A system for providing air to a compressor of an auxiliary gas turbine engine of an aircraft. A system turbine has an inlet adapted to receive compressed air from the aircraft. A system compressor is mechanically coupled to the system turbine and has an inlet adapted to receive atmospheric air. 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. A method includes providing compressed air from an aircraft to an inlet of a system turbine mechanically coupled...
The invention claimed is: 1. A system, for providing air to an inlet of a compressor of a non-aircraft-propelling auxiliary gas turbine engine of an aircraft having an aircraft-propelling gas turbine engine, comprising: a) a system turbine having an inlet and an outlet, wherein the inlet of the system turbine receives compressed air from the aircraft; b) a system compressor mechanically coupled to the system turbine and having an inlet and an outlet, wherein the inlet of the system compressor receives atmospheric air, and wherein the outlets of the syst...
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