-------
i' '""nil, ' Eh., Cilinfil'f, ITU!
The thermal oxidizer is provided with special burners and burner
guns. Each burner is a combination fuel-waste liquid unit. The
absorber vent stream is introduced separately into the top of the
burner vestibule. The flows of all waste streams are metered and !
sufficient air is added for complete combustion. Supplemental natural
gas is used to maintain the operating temperature required to combust
the organics and to maintain a stable flame on the burners during
rainiraum gas usage. Figure D-5 gives a plan view of the incinerator.
2. Sampling and Analytical Techniques, the vapor feed streams
(absorber vent) to the thermal oxidizer and the effluent gas stream
were sampled and analyzed using a modified analytical reactor recovery
run method. The primary recovery run methods are Sohio Analytical
Laboratory procedures.
The modified method involved passing a measured amount of sample i
gas through three scrubber flasks containing water and catching the
scrubbed gas in a gas sampling bomb. The samples were then analyzed
with a gas chromatograph and the weight percent of the components was
i' ". , . . ...... , , ' ", ., :|: ; ''I 1v ,'„> :',, ': „ < ' ; I
determined.
, " . '.!'" •' h i ; ',:»!' -i"'" •. ' 1
Figure D-6 shows the apparatus and configuration used to sample
the stack gas. It consisted of a sampling line from the sample valve!
to the small water-cooled heat exchanger. The exchanger was then
connected to a 250 ml sample bomb used to collect the unscrubbed
..... r • ' f t ' : "'I- 1" : ' ;• "• , ....... |
sample. The bomb was then connected to .a pair of 250 ml bubblers,
each with 165 ml of water in it. The scrubbers, in turn, were connecied
to another 250 ml sample bomb used to collect the scrubbed gas sample
which is connected to a portable compressor. The compressor discharge
then was connected to a wet test meter that vents to the atmosphere.
After assembling the apparatus, the compressor was turned on
drawing the gas from the stack and through the system at a rate of
about 90 cm3/s ( 0.2 ft3/min). Sample gas was drawn until at least
0.28 m3 (10 ft3) passed through the scrubbers. After the 0.28 m
(10 ft3) was scrubbed, the compressor was shutdown and the unscrubbed:
bomb was analyzed for CH4, C2's,
and C3Hg, the scrubbed bomb was
analyzed for N£, air, 02, C02> and CO, and the bubbler liquid was !
analyzed for acrylonitrile, acetonitrile, hydrogen cyanide, and total
D-32
-------
organic carbon. The gaseous samples were analyzed by gas
chromatography.
3. Test Results. The Monsanto Chemical Intermediate Company
conducted emissions testing at its Alvin (Chocolate Bayou), Texas,
acrylonitrile production facility during December 1977. The VOC
destination efficiency reported was 99 percent. (Residence time
information was not available and the temperature of the incinerator
is considered confidential information by Monsanto.)
D.2.4 Union Carbide Lab-Scale Test Data12
Union Carbide test data show the combustion efficiencies achieved
on 15 organic compounds in a lab-scale incinerator operating between
430° and 830°C (800° and 1500°F) and 0.1 to 2 seconds residence time.
The incinerator consisted of a 130 cm, thin bore tube, in a bench-size
tube furnace. Outlet analyzers were done by direct routing of the
incinerator outlet to a FID and GC. All inlet gases were set at
1000 ppmv.
In order to study the impact of incinerator variables on efficiency,
mixing must first be separated from the other parameters. Mixing
cannot be measured and, thus, its impact on efficiency cannot be
readily separated when studying the impact of other variables. The
Union Carbide lab work was chosen since its small size and careful
design best assured consistent and proper mixing.
The results of this study are shown in Table D-7. These results
show moderate increases in efficiency with temperature, residence
time, and type of compound. The results also show the impact of flow
regime on efficiency.
Flow regime is important in interpreting the Union Carbide lab
unit results. These results are significant since the lab unit was
designed for optimum mixing and, thus, the results represent the upper
limit of incinerator efficiency. As seen in Table D-7, the Union
Carbide results vary by flow regime. Though some large-scale incinerators
may achieve good mixing and plug flow, the worst cases will likely
require flow patterns similar to complete backmixing. Thus, the
results of complete backmixing would be relatively more comparable to
those obtained from large-scale units.
D-33
-------
Table D-7. DESTRUCTION EFFICIENCY UNDER STAYED CONDITIONS
BASED ON RESULTS OF UNION CARBIDE LABORATORY TESTSa
',(!.,':„ i II .";;i'":,f,::Ti'«
Destruction Efficiency of Compound in Percent
at Residence Time
0.75 second
Flow b
Regime
Two-stage
Backmixing
Complete
Backmixing
Plug Flow
Temperature
1300
1400
1500
1600
1300
1400
1500
1600
1300
1400
1500
1600
Ethyl
Aery late
99.9
99.9
99.9
99.9 .
98.9
99.7
99.9
99.9
99.9
99.9
99.9
99.9
Ethanol
94.6
99.6
99.9
99.9
86.8
96.8
99.0
99.7
99.9
99.9
99.9
99.9
;• • 1 , ,i'L IJ'I ;,;, [
Ethyl ene
92.6
99.3
". 99.9
99.9
84.4
95.6
98.7
99.6
99.5
99.9
99.9
99.9
Vinyl
Chloride
78.6
99.0
99.9
99.9
69.9
93.1
98.4
99.6
90.2
99.9
99.9
99.9
0.5/1.5 sec
Ethyl ene
87.2/97.6
98.6/99.8
99.9/99.9
99.9/99.9
78.2/91.5
;93.7/97.8
98.0/99.0
;99.4/99.8
97.3/99.9
99.9/99.9
^ 99. 9/99. 9
99.9/99.9
aThe results of the Union Carbide work are presented as a series of equations. These
equations relate destruction efficiency to temperature, residence time, and flow
regime for each of 15 compounds. The efficiencies in this table were calculated
from these equations.
bThree flow regimes are presented: two-stage backmixing, complete backmixing, and
plug flow. Two-stage backmixing is considered a reasonable approximation of actual
field units, with complete backmixing and plug flow representing the extremes.
D-34
-------
D.3 VAPOR RECOVERY SYSTEM VOC EMISSION TEST DATA13
On July 14, 1980, Mobil Company collected samples of hydrocarbon
emissions from the exhaust vent of the Vapor Recovery/Knockdown System
at its Santa Ana, California polystyrene plant. The samples were
taken using a MDA-808 Accuhaler^ pump while velocity was determined
using a Kurz^ Model 441 air velocity meter. Samples were taken while
the plant was in normal operation. One set of samples was taken while
a vacuum was drawn on dissolver tanks. Another set of samples was
taken while a vacuum was drawn on the flash tank. Both sets of samples
were analyzed for styrene and ethyl benzene by an independnet laboratory.
Computations for emission rates were made based on velocity, sample
volume and sample time. The test results, submitted by the company,
indicate that 0.942 kg/day of ethyl benzene and 10.018 kg/day of styrene
are emitted from the exhaust vent of the vapor recovery/knockdown
system. No more information was provided regarding the sampling and
analysis procedure used by Mobil or the laboratory. It is assumed
that standard industrial practices were used, thus generating valid
estimates of emissions. However, the data should not be used as a
significant basis for emission limitation.
D.4 DISCUSSION OF TEST RESULTS AND THE TECHNICAL BASIS OF THE POLYMERS
AND RESINS VOC EMISSIONS REDUCTION REQUIREMENT
This section discusses test results as well as available theoretical
data and findings on flare and incinerator efficiencies, and presents
the logic and the technical basis behind the choice of the selected
control level.
D.4.1 Discussion of Flare Emission Test Results
The results of the five flare efficiency studies summarized in
Section 3.1.1.1 showed a 98 percent VOC destruction efficiency
except in a few tests with excessive stream, smoking, or sampling
problems. The results of the Joint CMA-EPA study, summarized in
Table D-2,. confirmed that 98 percent VOC destruction efficiency was
achievable for all tests (including when smoking occurred) except when
steam quenching occurred within the range of flare gas velocities and
heating values tested. Flare gas velocities for the tests reported
to date go up to a high of 18.2 m/s (60 fps) and lower heating values
go as low as 11.2 MJ/m3 (300 Btu/scf). Additional testing is currently
D-35
-------
being undertaken to determine the effect of higher velocities, in
particular, on destruction efficiencies.
D.4.2 Discussion of Thermal Incineration Test Results |
Both the theoretical and experimental data concerning combustion
efficiency of thermal incinerators are discussedin this section. A
theoretical consideration of VOC combustion kinetics leads to the
conclusion that at 870°C (1600°F) and 0.75 secondresidence time,
mixing is the crucial design parameter.14 Published literature indicates
that any VOC can be oxidized to carbon dioxide and water if held at
sufficiently high temperatures in the presence of oxygen for a sufficient
time. However, the temperature at which a given level of VOC reduction
is achieved is unique for each VOC compound. Kinetic studies indicate
that there are two rate-determining (i.e., critically slow) steps in
the oxidation of a compound. The first slow stepof the overall
oxidation reaction is the initial reaction in which the original
compound disappears. The initial reaction of methane (CHzj.) has been
determined to be slower than that of any other nonhalogenated organic
compound. Kinetic calculations show that, at 870°C (1600°F), 98
percent of the original methane will react in 0.3 seconds. Therefore,
any nonhalogenated VOC will undergo an initial reaction stepwithin
this time. After the initial step, extremely rapid free radical
reactions occur until each carbon atom exists as carbon monoxide (CO)
immediately before oxidation is complete. The oxidation of CO is the
' second slow step. Calculations showthat, at 87(5°C (16006F), 98
percent of an original concentration of CO will react in 0.05second.
Therefore, 98 percent of any VOC'would be expected to undergo the !
initial and final slow reaction steps at 870°C(1600°F) in about 0.35
second. It is very unlikely that the intermediatefreeradical reactions
would take nearly as long as 0.4 seconds to convert 98 percent of the
organic molecules to CO. Therefore, from a theoretical viewpoint, any
VOC should undergo complete combustion at 870°C (1600°F) in 0.75
second. The calculations on which this conclusion is! baseci have taken
into account the low mole fractions of VOC and oxygen which would be
found in the actual system. They have also provided for the great
decrease in concentration per unit volume due to the elevated temperature.
D-36
-------
However, the calculations assume perfect mixing of the offgas and
combustion air. Mixing has been identified as the crucial design
parameter from a theoretical viewpoint.
The test results both indicate an achievable control level of
98 percent at or below 870°C (1600°F) and illustrate the importance of
mixing. Union Carbide results on lab-scale incinerators indicated a
minimum of 98.6 percent efficiency at 760°C (1400°F). Since lab-scale
incinerators primarily differ from field units in their excellent
mixing, these results verify the theoretical calculations and suggest
that a full-size field unit can maintain similar efficiencies if
designed to provide good mixing. The tests cited in Table D-6 are
documented as being conducted on full-scale incinerators controlling
offgas from air oxidation process vents of a variety of types of
plants. To focus on mixing, industrial units were selected where all
variables except mixing were held constant or accounted for in other
ways. It was then assumed any changes in efficiency would be due to
changes in mixing.
The case most directly showing the effect of mixing is that of
Petro-Tex incinerator. The Petro-Tex data show the efficiency changes
due to modifications on the incinerator at two times after startup.
These modifications (see Section D.2.3.1, 3. Test Results) increased
efficiency from 70 percent to over 99 percent, with no significant
change in temperature.
A comparison of the Rohm and Haas test versus the Union Carbide
lab test, as presented in Table D-8, indirectly shows the effect of
mixing. The UCC lab unit clearly outperforms the R&H unit. The data
from both units are based on the same temperature, residence time, and
inlet stream conditions. The more complete mixing of the lab unit is
judged the cause of the differing efficiencies.
The six tests of in-place incinerators do not, of course, cover
every feedstock. However, the theoretical discussion given above
indicates that any VOC compound should be sufficiently destroyed at
870°C (1600°F). More critical than the type of VOC is the VOC
concentration in the offgas. This is true because the kinetics of
combustion are not first-order at low VOC concentrations. The Petro-Tex
D-37
-------
Table D-8. COMPARISONS OF EMISSION TEST RESULTS FOR UNION CARBIDE
LAB INCINERATOR AND ROHM & HAAS FIELD INCINERATORS
Compound
Rohm and Haas Incinerator
Inlet Outlet
(Ibs/hr) (Ibs/hr)
Union Carbide Lab Incinerator
Inlet Outlet
(Ibs/hr)
(Ibs/hr)
Propane
Propylene
Ethane
Ethvlene
IM V 1 1 J 1 \* 1 I V*
TOTAL
900
'l800b
10
30
2740
150
15'ob
;
375
190
865
'•i' •;'.; >•*,•'•? iv .:
71.4
142.9
,„ :,,,, :h ,'' i,! ,, ,1; i1'. ,, i •, ,
0.8
2.4
217.5
1 'i, :»; fly, ,',;"
0.64
5.6
""'3.9"""
3.4
13.54 '
Overall VOC
Destruction
Efficiency:
68.4%
93.!
aTable shows the destruction efficiency of the four listed compounds for the
Rohm & Haas (R&H) field and Union Carbide (UC) lab incinerators. The R&H
results are measured; the UC results are calculated. Both sets of results
are based on 1425°F combustion temperature and one second residence time.
In addition, the UC results are based on complete backmixing and a four-step
combustion sequence consisting of propane to propylene to ethane to ethylene
to C02 and HgO. These last two items are worst case assumptions.
bAre not actual values. Actual values are confidential. Calculations with
actual values give similar results for overall VOC destruction efficiency.
D-38
;„;„;,! ijia!":• SMsmha •. I •'•iAji^i.i.'iiki •;<
-------
results are for a butadiene plant, and butadiene offgas tends to be
lean in VOC. Therefore, the test results support the achievability of
98 percent VOC destruction efficiency by a field incinerator designed
to provide good mixing, even for streams with low VOC concentrations.
The EPA tests at Union Carbide and Rohm and Haas were for residence
times greater than 0.75 second. However, theoretical Calculations
show that greater efficiency would be achieved at 870°C (1600°F) and
0.75 second than at the longer residence times but lower temperatures
represented in these two tests. The data on which the achieveability
of the 98 percent VOC destruction efficiency is based is test data for
similar control systems: thermal incineration at various residence
times and temperatures. If 98 percent VOC reduction can be achieved
at a lower temperature, then according to kinetic theory it can certainly
be achieved at 870°C (1600°F), other conditions being equal.
A control efficiency of 98 percent VOC reduction, or 20 ppm by
compound, whichever is less stringent, has been considered to be the
acheivable control level for all new incinerators, considering available
technology, cost and energy use.*4 This is based on incinerator operation
at 870°C (1600°F) and on adjustment of the incinerator after start-up.
The 20 ppm (by compound) level was chosen after three different incinerator
outlet VOC concentrations, 10 ppm, 20 ppm, and 30 ppm, were analyzed.
In addition to the incinerator tests cited earlier in this Appendix,
data from over 200 tests by Los Angeles County (L.A.) on various waste
gas incinerators were considered in choosing the 20 ppm level. However,
the usefulness of the L.A. data was limited by three factors: (1) the
incinerators tested are small units designed over a decade ago; (2) the
units were designed, primarily, for use on coating operations; and
(3) the units were designed to meet a regulation requiring only 90 percent
VOC reduction.
The 10 ppmv level was judged to be too stringent. Two of the six
non L.A. tests and 65 percent of the L.A. tests fail this criteria.
Consideration was given to the fact that many of the units tested were
below 870°C (1600°F) and did not have good mixing. However, due to
the large percent that failed, it is judged that even with higher
temperatures and moderate adjustment, a large number of units would
still not meet the 10 ppmv level.
D-39
-------
The 20 ppm level was judged to be attainable. All of the non L.A,
and the majority of the L.A. units met this criteria, there was
concern over the, large number of L.A. tests that failed, i.e. 43 percent.
However, two factors outweighed this concern.
First, all of the non L.A. units met the criteria. This is
significant since, though the L.A. units represent many tests, they
represent the same basic design. They all are small units designed
over a decade ago to meet a rule for 90 percent reduction. They are
for similar applications for the same geographic region designed in
many cases by the same vendor. Thus, though many failed, they likely
did so due to common factors and do not represent a widespread inability
to meet 20 ppm.
Second, the difference between 65 percent failing 10 ppmv and
43 percent failing 20 ppm is larger than a direct comparison of the
percentages would reveal. At 20 ppm, not only did fewer units fail,
but those that did miss the criteria did so by a smaller margin and •
would require less adjustment. Dropping the criteria from 10 ppm to
20 ppm drops the failure rate by 20 percent, but is judged to drop the
overall time and cost for adjustment by over 50 percent.
The difference between the two levels is even greater when the
adjustment effort for the worst case is considered. The crucial point
is how close a 10 ppm level pushes actual field unit efficiencies to
those of the lab unit. Lab unit results for complete backmixing !
indicate that a 10 ppm level would force field units to almost match
lab unit mixing. A less stringent 20 ppm level increases the margin
allowed for nonideal incinerator operation, especially 'for the worst
cases. Given that an exponential increase may occur in costs to ;
improve mixing enough for field units to approach lab unit efficiencies,
a drop from 10 ppm to 20 ppm may decrease costs to improve mixing in
the worst case by an order of magnitude.
The 30 ppm level was judged too lenient. The only data indicating
such a low efficiency was from L.A. All other data showed 20 ppm. •
The non-L.A. data and lab data meet 20 ppm and the Petro-tex experience
showed that moderate adjustment can increase efficiency. In addition,
the L.A. units were judged to have poor mixing. The mixing deficiencies
D-40
fci I
-------
were large enough to mask the effect of increasing temperature. Thus,
it is judged that 20 ppm could be reached with moderate adjustment and
that a 30 ppm level would represent a criteria not based on the best
available control technology cost, energy, and environmental impact.
D-41
-------
D.5 REFERENCES FOR APPENDIX D
1. McDaniel, M. Flare Efficiency Study, Volume I. Engineering-Science.
Austin, Texas. Prepared for Chemical Manufacturers Association,
Washington, D.C. Draft 2, January 1983.
2 Lee, K.W. et al., Polymers and Resins Volatile Organic Compound
Emissions from Incineration: Emission Test Report, ARCO Chemical
Company, LaPorte Plant, Deer Park, Texas, Volume I Summary of
Results. U.S. Environmental Protection Agency, Research Triangle
Park, North Carolina. EMB Report No. 81-PMR-l. March 1982.
"• • i
3. SRI International, 1982 Directory of Chemical Producers.
4 Maxwell, W. and G. Scheil. Stationary Source Testing of a Maleic
Anhydride Plant at the Denka Chemical Corporation, Houston,
Texas. U.S. Environmental Protection Agency,, Research Triangle
Park, North Carolina. Contract No. 68-02-32814, March 1978.
