HomeMy WebLinkAboutGLSD Organicas to Energy Project - Miscellaneous - 240 CHARLES STREET 8/1/2019 R -TRO' '
D,S M11111
I J,
N'rds'' sl,a r p",gi
o Oomo,1,
sterO trad6nia Flol,
..............I'll
hl
'VAAL,
I'M
LG
Jo
I've
PD/
IRV,
..........
14
Omwo
I j 41j,",
zv /li�j'
.........
...........
",001,r 114-OOOOF /if(
low",
L YIN vvw mAr&-w L"vAE
)VA L
gi,i Wii :11 ii:ii 1
G
V
WI hy use ,Polyvalve P'O1yxPG,asO Valves.9
Polyvalve valves are everything you'd expect from the company
that invented polyethylene valves.,
Millions, halve Poly-GasO valves have been sold since 1976 and are
in use, throughout the world. Here's why: '**I`,tva4
NI
Rugged and reliable Polyvalve
Poly-GI(asO valves are the
i
strongest part of a polyethylene 2" -12" design
piping system.
W No
G'
j
;
metal 'Internal pars.
RK
1
Bubble-tight shutoff from
dual elastomeric seat.
IF
r/
/
j
J�i i
rr Wt�ffj%(f Art,S
Fused body shell eliminates, leak
II pppp^^
!;�P�M��i'PVli�i �„ I�''�ylll Illl�lrl'dlrWiWlWrillflw�'
/
f
paths to,atmosphere.
I
High-,grade polymeric materials
eliminate corrosion.
Multiple Il st r ri stem seals. 1/2" 211
POJVVaI IIT °
( -style)din
■ Smooth bore gives excellent floW
1
h r cterlstl s In both full and
reduced port designs.
/
1
Note:Has high-strength stainless steel stem* "C-style Its r uced bor ainl e
2
ww.Polyvalv
,Ma,teriwals Codes and S'tandards.., A , 1'tciati'ons
Materials
f
Materials of Construction Body arterials Chart
------------- ............................
Resin Material
Supplier Designation Nnsilty
(C-Style) Designation
Body Polyethylene Polyethylene CP Chem T -41
Ball' Acetal Polypropylene
Seat tier t N Pol r le Dow G � Blau E 47110/34081 High
Seat Blum N Buna
""ate: n "full bare I. 1 tt Iorol only the ialt l section
Stern Stainless Steel Acetal Is in DGDA 2490 material,Different Ope ends are fused on to
gait customier's spiecific matartal requirements.
Stem Seal BunaBuns
Ground Water Seal' Neoprene Neoprene
Wrench Adapter Acetal Polypropylene
Adapter Screw Stainless Steel
[:Adapter Button Acetal
Vole "has gear boxand'cast iron "square rout adaptor.
"will have, choke of either gai or vitanchi,
114"and TC-style is Standard Bore n .
Available to Copper Tu,bing Stan ar Baas t T I,
Codes and standards, Applifficafl*
cins
Polyvalve Roly-Gae valves meet or For use in:
exceed the requirements of: Natural gay,distribution.
m AN S 1131 . Natural gay,gathering.
,S 2513 Landfill gas (methane').
U.S. Department of Trans portation 4,9CFR,, Part 192 * Hydrocarbon fuel gasps.
In addition, as required Iy custor s, certain Hydrogen.
ogen.
sizes and materials cif valves neat or exceed the in
requirements f CSA 13137.0and 13137A Other i e rt gases (helium, argon, neon).
Certain Pol'yvalve Poly-,GasO valves have succiessifully
passed' 1 0,,000-hour tests to ISO 37.
Polyvalve,i's an ISO 9001 certified company.
a
t• / ;; o iiii/ %
n will m
r/a/�
dY lr-
I
a
c,, r
°7
01-'
r � III
r If�y
+"l
i I�IVIpV III'�r
r
1 r
NOW r
I
fusion operation
3
,��otivr�raj,
��/
On AMORONACO INDUSTRIES coftipan'y
PolyxwGasO Valve A'vaila,hi'lity
Poly-Gass Val Il �Chart (Ball Valves for Nato li s
End
j jiet of I
9 an
16-20 2 full r BF or SF 260 2 91
IN , 2 gill t BF 3,61 3.,2 9.3j,1 11 1
11 32, 2 standard t BF 40 577 3.81 9.3111113.5
45 649 9.6, 93 111 115
2 55,63, 3 fall 175 2528 3.181 .3111,17
50-63 2 standardt BF 110 1586 91.6 . 111,17
90 3 full BF 3 5.3 9.3,111113.5,17
90 3 standard 1 14.1 9.311 111 ,. 117
1 .1�
4 10 3 full BF 710�O10094 5.8 9.31111113.5117
1! �111 tndard 7 17. . ,11 o 1 3,5,17
6 1 -1 -1 1 dull_ Ir 1800 25957 6.1 9.3,11$13.w,17
1 -1 standard BF 900, 12978 3 . ,11,1 , ,[17
full 3650,, 3 .51 11113. 117
2,25 3 standard BF 13 17 40.3 9-3,11,1 .,5,17
Note: i � " Psi
A P Butt Fusion
., ,r filrasl airr f barA S aIFusin
Dimension Datat Polyw/ve 1,1"11
-Sve Valves
I
0
ANSI Valve Di"'wlensions Metric Valve Dimensions
Weight
welighti
full 10.0 .�d 4.8 2.8 0.501.2 1 -20 full '254 711 86 122 71 123 0.5
gull,, 10.0 3A 4.8 2. .7 1.2 25 full 254 86 122 71 19.1 0.51
1standard 10.0 .d 4.8 2. .91011.2 32 standard 254 8:6 122 71 22.9 0.5
1 1 �. , . , 1 M standard, 5 1 22 71 '.' .5
full 4.0
1 M 1�1. �. � � . dull 1� � - �� �
�
standard , 1' 21 :::1 48.0 2.0
standard 12.8 6.4 9A 3.6 1.95 4.5 full 508 264 381 77 91.9 8.8
.
