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특허 상세정보

Multi role primary/auxiliary power system with engine start capability for aircraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/268    F02C-007/32   
미국특허분류(USC) 60/3907 ; 60/39142
출원번호 US-0502902 (1983-06-10)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 50  인용 특허 : 1
초록

The invention is a multi role primary/auxiliary power system with engine start capability for aircraft that provides electric, mechanical and air conditioning power as well as engine starting functions. The compressor (20), turbine (26) and motor/generator (24) are coupled to a drive shaft (14) of the aircraft\s engine (12) with the motor/generator (24) mounted between the compressor (20) and turbine (26). A first clutch (28) is mounted on the drive shaft (14) between the motor/generator (24) and the turbine (26). Coupled to the outlet (29) of the compre...

대표
청구항

A multi role primary/auxiliary power system for an aircraft having at least one engine, said engine having a drive shaft, said power system comprising: a turbine coupled to said drive shaft; a compressor coupled to said drive shaft; a motor/generator coupled to said drive shaft, said motor/generator mounted between said compressor and said turbine; first passage means coupling the outlet of said compressor to said inlet of said turbine; a combustor mounted in said first passage means; first clutch means mounted on said drive shaft adapted to disengage sa...

이 특허를 인용한 특허 피인용횟수: 50

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