Transcription of The Aircraft Engine Design Project Fundamentals of Engine …
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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 requirementsff
X XX X Design Considerations Process Centering and Variation X XX X XXX X X X X X X X On-Target X X Reduce Spread Center Process X X X X X XXXXXX X Six Sigma Methodology Applies Statistical Analyses to Center 17 ggypp y Processes and Minimize Variation General Electric Aircraft Engines.
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