full
10.E '15.0 3.1 3.62 19.5 1 -11
1 w 11. . tand rd 1 3 63.5
4.0
standard 5,
6
full 1. 1 . 18.6 9,. . � 1 1 1 Ill 3 72 '99 132.1 17.2
80
standard 20.01 10.4 15.0 . 2 23.0, 125-1 surdsrd 501 263 381 133 911.910.4
dull 29.0 12.E 19.9 7.0 6.601. 2,25 frill 1773,,t 1 1 1 44.E
ndar'd 12.E 1 v . ,7 . standard , _ 20,"' L"47.2 102 121.4 19,3
Gear Operaled Gear Operated
fall 29.E 14.8 ,--2 2.2, 7. , 630 61.0225 full 1773 376 564 6,10160 60.8
1 ttu�ll 3. 17. 7�.7 301,E � 1 � � �1 1 111 12 7 7' 2151.7 1
Note:Valves are generally available In these metric sizes and may be available in other mattic dimensions.Dve to wall thickness considerations,80s,In Some sizes may not be
available.donta tyo r Polyvalve representative,Mrspecific SOIR availability.
Hole,PoWalve,proudly offers pub'/an,9ths to customer specifications.
4
w,w,w.PolkvalveUSA.com
I
Order,
How to I
Please provide,the following information when you or r:
Valve size
Valvebody material
Bore type 111 or reduced) °
w Standard i m e n s i l l!� t i S n u r r l" rrr � �y„,,,,,,,,,,,,,,.
;t
Tubing Standard00
twit
io
• End c #III afi (butt '�q��sion or� socket fusion)[,,., f:, �/
• Special serviceconditions
"a Nlnll(IIV�
�, /I� frvl�0ai,r n
r
I
I
t
I
f 1 1 1 �I
r✓ r /
1 �
� � r
/
From the 2"hall valve to lire iun a lr 's first -inch piolyelhyleRe ball valve,
Polyvalve P,aly-GasOvalves are available In the wrest range 17 on the;
market today.11'through "standard porl are shipped in cartons to shield
them from ultraviolet light and to protect the valve nd fr a damage*
Pcily'valve Poly-GasO Valve Figure Number System
The I - s valve figure number system utillizes a five digit number which describes the valves as shown be1ow.
Specifles Pipe Size.
Identifies the.vailve as a Pol v lv P i .G valve
for natural gas d1stri uullon service:,
Material designatiomi
. Dow DGDA2490(UAC3700).
Defines flog passage(Ball or reduced)and end con-
nection(ANSI or Metric i n ion
1. Full Opening-American Iron pipe size nds'',
. Reduced opening-American:iron pros size ends.
. Full opening-Metric endue.
. Reduced opening-Metric ends.
5. Full opening-1 CTS ends or Other special features.
. Reduced p in -CTS ends or special feature
ends.
i
t
t
Standard Dimensions Ratio
(00 other special feature')
I2- XXXX
Special feature end's include Integral socket eructs,stub egad SDR,CTS will thickness,etc.
l
1
I P 0 Ivan I ve
4855 Broladmoor Ave
Kentwood, Mi.49512
Ph.616.656-2,260
Fax 1616.6,56-26
f �r
www.Po1yva1veUS,A.com
f
�, ,,
i r i(�u m1i i/ f
2("Ok 0
To
/
i
find your,local Polyvalve representative,
visit ww,w.PolyvalveUSA.i com or call 616-6'56-2260 POLYVALVE
I ,, it � i� during its usefrai brie.�i^e��r,the Purchaser�r���� q
Po�++i�ale has established iusl� leadership,qru the design and ruulaciuwre ot Its products.When propRfqy egegarfl,this Po1;�apva ,r,odutt Is dasl,pned to perform,its ru�a�e function���� �
WfNe,plroft:a be arwre that Po?j�ahm productszght be used in namerarus applkatlim,s undr a vAdt vafitty of 1uWr<aq SeMce conditorrs.Alulough pb!�,mNt Can(and On does)P(Wde generall gWdellnas,It cannot prov1da sped:fic
� �,.�� for �proper arru r���a����ru����� �� rain���+�� � ���'�� ,. �anurha�slsrs,er�u��r d urudersi,a the Irustao�
a.rrutus�'�� � s���d acat9��„ r� �urchas�rr�rua�r�uust ihereiore asuu ugt7raua'a �� s � � a � P
Oimrallon MalAterinc (lOM)lostroctons,iirur hide, ii the ptodiucl,and train its err playea,s iud contractorsin the safe u a o[Wy ahv pioducts In coarwbion with the spe6fic application.