, i
5 Blackburn, J. Emission Control Options for the Synthetic Organic
Chemicals Manufacturing Industry, Trip Report. U.S. Environmental
Protection Agency, Research Triangle Park, North Carolina. EPA
Contract No.
68-02-2577, November 1977.
6 Scheil G. Emission Control Options for the Synthetic Organic [
Chemicals Manufacturing Industry, Trip Report. U.S. Environmental
Protection Agency, Research Triangle Park, North Carolina.
Contract No. :
68-02-2577, November 1977.
7. Letter from Lawrence, A., Koppers Company, Inc., to Goodwin, D.
EPA. January 17, 1979.
8 Air Oxidation Processes in Synthetic Organic Chemical Manufacturing
Industry-Background Information for Proposed Standard Preliminary
Draft EIS. U.S. Environmental Protection Agency. Research
Triangle Park, North Carolina. August 1981. p. C-7 and C-8.
9. Letter from Towe, R., Petro-Tex Chemical Corporation, to Farmer, J.,
EPA. August 15, 1979. ;
10 Broz, L.D. and R.D. Pruessner. Hydrocarbon Emission Reduction j
Systems Utilized by Petro-Tex. Presented at 83rd National Meeting
of AIChE, 9th Petrochemical and Refining Exposition, Houston,
Texas, March 1977.)
11. Letter from Weishaar, M., Monsanto Chemical Intermediates Co., to
Farmer, J., EPA, November 8, 1979.
12 Lee, K., J. Hansen and D. Macauley. Thermal Oxidation Kinetics
of Selected Organic Compounds. (Presented at the 71st Annual
Meeting of the APCA, Houston, Texas, June 1978.)
D-42
-------
13. Letter and attachments from Bowman, V.A. Jr., Mobil Chemical
Company, to Farmer, J.R., EPA. September 9, 1980. p. 13-16.
Response to Section 114 letter on polystyrene manufacturing
plants.
14. Memorandum from Mascone, D.C., EPA. June 11, 1980. Incinerator
efficiency.
D-43
-------
-------
APPENDIX E: DETAILED DESIGN AND COST ESTIMATION PROCEDURES
E-l
-------
I'«:'ii'VV 'i1:"'-:!'/!
APPENDIX E: DETAILED DESIGN AND COST ESTIMATION PROCEDURES
E.I GENERAL ;
This appendix consists of a more detailed presentation of the
bases, assumptions, and procedures used to estimate"equipment designs
and corresponding capital and operating costs forflares, thermal
incinerators, catalytic incinerators, shell-and-tube condensers, and
piping and ducting. The basis of design and cost estimates are presented
In the following sections: E.2, flares; E.3, thermal incinerators;
E.4, catalytic incinerators; E.5 shell-and-tube condensers; and E.6,
piping and ducting. The installation cost factors used in each analysis
and the annualized cost factors used in all of the cost analysis are :
given in Tables 5-2 and 5-3, respectively.
E.2 FLARE DESIGN AND COST ESTIMATION PROCEDURE <
Flares are open combustion devices that can be used to effectively
and inexpensively reduce VOC emissions. The polypropylene and polyethylene
industries commonly use flares to control large emergency releases arid
some high VOC streams. Elevated flares were costed based upon 60 fps
exit velocity and a minimum of 300 Btu/scf. Flare height and diameter,
which are the primary determinants of capital cost, are dependent on'
flare flow rate, heating value, and temperature. Associated piping and
ducting from the process sources to a header and from a header to the
flare were conservatively designed for costing purposes. Operating :
costs for utilities were based on industry practice (1 fps purge of ,
waste gas plus natural gas for continuous flow flare"; 80 scfh natural
gas per pilot, number of pilots based on flare tip diameter; 0.4 Ib .
steam/1b hydrocarbon at maximum smokeless rate).
E.e.l Flare Design Procedure. Design of flare systems for the
various combinations of waste streams was basedonstandard flare
design equations for diameter and height presented by IT Enviroscience.1
These equations were simplified to functions of the following waste 'gas
E-2
•y',.:,,ijtti:r:, u ,•'&'<'*,'.'iv.'iaswi. -i i i" M
-------
characteristics; volumetric flow rate, lower heating value, temperature,
and molecular weight. The diameter expression is based on the equation
of flow rate with velocity times cross-sectional area. A minimum
commercially available diameter of 2 inches was assumed. The height
correlation premise is design of a flare that will not generate a
lethal radiative heat level (1500 Btu/ft2 hr, including solar radiation2)
at the base of the flare (considering the effect of wind). Heights in
5-foot multiples with a minimum of 30 ft. were used.3 Natural gas to
increase the heating value to 115 Btu/scf is considered necessary by
vendors to ensure combustion of streams containing no sulfur or toxic
materials.4 A minimum lower heating value of 300 Btu/scf has been
shown to help ensure a 98 percent efficiency for steam-assisted flares.
For flares with diameters of 24-inches or less, this natural gas was
assumed to be premixed with the waste gas and to exit out the stack.
For larger flares, a gas ring was assumed if large amounts of gas were
required because separate piping to a ring injecting natural gas into
the existing waste gas is more economical than increasing the flare
stack size for large diameters. The flare height and diameter selection
procedure is detailed in Table E-l.
Natural gas was assumed at a rate of 80 scfh per pilot flame
to ensure ignition and combustion. The number of pilots was based on
diameter according to available commercial equipment.5 Purge gas also
may be required to prevent air intrusion and flashback. A purge velocity
requirement of 1 fps was assumed during periods of continuous flow for
'standard systems without seals.6
Steam was added to produce smokeless combustion through a combined
mixing and quenching effect. A steam ring at the flare tip was used
to add steam at a rate of 0.4 Ib steam/1b of hydrocarbons (VOC plus
methane and ethane) in the continuous stream.'' Availability and
deliverability of this quantity of steam was assumed.
Piping (for flows less than 700 scfm) or ducting (for flows equal
to or greater than 700 scfm) was designed from the process sources to
a header combining the streams and from the header to the base of the
flare. Since it is usual industry practice, adequate pressure (approximately
3 to 4 psig) was assumed available to transport all waste gas streams
without use of a compressor or fan. The source legs from the various
E-3
-------
Table E-1. PROCEDURE TO DESIGN 98 PERCENT EFFICIENT (60 fps, 300 Btu/scfJ
ELEVATED STEAM-ASSISTED SMOKELESS FLARES
Itm
Value
I. Haste gas flow rate, Qwg (scfm)a
Z, Lower heating value of waste gas, LHVwg (Btu/scf)
3. Teaperature of waste gas, Twg (°F)
4. Holecular weight of waste gas, MWW<
5. Ueight percent of hydrocarbons, wt. % HC
6. Auxiliary natural gas flow rate, Qng (scfm)b
7. Total flare gas flow rate, Qfl_g (scfm)
8. Lower heating value of flare gas, LHVfl>g (Btu/scf)
9. Teaperature of flare gas, Tfl (°F)C
10. Holecular weight of flare gas, MWfl (Ib/lb-mole)
II. Calculated flare diameter, D calc. (in.)
12. Selected flare diameter, D(in.)e
13. Flare tip pressure drop.Ap (in. H20)
1*. Actual exit velocity, Vg (fps)9
IS. Plane angle, 0h
16. Calculated flare height, Hcalc> (ft)1
17. Selected flare height, H (ft)
18. Safe pipeline length, L (ft)j
from Chapter 5
from Chapter 5
from Chapter 5
from Chapter 5
from Chapter 5
0, if LHV >300;
(300-LHV )0
".. • if LHVwn<30° Btu/scf
{555}
wg
^wg ng
300, if Qng > 0;
LHV if "ng - °
70, if Qng = OorTwg-70;
«wg x "V + (17'4 X V
"ng'
, if
(2.283 x 10"2) IQfl _g /MWf1 _g (Tfl
-------
1
LU
QJ
Ol
O
U
•o
TO
01
O)
S-
o
s_
01
0
"TO
L.
3
c
ra
X
-D
0)
CD C
4-> C
S "
J= E
!_ i.
c as
(J 1-
3 4->O
S- 01 O
4-> fl) O
01 4-> f— 1
QJ - —
"°£u.
4J TOO
c^-o
O)<*- r^
o
!_«: 4J
0) Q. re
Q.LU
CO «I O
01 E: 01
o — .
3 C CO
in o o
TO "-5 CO
Bai
J= <4-
4-> O
L. t|_ 01
re o TO
01 en
Ol Ol
QJ 4-> r—
O i — TO
O> 3 L.
C 01 3 0)
Q) 4-* O
a> i. TO c
3 CO
r— OJ r—
TO -C 4- TO
> 4-> O J3
g=
U
. . 01
u
Ol C
3 ^
CQ X
O
O
CO
X
.-^ it-
en u
S 01
o- ~-
3
CO
en — -
£=
cy en
>
u S
1
Ol 1
>S o
3= O
_J CO
I
X
en
It
— 1"
en i*-
C 0
*c
>
U -Q
3 CU
^ re
en x
>c £
nr a.
_1 Q.
~~~^ at
i.
3
4-3
X
-E
O
O}
S-
01
C£
01
CJ
c:
0)
o
01
o
£-
en 03 »P- c:
x c
en
s_
i
i—
0
cr
ID
o.
LU
g
U.
XI
JT1
en
^^
0
to
+
LL.
o
I1
1—
X
i-
^.
Ol
cy
x
CO
o
r-t
X
OJ
r-~
OJ
OJ
— > en
o c
CM re
3C
c re
O- i.
< t£
C
ro
3
CT
O
C
LD
tn
a.
M-
0)
(__i
LO
LO
II
^
^.
a.
en
c:
4_)
tn
O)
4-*
0)
J^
g
LU
g
4->
c
o
O)
4->
j=
4->
4J
_
O
U
o
re
.o
3
*
en
r-^
*gF
*^-
O*
IO
i1
J—
u
^•v^
•r—
0
to
X
"o
E
;£
""^
£^,
en
'5;
•Tg
X
c
'i
14-
o
in
en
o-
X
CO
I— 1
X
CM
r-*
(XI
1
CM
o
**
o
X
CO
CO
^.
^^"•^
X
Ol
"o
E
1
*-^
o
o
r^.
TO
CJ
Ol
1 —
CO
i i
u
c=
^,
a
.
fr
01
en
n.
-C
01
c
o
TO
*0>
jr
S
01
OJ
01
g"
u
tn
•*-
S- 4->
CO X
40 0)
0) C
TO 4->
•r- O
•O 0)
•a "o!
d> 01
TO «
r- O
3 Ol
U
15 -r-
o
41
01 a)
01 N
O) •<-
i — Ol
c
3 t-
0)
s- en
ai s-
4-> a
TO 4->
-O O>
c
S -o
TO TO
"5 L.
u oi
"TO I—
O TO
TO
J= 4->
4-> X
a>
Ci> d
M
in 0)
a;
TO a>
03 t— •
4J TO 0)
in > M
S-v-
t. QJ Ol
a> 4->
TO TO
o c
4-J TO
X *« 4->
a> o 01
C i-«
4J C O)
O -i-i—
a) j=t—
"a! -r- E
oo 3: ol
QJ
a)
>
5
TO
•o.
01
O
£
o
1=
E
0)
en
a
o
c:
0
4-9
TO
3
S"
ai
o
c
a>
u
01
o
•r—
cz
LU
E
j^
LU
it-
s'
O
to
Ol
S-
c
E
C3
to
'^-^
X
"aT
"o
Jit
^^,
en
^~
g
X
E
*l
u
(/} .
•^— '
en
cy
x
CO
o
X
CM
CVJ
C\J
X
^
01
"o
E
£
^^
o
o
1 —
TO
<4-
O
in
r-^.
CO
CO
t
II
O
,
c
CL
E-5
-------
a
o
o
in
tn
CM
*J «
10 O-—
4-> +•>
C "
STBu
•E = 5
-cU1""
s_ en
co c
.c tn T-
•=_; §
(O
O) CH-
O O I
E-6
; ;!; .j|;, ;.•„!' ..... ' ...... i ...... '1^2 ..... i ........
...... >A: ...j '.::J'i;& "i, ..... i'-l1:;?-':;:!! ..... .- , ..... J>' ...... J ....... : ..... liiit ...... W M ..... lay
-------
sources to the flare header were assumed to be 70 feet in length,8
while the length of pipelines to the flare was based on the horizontal
distance required to provide a tolerable and safe radiation level for
continuous working (440 Btu/hr-ft^, including solar radiation).5
Piping and ducting were selected and costed as outlined in Section E.6.
£.2.2 Flare Cost Estimation Procedure. Flare purchase costs
were based on costs for diameters from 2 to 24 inches and heights from
20 to 200 feet provided by National Air Oil Burner, Inc., (NAO) during
November 1982 and presented in Table E-2.5 A cost was also provided
for one additional case of 60 inch diameter and 40 feet height.1
These costs are October 1982 prices of self-supporting flares without
ladders and platforms for heights of 40 feet and less and of guyed
flares with ladders and platforms for heights of 50 feet and greater.
Flare purchase costs were estimated for the various regulatory alternatives
by either choosing the value provided for the required height and
diameter or using two correlations developed from the NAO data for
purchase cost as a function of height and diameter. (One correlation
for heights of 40 feet and less, i.e., self-supporting flares and one
for heights of 50 feet and greater, i.e., guyed flares.) Purchase
costs of large diameter, 40-ft. high flares were approximated using a
curve developed from the NAO data (see Figure E-l). Purchase costs for
fluidic seals were approximated using a curve based on data provided by NAO?
(see Figure E-2).
A retrofit installation factor of 2.65 (see Table 5-2) was used to
estimate installed flare costs. Installed costs were put on a June
1980 basis using the following Chemical Engineering Plant Cost Indices:
the overall index for flares; the pipes, valves, and fittings index for
piping; and the fabricated equipment index for ducting. Annualized
costs were calculated using the factors presented in Table 5-3. The
flare cost estimation procedure is presented in Table E-3.
E.3 THERMAL INCINERATOR DESIGN AND COST ESTIMATION PROCEDURE
Thermal incinerator designs for costing purposes were based on
heat and mass balances for combustion of the waste gas and any required
E-7
-------
rrt
O C/>
LU o:
S S
is
a.
CM
CO CO
LU cn
i — i—
•ice
i— i LU
|— CO
co o
LU H-
O
1—0
CO
O 21
<_> 1-1
LU «
0
O 4-*
I*5"
TJ
tn c
2 re
re in
I — S-
-a
en -a
'fj r~
O •!->
3
in V)
tn <4^
o "S
M- >>
0) cn
re i-
tn
-------
oo
o
o
CO
O
CJ
in
ea
90,000-i
80,000-
70,000-
60,000—
50,000-
40,000—
30..000-
20,000-
10,000-
10 20 30 40 50 60 70
Flare Tip Diameter (in.)
«•
Figure E-l. Estimated Flare Purchase Cost for 40 ft Height
E-9
-------
o
kO
4J
>
O
0)
+J
(O
O)
I/)
O
•r-
T3
Q
O.
CD
03
X
o
Q.
Q.
T
8
o
o
o
o
o
o
(286L '*><)) $ '
-------
auxiliary fuel, considering requirements of total combustion air.
Costs of associated piping, ducting, fans, and stacks were also estimated.
E.3.1 Thermal Incinerator Design Procedure
Designs of thermal incineration systems for the various combinations
of waste gas streams were developed using a procedure based on heat
and mass balances and the characteristics of the waste gas in conjunction
with some engineering design assumptions. In order to ensure a 98 percent
VOC destruction efficiency, thermal incinerators were designed to
maintain a 0.75 second residence time at 870°C (1600°F).9 The design
procedure is outlined in this section.
Streams with low heat contents, which require auxiliary fuel to
ensure combustion and sometimes require air dilution or fuel enrichment
to prevent an explosive hazard, are often able to utilize recovered
waste heat by preheating inlet air, fuel, and perhaps, waste gas. The
*• '•*•
design considerations for such streams are noted in the following
discussion, but the combustion calculations, etc. are not detailed
because all combined streams to thermal incinerators for polymers and
resins regulatory alternatives had sufficient waste gas heating values
to combust at 870°C (1600°F) without preheating the input streams.
Therefore, only the design procedure for high heat content streams,
independently able to sustain combustion at 870°C (1600°F), is detailed
in this section.
The first step in the design procedure was to calculate the
physical and chemical characteristics affecting combustion of the
waste gas stream from the model plant characteristics given in Chapter 2,
using Table E-4. In order to prevent an explosion hazard and satisfy
insurance requirements, dilution air was added to any individual or
combined waste stream with both a lower heating value between 13 and
50 Btu/scf at 0°C (32°F) (about 25 and 100 percent of the lower explosive
limit) and an oxygen concentration of 12 percent or greater by volume.
Dilution air was added to reduce,the lower heating value of the stream
to below 13 Btu/scf. (Adding dilution air is a more conservative
assumption than the alternative of adding natural gas and is probably
more realistic as other streams often have enough heat content to
sustain the combustion of the combined stream for the regulatory
alternative.)
E-ll
-------
Table E-3. CAPITAL AND ANNUAL OPERATING COST ESTIMATION PROCEDURE FOR
STEAM-ASSISTED SMOKELESS FLARES
Item
Value
Capital Costs
Flare purchase cost, C'"fi
(Oct. 1982 $)
Fluidic seal purchase cost, C'"fi.s,
(Oct. 1982 $)
Flare system purchase cost, C''fi
Select from Table E»2 if value given
or use equations:
(3905.7) + (35.054) H x D + (900.36) D.
- (126.08)D2, for 20 < H < 40 ft and D < 8 in.
(6275.6) + (224.10) H -f (12.782) H x D
+ (24.856)02, for 50 < H < 200 ft.
or from Figure E-2 if H = 40 ft and p > 8 in.
See footnote a.
C'"fl + C'"flc>s.
'.< . ,,!! , „'. II i|l;|..|r '"If '"P"' ',,11
Flare installed cost, C'fj
(Oct. 1982 $)
Total installed piping costs, C'p
(Aug. 1978 $)
Total installed ducting costs, C'
(Dec. 1977 $)
June 1980 Installed costs
Piping0, Cp
Ductingd, Cd
Flare6, Cf-| ^
Total flare system cost,
csys
C"fl x 2.65
Method of Appendix E.6
Method of Appendix E.6
C'p x 1.206
C'd x 1.288
C'
fl x 0.818
(Cp + Cd + Cfi)
;t JB;.. is .•;-)
E-12
ilf ', » |.J,:1! " J1. V .,"•!":
; iii»^^^^^^ !
