All/More Electric Aircraft Engine & Airframe Systems - Turbo & Jet ...

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Effects of Takeoff on Turbine Entry Temperature (TET) TET increases in proportion to the percentage of takeoff power relative to the total power within the core of the engine Unclassified 10
Effects of Bleed Air and Shaft Power on Compressor Characteristics • Taking bleed air from the compressor requires an increase in fuel flow and hence temperature. • When shaft power is extracted the turbine has to deliver extra work at a given speed and this can occur by increasing TET. Unclassified 11
Page 1 and 2: The 9th Israeli Symposium on Jet En
Page 3 and 4: Evolution of the All/More Electric
Page 5 and 6: “Conventional” Philosophy (Cont
Page 7 and 8: “Conventional” Philosophy (Cont
Page 9: Effects of Takeoff on Aircraft Oper
Page 13 and 14: “Electric Aircraft” Philosophy
Page 17 and 18: “Electric Aircraft” Unclassifie
Page 19 and 20: “Electric Aircraft” Improved re
Page 23 and 24: Secondary Power Systems (SPS) Distr
Page 25 and 26: Conventional Secondary Power System
Page 27 and 28: Typical Power Level of Electrical L
Page 29 and 30: AC Power Generation & Regenerative
Page 31 and 32: B787 “Bleedless” System Archite
Page 33 and 34: B787 Hybrid Electrical Power Distri
Page 35 and 36: Conventional Vs. Electric ECS Conve
Page 37 and 38: Actuation System The four‐engine
Page 39 and 40: Impact of Aircraft and Engine Desig
Page 41 and 42: Impact of Aircraft and Engine Desig
Page 43 and 44: Impact of the AEA Concept Implicati
Page 45 and 46: More Electric Engine (MEE) Challeng
Page 47 and 48: IAI More “Electric Aircraft” B7

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