Po
' hu�the Information and ��ifi a ia,�a,er�tairued In this literature aft;balfieved t beae�nWuraaraa they�,r supplied for ini"orr��a use purposes, q.�+�� �and should not he considered rrfih�e or as a guafantet of aatlslaetory resugts by req area thereon.
Nolhing,contained herain is to he coinsirued as a vlarranly or urArantee,express or implied,,regarding any matter Wth reape t to this product.Because Polyvalve is continually Improving andupgrading its product Osign,the specuh Cations,
diremsiars and Information contarred herear are subject 110 change rthut mot1rn Should Orry quetar arsa e:reerinprovisions,tiase tha i r haspr/s�r h uiq�contact Po qVaqve at any One 0I its or Alde O�erasion$or 0I1i cm20,12 Polyvalve,Kentwood,MIS USA.
GAS ENGINE TECHNICAL DATACRERPILUR�
G3520C
ENGINE POWER(blip): 2242
ENGINE SPEED rpm): 1200
EXHAUST MANIFOLD: DRY JACKET► ATER OUTLET(-F): 230
COOLING SYSTEM: J +IAC,O +2AC
INLET MANIFOLD AIR TEMP(IC):
SCAC Systems
10D 43
039
100 rpm
35
0
a
t 0 22'9
0 17
13
0
20
Q �
Coal a rat F low g allans per ninute)
Coolant Flow vs.Allowable External Restriction
Engine Speed(rpm) 1200
FAO PM Restriction(feet H2 )
0 81.0
1100 .6
20 Notes:
0." -2006443,2354536,25778BB SLAG Pump
Drive Ratio 2:1
Curves indicate maximum allowable external resistance.
Do not project curves beyond range shown.
•PSI conversion based on specific gravity of 1.0
DM5728
Data generated by Gas Engine e Rating Pro Version 6.01.01
Ref.data Set DM58 -00.001,Printed 26May2016 page 2 of
G3520C SAS ENGINE TECHNICAL DATA CATERPILLAR�
ENGINE POWER(bhp): 2242
ENGINE E FEED(rpm)* 1200
EXHAUST MANIFOLD' DRY JACKET WATER OUTLET ff)- 230
COOLINGSYSTEM: J +1A ,G +2AO
INLET MANIFOLD Alfa TEMP(IC).-
Jacket Water Sys
1
R
0 35
0 26'9
404 1
Lw
0
ID L 0
Coolant Flow(gallons per in
Coolant Flow vs.Allowable External Restriction
Engine Speed(rpm) 1200
FIOw PM Restriction(feet H2 )
400 89.0
2098232,2354535 JW Pump
550 45.3 -Dave Ratio 2A
60g 30.7 -Curves indicate maximum allowable external resistance.
Do not project curves beyond range shown.
•Pi conversion based an specific gravity of 1.0
5
Data generated by Gas Engine Rating Pro Version 6.01.01
Fief.Data Set D 8 -0 -001,Printed 2 I ay2018 Page 1 of
GAS ENGINE TECHNICAL CRERPILLAR
G3520C
ME FIELD:M ECHAN 1 AL&'EXHAUSTN 01SE:.::
MECHANICAL: Sound Power '11 Octave Fre uen ie
............... .
eta over: ercen .:.'.:Engine
Without Fan Load ::Ra�re�r::::::. ::::.��rerail ::100 Hz -.'-:125 Hz ':-:-':fi60 Hz .:�200 Hz :.: 501-�z :.::39 Fez 400 Hz �00 Hz 83� �1z
ekW % bhp dB dB(A) dB(A) dB(A) dB(A) dB(A) dB(A) dB(A) dB(A) dB(A dB(A)
1600 100 2248 116.6 77.2 87.0 87.7 90.4 96.6 98.1 98.9 101.2 93.8 102.6
1200 75 1683 115.5 76.3 84.2 84.9 88.9 93.3 97.2 94.3 99.0 92.5 100.8
800 50 1 1128 113.7 73.8 81.0 80A 87.2 90.5 93.2 92.4 98.1 90.5 99.6
MECHANICAL:AL:Sound Pourer 113 Octave Fre u tr1
en:Po r:':: :.
:.. .ercent
....:.........:...................:........ ...
