The Aircraft Engine Design Project Fundamentals of Engine ...

GE Aircraft EnginesgGE AviationThe Aircraft Engine Design Project Fundamentals of Engine CyclesKen GouldPhil WeedSpring 20091GE Aircraft EnginesgGE Aviation Technical HistoryGE Aviation Technical jet turboprop engineVibl ttiVariable stator engineMach 2 fighter engineMach 3 bomber engineHigh bypass engineVariable cycle turbofan engineUnducted fan engineI-A - First jet engineGE90 on test(Developed in Lynn, MA, 1941)Unducted fan engine30:1 pressure ratio engineDemonstration of 100k+ Engine thrustCertified double annular combustor engineFirst turboprop powered Aircraft , Dec. 19452T L I K O P F T L I K O P F GE Aircraft EnginesgFlowdown of RequirementsThe Customer: Overall system requirementsMTOW, Range, Cost per seat per mileThe Airframer: Sub-system requirementsTechnical: Wing (lift/drag),Engines(Thrust/SFC)CSProgram :Cost and ScheduleFAA/JAAE ngines Systems: Module requirementsfffFAA/JAAS afety/reliabilityNoise/emissionsQualifie d ProductTechnical: Pressure ratio, efficiency, weight, lifeProgram:NRE, part cost, schedule, validation plan3 Design & ValidationGE Aircraft EnginesgThe Aircraft Engine Design ProjectHPT CombustorThe Aircraft Engine Design Project Fundamentals of Engine CyclesCompressorCombustorExhaustTbjtE iairflow4 Turbojet EngineInletGE Aircraft EnginesgEngine Modules and ComponentsTurbojet StationsCompressorEngine Modules and ComponentsCombustorHPT Inlet Exit

g GE Aviation Technical History GE Aircraft Engines U.S. jet engine U.S. turboprop engine Vibl tt iVariable stator engine Mach 2 fighter engine Mach 3 bomber engine High bypass engine Variable cycle turbofan engine

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