Electric power generation using power turbine aft of lpt

F - Mech Eng,Light,Heat,Weapons – 02 – C

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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).

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