A unique airborne electrical power and thermal management system and a unique aircraft having a unique airborne electrical power and thermal management system are provided. The electrical power and thermal management system includes a turbine, which may power loads, for example but not limited to, a generator and a refrigerant compressor. The turbine may be in fluid communication with a gas turbine engine bleed air source to extract power from bleed air for powering the loads. A combustor may be fluidly disposed between the bleed air source and the turbi...
1. An airborne electrical power and thermal management system, comprising: a first gas turbine engine having a first combustor, a first turbine and a bleed air port, the first gas turbine engine operable for producing propulsive power for an aircraft;a second gas turbine engine including: a second combustor in fluid communication with the first gas turbine engine bleed air port; anda second turbine in fluid communication with the second combustor;a generator powered by the second turbine and configured to provide electrical power to an electrical load;a ...
이 특허에 인용된 특허 (14)
- Evans Hugh G. (W. 214 6th Ave. Spokane WA 99204) Speer Stephen (S. 358 Couer d\Alene Apt. #6 Spokane WA 99204) Christy James S. (E. 10918 26th Spokane WA 99204) Lafrenz Stanley S. (P.O. Box 1356 Sand. Aircraft air conditioning system. USP1983084399665.
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