System and method for providing air to a compressor of an...

B - Operations – Transporting – 64 – D

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Details

B64D 41/00 (2006.01) B64D 13/00 (2006.01) B64D 27/00 (2006.01) B64D 33/02 (2006.01) F01D 13/02 (2006.01) F02C 1/02 (2006.01) F02C 7/04 (2006.01)

Patent

CA 2582806

A system (10) for providing air (12) to a compressor (16) of an auxiliary gas turbine engine (18) of an aircraft (20). A system turbine (26) has an inlet (30) adapted to receive compressed air (34) from the aircraft. A system compressor (28) is mechanically coupled to the system turbine and has an inlet (36) adapted to receive atmospheric air (40). The outlets of the system turbine and the system compressor are fluidly connectable to the inlet of the compressor of the auxiliary gas turbine engine.

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