�Witho'ut Fain :.::.::Lip
t#. .. Poe :.:'� CHz kHz ::f:B H klz Hz:k .'151C-1z: ::. NCH kHz::;.::: .:.;fi. Ftz:: :::: C#z : : 0 1-1
ekW % bhp dB(A) d6 dB(A) dB(A) dB dB A d A dB(A dB(A) dB(A) dB(A)
1600 100 2248 107.9 105.E 108.7 105.6 103.3 102.6 101.3 101.0 101.2 105.9 110.0
1200 75 1683 T07.9 103.4 105.7 104,3 101.2 101.1 100.1 100.1 100.7 110. 99.2
00 50 1128 108.2 101.3 104. 105. 99.7 'l ft0.'i 98,8 98. '102.7 98.0 95.2
EXHAUST: ........Sound Power 11 tap a Frequencies
Peres n t
Ioa Power -.-.. ►reral�:-. - � 0 #�z '126 Hz .�'1 0 H ::. 410 Hz50 Hz ::: 1 Hz SOD Hz500 Hz ::::. 30 Hz 8Q0 Hz
ekW % b d dB A dB(A) dB(A) dB dB dB dB dB(A) dB
1600 100 2248 117.6 107.2 98.2 98.0 88.0 106.8 97.7 106.0 100.2 94.2 102.5
1200 75 1683 117.1 106.8 96.7 96.0 92.9 110.8 99.0 105.6 97.8 95.8 102,1
800 50 1128 114.8 106.3 95.0 93.9 1 89.4 1 10810 96.0 101.8 94.2 94.8 98.8
EXHAUST:Sound Pourer 113 tave Fre uencle
e Pawei�:::: ::: ere
a::::
n P r nt..�n
.....:... .
Without Oan :::L ti
Power :' kHz kHz: ::::.i.6 kHz -:-`::- kHz':-...--.. . JkH .1 kHz :.::::.+�kHz,-::" 51C�iz.:`. kFiz : <::8 kHz :'10 kHz
ekW % bf dB dB( dB(A) dB dB dB dB(A) dB dB(A) dB dB(A)
1600 100 2248 100.4 102.1 101.7 101.9 104.9 106.9 107.2 107.4 105,8 104.8 107.9
1200 75 1683 97,9 100.9 101.6 98.9 103.0 105.2 105.9 106.6 105.3 101.0 105A
800 50 1128 94.7 97.6 98.5 95.1 101.0 103.9 103.9 103.9 101.3 101.5 100.8
----
SOUND PARAMETER DEFINITION:
Sound Power Level Data-€M8702-0
Sound power is defined as the total sound energy emanating from a source irrespective of direction or distance.Sound power level data is presented
under tvw index headings:
Sound power level Mechanical
Sound power level--Exhaust
Mechanical,Sound power level data is calculated in accordance with ISO 3747.The data is recorded uWh the exhaust sound source isolated.
Exhaust:Sound power level data,is calculated in accordance Wth ISO 6798 Annex A.Exhaust data Is post-catalyst on gas engine ratings labeled as
"Integrated Catalyst".
Measurements made to accordance with 18O3747 and ISO 6798 for mechanical and exhaust sound level only.Frequency bands outside the displayed ranges are not measured,due to
physical test,and environmental conditions that affect the accuracy of the measurement. No cooling system noise is included unless specifically indicated.Sound level data is indicative
of noise levels recorded on one engine sample In a survey grade 3 environment.
How an engine is packaged,installed and the site acoustical environment will affect the site specific sound levels.For site specific sound level guarantees,sound data collection needs
to be done on-site or under similar conditions.
Data generated by Gas Engine Rating Pro Version 6.02.00
Fief.Data Set DM5855-04-001,Printed 27Sep2016 Page 4 of
G3520C SAS ENGINE TECHNICAL DATA CATERPILLAR"
Load Acceptance
10 10
8 8
i
4 4 Max
0
J
0 0
0 10 20 30 40 50 60 70 80 90 100
InItIal Load( )
Train i nt L oad"A p tang
as
Frequency Deviation+fY Voltage Deviation+l� Recover lasslfication
Load Step °o} { } Time Defined by Hates
sec IS0 8 8-5
5 + 1-25 +25/- 5 45
-5 +251- 5 +251- 5 45
Recovea S eclk atlon +1.761-1.75 + 1-5
stead State Specification +1. 51-1 P25 + 1-
Transient Information
The transient load steps fisted above are stated as a percentage of the engine's full rated load as Indicated in the appropriate performance technical data sheet.Site ambient conditions,
fuel quality,Inlet/exhaust restriction and emissions settings WO all affect engine response to load change.Engines that are not operating at the standard conditlons stated In the
Technical data sheet should be set up according to the guidelines included In the technical data;appl+ing timing changes and/or engine de rates as needed.Adherence to the engine
settings guldelines will allow the engines to retain the transient performance stated in the tables above as a percentage of the site derated power(where appropriate). Fuel supply
pressure and stability 1s critical to transient performance.Proper installation requires that a fuel train components(including tillers,shut off valves,and regulators}
be sized to ensure adequate fuel be defivered to the engine.The following are fuel pressure requirements to be Measured at the engine mounted fuel control valve.
a.Steady,State Fuel Pressure Stability+1-.15 psUsec
b.Transient fuel Pressure Stability+{_.15 psllec
Inlet grater temperature to the SCAC musk be maintained at specified value for all engines.It Is Important that the external cooling system design Is able to maIntain the Inlet water temp to
the SLAG to within+}-i*C during all engine-operating cycles.The SCAC Inlet temperature stability+c6tedon Is to maintaln stable 1Met nnanifold air lemperature. The Air Fuel Rat io con trot
system requires up to 180 seconds to converge after a Ioad step has teen performed for N Ox to return to norn Ina I setting.If the stabilization tirne Is not,net between load steps tine
transient perforrnance listed In the document may not be met. Differences In generator Inertia may change the transient response of engine, Engine Governor galns and Voltage
regulator settings may need to be tuned for site conditions. The time needed to start and stabilize at rated engine speed Is a minimum of 80 seconds after a successful crank cycle.
