Company
     Scientific Research Laboratory
     Dearborn,  Michigan
     Telephone  No:   313 - 322-3494

6.    CONTRACTOR

     None.
*
 Because of the unavailability of synfuels, the fuels used in some of these
 programs were not "true" synfuels (e.g., methanol-derived from natural gas was
 used instead of coal-derived methanol).  These studies, however, are included
 in this report because they were conducted to show what might be expected from
 the combustion of actual synfuels in the indicated combustion systems.


                                   A-167

-------
 7.   TEST CONDITIONS

     The vehicle was  operated  at  steady  state and over a Federal  test procedure

     CVS-C/H certification  cycle  on  a  chassis dynamometer.   The engine was run

     at steady-state  conditions using  the  following speed/load map:

               Point  1:     Speed  = 1000  rpm
                           Load   = WOT
                           0 FA   =1.1
                           Spark  = MBT

               Point  2:     Speed  = 1000  rpm
                           Load   = 25  percent of WOT
                           0 FA   = 0.95
                           Spark  = MBT

               Point  3:     Speed  = 3000  rpm
                           Load   = WOT
                           0 FA   =1.1
                           Spark  = MBT

               Point  4:     Speed  = 3000  rpm
                           Load   = 25  percent of WOT
                           0 FA   = 0.95
                           Spark  = MBT

 8.   ENVIRONMENTAL MONITORING

     Total  hydrocarbons  (as propane) and specific organics.

 9.   PROJECT STATUS

     Project completed and  presented in  February 1981.

10.   RESULTS

     A summary of the results  are presented in Figures A-22  to A-24;  general

     findings are listed below:

     Vehicle Chassis  Dynamometer  Test

     •  M-20 fuel gave significantly higher hydrocarbon and  aromatic  emissions
        than Indolene fuel  without a catalyst.  M-20 fuel gave only slightly
        higher aliphatic hydrocarbon,  aldehyde, and aromatic emissions than
        Indolene in the  presence  of  a  catalyst.

     Engine Dynamometer  Test

     •  Methanol and  aldehyde  emissions  from 100 percent methanol fuel com-
        prised more than 98 mole  percent of total measured hydrocarbons.

     t  Methanol comprised  about  50  percent of the hydrocarbon emissions at
        lower operating  speeds of engine with M-20 fuel.


                                    A-168

-------
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xl xlO xlO x5 xlO
                     Figure A-22. A Comparison of Tailpipe  Emissions  (Post-catalyst)  From a
                                  Vehicle  Burning 20%  Methanol/80%  Indolene  and  100%  Indolene
                                  (CVS C/H - Cycle #1)

-------
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                             Using 100% Indolene Fuel

-------
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 TOTAL
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             Figure A-24.  The Effect of Engine Parameters  on Emissions Using
                          20% Methanol/80%  Indolene Fuel

-------
     •  Total  aldehyde emissions from pure methanol fueled engine were 2-3
        times  higher under most operating conditions than those emitted from
        Indolene clear and M-20 fueled engines.

     •  In general,  all  hydrocarbon species decrease in concentration with
        increasing exhaust temperatures (higher  rpm).

11.   REFERENCE

     Schuetzle,  D.,  T.J.  Prater, and R.D.  Anderson.  "Characterization of Emis-
     sions From  Methanol/Gasoline Blended Fuels".   SAE Technical  Paper No.
     810 430.  23-27 February  1981.
                                  A-172

-------
                                   TEST 39
            COMPARATIVE MUTAGENICITY OF COMBUSTION EMISSIONS OF A
                 HIGH QUALITY NO. 2 DIESEL FUEL DERIVED FROM
             SHALE OIL AND A PETROLEUM-DERIVED NO. 2 DIESEL FUEL

1.    FUELS TESTED
     Synfuel:   diesel fuel marine (refined from Paraho crude by SOHIO).
     Reference fuel:  petroleum-derived No. 2 diesel fuel (see Table A-55)

                        TABLE A-55. FUELS ANALYSIS

Analysis
API Gravity
Density @ 15°C Kg/liter
% Sulfur
Cetane Index
% Carbon
% Hydrogen
% Nitrogen
Distillation Range
IBP
10%
50%
90%
EP
FIA
% Saturates
% Olefins
% Aromatics
Shale
38.8
0.8359
0.024
57.0
84.08
14.96
<0.01

395°F
450°F
503°F
553°F
574°F

61.6
4.1
34.3
Petroleum #lf
35.5
0.8469
0.16
48.0
84.59
14.81
<0.01

380°F
427°F
504°F
600° F
642°F

66.2
1.3
32.5

     t
Hydrotreated Diesel Fuel Marine courtesy of Navy Shale Oil refining
run.
Local #2 diesel fuel from Phillips Petroleum, Couch V.
                                    A-173

-------
2.   TEST EQUIPMENT

     Test vehicle was a prototype turbocharged diesel Volkswagen Rabbit

     (European Golf).  The vehicle was equipped with a 1.5 liter prototype

     injection engine with a rated 70 hp at 4,800 rpm.

3.   TEST SITE

     U.S. Department of Transportation, Cambridge, Massachusetts.

4.   TEST OBJECTIVE

     •  To determine the relative quantity of mutagenic materials contained
        in diesel fuels from synfuels as compared to those prepared from
        petroleum.

5.   SPONSORING AGENCIES

     U.S. Environmental Protection Agency
     Environmental  Research Center
     Research Triangle Park, North Carolina

     U.S. Department of Transportation
     Transportation Systems Center
     Cambridge, Massachusetts

     Project Officer:  J.  Sturm
     Telephone No:    617- 494-2716

6.   CONTRACTOR

     None

7.   TEST CONDITIONS

     The vehicle was repetitively operated on a chassis dynamometer to simulate

     an actual driving pattern; the highway fuel  economy test cycle (HWFET).

     This cycle is  12.75 minutes long over 10.24 miles at an average speed of
     48 miles per hour.

8.   ENVIRONMENTAL  MONITORING

     HC, NOX, CO, particulates, particulate matter composition, and mutagenici-
     ty of particulates (Ames test).

9.   PROJECT STATUS

     Project is completed.   Paper presented June 23-24, 1980.
                                    A-174

-------
10.   RESULTS

     Generally, the HC and CO emissions were found to be lower and NO  levels
                                                                     A
     higher for the shale-derived fuel as compared to the petroleum-derived

     fuel.  The particle emission rate and fuel economy values were similar

     with both fuels.  The emissions from the shale-derived fuel were somewhat
     higher in extractable organics.

     The emissions were measured by DOT as 0.14/0.89/1.07 grams per mile of

     HC/CO/NO  , respectively.  Using the Federal Test Procedure driving cycle,
             ,A
     this vehicle emitted 0.17 grams of particles per mile, which would meet

     the newly proposed EPA standard of 0.2 g/mile (the fuel used in these

     tests was not specified).

     The mutagenic activity of the organics from the particle emissions was

     similar for the two fuels, but because the shale-fuel sample was somewhat

     higher both in mutagenic activity and extractable organics, the rever-

     tants/mile was greater for the shale-derived fuel (see Table A-56).

