Transcription of General Electric CF34 Engine - MrMoo.net
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SINGLE STAGE FANBYPASS RATIO :1 SPINNERFAN BLADECONTAINMENT CASINGACCESSORYGEAR BOXFAN VANE14 STAGEHIGH PRESSUREAXIAL COMPRESSORFLOW THROUGHANNULARCOMBUSTION4 STAGELOW PRESSURETURBINE2 STAGEHIGH PRESSURETURBINEG eneral Electric cf34 EngineChallenger 601 Developed for Training PurposesNovember 19974-175 PowerplantCAE SimuFlite4-176 Developed for Training PurposesChallenger 601 November 1997 Challenger 601 Developed for Training PurposesNovember 1997 Engine Oil SystemOIL TANK21675432 ACCESSORYGEARBOXORIFICEHEATEXCHANGERFILT ER ELEMENTBYPASS VALVERELIEF VALVECHECKVALVEFUELIMPENDINGBYPASSSENSOR LUBE AND SCAVENGEPUMP ASSEMBLYELECTRICMASTER CHIPDETECTORDRAINPORTSCAVENGE SCREENS(8 PLACES)A-SUMPSCAVENGEPUMPTANK PRESSURERELIEF VALVEDEAERATORSUPPLY OILSCAVENGE OILVENTCHIP DETECTOR,INSTALLED ON 1A/3A;OPTIONAL ON 3 RPRESSURETRANSMITTER1C-SUMP6 & 7 BEARINGB-SUMP4 & 5 BEARINGA-SUMP1, 2 & 3 BEARINGOIL LEVEL PROBEOIL TEMP PROBESCAVENGEELEMENTS(6)PRESSUREELEMENT1 111B-SUMPVENT AIRREGULATINGVALVE1114-177 PowerplantCAE SimuFlite4-178 Developed for Training PurposesCh
Powerplant Challenger 601 Developed for Training Purposes 4-181 November 1997 Powerplant Two General Electric CF34 turbofan engines power the Canadair Challenger CL-601-1A/-3A/3R aircraft (see Table 4-N). CL-601-1A CF34-1A CF34-3A/-3A2
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