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

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All/More “Electric Aircraft” Architecture Unclassified (2.5%) 26
Typical Power Level of Electrical Loads Power User Comments Typical Power Level Air Conditioning ECS 4 x 70 kW+ Flight Controls Primary & Secondary 3 kW to 40 kW Unclassified short duration at high loads Fuel Pumps About 10 kW Wing Ice Protection Thermal mats or similar 250 kW+ Landing Gear Retraction, steering and braking Engine Starting May be used for additional applications 25 kW to 70 kW short duration 200 kW+ Short duration 27
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 and 10: Effects of Takeoff on Aircraft Oper
Page 11 and 12: Effects of Bleed Air and Shaft Powe
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: Conventional Secondary Power System
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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