11.   REFERENCE

     Huisingh, J.L., et al.  Comparative Mutagenicity of Combustion Emissions
     of a High Quality No. 2 Diesel Fuel Derived From Shale Oil and a Petro-
     leum Derived No. 2 Diesel Fuel.  In:  Proceedings of the Symposium on
     Health Effects Investigation of Oil Shale Development, Sponsored by the
     U.S. Environmental Protection Agency, Gatlinburgh, Tennessee, June 23-24,
     1980.  Ann Arbor Science Publishers, Inc., Ann Arbor, Michigan, 1981.
     255 pp.


          TABLE A-56. COMPARISON OF THE MUTAGENIC EMISSION RATE*
                      BETWEEN A PETROLEUM AND SHALE DERIVED FUEL IN
                      SALMONELLA TYPHIMURIUM TA98 WITHOUT ACTIVATION



Petroleum
Shale
Rev/
yg Org.
5.10
7.68
% Ext
17.8
21.4
Rev x 105/
gm Part.
9.08
16.43
Per
gm/mi
0.18
0.17
Revertants/
Mile
163,000
279,000

      Turbocharged VW Rabbit diesel vehicle  (56.4 mi/gal).
                                    A-175

-------
                                   TEST 40

        REPORT ON THE METHANOL-POWERED BANK OF AMERICA VEHICLE FLEET

                       IN SAN FRANCISCO AND LOS ANGELES


1.    FUELS TESTED*

     Reference fuels:  simple blends of methanol and gasoline ranging between

     2 and 18 percent by volume.

2.    TEST EQUIPMENT

     93 vehicles from the Bank of America fleet.  44 were control vehicles, 49

     were run on the blends.

3.    TEST SITE

     San Francisco and Los Angeles areas.

4.    TEST OBJECTIVES

     •  To demonstrate the practicality of using the various kinds of blends.

5.    SPONSORING AGENCY

     Bank of America
     San Francisco, CA  (Headquarters)

6.    CONTRACTOR

     Carson Associates
     4117 Robertson Boulevard
     Alexandria, VA  22309

     Project Manager:  Mr. Gavin  McGurdy
     Telephone No:  703-780-8284

7.    TEST CONDITIONS

     Fleet tested in California from February 1980 to present.
*
 Because of the unavailability of synfuels, the fuels used in some of these
 programs were not "true" synfuels (e.g., methanol-derived from natural  gas was
 used instead of coal-derived methanol).  These studies, however, are included
 in this report because they were conducted to show what might be expected from
 the combustion of actual synfuels in the indicated combustion systems.


                                    A-176

-------
 8.   ENVIRONMENTAL  MONITORING
     CO,  NO,  and unburned hydrocarbons.
 9.   PROJECT  STATUS
     Intensive data gathering in November,  December,  and  January  (80-81).
     Bank now expanding use of blends at 2  and 4 percent  levels.   The  contrac-
     tor  is continuing to supply support.
10.   RESULTS
     •  Use of 2 and 4 percent blends recommended.
     •  Blends are practical and economical, result in improved mileage  in  new
        cars  and decrease emissions of CO and unburned hydrocarbons.
     •  An operating cost decrease of l
-------
                                   TEST 41

                       ADVANCED COMBUSTION  SYSTEMS FOR

                       STATIONARY GAS TURBINE ENGINES


1.    FUELS TESTED

     Synfuel:   shale-derived diesel  fuel marine (DFM).

     Reference fuels:   No.  2 fuel, No. 2 fuel with 0.5 percent nitrogen.

2.    TEST EQUIPMENT (See Figures A-25 and A-26)

     Utilizing a Rich  Burn/Quick Quench concept from bench scale model evalua^

     tions, two configurations of a full-scale prototype (25 megawatt engine

     size) gas turbine combustor were constructed and tested.

3.    TEST SITE

     Pratt and Whitney Aircraft, West Palm  Beach, Florida.

4.    TEST OBJECTIVES

     •  Identify, evaluate,  and demonstrate alternative combustor design con-
        cepts  for significantly reducing the production of NOX in stationary
        gas turbine engines.

     •  Program goals  were  50 ppmv NOX (at  15 percent 03) for non-nitrogenous
        fuels, and 100 ppmv  NOX (at 15 percent 02) for oil or gas containing
        0.5 percent nitrogen by weight.  The goal for CO was 100 ppmv (at 15
        percent 02).

5.    SPONSORING AGENCY

     U.S. Environmental Protection Agency
     Industrial Environmental Research Laboratory
     Office of Environmental Engineering and Technology
     Research  Triangle Park, NC

     Project Officer:   W.  S. Lanier
     Telephone No:  919-541-2432

6.    CONTRACTOR

     United Technologies Corporation
     Pratt and Whitney Aircraft Group
     Government Products Division
     West Palm Beach,  Florida

                                    A-178

-------
I




WD
                                  Figure A-25.  Full-Scale Combustor  Scheme  FS-03A
                                   Figure A-26.   Full-Scale  Combustor Scheme FS-04

-------
     Program Manager:   Robert M.  Pierce
     Telephone No:   305-840-2239
7.   TEST CONDITIONS
     Test conditions are summarized in Table A-57 below.  (For a complete list
     of test parameters, see referenced document.)
                         TABLE A-57.   TEST CONDITIONS

Combustor
Configuration
FS-03A
FS-03A
FS-03A
FS-03A
FS-03A
FS-03A
FS-04B
FS-04B
FS-04B
FS-04B
Fuel Type
No. 2 fuel with 0.5% N
No. 2 fuel, No. 2 fuel
with 0.5% N
No. 2 fuel, No. 2 fuel
with 0.5% N
Shale DFM
Shale DFM
No. 2 fuel
Shale DFM
Shale DFM
No. 2 fuel
No. 2 fuel
Power
Level
100%
100%
100%
100%
100%
100%
Idle
50%
Idle
50%
Inlet Air
Temp., °F
400
450
575
475
570
570
320
550
320
550
Rig Pressure
psia
50
50
100
50
100
100
40
96
40
96

8.    ENVIRONMENTAL MONITORING
     NO ,  CO,  and unburned  hydrocarbons.
       A
9.    PROJECT STATUS
     Research  was conducted from 1  January 1978 through 12 April  1979.   Final
     report is dated January 1980.
10.   RESULTS
     The results  of the Rich Burn/Quick  Quench  combustor emission tests are
     summarized in Figures  A-27 through  A-34,  and highlighted below.
                                   A-180

-------
500
                           FS-03A 10)

                              D NOX No. 2 Fuel
                              OCO No. 2 Fuel
(Runs FS03A 1
                                 NOX No. 2 Fuel
                                  With 0.5% N
                                 CO No. 2 Fuel
                                  With 0.5% N
                                      50 psm
                                      450°F
                                                          500
              0.1         0.2         0.3

                Overall Equivalence Ratio
(Runs FS-03A-11-*-FS-03A-20)
     I           I
   NOX No. 2 Fuel With 0.5% N
   CO  No. 2 Fuel With 0.5% N
                                                                                                50 psia
                                                                                                400°F
                                                             0.1         0.2         0.3