Engines must be Maintained In accordance to guidelines specified In the Daterpiliar Service Manuals applicable to each engine.Wear of components outside of the specified tolerances
will affect the transient capability of the engine. Transient performance data is representative of a*Hot"(previously loaded or fully heat soaked)genset.
NOTES
PREPARED BY:
Data generated by Gas Engine Rating Pro Version 6.02.00
Ref.Data Set DM5855-Q4-001,Printed Mep2016 Page 5 of 5
Constituent Abbrev mole 0b form
................
Water Vapor H20 0.0000 0.0000
Methane CH4 54.8000 54.8000 Fuel Makeup: Low Energy
Ethane C2H6 0.0000 0.0000 Unit of Measure: English
Propane G3H8 0.0000 0.0000
l obutane iso-C4HIO 0.0000 0.0000
Calculated_Fuel Properties
lorbutarr nor-C4H10 0.00000.0000 Caterpillar MethaneNumber: 1 .0
lsopentane 1soµC H12 0,0000 0.0000
Iorpentane nor-05HI2 0,0000 0,0000
Flee acne C0H14 0.0000 0,0000 lower Heating Value Btuls o 00
Fleptalne C71116 0.0000 0.0000 Higher Heating Value Btu1s = 555
Nitrogen l 2 2.2000 2.2000 W BBE Index Btul f: 505
Carbon Dioxide C 2 43.0000 43.0000
Hydrogen Sulfide 142S 0.0000 0.0000 THC:Free inert patio: 1.21
Carbon Monoxide co0.0000 0.0000 Total%Inert °o N2,C2,He : 45.2%
Hydrogen H2 0.0000 0.0000
O
I
c en 2 0.0000 0.0 O PC %) To 90 Btu1s f Fuel): 9 %
Helium HE 0.0000 0.0000
f eopentane neo-C 1112 0.0000 0.0000 Compressibility Factor-- 0.997
Octane C8H18 0.0000 0.0000 Stoich AIF Ratio VolNo l: 5.22
i onene C9H20 0.0000 0.0000 tol is A/F Ratio (Mass/Mass): 5.34
Ethylene C2H4 0,0000 0.0000 Specific Gravity(Relative to Air): 0.97
Propylene C3H0 0.0000 0.0000
TOTAL(Volume%) 100.0000 100.0000 Specific Heat Constant K). 1.30
CONDITIONS AND DEFINITION
Caterpillar Methane dumber represents the knock resistance of a gaseous fua1. It should be used with the Caterpiliar Fuel Usage Guido for the engine and rating to determine the rating far the fuel
specified. A Fuel usage Guide for each rating is included cn page 2 of its standard technical data sheet,
RPC aWays applies to naturaiiy aspirated(NA)engines,and turbocharged(TA or LE)engines only when they are Berated for altitude and ambient site conditions.
Project spect0c technical data sheets generated by the Caterpillar Gas Engine Rating Pro program tale the Caterpillar Methane Number and RPC into accountwhen generating a site rating.
Fuel properties for Btulscf calculations are at 6OF and 14.696 psis.
atefpiIlar sha11 have no 1i abi I ity in law or egufty,for damages,consequently or othefv4se,aTis€rig from use of progtarn and related material or any part thereof.
FUEL LIQUIDS
Fief#gases,well head gases,and associated gases typtcaIly contain Fquid water and heavy hydrocarbons entrained in the gas.To prevent dotonatron and severe damage to the engine,hydro arbor
Iiqulds must not be allowed to enter the engine fuel system, To remove liquids,a liquid separator and coalescing filter are re corn rnended,%PAth an automatic drain and collection tank to prevent
con ta M 1nation of the+ground in accordance Wth boat nodes and standards.
To avoid grater condensation in the engine or fuel lines,limit the rera ve humidity of water in the fuel to 0 at the rnirilmum fuel operating temperature,
WARNIN§
1.Ccntinuous operation at rated povm r above 4g (104F)ambient air temperatures may contribute to faster degradation of generator irisalati:on.Consult TM for degradation curves.
PREPARED Br.
Data generated by Gas Engine Rating Pro Version 6.01.01
Reif.Data Set DM885 -0 - 01,Printed 20May2016 Page 4 of 4
G3520C GAS ENGINE SITE SPECIFIC TECHNICAL DATA CATERPILLAR*
ENSET APPLICATION
NOTES
1.Generator efflciencie s.power factor,and voltage are based on specified generator. [ enset Power(ek1 )is calculated as:Engine Power(bkW)x Generator Efficiency),{ ens t
Power(k11A)is calculated as:Engine Power(bkW)x Generator Efficiency 1 Power Factor]
2.Rating is Wth hvo engine driven water pumps. Tolerance is(+)3,(-)0%of full load.
.Genset Ef ieclency published in accordance with ISO 04 11.
4.Thermal Efficiency is calculated based on energy recovery from the jacket water,1st stage aftercool r,and exhaust to 0"F Wth engine operation at ISO 304611 Genset
Efficiency,and assumes unburied fuel is converted in are oxidation catalyst.
5.Total efficiency is calculated as:Genset Efficiency+Thermal Efficiency.Tolerance is±10%of full load data.