-------
Table E-3. CAPITAL AND ANNUAL OPERATING COST ESTIMATION PROCEDURE FOR
STEAM-ASSISTED SMOKELESS FLARES (Concluded)
Item
Value
Annualized Costs^
Operating labor,
Maintenance, Cm
Utilities
scfh
scfh
Cost natural gas, Cn n 1
1 1 • y •
Cost steam,
Taxes, admin. & insurance, Ctax
Capital recovery, Ccr
Total annualized,
620 hr/yr x $18/hr = $11,160
0.05 x Csys
80 scfh, for 2 < D < 8;
160 scfh, for 10 < D < 20;
240 scfh, for D = 24;
320 scfh, for D = 60.
C(0.3272)(D in)2 -
scfm
cont] x 60
E
aux-
scfh
53.45 C(Qn.g., pilot +
(qscfh) purge)]
n.g.
3.296[QW _ (scfm) x MW x wt. % HC] cont,
'y* 100% fl.g.
Cqv«; X 0.04
0.1315 Cfi + 0.1627 (Cp +
CT + Cm + Cn.g. -t- Cstm + Ccr + Ctax
E-13
-------
Footnotes for Table E-3
apluidic seal is costed only if cost of purge gas without seal is greater
than the annual i zed cost of the seal plus any purge gas required with
the seal, i.e., taking the October 1982 purchase cost of a seal, Cf|.s.
from Figure E-2 for D, if '
53.45
60
™ {0.372
cont .
I
L
(0.1315 + 0.05 + 0.04)
$ capital
x 0.818 Jun- '80$ x 2.1 insta11ed x Cfl ". 1
Oct. '80$ purchase TI.S.J
53.45 I/IL
scfh
j A) .45
or, simplifying,
if 1169|D(in.)|2 - 3154 /Q^f"1 \ > (0.3805 x Cfl.s.)
L J \fl.g./cont.
then C'-'fT.s. = Cfl.s.
Note: This condition will be in error to the degree that1
[0.45 D2 - (QSCfm) ] < 0
fl.g. cont.
Otherwise,
C1" = 0
fl.s.
bFor installation cost factor breakdown, see Table 5-2.
^Updated using Chemical Engineering Plant Cost pipes, valves and fittings
index from August 1978 (273.1) to June 1980 (329.3).
^Updated using Chemical Engineering Plant Cost fabricated equipment index
from December 1977 (226.2) to June 1980 (291.3),.
eAdjusted using Chemical Engineering Plant Cost Index from October 1982
(317 estimated) to June 1980 (259.2).
fpor annualized cost factors, see Table 5-3.
QBased on vendor information for pilots without energy conservation [
(Reference 5). j
"Ensures continuous flow of at least 1 fps for flare with any continuous
flow not using fluidic seal: ,
ft'
x (1 fps) x (60 sec/min)
"•" " 144 1
- CQfl.g. (scfm)] cont. [ 60 min/hr
E-14
'.. , .',ii,, ...J .i'lSW,,,! ;. I,,'!! :£« E; "III;.; id
-------
Footnotes for Table E-3 (Concluded)
Ensures sufficient continuous flow per vendor information for flare
with any continuous flow using a fluidic seal:
0.45 scfh x CD(in.)]2
in
1<2CQn n (scfm).j x 60 min/hr x (t-j operating hours per year
." at stream combination i)
CQpilot(scfh)
x 8760 hr/yr
x 520°R scf at 60°F x 1,040 Btu (HHV) y _ $5.98
530°F scf at 70°R scf at 60°F (106 Btu (HHV)
16
„ (10° Btu)
x g
10 BTU
JAssumes steam at 0.4 Ib/lb of hydrocarbon at maximum continuous flaring
rate for 8600 hr/yr:
Qcont (scfra) X MWcont x ( wt.% HC\ x 8600 hr/yr x 60 mi
\ 100% /cont.
x (lb-mole/387 scf at 70°F) x (0.4 Ib steam/lb HC) x (1000 1b steam)
1000 (Ib steam)
x $6.187(1000 Ib steam)
or simplifying,
3.2961Q „ (scfm) x MW x wt.% Hclcont.
Lw-9- HHWjfl.g
E-15
-------
-p
O)
to
o
§
£)£•->•
UJ <4-
I— O
O t/)
^C 4-*
ac cn
o
O 0)
UJ i—
U_T-
°«
3C O
O -G
»—i
51
-=> o
Or—
UJ
UJ i-
ac itj
COr—
DC U
O 4>
O) E
« J. o~5-
Q> C O)
r- CJ C
>> O, rt)
D. O DL
£ fe. £
(A
1C
uo o o
U b J3
i -a t-
OJ >, rt)
O -C O
QJ ex r- o
e o TS c
«j i_ j= ra
LO r— t.
E-16
I' I i',;,
'';" ii!i:,! M,!'. if:i
.',- i,;;,:;!«,:J! I
-------
X U_
x:
cn
1
s-
to
*^^
o
t/1 O5
•a; c
CD ••—
1— O)
(/) -E
§ j_
O)
U- S
0 0
Jg;
o «
I— i t— re co
^ ^l^-a
c
*•» ' O O) **•* <
— o 3x a) jo
S. ir-ol'~
0 10° 10
O JO O H JO O.
5
a.
o se cn •**. c
O (A « tA «
E (U^ax^ei) ^3
U 1 O 1 O
•s ja o a JD o
£
^ . "^4
**». tn • to
0 0) 3X 0> 3
3 f-t* j3 »— JS
E *~" CO tl '"
cn 10 To
-i£ JD O It JO O
r-^i^^r. ^H
*-^
*^«. • t
cj cn *•*».
tA • cn 3
^^
o "o o*oi ^-*
"J/I
tA
I
r— re
re re
U i—
II
JC O
0 U-
!
p
oil
cs
•°
J^
o •
.. O 4->
O *--
4-*
CO
o
-£5 CM
=3 l«-
O9 vi
H
Cn
>*'
5
U • It
cn
1O — i O =9
SCh C3 4J
mo CQ
" OJ .
^ II
* * * tl -M ES
• ^ t;
en cn
• in
=1
x
..
H H n
«^j-
«
4- cn
•V
CM <- O
*-4 i-l CM «
XXX S
H fi (1
CO
o
ti-
ll o
W .
tO tO *-4 •• *^.
XXX U O
o
ff
H
cn
B*
ae c "•
»A • 3C "*f—
--» 0) *
o *—
v-4 t-*4 (O E
• . ^-* i o u.
SVO "C^ JQ O O
oo ««r i— ^i cxi
v-4 . m
w ^ 1
*— ^. VI
C3
CM
Cvt *cf •
ar^rcT* T-« CM
tJ O -^- C JC-~- 1^
o> jp a» c S c e o j g ^ ^i o-g go*.
*UJE: o ts t- j= o> re Sco x
>» 1 *-l >» (O •— *
e= o j=? u x
^» _>
«J rt c^
r>. ti
H C\J *J
0
O 11
» o. a™
* o-* ^
OJ
tA
o>
o
2
o
c
(A
4J
t
Q)
^
*
•M
U
Q)
4J £ C
tj S
« O
t- eu H.
(O (A E
>— 0 ^ £u
1C 0) E 0
r— O. k.
"«
fc- X
O) O> * 4-> O
4-» e c re t-
§^ O O) CL
f- je a.
v- E 4J re
x o re c re
O r— JC O L.
t- 10 *->
"O > E TJ X
i= o 3> o>
T- en t- IA
c »+- re £
O) 4J -p S-
(A « 01 T3 M-
0) Q) 4-> tt>
cr s- s E E
-------
.i "
;;;viS '»! .1 '•'« 1
, , '••• ' .("• ii ',• „ H"1 ,'•'•" , :, , . i " 'i;,,,,:"!,
The combustion products were then calculated using Table E-5
assuming 18 percent excess air for required'combustion air, but 0 percent
excess air for oxygen in the waste gas, i.e., oxygen thoroughly mixed
with VOC in waste gas. The procedure wouldinclude a calculation of
auxiliary fuel requirements for streams (usually with heating values
less than 60 Btu/scf) unable to achieve stable combustion at 870°C
(1600°F) or greater. Natural gas was assumed as the auxiliary fuel as
it was noted by vendors as the primary fuel now being used by industry.
Natural gas requirements would be calculated using a heat and mass
balance assuming a 10 percent heat loss in the incinerator. Minimum
auxiliary fuel requirements for low heating content streams would be
set at 5 Btu/scf to ensure flame stability.10
I ' •'». ' M. i." ;,; '. . ;l j ; '• ; ' 1 ' '.(.;•.
The design procedure for streams able to maintain combustion at
870°C (16b6°F) is presented in fable E-6. Fuel was added for flame
stability in amounts that provided as much as 13 percent of the lower
heating value of the waste gas for streams witn heating values of
650 Btu/scf or less. For streams containing morethan 650 Btu/scf,
| i.. , • - j ,Mi,i i:"!,,1 fcii ' t -:."- • • •",!:!::'» r :v"; • ' . :" i '>
flame stability fuel requirements were assumed to be zero since coke
oven gas, which sustains a stable flame, containsonly about 590 Btu/scf.
In order to prevent damage to incinerator construction materials,
quench air was added to reduce the combustion temperature to below the
incinerator design temperature of 980 °C (1800 °F) for the cost curve
given by IT Enviroscience.H
The total flue gas was then calculated by summing the products of
combustion of the waste gas and natural gas along with the dilution
air. The required combustion chamber volume was then calculated for a
residence time of 0.75 sec, conservatively oversizing by 5 percent
according to standard'industry practice.12 The design procedure
assumed a minimum commercially available size of 1.01 m3 (35.7 ft3)
based on vendor information13 and a maximum shop-assembled unit size
of 205 m3 (7,238 ft3).14 |
The design procedure would allow for preiireating of combustion
air, natural gas, and when permitted by insurance guidelines, waste
gas using a recuperative heat exchanger in order to reduce the natural
gas required to maintain a 870°C (1600°F) combustion temperature. If
E-18
'!! I
-------
(Si
o
o
C/)
CO
o
o
LU
S
O
LU
M
LU
z:
LU
I
LU
(U
oi "o >,
s t2 "5
•— -t- o
O o ""
O (/» CJ
I—I r— O
g.
t/t f-
a E
1.
0
Z r- 10
- o g
CO -—
OJoj
„ s
rd r-t
S S.
T
5 ?
I
o
eo
°l
E-19
-------
r
X
3
O)
"o
I
2
II
01
3
.0
O S-
2 '5
M 01
o
ir- V) «P-
r— 3 4J
° ^S
3
CJ
E-20
-------
vo
1
LU
CU
_a
10
1
t/>
0)
4->
O
C
4->
O
O
u_
or greater can attain 1600°F combustion temperatures withoi
rocedure are 32°F and 1 atm.
„_ °-
o c
co cn
3 to
+3 cu
CO T3
O £-
CO O
4^
^£
o cu
XI C
re -i-
u
t- c
O •¥-
s» "re
zc E
_J E
•*^ QJ
x:
CO 4^
CU
3 S-
•— O
re i»-
>
to
cn cr
_c ,°
4J 4J
ra ••—
cu -o
x: c
•-8
ST
o C
r— ra
•o
£ i
•i- 4->
3: ty>
tn
QJ OJ
t. =j
•M V-
tn
tn ra
Table E-4) to be supplied by auxiliary fuel. Amounts
2 of Reference 10.
g j^
<*- >--i
, £
re 3
cu iZ
andard cubic foot of wasi
pproximation of curve in
= percentage of LHV per st
based on a conservative a
ra C -a
cn o »*^ QJ
«s § §,
4J -r- « •.-
to -o «
ra T3 *< to
rs ra ~ — «
ra X)
to
re
cn
c
cu
o
1
in LU
ra
3: QJ
O ra
cu "-
1- £
3 £
QJ in
Q- ro
1? cn
4J CU
4-1
4J CO
a) ra
"c
•r- If—
II
XI
cn1"
_»§
-o
c
3
0
S
ra
X>
o
o
S-
re
c
o
cr
•o
ra
to
cn
cu
CO
S
cu
o
1
1
3
CU
re
cr
CU
•a
ra
CM
U-
o
o
cu
x>
o
3
to
to
S-
re
c
o
3
t>S
re
TJ
O_
O
O
C
1
CU
X)
U-
0
XI
3
4J
ca
_c
^~c
to
4J
re
cu
x:
o
U
cu
o.
to
c.
re
cu
CO
L
CO
to
cu
X
HI
2 stability at 18 percent
re
o
4J
to
o
Q.
0
to
re
cn
i.
to
c
L
S-
CO
CM
0
C
o
o
CO
o-
CM
0
CM
z:
j.
o
cn
to
CM
o
fl
CM
i.
o
to
o
CM
O
t-3
O
o
l[
o
U_
o
o
CO
3 Btu/lb = 1000 Btu/scf). Therefore, for combustion of 1 mo
CO
CrT
CM
II
rc
— i
o
•el-
r-4
II
CM
CU
CU
O-
CM
C ••
ra to
CO to
re re
CO X>
CJ
cu
CM O
E
A
CO «
re
CM C
0 O
»< to
cn
-n
r \ c_
fc* 4^
CM ro
01 c
•4-
j=
1
re
c
o
cn
c
4^
+->
s.
*o
c
CO
CO
o
CM
CO
o
CD
-t-
:n
XI
.—i
^-1
CM
+
CM
S
CO
CD
CM
CU
o
cr
re
"re
X)
cu
<=
cu
CO
to
re
cn
re
re
c
<*-
o
"
r- 1
•o
C
o
"43
JD
U
S-
1
=5
I-
ro
C
o
ZJ
•a
•a
c
VI
ra
cn
t/i
c
OJ
o
J3
ID
LO
cn
•
+ =5 31
tn _t
• t/>
cncu -o
c o. re
s»
3: *-> •
_j c Li-
re o
. — . 4J O
• to 0
• O 1
S U U-
>» o
in 4-> o
— I re co
X CO 4-»
3 4J 3
re re o
%^ CU X3
-— x: re
X 0 >,
C*|— «
•r* CU CU
0.0. c
u to cu
Cn
^^ cu cn
— . a. CD
C3 »•>,
O f in >—
o cn cu
CO -r- U. >
f< CU O *r-
. 0 tj
+ II CO CU
*H O.
» 3 00
• O
cn • 4J
• to
S ra LJ_
1— cn o
1 0
c? cu co
S +J ,
CO co S-
ri g cS
1J° S
' T3 S- 0
0 3 O
S- 4-> 0
o. « co
to CU
re o. o
cn E 4^
CU 4J
4-* cr
to 40 .
re cu s
*•— K-
~~ °
••- QJ
CL • Cn
o cn c
•r- • rO
S (-* "S
l/^Vj QJ QJ
I- i.
VI QJ 3
i — i 3: ra
"- - j-
O •> QJ
«— 4 1 1 F=
rO CL S-
tj O
+ ir>
ra
4-»
o
tn
OJ
ra
>
cn
c:
j_
Q)
|
II
O)
—1
-o
c
ra
u natural gas required/100 Ib waste gas * (20,660 Btu n.g.,
+j
.CO
r— i
cn
^SE
1C
=}
ro
i i
X
r—i
tn
ro
cn
"m
S-
3
rO
C
QJ ^.
o cn
I c:
•— QJ
•»•"*• O
r^ E
CO 1
• XI
O i—
cn
CM
O C
O XI
•*
O r-^
CM
CO cn
o •
• c
T— 4
QJ *~" 1
X
c
'E
CO
s-
x:
X
S-
x:
XI
cn
cf
X
cn
3
X)
o
o
cn
S
XI
CD
^H
X
cn
S
XI
o
0
to
cu
"o ,
E
1
XI
re
5 cu
o.'o
E
• i
cnx)
4- 0
CM
• CO
-o
O 4->
o.10
11-
• o
cn to
S cn
Cr LO
CM
CU
O
C
(U
i.
1
i.
o
o
re
14-
iff
ro
C
.°*
cn
QJ
•u
O
*— i
o:
o
OJ
?
o
u?
«er
+
o
o
CO
I— 1
X
0
QJ
t/l
O
«x>
£=
E
X
0
Q}
tn
LO
r-
O
x
u
v>
o>
o-
cn
and redesign.
*r-
ro
•o
-o
cn
3
ro
tn ,
(U
f—
JD
ra
ro
*«
35.7 ft' (mfnimum commerci
V
u
o
M-
-E
equire field fabrication; therefore, assume multiple
£-
-a
1
to
4->
CU
I"
QJ
tn
ro
1
o.
0
E
1 to'
" QJ
tsi
CO -r-
co "03
CO =)
oj cr
A tt-
o
Otn
>• -*->
E-21
-------
:syf
'ft '
a plant had a use for it, heat could be recovered. (In fact, a waste
heat boiler can be used to generate steam, generally with a net cost
savings.) |
E.3.2 Thermal Incinerator Cost Estimation Procedure ;
Thermal incinerator purchase costs for the calculated combustion
chamber volume were taken directly from Figure E-3, (Figure A-l in the
IT Enviroscience document, Reference 11). A retrofit installation
cost factor of 5.29 (see Table 5-2) was used based on the Enviroscience
document.15 The installed cost of one 150-ft. duct to the incinerator
and its associated fan and stack were also taken directly from Figure
E-4 (Figure IV-15, curve 3 in the IT Enviroscience study16). A minimum
I . . l:1 ' «,' ...I ' : ..:>. ,• ' }' I
cost of $70,000 (in December 1979) was assumed for waste gas streams
with flows below 500 scfm. the costs of pipingor ducting from the
process sources to the 150-ft. duct costed above were estimated as for
flares. Installed costs were put on a June 1980 basis using the
following Chemical Engineering Plant Cost Indices: the overall index
for thermal incinerators; the pipes, valves, and fittings index for
piping; and the fabricated equipment index for ducts, fans, and stacks.
Annualized costs were calculated using the factors in Table 5-3. The
I ! , !•, , • I ' ' 1 ' ' '
electricity required was calculated assuming a 6-inch ^0 pressure
drop across the system and a blower efficiency of 60 percent. The
cost calculation procedure is given in Table E-7. ;
: , . , Vii ,. I ••.; '• "i, . i .1
E.4 CATALYTIC INCINERATOR DESIGN AND COST ESTIMATION PROCEDURE :
Catalytic incinerators are generally cost effective VOC control
devices for low concentration streams. The catalyst increases the
chemical rate of oxidation allowing the reaction to proceed at a lower
energy level (temperature) and thus requiring a smaller oxidation
chamber, less expensive materials, and much less auxiliary fuel
(especially for low concentration streams) than required by a thermal
incinerator. The primary determinant of catalytic incinerator capital
cost is volumetric flow rate. Annual operating costs are dependent on
emission rates, molecular weights, VOC concentration, and temperature.
Catalytic incineration in conjunction with a recuperative heat exchanger
** i ..'.'•,'-,; ';„ .;: : - ; ; |
can reduce overall fuel requirements.
.jj: r.
E-22
-------
o
o
a
o
a
o
O
o
CO
I
'. o
o
C_5
I/)
XI
o
o
n
CO
I
to
zs
s_
O'
4->
fC
O)
•i—
O
S_
O
to
O
O
a>
to
3
CT>
(000' L$)
isBpng 5^5
E-23
-------
!!, V'll VII. „ ;, ill:.1! IV*!'
