Cat C280-8 Genset Spec Sheet
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PATE R PI LLAR" & diesel electr|c 2300 bkw (^84 actual engine *A new S»OSSM analysis must be done to determine actual oil change intervals. STANDARD EQUIPMENT_ Aftercooler — fresh water, corrosion resistant coated (air side); air inlet shutoff; breather — crankcase, top-mounted; turbocharger — engine oil Control System Single ADEM™ A3 electronic control unit (ECU) with electronic unit injector fuel system, rigid wiring harness (10 amp, 24 volt power required to drive Cooling System Engine coolant water drains Exhaust System Dry, gas tight, exhaust manifold Fuel System Distillate fuel (requires viscosity ranging from 1.4 cSt to 20 cSt at 38° C), fuel transfer pump (mounted on left-hand side), duplex fuel filters, electronically controlled unit injectors Centrifugal oil filters with single shutoff, service side engine mounted on cylinder block inspection covers includes installed oil lines and single shutoff valve, filters centrifuge bypass oil from the main lubricating oil pump, can be serviced with the engine running, oil filler and dipstick valve, oil pressure regulating valves, crankcase explosion relief valves Caterpillar yellow paint; gear-driven pumps: fuel, oil, jacket water, aftercooler/oil cooler water; service Factory-designed systems built at Caterpillar

C280-8 AUXILIARY & DIESEL ELECTRIC PROPULSION PERFORMANCE DATA DIESEL ENGINE TECHNICAL DATA JACKET WATER INLET (°C): 90 FIRING PRESSURE, MAXIMUM (kPa) 17300 IMO/EPA MARINE TIER I TURBOCHARGER PART #: FUEL TYPE: ASSUMED GENERATOR EFFICIENCY (%): ASSUMED GENERATOR POWER FACTOR MEAN PISTON SPEED (m/s): ENGINE DATA FUEL CONSUMPTION (NOMINAL) FUEL CONSUMPTION (90% CONFIDENCE) INLET MANIFOLD PRESSURE INLET MANIFOLD TEMPERATURE EXHAUST STACK TEMPERATURE EXHAUST GAS FLOW (@ stack temp, 101.3 kPa) EXHAUST GAS MASS FLOW ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046/1 ANDSAE J1995...

C280-8 AUXILIARY & DIESEL ELECTRIC PROPULSION PERFORMANCE DATA

C280-8 AUXILIARY & DIESEL ELECTRIC PROPULSION ENGINE DIMENSIONS RATING DEFINITIONS AND CONDITIONS CONTINUOUS POWER - 8,000 hrs./yr., for applications with load factors less than or equal to 100%. 10% overload available. RATINGS are based on SAE J1995/ISO3046 standard 30% relative humidity at the stated charge air cooler water temperature. Ratings also meet classification society maximum temperature requirements of 32°C (90°F) seawater temperature without derate. Additional ratings may be available for specific customer requirements. Consult your Caterpillar representative for additional...

PATE R PI LLAR" & diesel electr|c 2530 bkw ^b,p) actual engine *A new S»OSSM analysis must be done to determine actual oil change intervals. STANDARD EQUIPMENT_ Aftercooler — fresh water, corrosion resistant coated (air side); air inlet shutoff; breather — crankcase, top-mounted; turbocharger — engine oil Control System Single ADEM™ A3 electronic control unit (ECU) with electronic unit injector fuel system, rigid wiring harness (10 amp, 24 volt power required to drive Cooling System Engine coolant water drains Exhaust System Dry, gas tight, exhaust manifold Fuel System Distillate fuel...

C280-8 AUXILIARY & DIESEL ELECTRIC PROPULSION PERFORMANCE DATA DIESEL ENGINE TECHNICAL DATA JACKET WATER INLET (°C): 90 FIRING PRESSURE, MAXIMUM (kPa) 17300 IMO/EPA MARINE TIER I TURBOCHARGER PART #: FUEL TYPE: ASSUMED GENERATOR EFFICIENCY (%): ASSUMED GENERATOR POWER FACTOR MEAN PISTON SPEED (m/s): ENGINE DATA FUEL CONSUMPTION (NOMINAL) FUEL CONSUMPTION (90% CONFIDENCE) INLET MANIFOLD PRESSURE INLET MANIFOLD TEMPERATURE EXHAUST STACK TEMPERATURE EXHAUST GAS FLOW (@ stack temp, 101.3 kPa) EXHAUST GAS MASS FLOW_ ENERGY BALANCE DATA FUEL INPUT ENERGY (LHV) HEAT REJ. TO JACKET WATER ENGINE...

C280-8 AUXILIARY & DIESEL ELECTRIC PROPULSION PERFORMANCE DATA

C280-8 AUXILIARY & DIESEL ELECTRIC PROPULSION ENGINE DIMENSIONS RATING DEFINITIONS AND CONDITIONS PRIME POWER - 6,000 hrs./yr., for applications with load factors less than or equal to 60%. Rated load (100%) usage is limited to 1 hour in 12. 10% overload available. RATINGS are based on SAE J1995/ISO3046 standard 30% relative humidity at the stated charge air cooler water temperature. Ratings also meet classification society maximum temperature requirements of 32°C (90°F) seawater temperature without derate. Additional ratings may be available for specific customer requirements. Consult your...

PATE R PI LLAR" & diesel electr|c 2460 bkw ^b,p) actual engine *A new S»OSSM analysis must be done to determine actual oil change intervals. STANDARD EQUIPMENT_ Aftercooler — fresh water, corrosion resistant coated (air side); air inlet shutoff; breather — crankcase, top-mounted; turbocharger — engine oil Control System Single ADEM™ A3 electronic control unit (ECU) with electronic unit injector fuel system, rigid wiring harness (10 amp, 24 volt power required to drive Cooling System Engine coolant water drains Exhaust System Dry, gas tight, exhaust manifold Fuel System Distillate fuel...

C280-8 AUXILIARY & DIESEL ELECTRIC PROPULSION PERFORMANCE DATA DIESEL ENGINE TECHNICAL DATA JACKET WATER INLET (°C): 90 FIRING PRESSURE, MAXIMUM (kPa) 17300 IMO/EPA MARINE TIER I TURBOCHARGER PART #: FUEL TYPE: ASSUMED GENERATOR EFFICIENCY (%): ASSUMED GENERATOR POWER FACTOR: MEAN PISTON SPEED (m/s): ENGINE DATA FUEL CONSUMPTION (NOMINAL) FUEL CONSUMPTION (90% CONFIDENCE) INLET MANIFOLD PRESSURE INLET MANIFOLD TEMPERATURE EXHAUST STACK TEMPERATURE EXHAUST GAS FLOW (@ stack temp, 101.3 kPa) EXHAUST GAS MASS FLOW ENGINE RATING OBTAINED AND PRESENTED IN ACCORDANCE WITH ISO 3046/1 AND SAE J1995...

C280-8 AUXILIARY & DIESEL ELECTRIC PROPULSION PERFORMANCE DATA DIESEL ENGINE TECHNICAL DATA ALTITUDE DERATION FACTORS ALTITUDE (METERS ABOVE SEA LEVEL) AFTERCOOLER HEAT REJECTION FACTORS ALTITUDE (METERS ABOVE SEA LEVEL) FREE FIELD MECHANICAL NOISE SOUND PRESSURE LEVEL dB(A) FREE FIELD EXHAUST NOISE TOTAL DERATION FACTORS: This table shows the deration required for various air inlet temperatures and altitudes. Use this information to help determine actual engine power for your site. The total deration factor includes deration due to altitude and ambient temperature, and air inlet manifold...