.ISO 304011 Genset fuel consumption tolerance is(+) ,(-)0%at the specified power factor.Nominal genset and engine fuel consumption tolerance is±2.5%of full road data at
tine specified power fac€or.
7.Air flew value Is an a'vies'basis. flow is a nominal value with a tolerance of;L 5°lo.
.inlet rnanifvld pressure is a nominal va a with a tale€ante of t 5%.
.Exhaust temperature is a nominal value with a tolerance of(+) "F$(-)54°F.
10.Exhaust flow value is on a"wet"basis. Flaw is a nominal valve with a tolerance of±6° .
11.Inlet and Exhaust restrictions are max[rnum allowed values at the corresponding leads.Increasing restrictions beyond what is specified will result in a significant engine derate.
12.Emissions data is at engine exhaust flange prior to any after treatment.
13.N Ox tolerance's are*18%of specified value.All other emission values listed are higher than nominal levels to allow for Instrumentation,rneasuremerit,and engine-to-engine
variations.They indicate the maximum values expected under steady state conditions.Fuel methane number cannot vary more than±3.TH ,NMH ,and NMNEHC do not
include aldehydes,adjusted to the specified N x level at 100%load.
14.V R Volatile organic compounds as defined in US EPA 40 CFR 60,subpart JJJJ
15,Exhaust Oxygen level is the result of adjusting the engine to operate at the specified NOx level. Tolerance is±0.5.
16.LHV rate tolerance is±2. %.
17.Heat rejection values are representative of site conditions.7alerenras,based on treated water,are i 10%for jacket water circuit,:k 0%for atmospheres:t 0%for lobe all
circuit,±10%for exhaust,and± %for after cool er circuit.
18.Pump power includes engine drivers jacket water and aftercooler water pumps. Engine braise power includes effects of pump power.
19.Aftercoolar heat rejection is nominal for site conditions and does not Include an afterccoler heat rejection factor. Aftercooler heat rejection values at part load are for reference
only.
20.Cooling system sizing criteria represent the expected maximum circuit heat rejection for the ratings at site,with appried plus tolerances.Total circuit:heat rejection Is calculated
using formulas referenced in the motes on the standard tech data sheet with the following qualifications.Aftercacler heat rejection data(1AC&2A )is based on the standard
rating.Jacket Water(JW)and Oil Cooler( )heat rejection values are based on the respective site or maximum column.Aftercooler heat rejection factors(A HRF)are specific
for the site elevation and inlet air temperature specified in the site or maximum column,referenced from the table on the standard data sheet
21,Minimum heat recovery values represent the expected rninimurr}heat recovery for the site,Wth applied minus tolerances.Do not use these values for cooling system sizing.
WARNING(51.
1.Continuous operabon at rated power above 40 ('104F)arnblent air temperatures may contribute to faster degradation of generator insutaUon. Consult 7 t for degradation curves.
PREPARED BY:
Data generated by Gas Engine Mating Pro Version 5. 1.01
Ref.Data Set RlIr1585 -06-00i,Printed 20May2016 rage 3 of
kpm% ,Oft CATERPILLARS
%3;3 52 0 C GAS ENGINE SITE,SPECIFIC TECHNICAL DATA
GENSET APPLICATION
Engineer vs, Inlet Air Temperature
IDa ta re p res,entste m peratu re sweep a t 60 ft a nd 12 00 rpm
2500,
I L -L I I I I I L
2500,
150,0 utr will
Range for Site Condl tion
CL C tinu a Operating
91000 100a
r
Range for Site ndit n
Low Load,Irlt rmAtent
" 5001 51100 W Operating Range
, 40 50 60, 70 80 90 '100 110 120 130,
Air T rrr r to r ,"
i
PREPARED BY:
Data generated by Gas E g ine Rating Pro r i of 6.