;"„«!,:,!-,i iVi;;,
i!1 ;i-i ;; ^"^ ',
,
CO!
3
JO
O
O
S-
OJ
>
o
O
O)
O +J
=3 co
Q >,
' 09,
O) i-
c— O
C 4J
l-H (O
i- d)
CO C
CO
O r—
O (C
a>
.
res S-
O O
M-
•"O
i ; a) .^i
r-j" O
4-? OO
01
c -a
t— i C
' (C
co
LlJ fO
I U_
0)
(000* L$)
6Z6L
_
E-24
-------
TABLE E-7. CAPITAL AND ANNUAL OPERATING COST ESTIMATES FOR
RETROFIT THERMAL INCINERATORS WITHOUT HEAT RECOVERY
ITEM
VALUE
Capital Costs
Combustion Chamber
Purchase cost
Installed cost
Installed cost, June 1980a
Piping & Ducting (from sources
to main incinerator duct)
Installed cost
Installed cost, June 1980b
Ducts, Fans & Stacks (from
main duct to incinerator
and from incinerator to
atmosphere)
Installed cost0
Installed cost, June 1980d
Total Installed Cost, June 1980
Annualized Costs6
Operating labor
Maintenance material & labor
Utilities
natural gas
electricity^
Capital recovery"
Taxes, administration & insurance
Total Annualized Cost
from Figure E-3 for Vcc
purchase cost x 5.29
installed cost x 1.047
see Section E.6 for Qw.g. (scfm)
installed cost x 1.206 for piping
installed cost x 1.288 for ducting
from Figure E-4 for Qw q ;
use $70,000 minimum
installed cost x 1.064
sum of combustion chamber,
piping & ducting, and ducts,
fans, & stacks
1200 hr/yr x $18/hr = $21,600
0.05 x total installed cost
(5.245 x 10'4) (% aux) x LHVW _
x Qw.g. (lb/hr) W*9'
(0.4610) x Qf>g> (scfm)
0.1627 x total installed cost
0.04 x total installed cost
operating labor + maintenance
+ utilities + capital recovery
+ taxes, administration &
insurance
E-25
-------
Footnotes for Table E-7
aUpdated using Chemical Engineering Plant Cost Index from December 1979
(247.6) to June 1980 (259.2).
bPiping updated using Chemical Engineering Plant Cost pipes, valves,
and fittings index from August 1978 (273.1) to June 1980 (329.3).
Ducting updated using Chemical Engineering Plant Cost fabricated
equipment index from December 1977 (226.2) to June 1980 (291.3).
cFrom Figure E-4 for no heat recovery from Enviroscience (Reference 16),
which assumed 150-ft of round steel inlet ductworkwith four ells,
one expansion joint, and one damper with actuator;, and costed according
to the CARD Manual (Reference 17). Fans were assumed for both waste
gas and combustion air using the ratios developed for a "typical
hydrocarbon" and various estimated pressure drops and were costed
using the Richardson Rapid System (Reference 18). Stack costs were
estimated by Enviroscience based on cost data received from one
thermal oxidizer vendor.
Although these Enviroscience estimates were developed for lower
heating value waste gases using a "typical hydrocarbon" and no dilution
to limit combustion temperature, the costs were used directly because
Enviroscience found variations in duct, etc., design to causeonly
small variations in total system cost. Also, since the duct,fan,
and stack costs are based on different flow rates (waste gas, combustion
air and waste gas, and flue gas, respectively) 'thecosts can not be
separated to be adjusted individually.
^Updated using Chemical Engineering Plant Cost fabricated equipment
index from December 1979 (273.7) to June 1980 (291.3).
eCost factors presented in Table 5-3.
. ' ''. f •. I . ' •':• ,'N Vil;M>!": , | '.''• ,':'• •;••' - ;1Ls:; ', \'\"
f[(% aux) x LHVw>g/20,660 Btu/lbn>g;] (100 lbn>g/100 lbw>gj x Q '(Ib/hr) x
(100 lbw.gj/100(lbw.gj x (8000 hr/yr) x (lb-mole/17.4 lbn.g.) x
(379 scf at 60°F/lb-mole) x (1040 Btu(HHV)/scf at WF) x $5.98/10^
; _ ,. • . I , ,'.'( ; ' ;; - :(•,!.•(' ] • [ ,:; •.'•• t,,; ;,,,„;;.:',; ';•. !
Btu (HHV) x (106 Btu)/106 (Btu).
SElectricity = (6 in. H20 pressure drop) x Qf.g. (scfm) x (8000 hrs/yr)
X (0.7457 kW/hp) x (5.204 Ib/ft2/in. H20) * [(60 sec/min) x (550 ft-lb/
sec/hp) x (0.6 kW blower/1 kW electric) x $0.049/kwh].
n!0 percent interest (before taxes) and 10 yr. life.
Hi!"
E-26
-------
E.4.1 Catalytic Incinerator Design Procedure
The basic equipment components of a catalytic incinerator include
a blower, burner, mixing chamber, catalyst bed, an optional heat
exchanger, stack, controls, instrumentation, and control panels. The
burner is used to preheat the gas to catalyst temperature. There is
essentially no fume retention requirement. The preheat temperature is
determined by the VOC content of gas, the VOC destruction efficiency,
and the type and amount of catalyst required. A sufficient amount of
air must be available in the gas or be supplied to the preheater for
VOC combustion. (All the gas streams for which catalytic incinerator
control system costs were developed are dilute enough in air and
therefore require no additional combustion air.) The VOC components
contained in the gas streams include ethylene, n-hexane, and other
easily oxidizable components. These VOC components have catalytic
ignition temperatures below 315°C (600°F). The catalyst bed outlet
temperature is determined by gas VOC content. Catalysts can be operated
up to a temperature of 700°C (1,300°F). However, continuous use of
the catalyst at this high temperature may cause accelerated thermal
aging due to recrystallization.
The catalyst bed size required depends upon the type of catalyst
used and the VOC destruction efficiency desired. About 1.5 ft^ of
catalyst for 1,000 scfm is required for 90 percent control efficiency
and 2.25 ft^ is required for 98 percent control efficiency.^ As
discussed earlier many factors influence the catalyst life. Typically
the catalyst may loose its effectiveness gradually over a period of
2 to 10 years. In this report the catalyst is assumed to be replaced
every 3 years.
Heat exchanger requirements are determined by gas inlet temperature
and preheater temperature. A minimum practical heat exchanger efficiency
is about 30 percent. Gas temperature, preheater temperature, gas dew
point temperature and gas VOC content determine the maximum feasible
heat exchanger efficiency. A maximum heat exchanger efficiency of
65 percent was assumed for this analysis. The procedure used to calculate
fuel requirements is presented in Table E-8. Estimated fuel requirements
and costs are based on using natural gas, although either oil (No. 1
or 2) or gas can be used. Fuel requirements are drastically reduced
E-27
-------
K '-ll';;' K. -I';*'''',,,:* '
when a heat exchanger is used. Total heat requirements are based on a
preheat temperature of 600°F. A stack is used to vent flue gas to the
I j, ' ' , ' " '! :„", ':•'• -/ilk! '.'U'.;! ! '> .if I':;.- -n ., •" I'-1
atmosphere.
E.4.2 Catalytic Incinerator Cost Estimation Procedure
The capital cost of a catalytic incinerator system is usually
based on gas volume flow rate at standard conditions. For catalytic
incineration, 70°F and 1 afm (0 p'sig) were taken as standard conditions.
The operating costs are determined from the gas flow rate and other
conditions such as gas VOC content and temperature.Table E-9 presents
. i ,!•"•:,•, ' i-;.' • "»V'" l!"!"1 ••! i' i ±~>f' ' ' *•'•' •' I ' '• - '
the basic gas parameters required for estimating system costs.
As noted earlier, equipment components of a catalytic incineration
system include blower, preheater with a burner, mixing chamber, catalyst
bed, an optional heat exchanger, stack, controls, and internal ducting
including bypass. Calculations for capital cost estimates are based
on equipment purchase costs obtained from vendors 19,20,21 and application
of direct and indirect cost factors. Table E-10 presents third quarter
1982 purchase costs of catalyst incinerator systems with and without
heat exchangers for sizes from 1,000 scfm to 50,000 scfm. The cost
data are based on carbon steel for incinerator systems and stainless
steel for heat exchangers. The heat exchanger cosis are based on
65 percent heat recovery. Catalytic incinerator systems of gas volumes
higher than 50,000 scfm can be estimated by considering two equal
volume units in the system. A minimum availableunit size of 500 scfm
was assumed.22'23 The installed cost of this minimum size unit (which can
be used without addition of gas or air for stream flows greater than
about 150 scfm23) was estimated to be $53,000 (June 1980). The heat'
exchangers for small size systems would be costly and may not be practical
Table 5-2 presents the direct and indirect installation cost component
factors used for estimating capital costs of catalytic incinerator
systems. The geometric mean of the two vendor estimates for each flow
rate was multiplied by the ratio of total installed costs to equipment
purchase costs of 1.82 developed for a skid-mounted catalytic incinerator.
Actual direct and indirect cost factors depend upon the plant specific
conditions and may vary with system sizes.
Since the equipment purchase cost presented in Table E-10
represents the third quarter of 1982, the cost data was adjusted to
E-28
•ii , .v,i i y. iJr ./(!, Jj''fei&&BSi:H!4:.VA iik.\\*. ^iii•:«.';i(j.
I:'1 i:11!"!1"'' "!!:l<:*"1"I:I!
.••'•r;^.^M
, 1!l|i"li'ii: S:ll! i'S
" ii Bi' rl^'.il
• 'i!»5, !,:«!*'
'i; ""»! '.S! iK-'t
-------
Table E-8. OPERATING PARAMETERS AND FUEL REQUIREMENTS
OF CATALYTIC INCINERATOR SYSTEMS
Item
Source of information or calculation
Waste Gas Parameters
(1) Flow rate (0.2), scfm
(2) Amount of air present in
the gas, scfm
(3) Amount of air required
for combustion at 20%
excess, scfm
(4) Net amount of additional
air required (0.3), scfm
(5) Total amount of gas to be
treated (04), scfm
(6) Waste gas Temperature at
the inlet of PHRb, °F
(7) Waste gas temperature at
preheater outlet or
catalyst bed inlet, °F
(8) Temperature rise in the
catalyst bed, °F
(9) Flue gas temperature at
catalyst bed outlet, °F
(10) Minimum possible temperature
of flue gas at PHR outlet, °F
(11) PHR efficiency at maximum
possible heat recovery**, %
(12) PHR design efficiency, %
From Table E-9
0, if the waste gas contains VOC and
nitrogen or other inert gas; and
[(1 - volume percent VOC) * (volume
percent VOC)] x VOC volume flow (O^)
scfm, if the waste gas contains VOC
and air
See footnote a.
Item (3) - Item (2); and 0 if
[Item (3) - Item (2)] is negative
Item (1) + Item (4)
From Table E-9
600°F
(25°F/1% LEL) x (%LEL from Table E-9)
Item (7) + Item (8)
See footnote C.
[Item (1) x (Item (7) - 25°F -
Item (6))] * [Item (5) x (Item (9) -
Item (6))]e
See footnote f
E-29
-------
I , '. ' "I , I ' • 11,
Table E-8. OPERATING PARAMETERS AND FUEL REQUIREMENTS
OF CATALYTIC INCINERATOR SYSTEM (concluded^
Item
Source of information or calculation
(13) Waste gas temperature at
PHR outlet,°F
(14) Amount of heat required by
preheater at additional 10%
for auxiliary, Btu/min
(15) Amount of heat required
for preheater and auxiliary
fuel, 106 Btu/h
(16) Amount of natural gas
required per year, 106 cfm
0.65 [Item (9) - Item (6)3 + Item (6)
Item (5) x [Item (7) - Item (13)] x
[Gas specific heatS, Btu/scf, °F] x
[Item (14) x 60 minutes/hour] x (lO%)n
x (106 Btu)/106 Btu
[Item (14) x (8,tiOO x 60) minutes/year]
x 10-3 * (1,040 Btu/cfm)
„„ volume basis (scfm/scfm): 11.45 for methane, 20.02 for ethane, 28.58 for
propane, 54.31 for hexane, 17.15 for ethylene, and 45.73 for pentane.
Values taken from p. 6-2 in Steam (Reference 24) for 100% total air and
multiplied by 1.2 for 120% total air or 20% excess air.
bPrimary heat recovery unit.
CHeat exchanger should be designed for at least 50°F above the gas dew point.
dThe heat exchanger will be designed for 25°F lower thanthe preheater
temperature so as to not cause changes in catalyst bed outlet temperature.
^Though the heat recovery to the temperature level of inlet gas is the
maximum heat efficiency possible, in some cases this may not be possible
due to gas dew point condition.
fCost estimates are based on calculated maximum possible heat recovery
up to an upper limit of 65 percent heat recovery.
9Gas specific heat varies with composition and. temperature. Useci 6.019 Btu/ft3°F
based on average specific heat of air for calculation purpose.
^Auxiliary fuel requirement is assumed to be 10 percent of total.
E-30
i
-------
TABLE E-9. GAS PARAMETERS USED FOR ESTIMATING CAPITAL AND
OPERATING COSTS OF CATALYTIC INCINERATORS3
ITEM
VALUE
Stream identification
Stream conditions
Temperature,°F
Pressure, psig
VOC content:
Emission factor, kg/Mg
of product
Weight % of total gas
Mass flow rate, kg/h
Ib/h
.Organic constituents, wt %
Average mol. wt. (M]_), IDS
Volume flow (Qi), scfm
Heat content
Btu/scf
Total gas:
Constituents
Mass flow rate, Ib/h
Molecular weight (M2)
Volume flow (0.2)5 scfm
Air volume flow rate, scfm
VOC concentration (A), %
of LEL
Heat content
Btu/total scf
Identify the vent and the polymer
industry from Chapters 2 and 5
(Emission factor, E, kg/Mg) x 1000 Mg/Gg
(Plant production rate, P, Gg/yr) *
(8,000 h/yr)
(kg/h) x (2.205 Ib/kg)
(VOC mass rate, Ib/h) * (60 min./h) 4
(Molecular weight (M^), Ibs/lb mole) x
385 scf/lb-mole at 68°F) = 1.768
(174.273)(2.521NC + NH)
VOC, air and others
(VOC rate, Ib/h) * (wt% of VOC in
gas, Wj/100%)
Gas mass rate, Ib/h) •* (60 min/h) *
(Gas molecular weight (M2), Ib/lb mole)
x (385 ft6 /Ib mole) = 1.768
(Total gas flow (Q2), scfm) - (VOC volume
flow (Qi), scfm)
(100) [(Volume flow of VOC, scfm) *
(Volume flow of air, scfm] * LEL"
From Chapter 5e
E-31
-------
Footnotes for Table E-9
^Obtain gas parameters from Chapter.2 of the CTG, and Chapter 3 of the
background information document for the polymer manufacturing NSPS,
except those to be calculated.
• ' ..'•.• iiiii, i. i« '
bCalculate using weight percent values of VOC components.
1 '•" ••• ""•'•'' ' ! •
cif the VOC heating value is not available, calculate it using heat of
combustion values of 14,093 Btu/lb from carbon converted to C02 and
51,623 Btu/lb from hydrogen converted to water. Nc and NH denote number
carbon and hydrogen atoms in VOC.
dlower explosion levels of ethylene, hexane, methanol, propane, butane,
and pentane are 3.1, 1.32, 7.3, and 2.5, 1.9,.and 1.4, respectively.
eiotal gas heat content averages 50 Btu/scf at 100 percent LEL.
E-32
aV,!,!, :; If.,
'"• " !R It/if: !![;'•¥' IW ii
.,. . [.'II '. til'., *'•'. I'M i
'
-------
o
CM
vt
en
*^t
1—
§
1—
00
o
o
OS
0
Q
•3*
111
I.U
^*
fV
O
i—
|— «•
f^
LU
^*^
t-H
C^
^g^
1— H
O
1— H
>-
-------An error occurred while trying to OCR this image.
-------
5,000
~ 1,000
o
o
0
t— <
(/>
0
"n.
<5
O)
E
H-H
§ 100,
Crt
rr«
LU
•ZL
1-3
10-
**•
^
,«
,,
..
<;
Key:
With 65%
Without h
^
s/
^
teat r
sat re
^
__.,,
^x
iCOV
cove
^
sry
•y
x
/
X
'
•^
X
x' y
-X
>
X
X
x
X
y
x'
^
i
/
0.5 1 10
100
Gas Flow Rate (1000 scfm)
Figure E-5. Installed Capital Costs for Catalytic Incinerators
With and Without Heat Recovery
E-35
-------
Table £-11. CAPITAL AND OPERATIONG COST'ESTIMATION" FOR
CATALYTIC INCINERATOR SYSTEMS
il; WJ
'
Item
Value
Capital Costs
Incineration system
Installed cost, June 1980
Installed retrofit cost, June 1980
Piping & ducting (from sources
to main incinerator duct)
Installed cost
Installed cost, June 1980a
Ducts, fans & stacks (from main duct
to incinerator and from incinerator
to atmosphere)
Installed costb
Installed cost, June 1980C
Total Installed Cost, June 1980
Annualized Costs
Direct costs
Operating labor
Maintenance material and
labor
Catalyst requirement
Utilities:
Fuel (natural gas)
From Figure E~5
Installed cost x 1.18, from Table 5-2
See Section E-6 for source flow
rates, scfm.
i
Installed cost x 1.206 for piping
Installed cost x 1.288 for ducting
'
From Figure E-4 for waste gas flow
(Q2), scfm; use $70,000 minimum
Installed cost x 1.064
Sum of incineration systems,
piping & ducting, and ducts,
fans, & stacks
$11,200 for systems with no heat
recovery; and $16,700 for systems
with heat recovery
(0.05) x (Total installed capital
cost, $ from Figure E-5)
I
$2.7 x (Total gas volume flow|(Q4)a
scfm, item 5 from Table E-8) =
($2.7 x Q4)
($6.22/103ft3) x (Amount of natural
gasrequired, 103ft3, Item 16 of
Table E-8)e
E-36
-------
Table E-ll. CAPITAL AND OPERATIONG COST ESTIMATION FOR
CATALYTIC INCINERATOR SYSTEMS (Concluded)
Item
Value
Electricity
Indirect Costs
Capital recovery
Taxes, insurance and
administrative charges
Total Annual!zed Costs
($0.312/scfm) x (Total gas volume
flow rate (0,4), scfm, Item 5 from
Table E-8) for units with no heat
recovery; and ($0.78/scfm) x (Total
gas volume flow rate (04), scfm,
Item 5 from Table E-8) for units with
heat recovery
(0.1627) x (Total installed capital
cost, $ from Figure E-5)
(0.04) x (Total installed capital
cost, administrative charges
$ from Figure E-5)
Sum of total direct costs and
total indirect costs
aUpdated using Chemical Engineering Plant Cost Index from December 1979
(247.6) to June 1980 (259.2).
