PERFORMANCE DATA [1HZ00788] JULY 09, 2014 For Help Desk Phone Numbers Click here Perf No: DM4683 Change Level: 02 General Heat Rejection Emissions Regulatory Altitude Derate Cross Reference General Notes Supplementary Data Perf Param Ref View PDF SALES MODEL: 3516B COMBUSTION: DI (BHP): 2,628 SPEED (RPM): 1,800 GEN WITH FAN (EKW): 1,825.0 HERTZ: 60 COMPRESSION RATIO: 14 FAN (HP): 59.5 RATING LEVEL: PRIME ASPIRATION: TA PUMP QUANTITY: 2 AFTERCOOLER TYPE: SCAC FUEL TYPE: DIESEL AFTERCOOLER CIRCUIT TYPE: JW+OC, AC MANIFOLD TYPE: DRY AFTERCOOLER TEMP (F): 140 GOVERNOR TYPE: ADEM3 JACKET WATER TEMP (F): 210.2 ELECTRONICS TYPE: ADEM3 TURBO CONFIGURATION: PARALLEL CAMSHAFT TYPE: STANDARD TURBO QUANTITY: 4 IGNITION TYPE: CI TURBOCHARGER MODEL: GTA5518BN-56T-1.24 INJECTOR TYPE: EUI CERTIFICATION YEAR: 2001 FUEL INJECTOR: 1504456 CRANKCASE BLOWBY RATE (FT3/HR): 2,627.1 UNIT INJECTOR TIMING (IN): 64.34 FUEL RATE (RATED RPM) NO LOAD (GAL/HR): 14.5 REF EXH STACK DIAMETER (IN): 12 MAX OPERATING ALTITUDE (FT): 4,921 INDUSTRY SUB INDUSTRY APPLICATION ELECTRIC STANDARD PACKAGED GENSET General Performance Data Top GENSET PERCENT WITH LOAD FAN BRAKE MEAN EFF PRES (BMEP) BRAKE SPEC FUEL CONSUMPTN (BSFC) VOL FUEL CONSUMPTN (VFC) INLET MFLD PRES EKW % BHP PSI LB/BHP-HR GAL/HR IN-HG DEG F DEG F DEG F 1,825.0 100 2,593 271 0.332 123.1 73.7 176.0 1,107.1 807.8 1,642.5 90 2,338 244 0.334 111.6 67.0 171.0 1,063.4 782.2 1,460.0 80 2,084 218 0.339 100.8 60.5 167.5 1,028.7 763.5 1,368.8 75 1,958 205 0.341 95.4 56.8 165.6 1,011.8 758.0 1,277.5 70 1,831 191 0.343 89.8 52.8 163.6 995.0 753.6 1,095.0 60 1,579 165 0.349 78.6 44.2 159.4 961.5 747.0 912.5 50 1,328 139 0.355 67.3 35.6 155.3 928.2 740.3 730.0 40 1,079 113 0.363 55.9 27.3 151.8 880.1 722.7 547.5 30 829 87 0.376 44.5 19.1 148.8 813.1 689.6 456.2 25 704 74 0.386 38.8 15.4 147.5 771.1 664.9 365.0 20 577 60 0.401 33.0 11.8 146.5 721.7 633.2 182.5 10 321 34 0.466 21.4 6.4 145.4 589.6 535.6 INLET MFLD TEMP EXH MFLD TEMP OUTLET TEMP GENSET WITH FAN PERCENT LOAD COMPRESSOR OUTLET PRES COMPRESSOR OUTLET TEMP WET INLET AIR VOL FLOW RATE OUTLET WET EXH GAS VOL FLOW RATE WET INLET AIR MASS FLOW RATE WET EXH GAS MASS FLOW RATE WET EXH VOL FLOW RATE (32 DEG F AND 29.98 IN HG) DRY EXH VOL FLOW RATE (32 DEG F AND 29.98 IN HG) EKW % BHP IN-HG DEG F CFM CFM LB/HR LB/HR FT3/MIN FT3/MIN 1,825.0 100 2,593 74 418.8 5,812.2 14,255.1 25,571.7 26,433.6 5,529.8 5,088.6 1,642.5 90 2,338 67 394.9 5,487.2 13,170.8 23,148.8 23,930.2 5,214.3 4,798.4
1,460.0 80 2,084 61 371.7 5,155.3 12,185.5 21,100.5 21,806.4 4,898.1 4,507.3 1,368.8 75 1,958 57 359.0 4,954.1 11,662.3 20,104.6 20,772.2 4,709.1 4,333.4 1,277.5 70 1,831 53 345.4 4,735.2 11,115.9 19,102.4 19,731.2 4,504.6 4,145.2 1,095.0 60 1,579 44 314.6 4,258.4 9,954.0 17,021.3 17,571.9 4,056.0 3,732.5 912.5 50 1,328 36 281.1 3,781.8 8,739.4 14,871.3 15,342.5 3,580.8 3,295.2 730.0 40 1,079 28 244.8 3,302.5 7,488.0 12,562.3 12,953.9 3,113.8 2,865.4 547.5 30 829 20 207.7 2,826.8 6,235.2 10,171.9 10,483.6 2,667.5 2,454.7 456.2 25 704 16 189.9 2,593.5 5,605.5 8,951.6 9,223.1 2,450.8 2,255.3 365.0 20 577 13 172.5 2,363.6 4,971.9 7,718.6 7,949.7 2,236.8 2,058.3 182.5 10 321 7 141.6 1,940.3 3,695.6 5,232.0 5,381.5 1,825.6 1,680.0 Heat Rejection Data Top GENSET WITH