INCINERABILITY RANKING OF HAZARDOUS ORGANIC COMPOUNDS

                            by
                   Robert E. Mournighan
                    Marta K.  Richards
                       Howard Wall
               Technology  Research Section
                Thermal Destruction Branch
            Waste Minimization Destruction and
                Disposal Research Division
          Risk Reduction Engineering Laboratory
           U.S.  Environmental Protection Agency
                     Cincinnati, Ohio
 For  Presentation at the  15th Annual Research Symposium on
Remedial Action, Treatment and Disposal of Hazardous Waste

                     Cincinnati, Ohio

                    April  10-12, 1989
          RISK REDUCTION  ENGINEERING  LABORATORY
            OFFICE OF RESEARCH AND DEVELOPMENT
           U.S.  ENVIRONMENTAL PROTECTION AGENCY
                  CINCINNATI, OHIO 45268

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                                 INTRODUCTION

      Since the regulation of hazardous waste by  the  USEPA, both the Agency and
the regulated community have been searching for means of evaluating incinerator
performance.   The concept of  a  "trial burn,"- a series of tests  designed  to
evaluate the ability of an  incinerator to  process  waste to certain standards,
was developed; and surrogates were introduced (1) for hazardous and solid waste
and for  Principal  Organic Hazardous Constituents, or POHCs.   In  essence,  the
incinerator's ability to destroy waste was based on its performance in destroying
the POHCs.

      Destruction  and  Removal  Efficiency   (DRE)  is used  by  EPA  to  express
incinerator performance.  The DRE of a  POHC is calculated as follows:
            ORE =  (^in  - Uput) x 100                 (2)
                       ^in
            Where win and W0ut are the mass flow rates of the POHC
            input and output (at the stack) respectively.(2)

      As regulations and  policies regarding trial burns developed,  it became
apparent to all concerned that DRE determinations were rapidly becoming extremely
expensive  and  time  consuming.    It  is not  unusual  to  see  trial burn  costs
approaching 2% of  the  capital  costs  of the facility.  Largely responsible for
these  costs was  the requirement  that several  types  of POHCs be evaluated,
resulting  in  the use of  multiple sampling  trains.  The process  of obtaining
representative samples  could take a  week,  or longer.    Sample processing and
analysis, also expensive, would  drag out  the time-span between trial burn and
results to over three months.  The objective  for  regulators and regulated alike

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was to search for a less expensive approach.  The approach was similar to that
taken for POHCs and solid waste:   find a  surrogate for the waste being burned
and develop a cheap,  quick analytical  method for  the analysis of the surrogate.
Several compounds, e.g., Sulfur  hexafluoride (SFg)  and Freons^ fluorocarbons,
were put forth as candidates.(3)

      Because of its high thermal  and chemical  stability  and the fact that it
is inexpensive and non-toxic, SFg received  much attention as a surrogate.  Quick,
relatively inexpensive, and  reliable  methods were developed for its analysis,
and initial evaluation began  in 1984.(4) A system employing a gas chromatograph,
equipped with  an  electron  capture detector (GC/ECD),  was  used  to  obtain SFg
concentrations in stack gas  every 2 to 4 minutes, a much shorter time than the
sampling time required  for sampling  trains.  Equipment set-up, operation, and
calculation of results  could be done in 1-1/2 days (4),  a far cry  from three
months.

      Since that time,  a great  deal  of effort,  time and money has been spent,
both in the United States and Canada (5), to exhaustively evaluate SFg as a POHC
or waste surrogate.

      During the same time period,  the concept of using a  standard POHC mixture
(a "POHC Soup") for trial burns, by employing a  group of compounds with a range
of chemical and physical characteristics, was developed.  A paper describing the
rationale and results of that effort  is being given at this  conference.(6)

      Both of these efforts  have been researched extensively at the laboratory
stage  (5, 6, 7).   An evaluation program at pilot scale  for  the  USEPA Combustion

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Research Facility (CRF) was proposed in 1987.  The CRF has two pilot-scale
(3 x  10^  Btu/hr) incinerators, a  liquid  injection system and  a  rotary kiln.
The SFg/"POHC Soup" program was performed  in the  liquid  injection system.  This
paper describes the ORE results and discusses the implication of this work and
of other researchers.