^Piping updated using Chemical Engineering Plant Cost pipes, valves, and
fittings index from August 1978 (273.1) to June 1980 (329.3). Ducting
updated using Chemical Engineering Plant Cost fabricated equipment index
from December 1977 (226o2) to June 1980 (291.3).
cSee footnote c, Table E-7 for discussion on application of these costs
developed by Enviroscience (Reference 25).
^Updated using Chemical Engineering Plant Cost fabricated equipment index
from December 1979 (273.7) to June 1980 (291.3).
eTotal gas flow including waste gas and additional combustion air.
E-37
-------
$0.335/scfm for units with no heat recovery (i.e., for 4 in. 1^0 pressure
drop) and $0.838/scfm for units with heat recovery (i.e., for 10 in. ^0
i
pressure drop).
E.5 SURFACE CONDENSER DESIGN AND COST ESTIMATION PROCEDURE
This section presents the details of the procedure used for
sizing and estimating the costs of condenser systems applied to the
gaseous streams from the continuous process polystyrene model plant.
Two types of condensers are in use in the industry: surface condensers
in which the coolant does not contact the gas or condensate; and
contact condensers in which coolant, gas, and condensate are intimately
mixed, " ' ' , '("' '' '",',' j
Surface condensers were evaluated for the following two streams
from the polystyrene model plant: the styrene condenser vent and the
styrene recovery unit condenser vent. These streams consist of styrene
and steam, which are immiscible, or of styrene inair, a non-condensable.
The nature of components present in the gas stream determines the
method of condensation: isothermal or non-isothermal. The condensation
method for streams containing either a pure component or a mixture of
two immiscible components is isothermal. In the isothermal condensation
i u ' •, "i ','i.r ,i , .• ,, . i« • >• -, , 1 , 1 •
of two immiscible components, such as styrene and steam, the components
condense at the saturation temperature and yieldtwo Immiscible liquid
condensates. The saturation temperature is reached when the vapor
pressure of the components equals the total pressure of the system.
The entire amount of vapors can be condensed by isothermal condensation.
Once the condensation temperature is determined, the total heat load is
calculated and the corresponding heat exchanger system size is estimated.
The condensation of styrene mixed with a non-condensable, such as air, _
can be considered isothermal if the temperatureof one fluid is nearly
constant. The analysis shows that the condenser coolant tempearture is
nearly constant for the combined material recovery vent stream from the
continuous polystyrene model plant. The condensation of styrene in
air, nevertheless, is accomplished less readily, and thus more expensively,
than the condensation of styrene in steam.
The following procedures and assumptions were used in evaluating
•; ; ; " ,,';,' ',' i ;„
the isothermal condensation systems for the two streams containing
E-38
-------
(1) styrene in steam and (2) sytrene in air from the continuous polystyrene
model plant.
E.5.1 Surface Condenser Design
The condenser system evaluated consists of a shell and tube heat
exchanger with the hot fluid in the shell side and the cold fluid in
the tube side. The system condensation temperature is determined from
the total pressure of the gas and vapor pressure data for styrene and
steam and sytrene in air. As the vapor pressure data are not readily
available, the condensation temperature is estimated for styrene in
steam by trial-and-error, and for styrene in air by a regression equation
of available data points'^ using the Clausius Clapeyron equation which
relates the stream pressures to the temperatures. The total pressure
of the stream is equal to the vapor pressures of individual components
at the condensation temperature. Once the condensation temperature is
known, the total heat load of the condenser is determined from the
latent heat contents of styrene and steam and, for styrene in air, from
the latent heat content of the condensed sytrene and the sensible heat
changes of styrene and air. Table E-12 shows the procedure for calculating
the heat load of a condensation system for styrene in air. The design
requirements of the condensation system are then determined based on
the heat load and stream characteristics. The coolant is selected
based on the condensation temperature. The condenser system is sized
based on the total heat load and the overall heat transfer coefficient
which is established from individual heat transfer coefficients of the
gas stream and the coolant. An accurate estimate of individual coefficients
can be made using such data as viscosity and thermal conductivity of
the gas and coolant and the standard sizes of shell and tube systems to
be used.
For styrene in steam, no detailed calculations were made to determine
the individual and overall heat transfer coefficients. Since the
streams under consideration contain low amounts of styrene, the overall
heat transfer coefficient is estimated based on published data for
steam.
For styrene-in-air, refrigerated condenser systems were designed
according to procedures for calculating shell side^S and tube side2^
heat transfer coefficients and according to condenser^ and refrigerant31>32
E-39
-------
Table E-12. PROCEDURE TO CALCULATE HEAT LOAD
OF A CONDENSATION SYSTEM FOR STYRENE I
Item
Heat exchanger type
Source identification
Source production capacity
(CAP), Gg/yr
Source emission factor (E),
kg VOC/Mg product
Desired emission reduction,
(% Red'n), %
Gas stream condition
Partial pressure of styrene
at inlet (P1n)
Composition of gas stream
at inlet;
Styrene mass flowrate
(Ms), lb/hrd;
Gas stream volumetric
flowrate (V), acfrn6
Gas stream mass flowrate
(W), lb/hrf
Partial pressure of styrene
at outlet (P0ut)> mm H9
Temperature required for reduction
Temperature required for reduction
(Tout). "F
Latent heat change of styrene
Btu/hrh
Value
Shell and tube heat exchanger
with hot fluid in the shell
side and the cold fluid in the
tube side
Identify the polymer industry and
the vent from Chapters 2 and 5
• H.1. r . i ;; ' ; i ..];•. • • : -
From model plant in Chapter 2
From model plant in Chapter 2
96.1% at 3.09 kg VOC/Mg of product
40% at 0.2 kg VOC/Mg of product
Assume^ saturated styrene in
air at 80°F, latm.
7.952 mm Hg
. ft3 styrene/ft3 gasb;
0.002764 Ib styrene/ft* gasc
0.2756 x CAP x E
361.79 x
4.415 x V
100-%Red'n x 7.952 mm Hg
100
4847.95 * [18,2440 - In (Pout)]
(1.8 x T'out) - 459.67
166.36 x W x (% Red'n)
E-40
111! I 111
-------
Table E-12. PROCEDURE TO CALCULATE HEAT LOAD
OF A CONDENSATION SYSTEM FOR STYRENE IN AIR (Concluded)
Item
Value
Average (bulk) gas temperature (Tb),°F
Density of air (pair), Ib/ft
Specific heat of air((cD)air),
Btu/lb-°F '
Sensible heat change of air (Qa-jr)»
Btu/hr
Specific heat of styrene ((CD) ),
Btu/lb-°F
(80 + Tout) * 2
1 * [(0.002517 x Tb) + 1.157]
From API Report 44k
V x pair x (c) . x (80-Tout) x
60 min/hr
p . -out
ai r
From API Report 441
Sensible heat change of styrene (Q'sty)
Btu/hr
Total design heat load (Qt0t)> Btu/hrm
(cp) x (80-Tout)
sty
1.2 (Qsty+Qair+ Q'sty)
Calculated from Clausius Clapeyron curve fit
(In p = m \ + b) of styrene vapor pressure versus
temperature data given on p. 3-59 of the Chemical Engineers' Handbook
(Reference 26) for 80°F (see temperature required for reduction).
bVolume fraction of styrene = 7.952 mm Hg = 0.01046 ft3 styrene/ft3 gas.
760 mm Hg
cAssuming ideal gas:
V _ RT = 1545 ft lbf/lb.m - °R x0540^°R = oqd Tjft3/u
n" " F" 14.7 lbf/in.2 x 144inz/ftz «•»•" /'L
styrene content (Ib/ft3 gas) -
0.01046 ft3 styrene x Ib-mole x 104.14 Ib styrene
"•° gas 394.13 ft3 1 b-mole
E-41
-------
Footnotes for Table E-12 (Concluded)
dCAP Gg product/yr x 1000 Mg/Gg x E kg VOC/Mg product
8000 hr/yr x 0.4b3b Kg/ID
eCAP Gg product/yr x 1000 Mg/Gq x E kg VOC/Mg procjuct = 92.26 x CAP x E
' 8000 hr/yr x 0.4b^6 kg/lb x u.uuz/64
fV, acfm @ 80°F x ^29 Ib/lb-mole x 60 min/nr
—394.13 acT/lb-mole e birt-
gsolving Clausius Clapeyron curve fit of styrene vapor pressure data
(?2 1 0.99995) referred to in footnote a for temperature.
hsiope, m, of Clausius Clapeyron curve fit = - X/R
latent heat of styrene,X= -m x R = ptu-lb-mole
4847 95 (°K) x 1.9853 cal/g-mole-°K x 1.8 cal/g-mole
'-— 104.14 Ib/lb-mole
1T 6R = T oc + 273.15 = 5. (T,dF-32) + 273.15 = 0..5556 T,°F + 255.37
9
an ideal gas (PV = mRT/MW) , £1 =
P2
at 0°C (ChE Hndbk, p. 3-72)
Pair @ T,°K = 0.0808 X
'all "
;' Pair = 0.08081
T,6K 0.5556 x f,°F + 255.37
k(cp) . = 0.796 (cp)N2 + 0.231 (cp)02, where (cp)N2 and (cp)02 are
! i , " i
specific heats of nitrogen and air, respectively, available by
interpolation from API Report 44, p. 652 (Reference 27).
V(c ) vs T,°F, values are available for interpolation on p. 682
P sty
of API Report 44 (Reference 27).
^including 20% safety margin.
E-42
i I
-------
characteristics given primarily in the Chemical Engineers' Handbook and
consistent with the 8-ft. long condenser with 1-inch outside diameter tubes
assumed by Enviroscience33 for cost estimation purposes. Then the total
heat transfer area is calculated from the known values of total heat
loads and overall heat transfer coefficient using Fourier's general
equation. A tabular procedure for calculating heat exchanger size is
presented in Table E-13 for styrene in steam and in Table E-14 for
styrene in air.
E.5.2 Surface Condenser Cost Estimation Procedure
For styrene in steam, the heat exchanger costs for each stream were
obtained from vendors.36>37,58 por styrene in air, condensation system costs
were based on IT Environscience3^ as well as vendor information.
A retrofit installation factor of 1.48 (See Table 5-2) was used to
estimate installed condenser costs for condensers of 20 ft2 or less and
2.58 for condensers 125 ft2 or greater. No additional piping was costed
for condensers with less than 20 ft2 of heat transfer area because
the condenser unit is so small ,( 1-2 ft. diameter) that it should
be able to be installed adjacent to the source. For condensers with
heat transfer areas of 125 ft2 or greater, piping was costed using the
procedures described in Section E-6. Table E-15 presents the estimated
total capital and annual operating costs for the condenser system of 20
ft2 heat transfer area for styrene in steam. Table E-16 presents the
procedure for estimating capital and annual operating costs for condensation
systems for styrene in air.
E.6 PIPING AND DUCTING DESIGN AND COST ESTIMATION PROCEDURE
Control costs for flare and incinerator systems included costs of
piping or ducting to convey the waste gases (vent streams) from the
source to a pipeline via a source leg and through a pipeline to the
control device. All vent streams were assumed to have sufficient
pressure to reach the control device. (A fan is included on the duct,
fan, and stack system of the incinerators.)
E.6.1 Piping and Ducting Design Procedure
The pipe or duct diameter for each waste gas stream (individual
or combined) was determined by the procedure given in Table E-17. For
flows less than 700 scfm, an economic pipe diameter was calculated
E-43
-------
Table E-13 PROCEDURE TO CALCULATE HEAT TRANSFER AREA OF AN
ISOTHERMAL CONDENSER SYSTEM
Item
Heat exchanger type
Gas stream condition
(including temperature
(T,)°F pressure (PJ..
psig, and composition)
Condensation temperature
(T2),°F
Total heat load (H), Btu/h
Coolant used0
Temperature, rise of
coolant, (AT),°F
Coolant outlet temperature
(T3),8F
Log mean temperature
difference (LMTD),°F
Heat transfer coefficient (U)
Heat transfer area (A), ft
Value
Cocurrent shel1 andtube heat
exchanger with the hot fluid
in the shell side and the cold
fluid in the tube side
Obtain from Chapters 2 and 5
water at 85°F, 25 gpm
H Btu/h * [(25 gpm x 500 Ib/h/gpm) x
(1 Btu/lb°F)]
85°F + AT
[(TrT3) - (T2 - 85)3 * in C(TrT3)/(T2-85)]
240 Btu/h ft°F
(H)/U(LMTD)
in P/Pr
(X/R) (1/T0 - 1/T)
and R is universal gas constant = 1.99 cal/g mole K.
The same equation can be rearranged to eliminate X and R:
ln(P/P)
(970 3 Btu/lb steam) and Ib/hr steam in stream.
cF1xed amount of 25 gpm is used in order to maintain turbulent flow.
s?eL andl6% |tyrene) of P"« «««l;«tfSR2sgJ
1,000 Btu/h ftz°F for steam and 35 Btu/h ft F tor
following relationship:
E-44
-------
Table E-14. PROCEDURES TO CALCULATE HEAT TRANSFER
AREA OF A CONDENSATION SYSTEM OF STYRENE IN AIR
Heat exchanger configuration
Source Identification
Coolant temperature, TC,°F
Shell-side heat transfer
Coefficient (h0), Btu
hr-ft2 - °F
Try 8" shell with 17 1-inch o.d.,
16 gage, 8-feet long brass tubes
on 1-1/4" square pitch9
Identify the polymer industry and
the vent from Chapters 2 and 5
Tout-10, rounded to next lower
multiple of 5.
Calculate using procedure in
Chemical Engineers' Handbook,
pp. 10-25 thru 10-28
(Reference 28)b
Coolant
Tube-side Reynold's Number (
Tube-side heat transfer
Coefficient (h0), Btu
Select chilled water at Tc > 35°F;
for Tout > 45°F; ethylene glycol-
water brine solutions at Tc > -40°F,
for Tout ^ -30°F; and Freon-12 or
or other direct expansion coolants
at TC<-40°F, for TQUt < -30°F.C
(12 x rH x p ) * fj.
Calculate using appropriate equations
for forced connection in pipes.6
Coolant flow (Wc), lb/hrf
Temperature change of coolant
(ATC),°F
Coolant flow (Vc),
Clean overall heat transfer
coefficient (Ur), Btu/ft^-hr-°Fh
757.9 x p
Qtot * (Cp x Wc)
94.5
[(1.149 * h0) + (0.0000839)
+ (1 * hj]-1
E-45
-------
1 1 •;: • ..;•."• f?l;V1"!:f ••'•I "v '•'•:';:>'•'if Mr
Table E-14. PROCEDURES TO CALCULATE HEAT TRANSFER
AREA OF A CONDENSATION SYSTEM OF STYRENE IN AIR (Continued)
Dirty overall heat transfer
coefficient (Ud), Btu/ft*-hr-°F
Log nvean temperature difference (LMTD), °F
Required heat transfer area (A), ft2
Total tube length required (Lt), ftj
Required heat exchanger length (LH.E.)> ft
Required refrigeration capacity (RC1), tons
Selected refrigeration capacity (RC), tons
[(1 * Uc) + 0.001]
-AT2) * In
-1
Qt t * (UD x LMTD); :
if A > 43.8 ft2, try a larger
heat exchanger1
A * 0.2618
Lt * 17
Qtot * 12>000
RC' or minimum of 1
^Condenser and tube characteristics from pp. 11-1 thru 11-18 of the
Chemical Engineers' Handbook (Reference 30):
Tube: outer diameter, D0 = 1.00 in.; inner diameter, D-j = 0.870 in.;
thickness, Xw = 0.065 in.; specific external surface area =
0.2618 ft2/ft;
cross-sectional area = 0.004128 fWtube
Condenser: shell inside area, Ai = 0.3553 ft*-;
total tube area, A = 0.09272 ft*;
net area = 0.2626 ft2, wetted perimeter = 6.54 ft;
hydraulic radius, r^ = 0.04001 ft.,
length, L = 8 ft, total cross-sectional area inside of
tubes = 0.004128 ft2/tube x 17 tubes = 0.07018 ft^.
Assuming baffle cuts, lr = 0.25 (shell diameter, Ds); shell outer tube
limit, D0tl «7.634 in. (7/16" clearance for fixed tube sheet for
Ds < 24"); baffle spacing, bs = Ds % 8 in.
cCoolant characteristics can be interpolated or extrapolated for the
coolant temperature, Tc, from The Chemical Engineers' Handbook:
pp. 3-71, 206, 213, & 214 (Reference 34) for water; pp. 12-46 thru 12-48
(Reference 31) for ethylene glycol water solutions; and pp. 3-191 and
3-212 thru 3-214 (Reference 31, plus p. E-26 (Reference 32) of The Hand-
book of Chemistry and Physics for Freon-12 (dichlorodifluoromethane).
Characteristics required are dynamic viscosity (fx), density (p),
specific heat (CB), thermal conductivity (k), and specific gravity (y)
* p/62.42, lb/fts.
dFor coolant velocity, V = 3 fps (3-10 fps recommended by Kern in Process
Heat Transfer (Reference 35).
E-46
-------
FOOTNOTES FOR Table E-14 (concluded)
eFrom The Chemical Engineers' Handbook, pp. 10-12 thru 10-15 (Reference 29).
(1) For turbulent flow (NRe > 10,000) (from Eq. 10-51):
h =
0.023 x V. ft/hr x plb/ft3 x Cn, Btu-lb-°F Y
— —- p_ x
2/3 0 2
(NPr) (NRe)
(\0 44
/id \ * «1, if properties
"V
at average of bulk (b) & wall (w) temperature.
(2) For transition flow (2000 < NRS < 10,000) (from Eq. 10-49):
h _ 0.029 k (NRe2/3 -
° rH
(3) For laminar flow (NRS < 2100) (from Eq. 10-40):
= 0.465k
H
where
NGz1/3
x Npr x 4 x
+ 0.87 (1 + 0.015 NQz1/3)
* L.
coolant velocity of 3 fps and total tube cross-sectional area of
0.07018 ft2: 0.07018 ft2 x 180 ft/min. x p , lb/ft3 x 60 min/hr.
9For coolant velocity of 3 fps, 0.07018 ft2 x 180 ft/min. x 7.48 gal/ft3.
hDQ/Di = 1.000 in. 4 0.870 in. = 1.149;
DO Xw =
KtDj_
where:
0.0542 ft x 1.000 in.
69.2 Btu/ft-hr-°F x 0.9335 in.
Kt = thermal conductivity of brass tube
(pp. 23-49 ChE Hndbk) (Reference 26)
= (D0 - Dj) * In
= (l.OO - 0.87) * In (1.00/0.87) = 0.9335.