FAN PERCENT LOAD REJECTION TO JACKET WATER REJECTION TO ATMOSPHERE REJECTION TO EXH EXHUAST RECOVERY TO 350F FROM OIL COOLER FROM AFTERCOOLER WORK ENERGY LOW HEAT VALUE ENERGY HIGH HEAT VALUE ENERGY EKW % BHP BTU/MIN BTU/MIN BTU/MIN BTU/MIN BTU/MIN BTU/MIN BTU/MIN BTU/MIN BTU/MIN 1,825.0 100 2,593 40,605 7,677 98,442 49,534 13,194 25,194 109,964 264,636 281,904 1,642.5 90 2,338 37,761 7,336 89,397 43,959 11,999 21,837 99,144 239,804 255,451 1,460.0 80 2,084 34,974 6,995 80,923 39,352 10,805 18,539 88,384 215,726 229,802 1,368.8 75 1,958 33,582 6,853 76,692 37,250 10,241 16,911 83,021 203,750 217,045 1,277.5 70 1,831 32,188 6,711 72,452 35,202 9,668 15,298 77,655 191,762 204,275 1,095.0 60 1,579 29,231 6,426 63,977 31,107 8,417 12,170 66,963 167,789 178,738 912.5 50 1,328 26,160 6,085 55,504 27,070 7,222 9,213 56,300 143,874 153,262 730.0 40 1,079 22,891 5,772 46,916 22,449 6,002 6,501 45,744 119,999 127,829 547.5 30 829 19,380 5,458 38,072 17,441 4,773 4,030 35,161 95,853 102,108 456.2 25 704 17,523 5,293 33,525 14,752 4,152 2,893 29,837 83,623 89,079 365.0 20 577 15,594 5,119 28,860 12,015 3,530 1,826 24,474 71,235 75,884 182.5 10 321 11,506 4,665 19,038 6,336 2,280-49 13,600 45,864 48,856 Emissions Data Top Units Filter All Units RATED SPEED POTENTIAL SITE VARIATION: 1800 RPM GENSET WITH FAN EKW 1,825.0 1,368.8 912.5 456.2 182.5 BHP 2,593 1,958 1,328 704 321 PERCENT LOAD % 100 75 50 25 10 TOTAL NOX (AS NO2) G/HR 23,895 13,317 8,009 4,298 3,054 TOTAL CO G/HR 2,676 1,857 1,483 1,513 1,584 TOTAL HC G/HR 440 438 346 242 234 PART MATTER G/HR 217.1 224.4 194.9 134.0 81.8 TOTAL NOX (AS NO2) (CORR 5% O2) MG/NM3 4,435.0 3,190.0 2,718.1 2,530.1 3,280.6 TOTAL CO (CORR 5% O2) MG/NM3 500.8 447.2 507.2 899.4 1,751.2 TOTAL HC (CORR 5% O2) MG/NM3 81.8 104.8 117.4 142.6 251.3 PART MATTER (CORR 5% O2) MG/NM3 40.3 53.8 66.1 78.8 87.9 TOTAL NOX (AS NO2) (CORR 5% O2) PPM 2,161 1,555 1,324 1,234 1,605 TOTAL CO (CORR 5% O2) PPM 401 358 406 720 1,401 TOTAL HC (CORR 5% O2) PPM 132 169 190 230 409 TOTAL NOX (AS NO2) G/HP-HR 9.22 6.80 6.03 6.11 9.52 TOTAL CO G/HP-HR 1.03 0.95 1.12 2.15 4.94 TOTAL HC G/HP-HR 0.17 0.22 0.26 0.34 0.73 PART MATTER G/HP-HR 0.08 0.11 0.15 0.19 0.26 TOTAL NOX (AS NO2) LB/HR 52.68 29.36 17.66 9.48 6.73 TOTAL CO LB/HR 5.90 4.09 3.27 3.34 3.49 TOTAL HC LB/HR 0.97 0.96 0.76 0.53 0.52 PART MATTER LB/HR 0.48 0.49 0.43 0.30 0.18 RATED SPEED NOMINAL DATA: 1800 RPM GENSET WITH FAN EKW 1,825.0 1,368.8 912.5 456.2 182.5 BHP 2,593 1,958 1,328 704 321 PERCENT LOAD % 100 75 50 25 10 TOTAL NOX (AS NO2) G/HR 19,913 11,098 6,674 3,582 2,545
TOTAL CO G/HR 1,487 1,031 824 841 880 TOTAL HC G/HR 331 329 260 182 176 TOTAL CO2 KG/HR 1,166 900 631 364 195 PART MATTER G/HR 155.1 160.3 139.2 95.7 58.4 TOTAL NOX (AS NO2) (CORR 5% O2) MG/NM3 3,695.8 2,658.4 2,265.1 2,108.4 2,733.8 TOTAL CO (CORR 5% O2) MG/NM3 278.2 248.5 281.8 499.7 972.9 TOTAL HC (CORR 5% O2) MG/NM3 61.5 78.8 88.3 107.2 189.0 PART MATTER (CORR 5% O2) MG/NM3 28.8 38.4 47.2 56.3 62.8 TOTAL NOX (AS NO2) (CORR 5% O2) PPM 1,801 1,296 1,103 1,028 1,338 TOTAL CO (CORR 5% O2) PPM 223 199 225 400 778 TOTAL HC (CORR 5% O2) PPM 99 127 143 173 307 TOTAL NOX (AS NO2) G/HP-HR 7.68 5.67 5.03 5.09 7.94 TOTAL CO G/HP-HR 0.57 0.53 0.62 1.19 2.74 TOTAL HC G/HP-HR 0.13 0.17 0.20 