                                                               Overall Equivalence Ratio
                 Figure A-27.
    Variation in Emission  Concentrations with
    Overall  Equivalence Ratio  for Scheme
    PS-03A,  First Test Series
                                                                  Figure A-28.
                                                     Variation  in Emission Concentrations with
                                                     Overall  Equivalence Ratio for Scheme
                                                     PS-03A,  Second Test Series

-------
       500
00
rsi
                                        NOX No. 2 Fuel
                                         With 0.5% N
                                        CO No. 2 Fuel
                                         With 0.5% N
500
                     0.1         0.2        0.3

                       Overall Equivalence Ratio
                                     50 psia
                                     475°F
                                     Shale DFM
              0.1         0.2        0.3

                Overall Equivalence Ratio
0.4
                          Figure A-29.
            Variation  in  Emission Concentrations with
            Overall  Equivalence Ratio for Scheme
            PS-03A,  Third Test Series
                 Figure A-30.
   Variation  in  Emission Concentrations with
   Overall  Equivalence Ratio for Scheme
   PS-03A,  Fourth  Test Series

-------
       500
3=.
i
co
OJ
                                          100psia
                                          570°F
                                          Shale DFM
   500
         0
                     0.1         0.2         0.3
                       Overall Equivalence Ratio
                                                             0^400
                                                              c.
                                                              0.
                                                              C
                                                              o
u
c
o
O
c
o
                                                              E
                                                             LU
   300
                                                                200
   100
                                                                          (Runs FS-03A-47
                                                                          QNO
                                                                          OGO
                                         100 psia
                                         570°F
                                         No. 2 Fuel
                 0.1         0.2        0.3
                   Overall Equivalence Ratio
                         Figure A-31.
           Variation  in Emission Concentrations  with
           Overall  Equivalence Ratio for  Scheme
           PS-03A,  Fifth Test Series
                     Figure A-32.
       Variation  in Emission Concentrations with
       Overall  Equivalence Ratio for Scheme
       PS-03A,  Sixth Test Series

-------
                                          (Runs FS-04B-8, 13. & 14)
 CM
o
a
3
ruo
800
500
400



NO,, CO Damper Setting
Q Q — ldl«
£ V iov« Po*«'
Sh»l» DFM ^


.-



**s




O £f-





\

°o o.i 0.2 o.:
                                                                   700
   600
 CM
O

ss
in

Z 500
                                                                E
                                                                Q.
                                                                a.
                                                                in
                                                                C

                                                                O
c
a.)
o
c
O
o


o
                                                                E
                                                               in
                                                                   400
                                                                   300
                                                                   200
                                                                   100
                                                                     0
(R





! 1
uns FS-04B-6, 7, and 9 to 12)
i i i
NOX CO Damper Setting
O
A
f*~^
y
i
JL 	
/
i
i
i
i
v— ^
jf\
1 \
lo\
o
V
No. 2


7

Idle
50% Po\
Fuel




ner




                        Overall Equivalence Ratio
                                                                      0       0.1      0.2      0.3      0.4


                                                                                Overall Equivalence Ratio
                                                0.5
                         Figure A-33.

           Variation in  Emission Concentrations with

           Overall Equivalence Ratio for  Scheme

           FS-04B Firing Shale DFM
                   Figure A-34.

      Variation in Emission Concentrations with

      Overall  Equivalence Ratio for  Scheme

      FS-04B Firing No.  2 Fuel

-------
     •   Both  combustor configurations (longer and shorter primary zone  resi-
        dence lengths) met emission goals of the program on  both non-nitro-
        genous and nitrogen-bearing fuels.

     •   The  Rich Burn/Quick Quench combustor also met the program emission
        goal  while operating on a shale-derived diesel  fuel  marine.   This
        indicates the potential for handling other alternative fuels  (both
        shale oil and coal derived) by this combustion concept.
     •   Variable geometry was successfully employed to vary  the  airflow ad-
        mitted into the primary combustion volume.  This demonstrated the
        ability to meet the program emission goals over the  range of  operating
        conditions experienced in a typical 25-Mw GTE.
     •   Unburned hydrocarbon emissions from combustor FS-03A ranged  from 0.9-
        7.3  ppmw for No. 2 fuel; 1.1-21.8 ppmv for No.  2 fuel  with 0.5  percent
        N; and 1.3-15.3 ppmv for shale DFM at 15 percent 02-

11.   REFERENCE

     Pierce,  R.M., C.E. Smith, and B.S. Hintan.  Advanced Combustion  Systems
     for Stationary Gas Turbine Engines:  Volume  III.  Combustor Verification
     Testing.  Prepared by United Technologies Corp. for U.S.  Environmental
     Protection Agency.   EPA-600/7-80-017c.  January 1980.
                                    A-185

-------
                                   TEST 42
                       ADVANCED COMBUSTION SYSTEMS FOR

                       STATIONARY GAS TURBINE ENGINES


1.   FUELS TESTED (See Table A-58)

     Synfuels:   SRC-II middle distillate fuel oil  and shale-derived residual

     oil.

     Reference  fuels:   No.  2 fuel and an Indonesian/Malaysian residual oil.

2.   TEST  EQUIPMENT (See Table A-59)

     A prototype full-scale (25 megawatt engine size) Rich Burn/Quick Quench

     gas turbine with  two combustor configurations.

3.   TEST  SITE

     Pratt and  Whitney Aircraft, West Palm Beach,  Florida.

4.   TEST  OBJECTIVES

     •  Identify, evaluate, and demonstrate the effects of a Rich Burn/Quick
        Quench  combustor on NOX formation while burning synthetic liquid and
        residual fuel  oils.

     •  Program goals  were 50 ppmv NOX (at 15 percent Q£) for non-nitrogenous
        fuels,  and 100 ppmv NOX (at 15 percent 02) for oil or gas containing
        0.5 percent nitrogen by weight.  The goal  for CO was 100 ppmv (at 15
        percent 02).