      Interest  in  assuring and  demonstrating  compliance  with  RCRA  permit
conditions has also concerned  the  hazardous waste community.  Trial burns are
prohibitively expensive to  carry  out on a  routine  or even  annual  basis, with
not much gained in the process. This approach still leaves "gaps in coverage,"
where incinerator performance may be unknown.  It  became  apparent, after initial
research at EPA,  that residence time,  temperature and  turbulence  were not the
only factors to consider in the evolution of incineration criteria.   The Toxic
Substance  Control  regulations   (8)   for  PCB   incineration  reflected  that
realization, and  stipulated not only time and  temperature,  but also a minimum
stack 02 concentration as well  as a minimum combustion efficiency of 9,9.9% are
required.
This paper concentrates on the evaluations  of SFg and the "POHC Soup" as trial
burn surrogates.

                            EXPERIMENTAL BACKGROUND

     The experimental program  was executed at  the USEPA Combustion Research
Facility's Liquid  Injection System (LIS).  Figure  1 is  a sketch  of the unit,
showing each of the elements that  make  up  the incinerator and the air pollution
control system.

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                                         Stack
                        Building wall
                Afterburner chamber _~
                (unfired)            \
   Sampling port
'Quench chambei
            Main  chamber
     Aux. propane
     Liquid feed'
Atomizing steam
 Combustion air
                          HEPA      Carbon bed
                          filter/^ absorber
                                                                              ..Ionizing wet
                                                                             /scrubber
              -4-Pack
                 column
                 scrubber
                            Venturl  scrubber-/
                    Scrubber liquid tank
                              Figure 1.   CRF liquid Injection  system.

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      The LIS  is fired  with liquid  waste,  and propane  is used  to maintain
temperature control.  Combustion air  is supplied by forced-draft fan.  The waste
mixture containing  the "POHC Soup" was  stored  in  a stainless steel, vessel and
pumped continuously to the LIS.(9)  SFg was  injected into the  liquid feed stream
as a gas, where it dissolved into the liquid phase just prior to incineration.

      Sampling of the stack gas  for both SFg and the  POHCs was done at the exit
of the air pollution control systems,  just after the ionizing wet  scrubber (IWS).
Even  though  the  gas passes  through  additional  gas  cleanup,  sampling further
downstream was not conducted. The  final  gas  cleanup  is unique to this facility
and is not standard for commercial  and private incinerators.  Table 1 shows the
experimental conditions and the ORE results for the SFg and the POHC components.

      Oxygen  and  incinerator temperature  were  varied as  part of  a designed
experiment.  All  other variables, such as waste composition and  flow rates, were
kept  constant.

      The compounds used  in the test mixture were  toluene (70%), chlorobenzene
(10%), pentachlorobenzene (10%) and tetrachloroethylene (10%). This combination
of compounds resulted in a mixture  which contained  both volatile components and
semivolatiles.   Stack  sampling  of these components  was  accomplished with the
VOST  (USEPA  Method  0030) and Modified Method 5 (USEPA Method  0010).  The SF6
sampling method was proportional gas sampling, with  the sample being fed directly
to GC/ECD.