0.26 0.55 PART MATTER G/HP-HR 0.06 0.08 0.10 0.14 0.18 TOTAL NOX (AS NO2) LB/HR 43.90 24.47 14.71 7.90 5.61 TOTAL CO LB/HR 3.28 2.27 1.82 1.85 1.94 TOTAL HC LB/HR 0.73 0.73 0.57 0.40 0.39 TOTAL CO2 LB/HR 2,571 1,984 1,392 803 429 PART MATTER LB/HR 0.34 0.35 0.31 0.21 0.13 OXYGEN IN EXH % 11.0 12.0 12.7 14.0 15.9 DRY SMOKE OPACITY % 1.8 2.2 3.0 2.6 2.0 BOSCH SMOKE NUMBER 0.61 0.76 1.11 0.95 0.66 Regulatory Information Top EPA TIER 1 2000-2005 GASEOUS EMISSIONS DATA MEASUREMENTS PROVIDED TO THE EPA ARE CONSISTENT WITH THOSE DESCRIBED IN EPA 40 CFR PART 89 SUBPART D AND ISO 8178 FOR MEASURING HC, CO, PM, AND NOX. *THE "MAX LIMITS" SHOWN BELOW ARE WEIGHTED CYCLE AVERAGES AND ARE IN COMPLIANCE WITH THE NON-ROAD REGULATIONS. Locality Agency Regulation Tier/Stage Max Limits - G/BKW - HR U.S. (INCL CALIF) EPA NON-ROAD TIER 1 CO: 11.4 NOx: 9.2 HC: 1.3 PM: 0.50 Altitude Derate Data Top ALTITUDE CORRECTED CAPABILITY (BHP) AMBIENT OPERATING TEMP (F) 30 40 50 60 70 80 90 100 110 120 130 140 NORMAL ALTITUDE (FT) 0 2,628 2,628 2,628 2,628 2,628 2,628 2,628 2,628 2,628 2,628 2,497 2,391 2,628 1,000 2,628 2,628 2,628 2,628 2,628 2,628 2,628 2,628 2,628 2,575 2,470 2,365 2,628 2,000 2,628 2,628 2,628 2,628 2,628 2,628 2,628 2,628 2,628 2,523 2,418 2,286 2,628 3,000 2,628 2,628 2,628 2,628 2,628 2,628 2,628 2,628 2,575 2,444 2,339 2,234 2,628 4,000 2,628 2,628 2,628 2,628 2,628 2,628 2,617 2,570 2,497 2,365 2,260 2,155 2,628 5,000 2,621 2,621 2,621 2,621 2,617 2,568 2,521 2,476 2,418 2,286 2,181 2,050 2,621 6,000 2,538 2,538 2,538 2,538 2,520 2,473 2,428 2,385 2,313 2,208 2,076 1,971 2,538 7,000 2,458 2,458 2,458 2,458 2,426 2,381 2,338 2,296 2,208 2,102 1,997 1,892 2,458 8,000 2,381 2,381 2,381 2,381 2,336 2,292 2,251 2,210 2,102 1,997 1,892 1,708 2,381 9,000 2,307 2,307 2,307 2,291 2,248 2,206 2,166 2,102 1,997 1,892 1,734 1,498 2,307 10,000 2,236 2,236 2,236 2,204 2,162 2,122 2,084 1,997 1,892 1,813 1,524 1,314 2,236 11,000 2,167 2,167 2,161 2,120 2,080 2,041 1,918 1,787 1,656 1,524 1,314 1,183 2,167 12,000 2,101 2,101 2,078 2,038 1,997 1,866 1,734 1,603 1,472 1,314 1,183 1,051 2,101 13,000 2,024 2,024 1,997 1,945 1,813 1,682 1,524 1,393 1,261 1,183 1,051 946 2,024 14,000 1,971 1,958 1,866 1,734 1,603 1,472 1,340 1,235 1,130 1,051 946 841 1,970 15,000 1,892 1,813 1,682 1,551 1,419 1,288 1,183 1,104 1,025 946 867 762 1,892 Cross Reference Top Engine Arrangement
Arrangement Number Effective Serial Number Engineering Model 1979039 1HZ02896 GS034 - Test Specification Data Engineering Model Version Test Spec Setting Effective Serial Number Engine Arrangement Governor Type 0K2955 GG0005 1HZ02896 1979039 ADEM3 0K5841 GG0218 1HZ02896 1979039 ADEM3 Default Low Idle Speed Default High Idle Speed General Notes Top DM4683-02 SOUND PRESSURE DATA FOR THIS RATING CAN BE FOUND IN PERFORMANCE NUMBER - DM8779 Supplementary Data Top Type Classification Performance Number SOUND SOUND PRESSURE DM8779 Performance Parameter Reference Top Parameters Reference: DM9600-06 PERFORMANCE DEFINITIONS PERFORMANCE DEFINITIONS DM9600 APPLICATION: Engine performance tolerance values below are representative of a typical production engine tested in a calibrated dynamometer test cell at SAE J1995 standard reference conditions. Caterpillar maintains