5.   SPONSORING AGENCY

     U.S.  Environmental Protection Agency
     Industrial Environmental Research Laboratory
     Office of  Environmental Engineering and Technology
     Research Triangle Park, NC

     Project Officer:   W.S. Lanier
     Telephone  No:  919-541-2432

6.   CONTRACTOR

     United Technologies Corporation
     Pratt and  Whitney Aircraft Group
     Government Products Division
     West  Palm  Beach,  Florida

                                    A-186

-------
        TABLE A-58.  COMPARISON OF FUEL PROPERTIES FOR TEST FUELS"

Specific Gravity

Viscosity,
centi stokes
Surface Tension
dynes/cm
Heat of Combustion
(net) Btu/lbm
Pour Point, °F

Flash Point, °F
Ultimate Analysis
Carbon%
Hydrogen %
Nitrogen %
Sulfur %
Ash %
Oxygen %
Conradson Carbon,
Residue %
End Point, °F
Atmos. Distillation
Carbon/Hydrogen
Ratio (by wt)
Hydrogen/Carbon
Molar Ratio
No. 2
(Typical)
0.84
(60°F)
5.0
(60°F)
25.7
(60°F)

18,700
<5

>130

87.0
12.8
<0.02
0.04-0.48
<0.003
<0.09

<0.30

640

6.537

1.823
SRC-II
Middle
Distillate
0.97
(609F)
6.3
(60°F)
33.3
(60°F)

17,235
<-45

>160

85.77
9.20
0.95
0.19
0.001
3.89

0.03

541

9.323

1.278
Indonesian/
Malaysian
Res id
0.87
(210°F)
11.6
(210°F)
22. 6-1-
(210°F)

17,980
61

210

86.53
11.93
0.24
0.22
0.036
—

3.98

NA

7.253

1.643
Shale
Res id
0.82
(210°F)
3.3
(210°F)
20. 6f
(210°F)

18,190
90
(remains waxy)
235

86.71
12.76
0.46
0.03
0.009
0.03

0.19

700

6.795

1.754

7t
 Fuel  properties are given at stand delivery temperatures to be maintained in
 test  program.

 Estimate on basis of fuel specific gravity.
                                    A-187

-------
                     TABLE  A-59.   SUMMARY  OF COMBUSTOR DESIGN  FEATURES
                              Premized Configuration
                               (Scheme FS-05A/B)
                               Nonpremixed Configuration
                                    (Scheme FS-07A)
                                    High Temperature
                                    Rise Configuration
                                   ^Scheme FS-08A)
Type Com bust or



I-ength (Primary)

length (Dilution)

length (O%'ernll)
Combustor  Can. Convert ivp
Primflry Zone Codling. Finned
Serondnry Zone

19.0 in.

8.0 in.

48.0 in. (including  transition
section  to turbine inlet)
Copibustor  Can.  Convertivp
Primnrv Zone Cooling. Finned
Secondary /one

19.0 in.

8.0 in.

4.'t.2 in. (including transition
section  to turbine  inlet)
Combustor  Can.  Convpctive
Primarv 7,one Cooling. Finned
Secondary Zone

19.0 in.

8.0 in.

4:1.2 in. (including transition
section to turbine inlet)
Outer Diameter

!nner Diameter

Combustor Reference
Area (Primary)
11.2* in.

9.R in.

75.4 in. sq
11.25 in.

9.8 in.

75.4 in. sq
11.25 in.

9.8 in.

75.4 in. sq
Type Nozzle (Initial
Configuration)
Single-zone  low-pressure
spr'aybars (12  with a  total of
.1G holes at O.O.'tl dial
Sonicore Model 281T boost-    Sonicore  Model  281T boosl-
air   no77lc.  compressed  ni-    air  no7.7.le.  compressed   ni-
trogen IHMISI  supply             trogen boost siipplv
Swirler (Initial
Configuntion)
.1.20 in. O.D.. 0.5fi in. I.D..  15
constant  soliditv vanes with
vented, flat  centerhodv (2f>
deg swirl angle)
•I in in  OH.. 1.75 in. I I).. 20    t.O.'t in. O.I).. 1.75 in. I.I).. 20
vane recessed swirler (45  deg    vane recessed svvirler ()•"> deg
swirl angle)                    swirl angle!
Combu.itnr Material
Outer Liner

Inne' Liner
Tvpe :147 SST

Slellite Ml (X40I
Tvpe :i47 SST

Stellile :ll IX 10)
Tv(ie :! 17 SST

Stellile  Ml (XlO)
Combu.ttnr Wall Thickness
Outer Liner

Inner Liner
O.OR25 in.

0.125 in. on  diiimi'ler with
0.125 high IIns
O.(Hi2fi in.
O.IMVJ.'i in.
0.125 in.  on  diameter wilh    0.125  in.  on diameter  wilh
n.125 high fins                  0.125 high fins
Design Point Cunditions
Fuel-Air Ratio

Volumetric Heal Release
0.01S9

2.05X10' Btu/lft'-hr-Atm)
001 Kit                         0 ()•«)•_)

2.05* |(t« Hlu/ll'.hr-Atm)        2.05 • I0« Blu/Ci'-hr-Alml
Rate Hased on:
Inlet Pressure 188 psia 188 psia
Conibuslor Airflow :il.5th/s :tl 5 ttVs
Conibuslor Reference 2!) 0 f/s 2!>.OI's
Velocity ( Primary 1
Conibuslor Total 5..V, 55',
Pressure Loss

188 psia
20.4 Ib/s
29.0 f/s
5. 5',
                                                      A-188

-------
     Program Manager:  Robert M. Pierce
     Telephone No:  305-840-2239

 7.   TEST CONDITIONS

     Inlet air temperatures (in °F), inlet total pressures (in psia), and exit

     equivalence ratios are given in Figures A-35 through A-42 of the results
     section.

 8.   ENVIRONMENTAL MONITORING

     NO , CO, unburned hydrocarbons, and smoke.
       A

 9.   PROJECT STATUS

     Research was conducted from 1  July 1979 through 12 October 1979.  Final
     report is dated January 1980.

10.   RESULTS

     The results are summarized in  Figures A-35  through A-42,  Tables A-60 and
     A-61, and highlighted below.

     •  All exhaust emission goals  of the program were met while burning the
        test synfuels and Malaysian residual oil.

     •  Sufficient residence time - A trade-off  was shown to exist between
        primary zone residence time and attainable NOX emission concentrations.
        This trade-off, however, appears to be asymptotic with increasing re-
        sidence time.  It is thought that the level of the asymptote (NOX) is
        a function of the degree to which each of the critical features  of the
        concept were executed.

     •  It was also shown in this program that the Rich Burn/Quick Quench con-
        cept essentially eliminates the adverse  effect that increased pressure
        can have on NOX formation (this effect is very evident in lean combus-
        tion and is ordinarily found to be proportional to the square root of
        the pressure ratio).

11.   REFERENCE

     Pierce, R.M., C.E.. Smith, and  B.S. Hintan.   Advanced Combustion Systems
     For Stationary Gas Turbine Engines:  Vol. IV.  Combustor Verification
     Testing (Addendum).   Prepared  by United Technologies Corp. for U.S. Envi-
     ronmental Protection Agency, EPA-600/7-80-017d.  January 1980.
                                    A-189

-------
   400
   300
 CM
o
=£
in
Q.
Q.
   200

-------
 CM

O

#
in
a
a
 c
 o

"•5
4—i

 0)
 o
 c
 o
O
 c
 o
'(0
 52
 E
in
                                                     Runs FS-05B-10to 15,

                                                     19 and 34 to 37
                                                     100psia

                                                     615°F

                                                     No. 2 Fuel
200
    100
                                 Overall Equivalence Ratio
Figure  A-36.
           Comparison  of Variation  in  NOX Concentration  With Overall

           Equivalence Ratio for  Schemes FS-05B, FS-03A, FS-04A, and FS-04B
                                       A-191