""See heat exchanger configurations for 1-in. o.d., 1-1/4-in. square pitch,
T.E.M.A. P or S on p. 11-15 of The Chemical Engineers' Handbook (Reference 30)
for 8-ft heat exchangers assumed by Enviroscience for cost basis: 17 tube
minimum unit, A = 35.6 ft2; for 30 tube next larger unit, A = 62.8 ft2;
assume need larger than minimum size for design (Enviroscience costing
curve is continuous for all areas) when A = 35.6 + (0.2 heat load design safety
margin + 0.1 allowable undersizing) x (62.8 - 35.6) = 43.8 ft2.
JA,ft2 * 0.2618 ft2 of tube external surface area/ft of tube.
kLt,ft of tubes * 17 tubes.
112,000 Btu/hr per ton of refrigeration capacity.
E-47
-------
Table E-15. CAPITAL AND ANNUAL OPERATING COST ESTIMATES
FOR A RETROFIT 20 ft2 CONDENSER SYSTEM FOR THE
STREAMS FROM THE CONTINUOUS POLYSTYRENE MODEL PLANT
Item
Value
Control system
Capital Cost:
Purchase cost
Installed capital cost3
Annualized cost;
Operating labor
Maintenance0
Utilities:
Water0
Electricity6
Taxes, insurance-and
administration
Capital recovery9
Total annualized cost
without recovery credit
Total amount of styrene
recovered from W Ib/hr
of styrene
Annual styrene recovery credit
at $0.3575/1b
.Total annualized cost after credit ($1,980 - $Z)
Heat exchanger with a maximum
capacity of 20 ft* heat transfer
area
$2,000
2,960
$1,080
150
$ 5
$ 140
$ 120
$ 480
$1,980
(W Ib/hr x 8,000 hr/yr x X heat exchanger
efficiency x 90% recovery efficiency
from the separator)
* 2,000 Ib/ton = Y tons/year
Y tons x 2,000 Ib/ton x $0.3575/1b = $Z
Cost effectiveness of emission
reduction ($/Mg)
($1,980 - $Z)/[W Ib/hr x 8,000 hr/yr
x X heat exchanger (VOC reduction)
efficiency/2,205 Ib/Mg]
Purchase cost times retrofit installation cost factor of 1.48 (see Table 5-2).
Operating labor cost = 1 hr/wk x 52 wk/yr x 1.15 (with supervision/
without supervision) x $18/hr (including overtime).
Maintenance cost = 0.05 x (installed capital cost).
dWater cost = 25 gpm x 60 min/hr x 8,600 hr/yr x 0.001 make-up/total
x $0.30/(1,000 gal) x (1,000 gal)/l,000 gal.
eElectricity consumption (equations from Reference 40) and cost:
hydraulic horsepower = 50 ft x (1.0 specific gravity) x 25 gpm/3960.» 0.3157 hp
brake horsepower = 0.3157 hp x 745.7 W/hp x 8,000 hr/yr
x kW/l,OOOW + 0.65 pump efficiency = 2,900 kWh/yr
Cost - 2,900 kWh/yr x $0.049/kWh
fTaxes insurance, and administration cost » 0.04 x (installed capital
cost).
; ' "iGi'» M ' ''
9Capital recovery factor = 0.1627, for ,10 percent interest (before taxes)
and 10 year life.
E-48
-------
Table E-16. CAPITAL AND ANNUAL OPERATING COST ESTIMATION
PROCEDURE FOR CONDENSERS WITH REFRIGERATION
Item
Value
Capital Costs
Condenser
Installed cost, Dec. 1979
Installed cost, June 1980a
Installed retrofit cost, June 1980
Refrigeration
Installed cost, Dec, 1979
Installed cost, June 1980a
Total Installed Cost, June 1980
Annualized Costsc
Operating labor^
Maintenance materials & labor
Utilities
Electricity, pumping
Electricity, refrigeration
Coolant, make-up
Capital recovery!1
Taxes, administration
& insurance
Total annualized cost
without recovery credit
Styrene recovery credit
Net Annualized Cost
after recovery credit
From Figure E-6 for A
Installed cost, Dec. 1979 x 1.047
Installed cost, June 1980 x 1.065,
from Table 5-2
From Fig. E-7 for RC & Tcb
Installed cost, Dec. 1979 x 1.047
Sum of condenser and refrigeration
$1,080
0.05 x total installed cost
See footnote e
See footnote f
See footnote g
0.1627 x total installed cost
0.04 x total installed cost
Operating labor & maintenance
+ utilities + capital recovery
+ taxes, administration &
insurance
2767 x Ws x (% Red'n. * 100)
Total annualized cost - styrene
recovery credit
E-49
-------
Footnotes for Table E-16
ll'i'i,:1
aUpdated using Chemical Engineering Plant Cost index from December 1979
(247.6) to June 1980 (259.2).
. j. , .. ••' '' ,.', I&v'ih -\ . '!:j •.:: ••;<'•:.
"Costs for the 1 ton minimum refrigeration capacity can be approximated
by exp (exp[(0.60784 x In (hp/ton)) + 0.31169]) .,
t: ' ' ' ! ' '• •: ' ' •' ;• -:*w [:y.j: •'': :
cCost factors presented in Table 5-3.
dOperating labor cost = 1 hr/wk x 52 wk/yr x 1.15 (with supervision/without
supervision) x $18/hr (including overtime).
eUsing Equation 6-2, p. 6-3 in The Chemical Engineers' Handbook
(Reference 40) for V = 3 fps (for condensers with a heat transfer area
of 20 ft2 or less and 125 ft2) or 10 fps (for condensers with a heat
transfer area of 185 ft2), assuming a pumping height of 50 ft. and a pump
efficiency of 65%:
i", . II-. !!il '•':
50 ft x V x Vc
3960 gpm ft/hp
x 0.7457 kW x
Fp
8000 hr/yr
0.65 pump efficiency
x $0.049/kwh
" , i i i' i
where 7= specific gravity of coolant = p* 62.42 lb/ft3
(the density of water)
• I ' • I;IM si'[?,' •"]•,'' ""]""' ''i" '","'' • ."'
Vc = volumetric flow of coolant; equal's 94.5 gpm for
condensers with heat transfer area of 20 ft* OP
less; equals 472 gpm for condensers with heat
transfer area of 125 ft2; and equals 1,575 gpm for
condensers with heat transfer area of 185 ft?
f RC' x (hp/ton of refrigeration for TC)
0.85 compressor efficiency x 0.85 motor eTficiency
x 0.7457 KW x 8000 hr/yr x $0.049/kwh
hp
where (hp/ton of refrigeration) for a particular coolant temperature
is given on Fig E-7 for multiples of 20°F between -60 and + 40°F
or can be calculated from the curve fit:
i
(hp/ton) = exp [-0.1777 + 0.01503 (45-T)]
9For chilled water, assume 99.9% recycle:
@ 94.5 gpm x 60 min/hr x 8000 hr/yr x 0.001 make-up
x $0.30/1000 gal = $14/yr, ,
use $20/yr;
E-50
-------
Footnotes for Table E-16 (Concluded)
For ethylene glycol-water brine solutions and Freon-12, assume one
replacement per year of coolant in condenser and refrigeration system
and coolant volume in condenser and refrigeration twice that of condenser
alone.
Coolant volume, gal = A x 0.004128 ft2 x-sect./tube
x 7.48 gal /ft3 x (2 x inside
tube volume in condenser) *
0.2618 ft2 surf ace/ ft tube
= 0.2359 x A
For ethylene glycol-water brine solutions:
cost of coolant = Xw ($0.30/1000 gal) + X£G ($0.27/lb xpEG lb/ft3
* 7.48 gal /ft3)
= $0.0003 XN + $2.02
where: X = volume fraction of water in brine solution,
= volume fraction of ethylene glycol in brine solution
For Freon-i2 solutions:
cost of coolant = $8.70/liter x 3.785 liter/gal based on 20 liter
lot price of trichlorotrifluoroethane reagent price of $8. 73/1 Her
from Fisher Scientific Co. 1979.
n!0 percent interest (before taxes) and 10 yr. life.
""W., Ib styrene emitted/hr x 8000 hr/yr x (% Red'n in condenser * 100)
x 0.90, fraction of reduction recovered x $0. 3575/1 b styrene.
E-51
-------
io,ooo
1,000
03
•»J
•I—
Q.
•o
-------
1,000
o
o
o
(O
a.
to
O
(U
(O
-p
to
C
i.
CD
-Q
OJ
O
O)
Q
100 -
10 10O
Refrigeration Capacity - Tons (12,000 Btu/hr)
Figure E-7. Installed Capital Costs vs. Refrigeration
Capacity at Various Coolant Temperatures for a
Complete Refrigeration Section
1,000
Er53
-------
based on an equation in the Chemical Engineer's Handbook41 and simplified
as suggested by Chontos.42»43>44 The next larger size (inner diameter)
of schedule 40 pipe was selected unless the calculated size was within
10 percent of the difference between the next smaller and next larger
standard size. For flows of 700 scfm and greater,, duct sizes were
calculated assuming a velocity of 2,000 fpm for flows of 60,000 acfm
or less and 5,000 fpm for flows greater than 60,000 acfm. Duct sizes
that were multiples of 3-inches were used.
E.6.2 Piping and Ducting Cost Estimation Procedure
Piping costs were based on those given in the Richardson Engineering
Services Rapid Construction Estimating Cost System18 as combined for
70 ft. source legs and 500 ft. and 2,000 ft. pipelines for the cost
analysis of the Distillation NSPS.45 (see Tables E-18 and E-19)
Ducting costs were calculated based on the installed cost equations
given in the 6ARD Manual.46 (See Table E-20.)
Costs of source legs were taken or calculated directly from the
tables. Costs of pipelines for flares were intefpotated for the safe
pipeline lengths differing by more than 10 percent from the standard
lengths of 70, 500, and 2,000 ft. Installed capital costs were updated
to June 1980 using the Chemical Engineering pipes'!! valves, and fittings
index for piping and the fabricated equipment index forducting.
E-54
-------
Table E-17. PIPING AND DUCTING DESIGN PROCEDURE
Item
Value
(1) Pipe diameter, D
(a) Piping3
(b) Ducting13
(2) Pipe length, L
(a) Flares
(b) Incinerators
+ 0.472, for Q<40 scfm
+ 2.85, for 40 12 in. or Q>700scfm
and Q^ 60,000 acfm
D (in.) - (0.1915)7Q(acfm), for D >60,000 acfm
Select size that is a multiple of 3 inches.
Assumed 70-ft. source leg from each source
to the pipeline.
Assumed separate pipelines for large (>40,000 scfm)-"
intermittent streams and for all continuous
streams together. Selected pipeline length of
70, 500 or 2,000 ft. if calculated safe pipeline
length within 10 percent of standard length; if
not selected calculated length between
standard values.
Assumed 70-ft. source legs from each source
to the pipeline.
Used duct, fan. and stack cost from
Enviroscience,'° which assumes a 150-ft.
duct cost based on the CARD Manual
(Reference 46)
Economic pipe diameter equations from Reference 44 (which is based upon References 41
and 42).
From continuity equation Q= -| D2V; assumed velocity, V, of 2,000 fpm for lower flows
and 5,000 fpm for higher flows.
E-55
-------
to
co
j—
UJ
SS
1
O
O
CD
tgr
i— -i
0-
i— <
Qu
•
CO
1
UJ
0)
Of
\—
0
0
o
CsT
(U
"r™
"CD
Q.
Q-
H-
4->
£=
QJ
Q.
•r-
0
UJ
o
£_
c.
z:
o
CD
in
* — '
01
•1—
^—
0)
0.
•r-
D_
O
to
in
(U
s-
Q-
Q
tJ
(U
U
$-
o
CO
c
O) O)
cL >>
1^^
cr
UJ
CO CM CO O CSJ O
CM i-l O
CsJ
i— H CO rH »"* *Q CO ^^ "^ LO »•"* CD CD CM^
CSJ CSJ LO ^J" C«*
in
r-t r-l t-H CVJ
f-H r~1 l~H r^>«
10 M-
(0 CL)
O1CO CD
C ft-
Wr- 4->
10 OJ 4-> O) (U
Q) ^> *f^ -NX r™" '
tn > i— -i- to 3
o> to i— OJ (C > CZ3 X» <1)
r— > 5» «/> C r— J—
(Oi— S- CnO-O • «O r— OJ toCU-r-CtoSCO
v/* t._ (f^ ^ 53^ f~ QJ TD •*
O QJ "1^ Ci-XiaJ i — a> i— s- x o' • *• •!-•!—
C_>- CDCJCOUJI — U- Q UJ CQ 3T U_ Ci_
^*
^.
(U
0
c
O)
i.
O)
<*-
O)
o;
E
O
i-
u.
(TS
E-56
..:..1:;;;,..,:.:"' KJIILJ. j
,?' > "iiii!1 is?! ::H:i :.
i lini I
-------
(O
CO
CO
S
O
LU
_1
_J
A
CM
a>
O_
s_
o
10
o
o
CO
en
r>
r>
en
O)
&.
o
to
0)
(/)
O)
o
en
(U
a>
o
o
co
OJ
its
o
OJ
Q.
OlTJinOLOOOOLOOCDCDLOOOCDCDCDOir)
i i— t T- 11— i cvJ CM co «3-voco cne\i«3-co
OLrtCDCSlOOLOOUlCSOOLOOOOCDCDOLr)
r-lt-4 CM CM CO «d" LO
CZ><£>COI~»-
• CM CMCOLO COOCOO
~ CO CO LO CM
CM
«*Lf>»£>cocor-»oir>cr>cooJC3i^. LOCM •— i co
CD CO
OOOOOOOOOOOOO Or-ii— ii— ii— I
O
O
d)
O
CL
O
O
(U
It3
X)
LO
0)
u
c:
o>
O)
l»-
o>
a:
CL
•f—
Q.
ra
O
CL,
S-
01
O
oo
CL.
to
c
O
(C
^ CO
(/> OJ
•r- O
Q C
I O)
H-4 S-
S Q)
O M-
O (U
CO C£
O O
S- S-
E-57
-------
to
co
ec
»"^
ti_ |
f
O
J^
o>
C£
UJ
cn
!b»j
o
UJ
•t
CO
o
l_ 1
g
o-
UJ
t—
CO
o
tJ
C£3
le^
1— 1
1 ,
o
o
o
lit
U-I
—I
l_
CO
t—i
o
OJ
1
UJ .
•il
C to
QJ *f"
0.0
c
B
a
*
(.
a
*•
f±
2
It-
CD
c
u
c
LL.
(^
in
(C
z
>,
I—
CT
a
a)
a
•*—
0.
(U
—
OJ
o
O-
4J
»-
O
D
^
0)
C
I
O-
<£
s
— '
c.
o
V)
t/
t
c
s
0)
u
u
c
to
.0
*— >
C
p:~
2 t
0) C
0. •!-
1—
CM
CM O -H
»— * CTt CO
VI VI VI
o a a
VI VI VI
SO CVJ
n r- 1
CM CM
O CD
CM
a in CM
CO fO
co ^r CM
i£> . •
• f— 1 T"H
1— 1
+ +
* ° °
Ci
*-H Ol
CO C3 CD
r-* CTV CO
r— CM CM
CO
+ + +
r- to o
CO CM T-<
III
CM
o
CO CM
O LO O
CO
CO «Cf CM
to • ro
• i-1 CM
t-H *
•t- t-4
0 ° +
r**. f*^
CO
m to en
o «i- •
t— 1 CO CO
r*.
4- 4- to
CO CO 4-
m •
•• * o
r~ o oj
to oj <•
OJ OJ OJ
a a o
o r^ ^J-
o to r*.
to co •— i
t-H 1— 1 1-1
4-4-4-
o a o
in in !--
OJ CO to
cs co «a-
OJ v-t i-*
*^* OJ t-H
in in oj
O CD —1
i— * *-H »— 1
OJ
oj a oj
o o
CD
CD in to
OJ OJ r-l
a o o
CO OJ CO
to OJ tr>
cn in co
CO CO OJ
4-4-4-
*^ CO CO
r^- co cn
O O •-!
OJ OJ OJ
to
•<*• <-< CO
T-< CO >-<
T3
0)
C
!S
§
u
to
•a-
T
in c
c
n) o
•O 0)
M (O
in •»-
0) -o
01 C
U O) S-
3 r— Z3 4
•o JD in
+J™ Q)
J= S-
cn c: ci-
Io '*" c
S- = 0
+J S 0.
in o 3
in * o
4-> in x
cz to ••
0) in o
CO) in
O O- O)
o u
«5 i
o."~
•s. & i
i— a. z
(U
ai-c 14-
•»-> o o
in 10
0) 0) 1
c u
o c c ^
ja T- - T3 I
10 in c: v
U J-> 0) —
c o.
t- 0) 0) 4
OCX)
•*- 0
CL C7>
WE C
C 0 •!-
0 O C
4-> cn E
A3 C 10
3-i- X
era. 01
0).i-
a. t-
§01
&> 4_>
t- O H-
U_ 4-
4
1
• *>~»
i — i +•> cn
CL in
in o.
X •
i-t O
^J- 1-1 t— 1
• 1
CD Al O
O
4- •
r— i o i*- E
O O I*—
• i- (O
CD in o
a. CD o
X O CD
r~- -o
CD • CD *
CD "3- CO O
OJ «t-- .. CO
* C Al
CO S Al V
^-1 O CD"
i — i c a. o-
OJ Jk! i-
1 — 1 S- O 1-
in o <4- o
a *- 14-
* =
s IO c
•^ a> •* »-H co
= 3t-l CO >-H
— in
— in II II II
£
CL
S-
OJ
t/}
(U
in *a
Q 0)
O E
13
J- in
O
-------
E.7 REFERENCES FOR APPENDIX E
1. Kalcevic, V. Control Device Evaluation: Flares and the Use of
Emissions as Fuels. In: Organic Chemical Manufacturing Volume 4:
Combustion Control Devices. U.S. Environmental Protection Agency.
Research Triangle Park, N.C. Publication No. EPA-450/3-80-026.
December 1980.
2. Reference 1, p. IV-4.
3. Memo from Sarausa, A.I., Energy and Environmental Analysis, Inc.
(EEA), to Polymers and Resins File. May 12, 1982. Flare costing
program (FLACOS).
4. Telecon. Siebert, Paul, PES with Straitz, John III, National Air
Oil Burner Company, Inc. (NAO). November 1982. Design, operating
requirements, and costs of elevated flares.
5. Telecon. Siebert, Paul, PES with Fowler, Ed, NAO. November 5,
1982. Purchase costs and operating requirements of elevated
flares.
6. Telecon. Siebert, Paul, PES, with Keller, Mike, John Zink Co.
August 13, 1982. Clarification of comments on draft polymers and
resins CTG document.