Ref.Data Set DM5,859-06-001,,Pdnted 20May2016Page,2 of
G3520C GAS ENGINE SITE SPECIFIC TECHNICAL DATA
ENSET APPLICATION
ENGINE SPEED(rpm): 1200 BATING STRATEGY' STANDARD
COMPRESSION RATIO: 11.3 RATING 0 LEVEL: CONTINUOUS
AFTERCOOLER TYPE: SCAG FUELSYSTEM: OAT LOW PRESSURE
AFTER COOLER-STAGE 2 INLET ff): 130 WITH AIR FUEL RATIO CONTROL
AFTERCOOLER-STAGE 1 INLET ff): 217 SITECONDITIONS:
JACKET ET WATER OUTLET ff): 230 FUEL: Lew Energy
ASPIRATION: TA FUEL P RESSLIRE RAN E(p ig): 1.5-5.0
COOLING SYSTEM- JW+iA ,OC+2AC FUEL METHANE NUMBER: 143.0
CONTROL SYSTEM: ADEM3 FUEL LHV{Btulsc : 500
EXHAUST MANIFOLD: DRY ALTITUDE(ft): 60
COMBUSTION: LOW EMISSION MA iMUM INLET AIR TEIUIPERATURE(°F): 104
NOx EMISSION LEVEL(glbhp-hr NOx)-+ 1.0 STANDARD RATED POWER: 2242 hbp@1200rpm
SET POINT TIMING, 29 POWER FACTOR- 0.8
VOLTAOE(V): 4160
MAXIMUM UM :.~ IT jWjNG':'AT MAXIMUM
0
::::: :..:.:......::.RATI N hI TE ... ..O � .:..... ...:::. :..10 ' .... p
EN ET POWER (WITHOUT FAN) (1)(2) ekW 1600 1600 1200 800
EN ET POWER (WITHOUT FAN) (1)(2) kVA 2000 2000 1500 1000
ENGINE POWER (WITHOUT FAQ) (2) bhp 2242 2242 1683 1120
INLET AIR TEMPERATURE *F 104 104 104 104
GENERATOR R EFFICIENCY {1) % 95.7 95.7 95. 951
OENSET EFFICIENCY (ISO 304611) ( ) % 39.2 39.2 37.5 36.6
THERMAL EFFICIENCY (4) % 38.1 38A 39.6 38.2
TOTAL.EFFICIENCY 5 % 77.3 77.3 77.1 74.8
ENG I N E DATA.::
GE 1 ET FUEL CONSUMPTION (ISO 304611) (6) BtulekW-hr 8697 8697 9100 9320
EN ET FUEL CONSUMPTION (NOMINAL (6) BlulekW-hr 8909 8900 9322 9547
ENGINE FUEL CONSUMPTION (NOMINAL ( ) Btulbhp-hr 6358 6358 6646 6771
AIR FLOW(a@inlet air temp,14.7 p ia) (WET (7) ft lm€n 4462 4462 3384 2354
AIR FLOW {WET (7) Ib1hr 18835 10835 14288 9940
FUEL FLOW(60°F,14.7 psia) s fm 476 476 373 255
INLET MANIFOLD PRESSURE (8) in Hg(ab ) 89.7 89.7 68.3 48.4
EXHAUST TEMPERATURE-ENGINE OUTLET (9) OF 915 915 988 982
EXHAUST OAS FLOW(a@engine outlet temp,14.5 p la) (WET) (10) fk3ftln 1 309 12309 9663 6822
EXHAUST GAS MASS FLOW (WET) (10) lb/hr 20959 20950 15947 11073
MAXINLET RESTRICTION (11) in H2O 10,04 10.04 10,04 10.04
MAXEXHAUST RESTRICTION 11 in H2 0.07 20.07 20.07 20.07
:. ... EMISSIONS DATA:`ENGINE OUT
NOx(as N ) (12)(13) 9lbbp-hr 1.00 4.00 1.00 1.00
(12)(13) g hp-hr 4.78 4.78 4.88 4.97
TH (rnol.wt.of 15.84) (1 )(13} glbhp-br 6.36 5,36 0.07 7.34
Nlv HC(rnol.wt.of 16.84) (12)(1 ) glbhp-br 0.80 0.80 0.91 1.10
NM EH ( ODs)(rnol.wt.of 15.84) (1 )(13)(14) glbhp-hr 0.54 0.54 0.61 0.73
H HC (Formaldehyde) (12)(13) glbhp-hr 0.44 0,44 0.44 0.49
02 (12)(13) glbhp-hr 736 736 765 806
EXHAUST OXYGEN (12)(15) %DRY 8.4 8.4 8.1 0.0
H EAT:REJ E TIOW
LHV INPUT (16) Btulmin 237586 237586 186440 127297
HEAT REJ.TO JACKET WATER(.l'W) 17) Btu/min 29397 29397 25887 21531
HEAT REJ.TO ATMOSPHERE (17) Btulmin 7210 7210 6013 4823
HEAT REJ.TO LU 3E OIL(]O) (17) Btulmin 7791 7791 6995 6197
MEAT REJE TIO 1 TO EXHAUST(LHV TO 3 50°F) (17) Btulmin 45379 4 379 3 862 24338
HEAT REJ.TO A/C-STAGE 1(1AC) (17)(i ) Btulmin 12077 12077 4700 -241
HEAT REJ.TO A/C-STAGE 2(2A ) (17)(19) Btulmin 8222 8222 5917 3766
PUMP POWER 18). Btulmin 1977 1977 1977 1977
D OLING-SY TEW I ING' F ITEF IA-::--.:
TOTAL JACKET ET WATER CIRCUIT(JW+1AC.) (20) Btulmin 48�125 4812
TOTAL STAGE 2 AFTEROOOLER CIRCUIT{0 +2A0) (20) Btu/min 1 327 18327
HEAT REJECTION TO EXHAUST LHV T 3b9°F 20 Btulmin 49917 49917
A coot ng system s a fety facto of 0%has beer`added to the coori ng system si in criteria.
MINIMUM HEAT RECOVERY:
TOTALJACK ET WATER I RGUIT(JW+1AC) ( 1) Btulmnin 37930 37930
TOTAL STAGE 2 AFTERGOOLER CIRCUIT(O0+2AO) (21) Btu/ in 14043 14043
HEAT REJECTION TO EXHAUST LH TO 360°F 21 Btulr'I. 37684 7A
CONDITIONS AND DE INITION
Engine rating obtai ned and presented In accordsnoe with ISO 304611.adjusted for fuel,site altitude and sito inlet air temperature.100%rating at maximum Inlet air temperature 1s the maximum engine
capability for the specified fuel at site alStude and maximum site inlet air temperature.Maximum rating is the maxfmum capability at the specified aftercooler Inlet temperature for the specified fuel at
site altitude and reduced inlet air temperature.Lowest load point is the lowest continuous duty operating load allowed.No overload permitted at ratite shown.