-------
 500
             (Runs FS-05B-16 to 18 and FS-05B-20 to 24)
                                                D NOX
                                                Oco
                                                   100 psia
                                                   610°F
                                                   SRC II Middle Distillate
                               Overall Equivalence Ratio
Figure A-37.   Variation in Emission  Concentrations With  Overall Equivalence
               Ratio for Scheme FS-05B  Using SRC-II Middle  Distillate Fuel
                                    A-192

-------
  300
                              D NO
                               O UHC
                       Test No. FS-05B-25 Thru 33
                        tOOpsia, 600°F
                0.2         0.3         0.4
                     Equivalence Ratio
                                   0.5
Figure  A-38.
Emission  Signature of  Scheme FS-05B
Firing  Shale Residual
                          A-193

-------
   300
   250
 CM
O
*-  200
o
O
O  150
a
ex
c
o
'o>
OT

UJ
   100
    50
                     n_
                         NOX
                         CO
                         UHC

             Test No. FS-05B-38 Thru 43
              100psia, 600° F
                 0.1         0.2         0.3

                       Equivalence Ratio
                                   0.4
300


250
'cvi
O
10 200
o
U
O
1
Q.
Q.
W 100
c
0
'55
OT
"E
LU
50


n























1
|
\
\
§NOX
CO
UHC
| Test No. FS-07A-1 Thru 11
i 100psia, 600° F
' / — Nox FromSch
r on No. 2 Fue
i
1
1
1
1

F\ i
*— *\ 1


/\*1/^


X^AVS
^\V

' \
uu hrom bcneme
FS-05B
on No. 2

Fuel 	
(~?\.^~










/^







-&"^Lrn
— — — *^


erne FS-05B




















i
0.1         0.2          v .3

      Equivalence Ratio
                                                  0.4
Figure  A-39.
Emission Signature of Scheme  FS-05B
Firing  Indonesian/Malaysian Residual
Figure A-40.   Emission Signature of Scheme  FS-07A
               Firing No.  2  Fuel

-------
UD
CJ1
300
250
'cvi
O
- 200
o
(Corrected 1
en
o
1
Q.
Q.
g 100
O
CO
CO
E
LU
50
n















§NOX
CO
UHC


Test No: FS-07A-12 Thru 14
100psia, 600° F





X

§

£







r®
\zf^











300
250
'c\i
O
in
^- 200
0
T3
0)
t;
QJ
k-
E
Q.
Q.
S 100
o
co
E
LU
50
0












n

•
I
m NO*
«>?• ^
<^ CO
© UHC
I

Test No. FS-07A-15 Thru 17
100 psia, 600°






Vv"i
^>






















                       0.1         0.2

                            Equivalence Ratio
                         0.3
0.4
0.1
0.2         0.3

     Equivalence Ratio
0.4
0.5
     Figure A-41
Emission Signature of Scheme  FS-07A
Firing Indonesian/Malaysian Residual
        Figure A-42.
        Emission  Signature of Scheme FS-07A
        Firing  SRC-II Middle Distillate

-------
TABLE A-60.   SUMMARY OF SAE SMOKE NUMBERS


Fuel
No. 2 Fuel



SRC II
Middle
Distillate

Shale Resid



Combustor
Configuration
Premixed
Nonpremixed


Premixed


Nonpremixed
Premixed

Nonpremixed
Indo/Malaysian Premixed
Resid.


Nonpremixed


Equivalence
Test No.
FS-05B-36
FS-07A-1
FS-07A-6
FS-07A-11
FS-05B-22
FS-05B-23
FS-05B-24
FS-07A-16
FS-05B-32
FS-05B-33
—
FS-05B-42
FS-05B-43
FS-07A-14
* 1 — primary equivalence ratio near the bottom of the
Ratio
0.1265
0.1354
0.2629
0.1988
0.2134
0.2590
0.1269
0.2190
0.1818
0.2490
—
0.2370
0.2047
0.1949
NO, bucket
Approximate
Primary Zone
Condition *
3
3
2
1
1
2
3
1
1
2
—
2
1
1

SAE
Smoke No.
(ARP 1179)
1.8
0.7
43.5
13.9
9.9
44.9
1.6
31.0
14.0
42.6
Not tested
51.2
46.3
23.2

2 — primary equivalence ratio overly fuel rich
3 — lean
primary equivalence ratio
TABLE A- 61. SUMMARY










Fuel
SRC II
(0.95% N)
Shale Resid
(0.46 'V, N)
Indo/Malay. Resid
(0.24% N)
OF APPROXIMATE NITROGEN CONVERSION RATES

Scheme Scheme
FS-05B FS-07A
12% 9%



Complete Conversion of

Fuel N to NO, (15% O2)
424

12% Not Tested 185

24% 15%


102

ppmv

ppmv

ppmv







                   A-196

-------
                                   TEST 43
                                  EMISSION
            ALCOHOL FUELS FOR USE IN STATIONARY COMBUSTION SYSTEMS
EVALUATION OF N0y EMISSION CHARACTERISTICS OF
                J\
1.    FUELS TESTED  (See Table A-62)
     Reference fuels:  residual oil, distillate oil, natural  gas,  propane,
     isopropanol, methanol, and 50 percent methanol and isopropanol.
2.    TEST EQUIPMENT
     An experimental refractory wall furnace designed and constructed by
     Aerotherm/Acurex to maintain a nominal 87,864 watts and a Dowtherm-cooled
     furnace designed and constructed by Ultrasystems, Inc.,  to incorporate
     the significant features of a firetube package boiler (1 MW).
3.    TEST SITE
     Refractory wall furnace test:  EPA (in house), IERL/RTP.
     Package boiler test:  Ultrasystems, Inc., Irvine, California.
4.    TEST OBJECTIVE
     t  Evaluate combustion data on alcohol fuels  in smaller stationary boilers
        and furnaces and compare the emission characteristics to those gener-
        ated from conventional fuels.
5.    SPONSORING AGENCY
     U.S. Environmental Protection Agency
     Combustion Research Branch
     Industrial Environmental Research Laboratory
     Research Triangle Park, N.C.
     Project Officer:  G. Blair Martin
     Telephone No:  919-541-7504
 Because of the unavailability of synfuels,  the  fuels  used  in  some of these
 programs were not  "true"  synfuels  (e.g., methanol-derived  from natural gas was
 used instead of coal-derived methanol).  These  studies,  however, are included
 in this report because  they were conducted  to show what  might be expected from
 the combustion of  actual  synfuels  in  the indicated combustion systems.