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               Table  1.  Data Table  - Temperature, Oxygen and
                                 DREs (number of nines)
          Afterburner                              ORE
             Exit                  Tetra-
           Tempera-  Exit          chloro-            Chloro-   Pentachloro-
Experiment ture, °C Oxygen %  SFg* ethylene* Toluene* benzene*    benzene*
]
2
3
4
5
6
7
8
9
10
Calculated
1030
1114
943
1274
1091
945
1310
1077
1175
1105
ORE by
2.3
3.3
5.6
1.3
5.1
8.2
4.5
9.2
8.0
4.7
4.35
3.59
3.33
7.00
5.31
4.17
5.33
3.44
5.70
3.96
the formula ORE
5.40
5.52
6.14
5.51
5.74
6.66
5.34
5.85
6.70
5.16
= -Log
6.19
6.21
7.10
6.11
5.85
6.68
5.59
5.74
7.55
6.39
C-DRE \
•m)
6.11
6.04
6.38
6.40
4.14
6.66
5.80
6,28
6.54
5.68

7.80
7.52
7.34
7.30
6.98
7.41
7.49
7.35
7.43
7.44

                          ANALYSIS OF RESULTS - SFg

      To gain as much information about the behavior of the POHC/SFg OREs with
respect to the two variables,  a  regression  analysis  was performed for each data
set,  one  for  each  compound.    Table 2  lists the  results  of  the  regression
analysis, the model used and the correlation  coefficient.

      Figure 2  is a contour plot vrith  independent  variables,  temperature and
afterburner exit  oxygen concentration,  on  the Y  and X  axis  respectively.  The
SFg ORE  (expressed in the  number  of nines)  is  displayed as contours  of the
regression surface.  This  figure demonstrates why  it is  so  hard to  make solid
judgments about  the relationship between  ORE and  a single variable.   As the
figure  clearly illustrates, whether  ORE  goes up  or down with  increasing §2

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    SF6  ORE  VS  T,  O2
1400
T

^1300H
P
E
R 1200
A
T
U 1100-
R
E
  1000 H
 900
         ^
        I   I   i  I   I   I  I   I   I
     0123456789  10

           O2 CONCENTRATION
       •  3-9's

       D  6-9's
   ORE

+ 4-9's

x 7-9'8
                      * 5-9's
           Figure 2. SF6 ORE vs. T,

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depends on the operating temperature.  At 950°C, ORE increases from about
3-nines to  nearly  4-nines as  oxygen increases.   At  1350°C, the  same  change
results in the opposite effect, dropping the  ORE  from  greater than 7-nines to
les§ than 5-nines ORE as oxygen increases.

                            Table  2.  Data Table
                                                        Correlation
                  Compound	Model	Coefficient
                  SFg                 1st Order           0.77
                  Toluene             1st Order           0.45
                  Tetrachloroethylene 1st Order           0.75
                  Chlorobenzene       2nd Order           0.76
                  Pentachlorobenzene  2nd Order           0.68
      At  this  point,  it  is  stressed that  the regression  analysis and  the
resulting  figures  developed  from  it should  only be  used  in  general,  not
predicting absolute DRE figures for specific compounds.  Until additional data
and developed,  these  relationships should only be applied to the CRF incinerator
and can only be used  to describe  the  relationship  between dependent  (DRE)  and
independent  (Temp,  and  02)  variables  within  the range  of the  experiment.
Extrapolation of the results outside the range is risky.

      In  the laboratory work  done on the thermal  decomposition  of SFg  at  the
University of Dayton Research Institute (UDRI) (7), it was determined that  SFg
destruction was independent of  oxygen concentration,  indicating  the  mechanism
to be unimolecular decomposition.   Although  Figure 2  shows  an effect of $% on
SFg DRE,  it may not mean that  02 specific!ally  causes  the changes.  What is  not
depicted  is  that  as  the  D£ concentration increases,  air to fuel ratios  and
incinerator residence times change concurrently.  The variation in SFg DRE  may

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be related to those effects and  is  not  necessarily  inconsistent  with the UDRI
results.
      Figure 3 is a plot  of  the SFg DREs versus temperature with 3  data sets
Illustrated.   The  data   shown  as  diamonds  were  the  SFg  DRE-temperature
relationship calculated from the data supplied  in References 5 and 7.  This was
calculated for a  2-second residence time and  represented  the  ORE  temperature
relationship for  SFg exclusive of any other physical or chemical  effects.