7. Telecon. Siebert, Paul, PES with Fowler, Ed, NAO. November 17,
1982. Purchase costs and operating requirements of elevated
flares.
8. Memo from Senyk, David, EEA, to EB/S Files. September 17, 1981.
Piping and compressor cost and annualized cost parameters used in
the determination of compliance costs for the EB/S industry.
9. Memo from Mascone, D.C., EPA, to Farmer, J.R., EPA. June 11,
1980. Thermal incinerator performance for NSPS.
10. Blackburn, J.W. Control Device Evaluation: Thermal Oxidation.
In: Chemical Manufacturing Volume 4: Combustion Control Devices.
U.S. Environmental Protection Agency, Research Triangle Park,
N.C. Publication No. EPA-450/3-80-026, December 1980.
Fig. III-2, p. III-8.
11. Reference 10, Fig. A-l, p. A-3.
12. Air Oxidation Processes in Synthetic Organic Chemical Manufacturing
Industry - Background Information for Proposed Standards. U.S.
Environmental Protection Agency, Research Triangle Park, N.C.
Draft EIS. August 1981. p. 8-9.
13. EEA. Distillation NSPS Thermal Incinerator Costing Computer
Program (DSINCIN). May 1981. p. 4.
14. Reference 10, p. 1-2.
E-59
-------
i ,.,'jm.: jiii-'
15. Reference 12, p. G-3 and 6-4.
16. Reference 10, Fig. V-15, curve 3, p. V-18.
17. Never-ill, R.B. Capital and Operating Costs of Selected Air
Pollution Control Systems. U.S. Environmental Protection Agency,
Research Triangle Park, N.C. Publication No. EPA-450/5-80-002.
December 1978.
18. Richardson Engineering Services. Process Plant Construction Cos
Estimating Standards, 1980-1981. 1980.
19. Telecon. Katari, Vishnu, Pacific Environmental Services, Inc.
with Tucker, Larry, Met-Pro Systems Division. October 19, 1982.
Catalytic incinerator system cost estimates.
20. Telecon. Katari, Vishnu, Pacific Environmental Services, Inc.,
with Kroehling, John, DuPont, Torvex Catalytic Reactor Company.
October 19, 1982. Catalytic incinerator system cost estimates
"•'" . . , i . •• I- / , ' . :<[,;,' ,! i1 • j,i",s" '••< - i
I " , , ,•'.'..•.',• '.i , ••.': , idlii K..'1;1 j'i V •
21. Letter from Kroehling, John, DuPont, Torvex Catalytic Reactor
Company, to Katari, V., PES. October 19, 1982. Catalytic incinerator
system cost estimates.
22. Key, J.A. Control Device Evaluation: Catalytic Oxidation. In:
Chemical Manufacturing Volume 4: Combustion Control Devices.
U.S. Environmental Protection Agency. Research Triangle Park,
N.C. Publication No. EPA-450/3-80-026. December 1980.
23. Telecon. Siebert, Paul, Pacific EnvironmentalServices, Inc., _'
With Kenson, Robert, Met-Pro Corporation, Systems Division. July 22,
1983. Minimum size catalytic incinerator units.
' • li . . j f: , ' ' " ' ", ii'niili i ',' l,''l, , 'i < i, ! HI, ' ' »,, ', I' -I i,1 'i '<
^ ' . '.ILj-filit. i ," -.' ::;'.". v:.. .'.:,• t1,,, -i:..'^ 'i'-l
24. Steam: Its Generation and Use. New York, Babcock & Wilcox Company,
1975. p. 6-10.
25. Reference 10, Fig. V-15, curve 3, p. V-18.
26. Perry, R.H. and C.H. Chilton, eds. Chemical Engineers' Handbook,
fifth edition. New York, McGraw-Hill Book Company. 1973. p. 3-59
27. Rossini, F.D. et al. Selected Values of Physical and Thermodynamic
Properties of Hydrocarbons and Related Compounds, Comprising the
Tables of API Research Project 44. Pittsburg, Carnegie Press,
1953. pp. 652 and 682.
28. Reference 26, pp. 10-25 through 10-28.
29. Reference 26, pp. 10-12 through 10-15.
30. Reference 26, pp. 11-1 through 11-18.
.ill I! ":"!!: "I",III I
I
• M1! "i-a.
E-60
-------
31. Reference 26, pp. 3-191, 3-212 through 3-214, and 12-46 through
12-48.
32. Weast, R.C., ed. Handbook of Chemistry and Physics, fifty-third
edition. Cleveland, The Chemical Rubber Company. 1972. p. E-26.
33. Erikson, D.G. Control Device Evaluation: Condensation. In:
Organic Chemical Manufacturing Volume 5: Adsorpiton, Condensation and
Absorption Devices. U.S. Environmental Protection Agency, Research
Triangle Park, N.C. Publication No. EPA-450/3-80-027. December 1980.
p. A-3.
34. Reference 26, pp. 3-71, 3-206, 3-213, and 3-214.
35. Kern, D.Q. Process Heat Transfer. New York, McGraw-Hill Book
Company, 1950. p. 306.
36. Telecon. Katari9 Vishnu, Pacific Environmental Services, Inc.,
with Mr. Ruck, Graham Company. September 29, 1982. Heat exchanger
system cost estimates.
37. Telecon. Katari, Vishnu, Pacific Environmental Services, Inc.,
with Glower, Dove, Adams Brothers, a representative of Graham
Company. September 30, 1982. Heat exchanger system cost estimates.
38. Telecon. Katari, Vishnu, Pacific Environmental Services, Inc.,
with Mahan, Randy, Brown Fintube Company. October 7, 1982. Heat
exchanger system cost estimates.
39. Reference 33, pp. A-4 and A-5.
40. Reference 26, p. 6-3.
41. Reference 26, p. 5-31.
42. Chontos, L.W. Find Economic Pipe Diameter via Improved Formula.
Chemical Engineering. 87(12):139-142. June 16, 1980.
43. Memo from Desai, Tarun, EEA, to EB/S Files. March 16,' 1982.
Procedure to estimate piping costs.
44. Memo from Kawecki, Tom, EEA, to SOCMI Distillation File. November. 13,
1981. Distillation pipeline costing model documentation.
45. EEA. SOCMI Distillation NSPS Pipeline Costing Computer Program
(DMPIPE), 1981.
46. Reference 17, Section 4.2, p. 4-15 through 4-28.
E-61
-------
-------
APPENDIX F
CALCULATION OF UNCONTROLLED EMISSION RATES
AT SPECIFIC COST EFFECTIVENESSES
F-l
-------
APPENDIX F.
CALCULATION OF UNCONTROLLED EMISSIONRATES
AT SPECIFIC COST EFFECTIVENESSES
• : ' ; (.;..,, ' ' ill I i : -, - . , ,. ,, . i i
This appendix details the procedures used to calculate the uncontrolled
emission rates equivalent to $1,000 per Mg, $2,000 per Mg, and $3,000 per Mg
when RACT is applied. Section F.I describes the procedures for flares,
thermal incinerators, and catalytic incinerators. Section F.2 describes the
procedures for condensers. ;
F.I. PROCEDURE FOR INCINERATION DEVICES
For the polypropylene and high-density polyethylene model process
sections, the question asked was what uncontrolled VOC emission rates when
reduced 98 percent (i.e., RACT level) corresponded to cost effectivenesses of
$1,000 per Mg, $2,000 per Mg, and $3,000 per Mg. fne foil owing sections
describe the procedures used to calculate these uncontrolled emission rates.
F.I.I General Procedure
The general procedure used is as follows:
First. For each process section identified in Tables 4-1 and 4-2,
the emission characteristics identified in Chapter 2 of the CTG and Chapter 6
of the background information document for the polymer manufacturing industry
J , ... i
and the control costs identified in Chapter 5 of the CTG were used as the
starting point. Table F-l summarizes the pertinent information.
Second. Uncontrolled emissions were adjustedproportionally by changing
volumetric flow proportional to the initial flow. Concentration of the
emissions was assumed to remain constant. Uncontrolled emissions needed to
be adjusted downward or upward depending upon the initial cost effectiveness.
For example, if the initial cost effectiveness was $l,500/Mg, the uncontrolled
emissions would be higher than the initial uncontrolled emissions in order to
j
correspond to $l,000/Mg and lower than the initial uncontrolled emissions in
order to correspond to $2,000/Mg and $3,000/Mg.
Third. Annual costs were adjusted to take into account the new flow
i ' ' ..'>.( ,.•' '.[Jir:1 ;..•!; '« , I',!1," •'•! •' 'I "' '••) II' I". ."i:V Ml!';;
conditions, which affect control device costs. Annual costs were divided
into three components: (1) those related to'"capital costs (C^, (2) those
related to operating costs (C2J, and (3) minimum and/or constant costs
F-2
tCii ( I
-------
a;
o
LL.
00
1 —
oo
o
o
_1
o
Q£ OO
1— UJ
CD ^t
C_5 C£
Q 2:
z: o
oo
oo oo
O i— i
1 — 111
oo
I— I Q
C£ LU
UJ _J
1— —1
0 O
cC rv
ce: h-
-C O
O O
2S — *
o
i — i U_
00 O
oo
1 — < ^
s: o
LU I-H
I—
— •! *^C
=^
h- C_3
' — 1 — 1
r""
1
LL.
M^
jQ
rd
1
r™
u
tn
{/I
0)
I flj CT
•M > E:
t/J -i- **-*
o u
OJ
u-
(4-
UJ
CO to
CO •»
tf> ~^,
to o
o
co tn
CO CU
0 C
s2
c:
•t- cu
5 -^
3
w in
^
**—
u
c/)
„
|
!Z
CO CU
o c
£- •!—
O _1
m
c
4^ O
•*- CU <-
E cn a.
-< O CO
CM CM CO —i
*— 4 .
CO to
CO CM -0
— < m *s- co
O »-t O CO
CM co in
r-4 to
CM
CM tr>
to r-~ to*o
C3 r-t tf m
o r~- co to
«3- CO
CO
O *3- O t—
r~t P^* CO tO
in CM co
CO •— 4 O CM
cn -H CM
f— t «3- r~4
""
o o to
O f O CM
CO
a.
E: ce ^ u_
cu
c
cu
a.
o
L.
a.
o
a.
co o
co '
co m
co r-~
cn
•3- O
in o
cn to
I*-- r-H
•a- o
o «a-
Cn r-4
cn to
CM in
T3
a\ to
V •
CO «•
o in
CM r-.
co-0
to in
cn .-4
to in
CM
co r-
*— 4 CO
CM
to cn
O CM
cn
to''
o'
1 — ^3-
CM O '
*y* 1 1
*£• i*,
>^ 03
••— CU
OO i
CU .C
O 4^
1 >
O>i—
— o
:c Q-
> O
t- 10
cu -a
o cu
O JT
CU 4->
13
i — £Z
10 IO
CU 1—
->-> o
§ cu
II -u
•y -f— •
CO
• -co c
CO) O
o *^* *^~
•f- 4J CO
4J ' -f- 00
O U -t-
(O (O S
CU Q. CU
t- a
U r—
C 10
O *J 3
•i- C C
4-> 03 Er
(O i — 03
M a.
f— r— CU
E ~O r—
2 %. t
O -4->
cu »- c . :
o o
.11 0
o c
a; -i- 3
(O 't -
... I_ O
c
o o c •
•»— 4J O t_
ttj >K 4^ ItJ
t. r— • O
CL O Q. t3 . O
£ £ •£ £ U
CL *^~ » OJ 3
a_ Of— tn o
eg. u. o. co LL.
ta jQ O T3
F-3
-------
fl !"'!:, i,.:1,;!"! !! Ilil'SIM1!",
I
;'! ^iORI'
Table F-2 summarizes these costs for each of the two polymers. The annual
costs were adjusted as follows:
o Capital-related costs, C]_, were adjusted using the equation
i0'6 where: Vj = total initial volume of flow from model process
section and
Vx = adjusted flow rate.
o Operating-related costs, C2, were adjusted using the equation
^ ' ', . '. , '. ' ', ' „, .,'.2',
Capital-related costs included capital recovery", maintenance,
1 , ,; ' , ,,!«„ "», ' ! 'I1 r , i ! • • , " „ ' .' | " „• "« : " ,•!! -'hi I
taxes, insurance and administration charges. Operating-related costs
included utilities (e.g., natural gas, steam, electricity). Operating
labor was assumed to be constant. \
Fourth. As flow rates vary, the size of the control device required
will also vary. No matter how small the flow, however, there are
certain minimum size control devices available; thus, control device
costs do not approach zero as flows become very small. In addition,
some utility requirements, such as natural gas purge rates, may be
constant, or even increase as flow rates become increasingly smaller.
Finally, a different control device design may be more cost effective
as flow rates change. For example, as flow rates approach 1.46 sefm
(70°F), a change in flare design was assumed to occur where a flare
with a fluidic seal was used for flows less than 1.46 scfm. Table F-3
summarizes the basic minimum costs associated with the various control
devices at flow rates that affect design criteria. i
Fifth. Using the above information and procedures, the following
basic equation was solved for Vx for each process section:
c. /Vx\0-6 + C^'/Vx',. ~,
3 = $l,000/Mg; $2,000/Mg;
— and $3,000/Mg
where:
C1 = the difference between the capital-related costs of
1 the control device controlling V-^ and the capital-related
costs of the control device controlling V2-
F-4
-------
oo
r"~~
t=ft- GO
0
•> o
GO
^— 1
GO <=t
O =D
o z. .
4 5
z.
CO
t/l O
o
o
-Q
co
+j
__
1 CM
EDO
f- 1^^'
to
CO
CL
-o
CU
re
1 <~~4
r- O
«3
Q.
US .
frt
> C
) O
CU -r-
O 4-5
0 0
t_ CO
Q- GO
••'• :
CO
p^
0
CL.
CO CO
i— i en
«^~ r —
A A
O .-4
CM CM
0 O
<£> 'O
t— < r-H
«s «\
r— 1 r- 1
^t" CT»
CM CO
A 0t
"^ "^
: VO O
cr> co
»^- to
Q.
s:
cn » — i
o to
«?J* ^^
*X A
CM CM
0 0
-H 1— 1
en o
t en
°o, o
»— H |^^
r-l CM
CO LO
P~- LO
OL
0 0
r- 1 F-,
LO r^
CO 0
t-l CO
t-H r-H
o o
0 0
vo , CU
+-> c:
•r- CO
t/) 1 —
£J?
Q -(->
1 CO
• -^ ^->
•r- 'o
:n CL.
o
o
t.
Cu
11
^
0
•r—
4-5
O
fl3
CO
£_
O
•r—
«
N
'^
CO
s
'o
CL
II
o;
a.
c
o
fO
£_
res
a.
CO
L-
Q.
5
CO
£=
S 0)
rt3 C
i- •*-
II en
Q. c
s: T-
F-5
-------
;?
Table
Control
Device
Flare, within
line
Flare, across
lines
Thermal
Incinerator
- within
line
- across
lines
Catalytic
Incinerator
- within
line
- across
lines
F-3.
Flow,
scfm
1.49
1.46
0.81
0.03
1.49
1.46
0.81
0.03
32.19
96.58
754.6
150
500
150
BASIC MINIMUM COSTS
',. ' .';,. '.;
Capital -Related
4,887b
4,964d
4,964d
4,964d
6,208b
d,304d
6,304d
6,304d
1,
75,240
78,000
i'"
42,260
37,260
45,480
43,060
1 i : ,',
t . ' ' , 1; ! '- .'
if, ', ,• i
AT VARIOUS FLOW
', ANNUAL CSSJS, $
Operating-Related
in i i :
4,276C
4,276C
4,276C
4,276C
4,276C
4,276C
4,276C
4,276C
: • . " l! " '. ' ! ' • "'
55
160 ;:
,, , .. ,
3,940
i,470'i:'""
'', , , v i " 1 ' ' ,1
2,620
1,730'
• ""• ' ' , „ ' ' i1"'
RATES3
- '-
Constant
11,160
11,160
11,160
11,160
11,160
11,160
11,160
11,160
21,600
11 " I!'1" "'
21,600
16,700
16,700
1 «" ,
16,700
16,760'
11 !| I1! /Iji'.'!'!^!!!:!^'!^1!!1!!!''! Hill
,' ' "•••! f«f ' -ii
1 III
Total
•'' I
'•.f,11
26.323C
26,400C
20,400C
20,400C
2^,644°
2i,740c
2l,740c
21.74QC
'i ' 1
96,895
''' |M !"
99,760
- ' ; ' JJ ' i1
62,900
'55,430 '
64,800
61,490
. '••
I'liejiis:
- f ''
i a
,1 . " i • ••< ', ' .. M'tl ',. ••!• , I .""'II i, I
The minimum costs for flares are based on a single emission stream (i.e., one source leg); per
process section. If more than one emission stream emanates from a process section, then 'minimum
capital costs will be higher than those reported in the table. The increase in capital-related
costs is about $690 per additional source leg at 1.49 scfm and about $670 per additional^source
leg at lower flows. The minimum incinerator costs are specific to the process sections for
which they were costed. >
Flare without a fluidic seal. ' ' '
CAdd steam costs at 1.49, 1.46, 0.81, and 0.03 scfm. Actual cost is dependent on molecular weight
of gas stream and weight percent of VOC.
d
Flare with fluidic seal.
F-6
-------
C2
c1
3
= the difference between the operating-related costs for
the control device controlling V-^ and the operating-
related costs of the control device controlling V2«
= the minimum costs associated with controlling V£.
C' = the difference in emission reduction associated with
4 controlling emissions at V-^ and emissions at V£.
C' = the emission reduction at V?.
5
V = the initial, or higher, flow rate.
V = the flow rate at the lower end of the design range.
Vx = Flow rate to be solved for.
Table F-4 summarizes the coefficients used in the calculations.
Sixth. Once the flow rates were found, the uncontrolled emission
rates were calculated by the following equation:
Vx x ER
where:
Vx = flow rate at $l,000/Mg ($2,000/Mg., $3,000/Mg)
Ml = initial flow rate from process section
ER = initial uncontrolled emission rate.
Table F-5 summarizes these results.
F.2. PROCEDURES FOR CONDENSERS
In calculating the uncontrolled emission rates for polystyrene,
the general question that was asked was: What uncontrolled emission rate,
when controlled to 0.12 kg VOC per Mg of product (i.e., to the RACT level),
yields a cost effectiveness of $1,000 per Mg ($2,000 per Mg, and $3,000
per Mg)? This is slightly different from incineration where, regardless
of the uncontrolled emission rate, 98 percent VOC reduction was assumed.
For polystyrene, the effective percent emission reduction varies as the
uncontrolled emission varies. The following paragraphs detail the
procedures used to calculate the uncontrolled emission rates associated
with the three cost effectivenesses.