                                    A-197

-------
                        TABLE A-62.  FUEL PROPERTIES
  Fuel
Chemical
Formula
Fuel Type
Higher Heating
Value 107 J/Kg
Refractory Wall Furnace Test
  Distillate oil

  Propane
  Methanol
  Isopropanol
  50% Methanol and
  isopropanol
Package Boiler Test
  Residual oil

  Distillate oil

  Natural gas
  Methanol
CH 1.78
0.025% N
0.035% S
CQHQ 90%
 o o
CH3OH
Mixture
C/H = 0.633
0.36% N
C/H - 0.565
0.05% N
CH4+
CH3OH
Commercial

LPG
Chemical grade
Chemical grade
Blend of
chemical grade

Commercial

Commercial

Commercial
Commercial grade
    4.58

    5.303
    2.27
    3.314
    2.79
6.    CONTRACTOR
     Ultrasystems, Inc.
     Irvine, California
7.    TEST CONDITIONS
     The refractory wall  furnace tests were conducted under the following
     conditions:   (1) nominal  nozzle flow and water content of selected fuels
     as shown in  Table A-63; (2) 115 percent theoretical  air for all runs;
     (3) all fuels were  run at swirl block positions 2, 4, 6, and 8 (increasing
     tangential air); and (4)  flue gas recirculation run at swirl block posi-
     tion 4 with  distillate oil, propane, methanol, and isopropanol.
     The package  boiler  simulator tests were conducted under the following
     conditions:   (1) a  baseline burner air distribution of 50 percent primary
                                    A-198

-------
                  TABLE A-63.   LIQUID FUEL NOZZLE SELECTION
Fuel
Distillate oil




Isopropanol

50% Isopropanol and 50%
Methanol
Methanol
Water Content
Mass % of Total Flow
0
21
32
42
54
0
29

0
0
Nominal Nozzle Flow
Rate x 10-6 cu.m./sec.
2.103
2.629
3.15
3.68
4.206
3.15
5.258

4.206
5.25

     and 50 percent secondary air; (2) baseline excess air was  chosen  to  be  17
     percent with variations up to 90 percent; and (3) full load heat release
     of 1  MW.

8.    ENVIRONMENTAL MONITORING

     NO ,  NO,  CO, hydrocarbons, aldehydes.
       /\
9.    PROJECT STATUS

     Project complete.   Final report dated 1977.

10.   RESULTS

     The results of the refractory wall furnace tests are highlighted below

     and in Figures A-43 through A-45.

     •  NO emission levels for the five fuels were as follows:   distillate
        oil >  propane > isopropanol > alcohol mixture > methanol.
     •  NO emissions decreased with increasing tangential air swirl for the
        alcohol fuels.
     •  NO trend for alcohol fuels is more similar to that for propane than
        that for distillate oil.
                                    A-199

-------
     •  NO emissions for all  fuels decreased with increasing fraction of flue
        gas recirculation.

     •  Theoretical  flame temperature is an important factor in explaining
        reduced NO phenomenon.
     •  CO and hydrocarbon  emissions were always below 50 ppm and smoke was
        not observed for any  fuel.

     The results of the package boiler simulator tests are highlighted below

     and in Figures A-46 and  A-47.

     •  NO emissions for methanol  were virtually constant at about 50 ppm for
        all primary air levels, which are lower than those for residual oil,
        distillate oil, or  natural  gas.

     •  Residual oil MO emissions  increased rapidly as excess 02 increased to
        4 percent, then leveled off, while methanol  NO emissions increased
        linearly with increasing excess  02-

     •  Methanol transferred  only  23.6 percent of the heat in the combustion
        zone,  while the residual oil transferred 36.4 percent in the same zone.

     •  Although there was  considerable  scatter in the data, aldehyde concen-
        trations were around  10 ppm for  methanol and there was no detectable
        difference between  methanol  and  natural gas aldehyde concentrations.

11.   REFERENCE

     Martin, G.B.  and M.P.  Heap.  Evaluation of NOX Emission Characteristics
     of Alcohol  Fuels for Use in Stationary Combustion Systems.   In:  American
     Institute of Chemical  Engineers Symposium No.  165,  Volume 73, 1977.
                                   A-200

-------
  no
  no
X
e
u
£_ 100
               ODBTILLATE OIL A eoraoMNoi  • METNANOI
               OPROPANE     O H%BOPHOPANOl • NKMETHANOL
                      4        I

                    tWRl HOCK POSITION
                    Figure A-43.

     Comparison of  Baseline Nitric Oxide
     Emissions for  Various  Fuels  as a
     Function  of  Swirl  Parameter.
                                                                 300
                                                                                             O DISTILLATE Oil
                                                                                             O PROPANE
                                                                                               ISOPROPANOL
                                                                                             O METHANOL
                                                                          006
              010       0.1S
            FRACTION RECIRCUlATEO.t
                                                                                                    OJO
                                                                                                             07S
               Figure  A-44.

Effect of Flue Ras Recirculation
on Nitric Oxide Emissions  for
Various Fuels.

-------
                                                                           400
  300
O
rxi
         a.
         O
O 100
u
5
                             9 DISTILLATE OIL WITH FOR
                             • DISTILLATE OIL EMULSIONS
                             * ISOPROPANOL
                             O 50% ISOPROPANOL • 60% METHANOL
                             OMETHANOL
                             ft ISOPROPANOL - WATER
   0
   1.900
                     1
                     1
1
                                                                         \
                                                                         >
                                                                         S no
                                   s
                                   X
                                   O

                                   f
                                   z

                                     100
                    1.800     1.700      1.600     1.&00

                    THEORETICAL FLAME TEMPEBATURE. 103*C
                                                     1.400
                                                                                 A  RESIDUAL OIL
                                                                                 •  DISTILLATE OIL
«                                                                                    NATURAL GAS
                                                                                    METHANOL
                                                                                  40      10      M

                                                                                   PRIMARV AIR, % OF TOTAL
                                                                                                        70
                         Figure A-45.

           Comparison  of Nitrix Oxide Emission
           Reduction as  a Function of Theoretical
           Flame  Temperature  for Various  Diluent
           Addition Techniques.
                                                                                    Figure  A-46.

                                                                      Comparison of Baseline Nitric Oxide
                                                                      Emissions for Various Fuels as  a
                                                                      Function of  Burner  Primary Air.

-------
  400
  -
oN



u

E

£

o

'U


O


O
u
t-
<_>
tu
E
C
O
U
g
O

X
o


K  100
  200
                           *T
 A RESIDUAL OIL

 • METHANOL

PRIMARY AIR • 60% OF TOTAL
             2       4        •        •


              FLUE CAS OXYGEN CONCENTRATION. %
                                              10
                   Figure A-47.


   Effect of Excess  Air on Nitric Oxide

   Emissions for "ethano! and Residual  Oil
                        A-203

-------
                                   TEST 44
                   THE CONTROL OF NITROGEN OXIDE EMISSIONS

                            FROM PACKAGE BOILERS


1.   FUELS TESTED*

     Reference fuels:  methanol5 natural gas, and No. 5 residual oil.

2.   TEST EQUIPMENT

     An industrial watertube boiler and an industrial firetube boiler.

3.   TEST SITE

     Essex County Correctional Center, New Jersey.

4.   TEST OBJECTIVE

     •  Evaluate NOX emission characteristics of alcohol and conventional
        fuels in industrial boilers.

5.   SPONSORING AGENCY

     U.S. Environmental Protection Agency
     Combustion Research Branch
     Industrial Environmental Research Laboratory
     Research Triangle Park, N.C.