     The data plotted  as  Xs  were data from the work conducted at the Alberta
Environmental Centre (5)  in which the effect of  the presence  of  refractory on
SFg ORE was  evaluated.  As one can see, the presence of refractory  in the reactor
had a marked effect on the DRE-temperature relationship, reducing the required
temperature by some 200°C.

      The third data set  plotted in Figure 3 was the CRF  data,  and  shows the
regression line for those data points.  Here, as with the Canadian data, there
is a  marked difference in SFg DRE-temperature behavior.   While some  of the
difference could  be  attributed to the presence  of refractory and residence time
changes in the incinerator, the authors feel that there  is more to it than that.
Since the laboratory data  (UDRI)  were taken with non-flame systems, in which the
substances underwent an extremely narrow temperature distribution,  SFg  ORE should
not be  expected  to  be  similar, since in flame conditions, SFg would "see" or
experience a wide range of temperatures  in  the  incinerator environment.  At any
rate, the behavior is  not the same,  and more investigation is  warranted.

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8
7
6
5
4
3
  SF6 THERMAL DECOMPOSITION
      PILOT/LAB COMPARISON
 ORE (-LOG(1-DRE/100))
                    D
D
                      D
800    900   1000   1100   1200   1300
          TEMPERATURE, DEG C
                          1400
     REF 5
     CRF REGRESSION
          -&- REF 6 and 7
          °  CRF DATA
     Figure 3. SF6 Thermal decomposition pilot/lab caparison.
                   10

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                                 POHC RANKING

     Figure 4 is  a contour plot of the relationship between conditions necessary
to achieve 6-nines SFfi ORE and that of the individual POHCs.   It also illustrates
why  looking  at  one variable  at   a  time  can  be  confusing.    At  low  02
concentrations, tetrachloroethylene requires only 900°C for 6-nines while at 4.5%
02, 1250°C is required, surpassing that for chlorobenzene, which was more stable
at the lower 02 concentrations.  Pentachlorobenzene DREs were never below
6-nines and therefore are not plotted.

      Ranking  the POHCs  is shown  in Figure  4.   This  figure  illustrates that
rankings  can  change, depending on  combustion  conditions.   This  is  also true
depending on the nature of the experimental device.

      Table 3 is a  list of  rankings  of POHCs derived from Figure 4  and from data
supplied by  UDRI  in  Reference 9.    Although  not  definitive,  the  research into
POHCs and POHC rankings have produced results which seem to make surrogate use
even more questionable than when it  was first suggested.

                       Table 3.  POHC Ranking With 02 Present3
                                                  LIS Incineration
                                 UDRI     Low 02  (1.5%)      High 02 (5%)
Tetrach 1 oroethy 1 ene
Toluene
Pentachlorobenzene
Chlorobenzene
1
2
5
3
4
1
4
2
5
3
2
3
1
5
4
            al being most stable; 5 being least stable.
                                        11

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                                 POHC RANKING

     Figure 4 is  a contour plot of the relationship between conditions necessary
to achieve 6-nines SFg ORE and that of the individual POHCs.   It  also illustrates
why  looking  at  one  variable   at   a  time  can  be  confusing.    At   low  02
concentrations, tetrachloroethylene requires only 900°C for 6-nines while at 4.5%
02, 1250°C is required, surpassing that for chlorobenzene, which was more stable
at the lower 02 concentrations.   Pentachlorobenzene DREs were never below
6-nines and therefore are not plotted.

      Ranking  the POHCs  is shown  in Figure  4.   This  figure illustrates that
rankings  can  change, depending   on  combustion  conditions.    This  is  also true
depending on the nature of the experimental device.

