F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 7/32 (2006.01) H02K 1/02 (2006.01) H02K 7/18 (2006.01)
Patent
CA 2612813
An inside out generator (20) disposed aft of the low-pressure turbine spool (46) to generate power for the electrical demands of an aircraft system. The low- pressure turbine (46) discharge flow is used to drive the power turbine (45), which is coupled to the generator (20). The generator (20) is able to extract power at idle conditions of the aircraft engine (10) from ducting the discharge through the inside out generator (20). The system eliminates the placement of a generator (20) in the hot gas path of the discharge, and enables the injection of power directly to the accessory gear box of the engine (10).
Chung Kiyoung
Compton Tom
Glynn Christopher
Kern John M.
Qu Ronghai
Company General Electric
Craig Wilson And Company
LandOfFree
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