ISO9001:2000 certified quality management systems for engine test Facilities to assure accurate calibration of test equipment. Engine test data is corrected in accordance with SAE J1995. Additional reference material SAE J1228, J1349, ISO 8665, 3046-1:2002E, 3046-3:1989, 1585, 2534, 2288, and 9249 may apply in part or are similar to SAE J1995. Special engine rating request (SERR) test data shall be noted. PERFORMANCE PARAMETER TOLERANCE FACTORS: Power +/- 3% Torque +/- 3% Exhaust stack temperature +/- 8% Inlet airflow +/- 5% Intake manifold pressure-gage +/- 10% Exhaust flow +/- 6% Specific fuel consumption +/- 3% Fuel rate +/- 5% Specific DEF consumption +/- 3% DEF rate +/- 5% Heat rejection +/- 5% Heat rejection exhaust only +/- 10% Heat rejection CEM only +/- 10% Heat Rejection values based on using treated water. Torque is included for truck and industrial applications, do not use for Gen Set or steady state applications. On C7 - C18 engines, at speeds of 1100 RPM and under these values are provided for reference only, and may not meet the tolerance listed. These values do not apply to C280/3600. For these models, see the tolerances listed below. C280/3600 HEAT REJECTION TOLERANCE FACTORS: Heat rejection +/- 10% Heat rejection to Atmosphere +/- 50%
Heat rejection to Lube Oil +/- 20% Heat rejection to Aftercooler +/- 5% TEST CELL TRANSDUCER TOLERANCE FACTORS: Torque +/- 0.5% Speed +/- 0.2% Fuel flow +/- 1.0% Temperature +/- 2.0 C degrees Intake manifold pressure +/- 0.1 kpa OBSERVED PERFORMANCE IS CORRECTED TO SAE J1995 REFERENCE AIR AND FUEL CONDITIONS. REFERENCE ATMOSPHERIC INLET AIR FOR 3500 S AND SMALLER SAE J1228 AUG2002 for marine engines, and J1995 JAN2014 for other engines, reference atmospheric pressure is 100 KPA (29.61 in hg), and standard temperature is 25deg C (77 deg F) at 30% relative humidity at the stated aftercooler water temp, or inlet manifold temp. FOR 3600 S Engine rating obtained and presented in accordance with ISO 3046/1 and SAE J1995 JANJAN2014 reference atmospheric pressure is 100 KPA (29.61 in hg), and standard temperature is 25deg C (77 deg F) at 30% relative humidity and 150M altitude at the stated aftercooler water temperature. MEASUREMENT LOCATION FOR INLET AIR TEMPERATURE Location for air temperature measurement air cleaner inlet at stabilized operating conditions. REFERENCE EXHAUST STACK DIAMETER The Reference Exhaust Stack Diameter published with this dataset is only used for the calculation of Smoke Opacity values displayed in this dataset. This value does not necessarily represent the actual stack diameter of the engine due to the variety of exhaust stack adapter options available. Consult the price list, engine order or general dimension drawings for the actual stack diameter size ordered or options available. REFERENCE FUEL DIESEL Reference fuel is #2 distillate diesel with a 35API gravity; A lower heating value is 42,780 KJ/KG (18,390 BTU/LB) when used at 29 (84.2), where the density is 838.9 G/Liter (7.001 Lbs/Gal). GAS Reference natural gas fuel has a lower heating value of 33.74 KJ/L (905 BTU/CU Ft). Low BTU ratings are based on 18.64 KJ/L (500 BTU/ CU FT) lower heating value gas. Propane ratings are based on 87.56 KJ/L (2350 BTU/CU Ft) lower heating value