      Table 3 is  a list of rankings of POHCs derived from Figure 4  and from data
supplied by  UDRI in  Reference 8.  Although not  definitive,  the  research into
POHCs and POHC rankings have  produced results which seem to make  surrogate use
even more questionable than when it  was first suggested.

                       Table  3.   POHC Ranking With 02 Present3
                                                 US Incineration
                                 UDRI     Low 02  (1.5%)      High 02 (5%)
Tetrachloroethylene
Toluene
Pentachlorobenzene
Chlorobenzene
1
2
5
3
4
1
4
2
5
3
2
3
1
5
4
            al being most stable; 5 being least stable.
                                        12

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RELATIVE POHC STABILITY
SF6
 6-9'S POHC DRE
+ TCE  * TOL

T
E
M
P
E
R
A
T
U
R
E

C

1,**UU

1,300-


1,200-

1,100-

1,000-

900-

onn -
#
*.-•'
..**
. • *
.•••''!**
» \Lf f^ ^^
•' ** i.-f
^#*** . ++
\L>H|u^ J»
^pr^ 4-

+
++
+
oi
4-+ °D°°°0D
+. '-'DDDDODDDDODDDDD^'


    1   23456789  10
       O2 CONCENTRATION
                        CLBZ
       Figure 4. Relative POHC stability.
             13

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                            CONCLUSIONS
o     SFg is a  limited surrogate.  Data showing reactivity with refractory
      and difficulty with using it may have reduced its apparent value
o     POHC ranking is not absolute and depends on combustion conditions
o     Toluene is the most stable of the organics at elevated temperature
      and 02 levels, while SFg  is  most stable  at intermediate and lower
      levels.

                          RECOMMENDATIONS
o     Modify the use of surrogates for trial burns, and specify
      minimum combustion conditions
o     Choose a minimum number of POHCs for trial burns
o     Use the most stable POHCs at low oxygen values, since that condition
      i.s present in most incinerator failures
o     Develop method  for  continuous monitoring  of toluene  and benzene,
      for performance monitoring.
                                  14

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                                  REFERENCES

1.    Oppelt, E.T.   Incineration of Hazardous Waste -  A Critical Review.  JAPCA.
      37:  558, 1987.

2.    40 CFR Part 264.343.

3.    Tsang, W.M. and Shaub, W.M.  Surrogates as  Substitutes  for  Principal
      Organic Hazardous Constituent Validation of  Incinerator Operation.   In:
      Proceedings of the Second Conference on Municipal,  Hazardous  and  CoaT~
      Wastes, Miami, FL 1983.  p. 241.

4.    England, W.G., Rappolt, T.J., Teuscher, L.H., Kerrin, S.L. and Mournighan,
      R.E.  Measurement of Hazardous Waste Incineration Destruction and Removal
      Efficiencies Using  Sulfur  Hexafluoride  as  a Chemical  Surrogate.   In:
      Proceedings of the 79th Annual  APCA Meeting, 1986.   106:162097W.

5.    Pandompatam, B., Liem, A.J., Frenette, R. and  Wilson, M.A.   Effect  of
      Refractory on the Thermal Stability of SF6.   JAPCA.   39:   310, 1989.

6.    Dellinger, B.  Testing and Evaluation of a  POHC/PIC  Incinerability
      Mixture.  U.S.  EPA 15th Annual Research Symposium, Cincinnati, Ohio, April
      April 10-12, 1989.

7.    Taylor, P.H. and Chadbourne, J.  Sulfur Hexafluoride  as a Surrogate.
      JAPCA.  37:  729 1987.

8.    40 CFR 761.70a.

9.    Waterland, I.E. and Staley, L.J.   Pilot Scale  Listing of  SFr  As A
      Hazardous Waste Incinerator Surrogate.  To be  Presented at  the  82nd
      National Meeting of the Air and  Waste Management Association, Dallas, TX,
      1989.  Paper 89-23B.4.
                                        15

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