     Project Officer:  G.  Blair Martin
     Telephone No:  919-541-7504

6.   CONTRACTOR

     Energy and Environmental Research Corporation
     2400 Michel son Drive
     Irvine, California

     Principal Investigator:  M. P. Heap
*
 Because of the unavailability of synfuels, the fuels used in some of these
 programs were not "true" synfuels (e.g., methanol-derived from natural gas was
 used instead of coal-derived methanol).  These studies, however, are included
 in this report because they were conducted to show what might be expected from
 the combustion of actual synfuels in the indicated combustion systems.


                                    A-204

-------
 7.   TEST CONDITIONS
     Excess air and load levels are reported in Figures  A-48 through  A-51  of
     the results.   Influence of flue gas recirculation was  also  tested.
 8.   ENVIRONMENTAL MONITORING
     N0x
 9.   PROJECT STATUS
     Project complete, report dated February 1977.
10.   RESULTS
     The effect of fuel type and excess air on NO  emissions from these  two
                                                 A
     boilers is shown in Figures A-48 and A-49.  The No. 5  fuel  oil  contained
     approximately 0.1 percent nitrogen, which accounts  for the  higher emis-
     sions of that fuel.  The lower emissions of the watertube boiler can  be
     attributed to the lower volumetric heat release rate.   The  influence  of
     flue gas recirculation  (FGR) for both boilers at constant excess air  on
     NO  emissions is shown  in Figures A-50 and A-51.  As seen here,  FGR was
       X
     capable of reducing methanol NO  emissions.  The effect of excess air
                                    J\
     level on thermal efficiency is shown in Figures A-52 and A-53.
11.   REFERENCE
     Cichanowicz, J.E., M.P. Heap, C. McComis, R.E. McMillan, and R.D. Zoldak
     "The Control of Nitrogen Oxide Emissions  From Package Boilers", February
     1977.  EPA Contract 68-02-1498.
                                    A-205

-------
             240
             200
             120
ro
o
o\
                                    (lb.m/hr.)
                              • 8500  No. S oil
                              A 8500  No. S oil
                              o 7300  natural gas
                              010.000 mtthanol
                              96000
                                                                          200
120
                      Load (Ib.m/hf.l
                     • 10.000  No. 6 oil
                     Q 8SOO   natural gn
                     7 6SOO   mMhanol
                                4   S
                                 02%
                      03%
                        Figure A-48.
           NOX  Emissions From a  Firetube  Boiler
           As a Function of Fuel  Type and Excess
           Oxygen.
             Figure A-49.
                From  a Watertube Boiler
As'a Function of Fuel  Type  and Excess
Oxygen.
NOX  Emissions

-------
             240
 i
ro
o
           o
           K
E
a
d

x"
O
                   Firetube
                   Flue Gas
                   Recircuiation
  Load (Ib.m/hr.) Fuel  (02)
• 6000   No.  5 oil    3.9
O 6000   Natural Gas  3.9
o 6000   Methanol    3.8
                                                                                  200
                                                                               o
                                                                               g  160

                                                                               o
                                                                                 120
                                                                               E
                                                                               Q
                                                                               O
                                                 *>
                                                                                  40
                                                                                             Load  (Ib.m/hr.)  Fuel  (02)

                                                                                           • 7500     No. 5 oil    4.6
                                                                                           O 7000     Natural Gas  3.5
                                                                                           O 8500     Methanol     3.5
                      10     20     30     40     50

                         Flue Gas Recircuiation,  mas %
                                                          10       20       30      40
                                                           Flue Gas  Recircuiation, mass %
                              Figure A-50.
              The  Influence of Flue  Gas  Recircuiation
              NO   Emissions From a  Firetube Boiler
                 X
                             on
                                                                                      Figure  A-51.
                                                                     The  Influence  of Flue Gas  Recircuiation on
                                                                     NOV  Emissions  From a  Watertube  Boiler
                                                                       A

-------
IS3
O
00
           85
           80
           75
                  Load (Ib.m/hr.) Fuel
                • 10,000      No. 5 Oil
                O 8,500      Natural Gat
                » 8,500      Melhanol
DD
                                                                             90
                                                                             76
                 1    2    3    4    E    6
                             Excea 01, *
                        789
                                                                   Load   Fual
                                                                 0 8.500  No. 6 Oil
                                                                 O 7,300  Natural Gat
                                                                 • 10,000  Methanol
                                                                                      O O
                                                                  123459789
                                                                            EXMB 03, *
                     Figure  A-52.
         The Effect of Excess Air Level  and  Fuel
         Type on  the Thermal Efficiency  of a
         Watertube  Boiler
                                                                        Figure A-53.
                                                         The Effect of  Excess Air Level  and  Fuel
                                                         Type on  the Thermal Efficiency  of a
                                                         Firetube  Boiler

-------
                                   TEST 45

                 IMPACT OF GASOHOL ON AUTOMOBILE EVAPORATIVE

                           AND TAILPIPE EMISSIONS


1.    FUELS TESTED* (see Table A-64)

     Non-synfuels:  Indolene clear (Fuel 1) ; Indolene with added  ethanol  (Fuel

     2); summer-grade unleaded regular octane fuel  with and without  added

     ethanol (Fuels 3 and 4); and blended gasohol with added ethanol  (Fuel  5).

2.    TEST EQUIPMENT

     Descriptions of the two light duty vehicles tested are provided  in Table

     A-65.

3.    TEST SITE

     "Raleigh Road Route", North Carolina.  EPA Environmental  Research Center,
     RTP, North Carolina.

4.    TEST OBJECTIVE

     a  To examine the impact of gasohol on vehicle evaporative and  tailpipe
        emissions.

5.    SPONSORING AGENCY

     U.S. Environmental Protection Agency
     Mobile Sources Laboratory
     Research Triangle Park, North Carolina

     Project Officer:   Frank M. Black
     Telephone No:   919 -541-3037

6.    CONTRACTOR

     Northrop Services, Inc.
     Research Triangle Park, North Carolina
 Because of the unavailability of  synfuels,  the fuels used  in some of these
 programs were not "true" synfuels  (e.g., methanol-derived  from natural gas was
 used instead of coal-derived methanol).  These studies,  however, are included
 in this report because they were  conducted  to show what  might be expected from
 the combustion of actual synfuels  in the indicated combustion systems.

                                    A-209

-------
TABLE A-64.  TEST FUEL SPECIFICATIONS

Specification
RVP
IBP, °F
10
50
90
EP
Ethanol (% vol )
API gravity
FIA (% paraffin)
FIA (% olefin)
FIA (% aromatic)
1
9.15
91
138
238
322
341
1.4
59.8
69.7
0.4
28.5
2 3
9.10 9.85
101 89
129 124
212 231
320 361
359 405
6.2 0.86
58.7 57.5
67.5 52.1
0.6 17.2
25.7 29.8
4
9.65
95
121
213
356
413
8.1
56.5
46.4
16.6
28.9
5
9.40
94
124
242
362
408
10.1
52.6
37.7
17.6
34.6

TABLE
A-65.
VEHICLE SPECIFICATIONS



Specification
Make
Manufacturer
Engine Family
Emissions Control
Mileage
Inertial weight (pounds)







Fuel tank capacity (gallons)
Vehicle 1
Mustang II
Ford
302 CID
EGR, CAT, PCV,
single canister
(fuel tank)
10,000
3,000
16
Vehicle 2
LTD II
Ford
351 CID
EGR, AIR,
dual cani
(carb. &
400
4,500
21




CAT, PCV,
ster
fuel tank)




                 A-210

-------
 7.   TEST CONDITIONS

     Each car was tested with Fuels 1-5 in sequential  order.   The  vehicles

     were driven on a standard road course 44 miles  long  involving 13  stops

     and an average speed of 45 mph.   One complete test included:   a diurnal

     evaporative test; an urban dynamometer driving  test;  and  a  hot-soak  eva-

     porative test.  For complete details, see referenced  report.