For notes information mnsuit page three.
"'WARNINGS ISSUED FOR THIS RATING CONSULTPACE ""
PREPARED BY-
Data generated by Gas Engine Hating Pro Version 6,01.01
Ref.Data Set Di 58 9-0 -401,Printed May2016 Page 1 of 4
PIPE
. 4 A I
'
71
f
/ r
/
z
r , r I
,
I
I
„�I.
„
v
W -The wall thickness,is rninimum per D2 1 and not a function of
.,
t�
i
I �"'I
r � r
r
,,...: ,r,r, ,,,,r, r
i r is ✓ r,
i 1 ,14
I „,
I.
r r rrrrrr//, rr
i /.
41,
,, / /,
ri
:
rr r
" / ;r
I
T11 r / r
,/, „, „r,,,,>,,,r„ ,,,..:/„/i,r ✓ rill ri„%„ ,
of ,
4— 3,' ,„ , , ,. %;,, i r ,,,�,.. ,,,,,,,,11
W172
"�spybkff �,�'�','� ,�
0 O :
70 3 ;,
�w41'111 � 12 2 n
So � )0
7 7121�3W40"or
►
bundles 1,1 ' 14 1 ,240'
RIJ
Iw „O
82,
i
6"' .6 „ �5
ft �rnd � I
m ® ° °
,.,,, »
80
�'u1I I�
" DR 11 8.6251 0384 100 848soft bundles
3,600-
DR 13.5 0.6319 812
"DR' 3IWO
J
1
join ayer
1 " DR 11 1 . 1 1.45,5 100 8 4 ' bulk (* 6 4 ' 1 w
I
DR 17 0.941 1 joints/layer 1
DR 11 1.636 100 31693 strip loads,w
18 DR 17 18,00110 1. ,5 47 40 chocks jointMay r 1 t
oo W
OR 1
DR 17 0 E:�1.176 6 31061 chocks lnintsAa er
This pr a t flyer is untended for reference purposes. It should not be used in plain of the nd ce from a licensed professional engineer. De sign Pressure,Ra tin i ca lau la te d per 49 CF
§192.121 and based on an
' operating temperature o F°Pipe weights are calculated in accordance with P l T -7°Nornina°l OD andMinimum wall plus i used in estimating fluid flow.
ActualII ill When designing components to fit the pipe ID,refer to pipe!dimensions and tolerances,in the applicable:pipe nanufa tun�specification.
r,
Bulletin PP 315May 2017 vApAv,performancepipexom 2017 Chevron Phillips Chemical Company L
PerformancePipe,a division of Chevron Phillips Chemical Company LP I5085 W.Park Blvd ,I Suite 51,00 1 Plano,TX 75,093 Phone: 00- 2 2 1 Fax: -5 - 329
i
y
PERFORMANCE,"ric
Divislo OF 011VRON P111111PSI 1 IPA
imp 11
YEL,LQ-N-Wb4N%T'KN=k1Pr%E@ 8j*%u1%u4% or%erwies
P N
HDPE Gas Distribution ipe
YELLOWSTRIPE@ HDPE
..........
needs
in compliance with AST
y
D2,513, NSF
I A�
192. Selected sizies conforlm to CSA
B 137.4, and UPC product standards.
ratedI Produced from only the highest
HDPE pipe material
YELLOWSTRIPEO 8,300 Series Pipe
manufactured from a,
PE 4171 O and
PE 1 resin listed in PPI ,TR, .
'Y'ELLOWSTRIPE@HDPE Pipe Advantages:
Durable V Fatigue, Free V Chem icall Resistant,
Leak Tight V Impact Resistant Y UV Protection
Excellent FV Trenchless Install V Flexibility
AbrasionRadiusEnvironmental
Material Des,ignat,ioin Code ASTM D2513 PE 710
Cell Classification, ASTM D335,055 C(black.)
Density[ ] ASTIR 1315051 0.961 (black); >0.9,47(colored)
Melt In [ ] ASTIVI D1238 0.08 g/10 in
Tensile Strength[5] ASTM D638,Type I 15 s1.
Color; 'fit Ill r[C] ST'M D3,350 Black
Color
RCP, Full Scale,at 3211F a °C ISO,13478 >667 psi bark)
This is not a product specificatlion and does not guarantee or establish specific r inl uum r maximum valuies or manufactuning tolerance for material or tubing,products t
be supplied.Values obtained from t ts of specimens t 'l n fr m tubing product may,vary from thiese typical values. 'Calculated value per correlation equation In ISO
4 based on S4 test data on "DR 11.
Bulletin,,PP 315,1 May 2017 wmperformaneepipexom 2017 Chevron Philllips Chlemica]Company LP
Performan,ce Pipe,a divist'llon of Chevron Phillips drill mpan LP 15085 W.Park Blvd I Suite 500 1 Pla,no,TX 7509,E 11 Phone: 0 - 7 i 2 1 Paw 972-599-7329