Transcription of General Electric CF34 Engine - MrMoo.net
{{id}} {{{paragraph}}}
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
spinner single stage fan bypass ratio 6.2:1 fan blade containment casing accessory gear box fan vane 14 stage high pressure axial compressor flow through annular combustion
Domain:
Source:
Link to this page:
Please notify us if you found a problem with this document:
{{id}} {{{paragraph}}}
A100 control valve, Pressure, A100 CONTROL VALVE Valve, Series 100 Valves, Valve, POSITIVE DISPLACEMENT ETERS, Trane, Sustaining, Chiller perormancf e testing program, Large Chilled Water System Design Seminar, PURE. PERFORMANCE, Pure Performance, Typical Specifications For Dynaforce® Hydronic, Typical Specifications For Dynaforce® Hydronic Heating