 8.   ENVIRONMENTAL MONITORING

     Tailpipe exhaust samples:  THC,  CO, C0~, NOV, and ethanol.
                                           £-    X
     Evaporative samples:  THC and ethanol.

 9.   PROJECT STATUS

     Project complete; report is dated February 1981.

10.   RESULTS

     Exhaust and evaporative emission results are summarized  in  Tables A-66

     through A-69.

     t  With both vehicles, the addition of ethanol  to gasoline  resulted  in  a
        decrease in THC and CO emissions, and an increase in  NOX emissions
        (lean shift in combustion due to oxygen content of ethanol).

     •  Use of gasohol in both cars substantially increased evaporative emis-
        sions.  The aggragate change, tailpipe plus evaporative, in hydrocarbon
        emissions with gasohol varied from no significant change with  Mustang
        II to a maximum increase of about  50 percent with the LTD II.

11.   REFERENCE

     Lang, J.M. and F.M. Black.  "Impact of  Gasohol on Automobile Evaporative
     and Tailpipe Emissions".  SAE Paper No. 810 438.  23-27 February 1981.
                                    A-211

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TABLE A-66.  EXHAUST EMISSION RATES  FOR  1977 MUSTANG  II

Fuel
1
2
3
4
5
Gram/mi 1 e
THC*
3.83
2.82
3.15
1.72
2.66
CO
26.7
19.8
27.0
17.2
25.5
N0x
NA
1.53
1.27
1.72
1.48
Ethanol
0
0.026
0.002
0.024
0.044
Fuel Economy
15.5
14.7
14.3
17.1
12.8

*
Sum
of hydrocarbons
and ethanol.
TABLE A-67. EVAPORATIVE
EMISSIONS
FOR 1977
MUSTANG II

Fuel
1
2
3
4
5

HCD
0.42
0.32
0.42
0.34
0.51

HCHS
10.60
22.10
18.80
36.10
22.90
Grams
Total
11.02
22.40
19.22
36.44
23.41

Ethanol
0.05
5.59
0.29
7.80
6.51

HC + Ethanol
11.07
27.99
19.51
44.24
29.92

                          A-212

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TABLE A-68. EXHAUST EMISSION RATES FOR 1979 LTD II
Fuel

1
2
3
4
5

THC*
0.50
0.37
0.60
0.46
0.55

CO
12.7
9.2
10.3
5.7
7.8
Gram/mile
NOX
1.36
1.83
1.85
2.20
2.10

Ethanol
0
0.002
0
0.012
0.023

Fuel Economy
11.3
11.4
11.0
10.9
11.4

*
Sum

of hydrocarbons
TABLE A-69.
and
ethanol .

EVAPORATIVE EMISSIONS FOR 1979

LTD II

Fuel

1
2
3
4
5

HCD
0.47
0.86
0.86
0.74
1.22

HCHS
1.07
3.53
1.65
6.49
4.86
Grains
Total
1.54
4.39
2.51
7.23
6.08

Ethanol
0.03
0.55
0.07
0.94
0.91

HC + Ethanol
1.57
4.94
2.58
8.17
6.99
                         A-213

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                                TECHNiCAL REPORT DATA
                          (Please read Instructions on the reverse before completing)
1. REPORT NO.
   EPA-600/7-82-015
                                                      3. RECIPIENT'S ACCESSION NO.
4. TITLE AND SUBTITLE         „„,,,.   ~,  ..    T-.
A Compendium of Synfuel End-Use Testing Programs
            5. REPORT DATE
              April  1982
                                                      6. PERFORMING ORGANIZATION CODE
7. AUTHOR(S)
 Masood Ghassemi, Sandra Quinlivan,  and
 Michael Haro	
                                                      8. PERFORMING ORGANIZATION REPORT NO.
9. PERFORMING ORGANIZATION NAME AND ADDRESS
 TRW, Inc.
 One Space Park
 Redondo Beach, California  90278
                                                      10. PROGRAM ELEMENT NO.
            11. CONTRACT/GRANT NO.

             68-02-3174, Task 18
 12. SPONSORING AGENCY NAME AND ADDRESS
                                                      13. TYPE OF REPORT AND PERIOD COVERED
 EPA, Office of Research and Development
 Industrial Environmental Research Laboratory
 Research Triangle Park, NC 27711
                                                       13. TYPE OF REPORT
                                                       Final; 3-9/81
            14. SPONSORING AGENCY CODE
              EPA/600/13
 15. SUPPLEMENTARY NOTES IERL-RTP project officer is Joseph A. McSorley, Mail Drop 61,
 919/541-2827.                                                                   '
 16. ABSTRACT
              report gives information on major, recently completed, current, and
 planned synfuel end-use testing projects. It is intended to promote the flow of infor-
 mation between synfuel testing programs , thereby reducing the duplication of effort
 and enabling design and implementation of cost-effective and systematic approaches
 to the collection of appropriate environmental data in conjunction with on-going and
 planned performance testing projects. EPA plans to update this compendium to
 include  results from current and future testing programs.  Projects  described in the
 compendium include testing of shale-derived fuels, SRC-IE middle distillates, EDS
 fuel oils,  H-coal liquids, and methanol/indolene mixtures in such equipment as util-
 ity boilers, steam generators, diesel engines (laboratory and full scale),  auto
 engines, and other combustors. Published reports on testing and discussions with
 test sponsors/contractors are the sources of data for the compendium. Agencies/
 organizations providing input  include DOD, DOE, NASA, EPRI, private synfuel de-
 velopers, and engine manufacturers.
17.
                             KEY WORDS AND DOCUMENT ANALYSIS
                DESCRIPTORS
                                          b.IDENTIFIERS/OPEN ENDED TERMS
                                                                   c. COSATl Field/Group
 Pollution
 Tests
 Fossil Fuels
 Synthetic Oils
 Carbinols
 Combustion
 Pollution Control
 Stationary Sources
 Synthetic Fuels
 Indolene
13 B
14B
21D,08G
11H
07C
21B
              iTEMEN
 Release to Public
                                          19. SECURITY CLASS (ThisReport)
                                          Unclassified
                         21. NO. OF PAGES

                             236
20. SECURITY CLASS (."hispage)
Unclassified
                                                                   22. PRICE
EPA Form 2220-1 (9-73)
                                       A-214

-------