Aircraft auxiliary gas turbine engine and method for operating

Details Aircraft auxiliary gas turbine engine and method for operating Aircraft auxiliary gas turbine engine and method for operating

B - Operations, Transporting

64

D

B64D 33/02 (2006.01) B64D 13/00 (2006.01) F02C 7/045 (2006.01) F02C 9/18 (2006.01)

Patent

CA 2576683

A non-aircraft-propelling auxiliary gas turbine engine (10) installable in an aircraft (12) having a cabin (16) adapted to be pressurized. The auxiliary gas turbine engine includes an auxiliary-gas-turbine-engine compressor (18) having an inlet (20), wherein the inlet is adapted to receive pressurized air (22) from the cabin.

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