gas. (NET) IS THE CORRECTED FLYWHEEL (GROSS) LESS EXTERNAL AUXILIARY LOAD Engine corrected gross output includes the power required to drive standard equipment; lube oil, scavenge lube oil, fuel transfer, common rail fuel, separate circuit aftercooler and jacket water pumps. Engine net power available for the external (flywheel) load is calculated by subtracting the sum of auxiliary load from the corrected gross flywheel out put power. Typical auxiliary loads are radiator cooling fans, hydraulic pumps, air compressors and battery charging alternators. For Tier 4 ratings additional Parasitic losses would also include Intake, and Exhaust Restrictions. ALTITUDE CAPABILITY Altitude capability is the maximum altitude above sea level at standard temperature and standard pressure at which the engine could develop full rated output power on the current performance data set.
Standard temperature values versus altitude could be seen on TM2001. When viewing the altitude capability chart the ambient temperature is the inlet air temp at the compressor inlet. Engines with ADEM MEUI and HEUI fuel systems operating at conditions above the defined altitude capability derate for atmospheric pressure and temperature conditions outside the values defined, see TM2001. Mechanical governor controlled unit injector engines require a setting change for operation at conditions above the altitude defined on the engine performance sheet. See your Caterpillar technical representative for non standard ratings. REGULATIONS AND PRODUCT COMPLIANCE TMI Emissions information is presented at 'nominal' and 'Potential Site Variation' values for standard ratings. No tolerances are applied to the emissions data. These values are subject to change at any time. The controlling federal and local emission requirements need to be verified by your Caterpillar technical representative. Log on to the Technology and Solutions Divisions (T&SD) web page (https://pdgt.cat.com/cda/layout) for information including federal regulation applicability and time lines for implementation. Information for labeling and tagging requirements is also provided. NOTES: Regulation watch covers regulations in effect and future regulation changes for world, federal, state and local. This page includes items on the watch list where a regulation change or product change might be pending and may need attention of the engine product group. For additional emissions information log on to the TMI web page. Additional product information for specific market application is available. Customer's may have special emission site requirements that need to be verified by the Caterpillar Product Group engineer. HEAT REJECTION DEFINITIONS: Diesel Circuit Type and HHV Balance : DM9500 EMISSIONS DEFINITIONS: Emissions : DM1176 SOUND DEFINITIONS: Sound Power : DM8702 Sound Pressure : TM7080 RATING DEFINITIONS: Agriculture : TM6008 Fire Pump : TM6009 Generator Set : TM6035 Generator (Gas) : TM6041 Industrial Diesel : TM6010 Industrial (Gas) : TM6040 Irrigation : TM5749 Locomotive : TM6037 Marine Auxiliary : TM6036 Marine Prop (Except 3600) : TM5747 Marine Prop (3600 only) : TM5748 MSHA : TM6042 Oil Field (Petroleum) : TM6011 Off-Highway Truck : TM6039 On-Highway Truck : TM6038 Date Released : 5/12/14