F-7
-------
Table F-4. SUMMARY OF COEFFlCtelts
Cost
Process Effectiveness, Coefficient
Polymer Section S/Hg Vj. V2 q ^2 C3
Polypropylene 1.00°
- within line RHP 2,000
3,000
1,000
PR 2,000
3,000
1 ,000
MR 2,000
3,000
0.81 0.0627 0 212 20,418
0.81 0.03 0 114 20,404
0.81 0.03 0 138 22,415
\ '" 1 000
PF 2,000
3,000
- across lines 1.00°
886.3 32.19 20,160 1,455 96,895
0.81 0.188 0 177 21,793
RHP slooo 0.188 0.03 0 44 21,749
1,000 1.46 0.81 0 95 21,858
PR 2,000
3,000
• i ,000
MR 2,000
3,000
1,000
PF 2,000
3,000
0.81 0.03 0 114 21,744
i, ' , "'. ,''",.' i' i , "' ,
1.46 6.81 0 IT3 27,916
0.81 0.03 0 138 27,778
! • "„ ::,; ";;,: ; '
2658.8 96.58 26,640 4,370 99,760
1 ; i "" • "' •.<" '. « ;;, .'"4 .if i 11! IS1, • I ;" :,,"
High-Density
Poly^htylene
-within line 1,000 69-63 l.« 2,349 6,099 20,456
m 2>00° | 0.81 0.03 0 69 20,403
3,000 >
[ j " i ;' ! , ':, "'I1,!1'. i'1 "'! ' " ' "
1,000 1754.6 251.5 4,370 2,390 '' 56 1 140'
PF 2>°°° I 251.5 150 630 80 55,430
3,000 )
1,000 208.9 1.49 7,555 18,565 ' 21,834
MR 2,000 1.46 0.81 0 59 21,812
3,000 0.81 0.03 0 69 21,743
- across lines
1,000 754.6 500 5,480 1,320 64,800
PF 2 ,000 ]
(500 150 2,420 890 61,490
3,000 ) , : ;, .
c\ .,;.
38.428
20.376
24.796
• • •
115.406
32
8.129
16.985
20.376
24.796
346.218
.;; „ ' | i ',
868.41
9.94
i:i' hi ,i r.iii , ,:!",
56.738
11.449
2,644.45
8.29
9.94
28.728
39.493
°f
3.224
0.I784
0.:954
4J35
9*67
1,5435
21,16
01784
'i
0.954
13.05
1EJ.99
0.38
281 .369
15.92
18.99
10.32
0.38
56.418
16.925
F-8
-------
Table F-5. SUMMARY OF COST EFFECTIVE FLOWS AND EMISSION RATES,
POLYPROPYLENE AND HIGH-DENSITY POLYETHYLENE PLANTS
Polymer
Polypropylene
- within line
- across lines
High-Density
Polyethylene
- within line
- across lines
Process
Section
RHP
PR
MR
PF
RMP
PR
MR
PF
MR
PF
MR
PF
Cost
Effectiveness
1,000
2,000
3,000
1,000
2,000
3,000
1,000
2,000
3,000
1,000
2,000
3,000
1,000
2,000
3,000
1,000
2,000
3,000
1,000
2,000
3,000
1,000
2,000
3,000
1,000
2,000
3,000
1,000
2,000
3,000
1,000
2,000
3,000
1,000
2,000
3,000
Vx * VX
0.3989
0.1989 0.0627
0.1325
0.7852
0.3915 7.175
0.2608
0.7088
0.3535 43.46
0.2354
875.85
406.39 886.3
262.67
0.4249
0.2119 0.188
0.1411
0.83665
0.4172 21.526
0.2779
0.8785
0.438 130.4
0.29175
841.6
398.4 2,658.8
259.35
1.6095
0.8033 69.63
0.535
537.4
248.8 251.5
164.38
1.7245
0.856 208.9
0.5701
608.4
279.9 754.6
133.67
Uncontrol led
Emission
x ER = Rate
0.445
0.07 0.222
0.1479
0.445
4.1 0.222
0.1479
0.489
30 0.244
Ovl62
2.569
2.6 1.192
0.771
0.1582
0.07 0.0789 .
0.0525
0.1582
4.1 0.789
0.0525
0.2021
30 0.1007
0.0671
0.823
2.6 0.389
0.254
0.2936
12.7 0.1465
0.0976
0.8675
0.406 0.4016
0.2654
0.1048
12.7 0.052
0.0347
0.3273
0.406 0.1506
0.0988
Annual
Emissions
(x relevant
capacity)
20.93
10.44
6.95
20.93
10.44
6.95
22.996
11.468
7.637
120.74
56.02
36.237
22.31
11.12
7.41
22.31
11.12
7.41
28.497
14.21
9.464
116.04
54.849
35.814
20.93
10.45
6.96
61.85
28.63
18.92
22.44
11.14
7.42
70.04
32.23
21.14
F-9
-------
'f Si?:1 'Wi If " ITS '1;:':'';!•
F.2.1 Styrene-in-Steam Emissions
. - . , ,•. , , , ,:,' , . ,. >,
The basic equation for calculating cost effectiveness is" as"as follows:
(1) CE = AC - (0.9 ERed x RC)
ERed"
where: CE = cost effectiveness, $/Mg
AC
iil*!.
= annual!zed cost of condenser to reduce uncontrolled
emissions to 0.12 kg VOC/Mg product, $/yr
RC = recovery credit, $/Mg, = $0.788/kg of styrene !
0.9 = efficiency of actually recovering the styrene
from the condenser
ERed = annual emission reduction from uncontrolled
to 0.12 kg VOC/Mg product, Mg/yr
For polystyrene, we are already dealing with a minimum-size condenser
and operating requirements (which were assumed constant) when the
uncontrolled emission rate is at 3.09 kg VOC/Mg product. In order to
get a cost effectiveness of $1,000 per Mg, a smaller uncontrolled
emission rate is needed. Thus', annualized costs associated with
polystyrene are a constant - equal to $8,300.
Emission reduction, in general, can be calculated with the
following equation:
(2) ERed = (Emission Rate x Capacity) - (0.12 x Capacity)
Capacity is given: 36.75 Gg for a process line and 73.5 Gg
for the plant. Thus the above equation reduces to:
For single process line:
(3) ERed = (ER x 36.75) - (0.12 x 36.75)
= 36.75 ER - 4.41
For two process lines:
(4) ERed = (ER x 73.5) -(0.12 x 73.5)
= 73.5 ER - 8.82
F-10
-------
Inserting the above information into the general cost-effective equation
(1), the following equation is derived:
For a single process line:
(5)
= $8,300 - [36.75 ER - 4.41] (0.9) [$788/kg]
(36.75 ER - 4.41)
For two process lines:
(6) CE = $8.300 - [73.5 ER - 8.82] (0.9) [$788/kg]
(73.5 ER - 8.82)
As we know CE (i.e., $l,000/Mg; $2,000/Mg; or $3,000/Mg), we can
solve directly for ER. Simplifying the above equations (5 and 6), we
get:
For a single process line:
(7) ER = 11, .428 + 4.41 CE
26,063 + 36.75 CE
For two process lines (i.e., the model plant):
(8) ER = 14.555 + 8.82 CE
52,126 + 73.5 CE
Substituting $l,000/Mg, $2,000/Mg, and $3,000/Mg into the last two
equations (7 and 8), yields the following results:
Emission Rate, kg VOC/Mg Product
$l,000/Mg
$2,000/Mg
$3,000/Mg
Single Line
0.2521
0.2034
0.1809
Two Line
0.1861
0.1617
0.1504
F.2.2 Styrene-in-Air Emissions
As with styrene-in-steam emissions, the basic equation for calculating
cost effectiveness is as follows:
F-ll
-------
(9)
CE = AC - (0.9 ERed x RC)
ERed
where:
CE =
AC =
0.9 =
ERed =
RC =
cost effectiveness, $/Mg
annualized costs, $/yr
efficiency of collecting recovered styrene
annual emission reduction, Mg/yr
recovery credit, $/Mg of styrene recovered
In calculating the cost effectiveness numbers and the uncontrolled
emission rates for the "across line" analysis, costs were initially
developed for two uncontrolled emission rates: 0.2 kg VOC/Mg product
and 0.15 kg VOC/Mg product. The resulting costs are summarized in
Table F-6. ' | ' ' ' ' V^,/ |/" ." '
As seen in Table F-6, the uncontrolled emission rates associated
with $l,000/Mg, $2,000/Mg, and $3,000/Mg lie between 0.2 and 0.15 kg
VOC/Mg product. Using the general equation (9) above and assuming that
refrigeration electricity and recovery credit vary proportionally with emission
rate, the following equation is developed:
111 ', II II1'! K iHI" ill!1"1 •'
where: AC' = Constant costs associated with an uncontrolled emission
rate of 0.15 kg VOC/Mg product
RElec = Refrigeration electricity associated with an uncontrolled
emission rate of 0.2 kg VOC/Mg product
RElec1 = Refrigeration electricity associated with an uncontrolled
emission rate of 0.15 kg VOC/Mg product
RC
RC1
ERed
= Recovery credit, $/yr, associated with an uncontrolled
emission rate of 0.2 kg VOC/Mg product
= Recovery credit, $/yr, associated with an uncontrolled
* Annual emission reduction associated with an uncontrolled
emission rate of 0.2 kg VOC/Mg product
ERed1 = Annual emission reduction associated with an uncontrolled
emission rate of 0.15 kg VOC/Mgproduct
ER = Emission rate to be solved for,, kg VOC/Mg product
F-12
-------
oo
o
*— H
oo
oo
*-H
^p-
UJ
a;
HH
^^
i
^f
— ^
H— 1
UJ
3S»*
LU
o:
oo
o
u_
1 —
oo
o
o
o;
1—
tezL •
o
to
1
u_
CD
| —
cfl
i
o e 2:
4-> »«-> *«*
O U- •!-
O LU 4J
TO
C
,— C 0
rO O "- C.
3 ••-*>>,
C (/> O
C (/) 3 O>
^C •••" ^J Z
1. 1 Q£
"io
4^
O
1—
«t
t/1
4J
(/I
O
0
s
f^
(O
3
C
C
<:
-a
o ai
u t-
3 C
1 13
a i—
^£ 0
n o
E 0
U
i^
0) LU >,
cn jj
C- O U
O£ 1o +J
O
OVi—
c- ^
5. o
E (U >%
3 ^— 4J
Q. UU -r-
1
0)
-U 01
c u
•F- C
s: c
t_
o
n3
_J
•a o
o ^— en +J ^,
o o •!- UT)
CO 00 CO
1 — O ^*
1 » •.
cvj r*.
I r^-
1
o o o
to ^o r-*
CV CM CO
un LO LO
t— t
o o o
cri m
r-H *-H U3
O LT) 0
^-l »-< ,-4
CO
CO
000
UT5 Lf> CO
CM
o o o
CM CM CVJ
UD to f^.
^-4 r-t «$•
O O O
CO CO r-v
O o r—
r-i ^( LO
i— i
LO CTl
r-H CM O
O O CO
cz
•r- (/I
-£=
U
3
O
L_
a.
o»
s:
cj
o
r>
C7>
^
CM
r- 1
O
O
(O
F-13
-------
Substituting the values from Table F-6 into equation 10 and then
simplifying* yields the following equations:
' ' "j ' • ' ' i' fit " ' ' ' '
For across lines:
(11)
= 16.065 - 52.000 ER
73.5 ER - 8.82
For within line ($3,000/Mg only):
(12)
CE = 12.950 - 26.000 ER
36.75 ER - 4.41
Solving for ER, equations 11 and 12 become:
For across lines:
(13)
ER = 16.065 + 8.82 CE
52,000 + 73.5 Ch
For within line ($3,000/Mg only):
(14)
ER = 12,950 + 4.41 CE
26,000 + 36.75 CE
For within line uncontrolled emission rates equivalent to $l,000/Mg
and $2,000/Mg, the calculations are complicated by the changing size of
the condenser. (All previous condenser calculations assumed the use of
a minimum size condenser). A cost-effectiveness equation was developed
to calculate the particular uncontrolled emission rates; which are
known to lie between 3.09 kg VOC/Mg product and 0.2 kg VOC/Mg (see last
column in Table F-6).
To start developing this equation, we know that at minimum the
costs and emission reduction are equivalent to those when the emission
rate is 0.2 kg VOC/Mg product. These' numbers provide a base, or minimum,
from which to start. In addition, we know that at most costs and i
emission reduction are equivalent to those when the emission rate is;
3.09 kg VOC/Mg product. The primary calculation is to determine how
costs vary from the minimum (i.e., at 0.2 kg/Mg) to the maximum (i.e.,
at 3.09 kg/Mg). We know that emission reduction, and, thus, recovery
credit, is proportional to the emission factors; that is, there is a
linear relationship between emission factor, emission reduction, and;
recovery credit. However, the annualized costs associated with increasing
F-14
-------
condenser sizes are not necessarily linear. Therefore, we assumed that
the costs varied exponentially with the ratio of the emission factors
between the costs at 3.09 kg/Mg and 0.2 kg/Mg. The exponents were
calculated using the following equation:
(15) exp -
- 0.12 \
- 0.12 I
where: AC^ = the relevant annualized costs associated with ERi
AC2 = the relevant annualized costs associated with ER2
= 3.09 kg VOC/Mg product
= 0.2 kg VOC/Mg product
The annualized costs were grouped as follows: (a) capital related
(maintenance, taxes, insurance, administration, and capital recovery
charge, (b) labor, (c) pumping electricity and make-up coolant, and (d)
refrigeration coolant. Table F-7 summarizes the costs and resulting
exponents.
Using the exponents from Table F-7 and the costs from Table F-6,
the following cost-effectiveness equation was developed:
(16)
(23,870 - 8>
CE =
8,170 + (15>770 .
t 15 - (77,485 - 2.
- 2,085
1.46
where: (23,870 - 8,170)
/ ER - 0.2 \
13.09 - 0.2J
= Incremental maintenance,
taxes, insurance, etc.
costs associated with an
uncontrolled emission
rate (ER) higher than
0.2 kg VOC/Mg product, $
F-15
-------
Table 7. EXPONENTS USED FOR CONDENSER WITHIN
LINE ANALYSIS, $1,000/Mg and $2,000/Mg
Item
Maintenance
Taxes, Insurance,
Administration, and
Capital Recovery
Labor
Pumping Electricity
and Make-up Coolant
Refrigeration
Electricity
Recovery
Credit
Emission
Rate
3.0^
0.2
3.09
0.2
1
V ! , • ,„ '•
3.09
0.2
3.09
0.2
3.09
0.2
i " « " T
Annuali zed
Cost Exponent
23,870
0.297 =0.3
8,170
15,770
0.742 = 0.75
1,080
2,875 6.455 =0.46
555
2,310 1.393 = 1.4
15
77,485 1.00 = 1.00
2,085
• l.l iilr „,! isi, ;".", • .: .,11.1 !il, .. ,;'!<;. . .
F-16
,.;„«!' • .J1.
-------
8,170 = Minimum maintenance, taxes,
etc. costs at 0.2 kg VOC/Mg
product, $
(15,770 -
(2,875 - 555)
1,080)/ ER - 0.2 V
\3.09 - 0.2/
X 1,080 '
= Incremental labor costs, $
= Minimum labor costs, $
/ ER - 0.2 \0-46 = in
13.09 - 0.2J el
' ' r-r\
= Incremental pumping
ectricity and make-up
coolant costs, $
555 = Minimum pumping electricity
and make-up coolant costs, $
(2,310 - 15)
/ ER - 0.2 \1-'
\3.09 - 0.2J
= Incremental refrigeration
costs, $
(77,485 - 2
,085)/ ER - 0.2\
\3.09 - 0.2J
15 = Minimum refrigeration costs, $
= Incremental recovery credit, $
2,090 = Minimum recovery credit, $
106
.21/ ER - 0.2\
G.09 - 0.2l
= Incremental emission
reduction, Mg
2.94 = Minimum emission
reduction, Mg
ER = Uncontrolled emission
rate, kg/Mg
Uncontrolled emission rates equivalent to $l,000/Mg and $2,000/Mg
were determined by trial and error, substituting different emission
rates into the above equation (16) until a cost effectiveness of $l,000/Mg
(or $2,000/Mg) was obtained. Table F-8 summarizes the uncontrolled
emissions rates for all styrene-in-air emission calculations.
F-17
-------
Table F-8. STYRENE-IN-AIR UNCONTROLLED EMISSION
RATES EQUIVALENT TO $l,000/Mg,
$2,000/Mg, and $3,000/Mg
Within Line
Across Line
Uncontrolled Emission Rates, kg/Mg
$l,OQO/Mg
0.4454
0.1983
$2,000/Mg
$3,000/Mg
0.2903
0.1694
0.1921
0.1561
F-18
-------
TECHNICAL REPORT DATA
(Please read Instructions on the reverse before completing)
EPA-450/3-83-008
3. RECIPIENT'S ACCESSION NO.
». TITLE AND SUBTITLE
Control of Volatile Organic Compound Emissions from
Manufacture of High-Density Polyethylene, Polypropylene
and Polystyrene Resins
5. REPORT DATE
November, 1983
6. PERFORMING ORGANIZATION CODE
8. PERFORMING ORGANIZATION REPORT NO
I. PERFORMING ORGANIZATION NAME AND ADDRESS
Pacific Environmental Services, Inc.
1905 Chapel Hill Road
Durham, NC 27707
10. PROGRAM ELEMENT NO.
11. CONTRACT/GRANT NO.
68-02-3511
'ONSORING AGENCY NAME AND ADDRESS
U. S. Environmental Protection Agency
Office of Air Quality Planning and Standards
Research Triangle Park, North Carolina 27711
13. TYPE OF REPORT AND PERIOD COVERED
14. SPONSORING AGENCY CODE
NOTES
Control techniques guidelines (CTG) are issued for the control of volatile
organic compounds (VOC) from certain polymer manufacturing plants to inform
Regional, State, and local air pollution control agencies of reasonably available
control technology (RACT) for development of regulations necessary to attain the
national ambient air quality standards for ozone. This document contains information
on VOC emissions and the costs and environmental impacts of RACT in polypropylene
liquid-phase process plants, high-density polyethylene slurry process plants and
polystyrene continuous process plants.
7.
KEY WORDS AND DOCUMENT ANALYSIS
DESCRIPTORS
Air Pollution
Volatile Organic Compounds
Polymers
Resins
Polyethylene
Polypropylene
Polystyrene
b.lDENTIFIERS/OPEN ENDED TERMS
Air Pollution Control
c. COSATI Field/Group
19. SECURITY CLASS (ThisReport}
Unclassified
Unlimited
2O. SECURITY CLASS (Thispage)
Unclassified
21. NO. OF PAGES
302
22. PRICE
EPA Form 2220-1 (Rev. 4-77) PREVIOUS EDITION is OBSOLETE
-------
:/, ,!£ ,,!;!• i/,,"1
-------