A gas turbine powered aircraft auxiliary power system is described. The system is capable of efficiently supplying all aircraft auxiliary services both in flight and on the ground. It is capable also of operating independently of the aircraft main engines. The system employs multiple gas turbine compressor stages, and utilizes the aircraft cabin as a plenum chamber between the first and second compressor stages, thereby accomplishing cabin pressurization, ventilation and heating.
Independent Power Generator
1976
16 pages
Report
No indication
English
NTRS | 1978
|POWER SYSTEM FOR HYBRID UNMANNED AERIAL VEHICLE USING INDEPENDENT MULTY PHASE GENERATOR
European Patent Office | 2019
|