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특허 상세정보

Mounting for coupling a turbofan gas turbine engine to an aircraft structure

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/20    B64D-027/12   
미국특허분류(USC) 244/054 ; 248/555 ; 248/556 ; 60/039.31
출원번호 US-0625356 (1996-04-01)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Cushman Darby & Cushman Intellectual Property Group of Pillsbury Madison & Sutro LLP
인용정보 피인용 횟수 : 94  인용 특허 : 1
초록

A mounting for connecting a turbofan gas turbine engine to an aircraft structure comprises three mounting points at the vertices of a triangle on the aircraft structure and three mounting points on the fan casing of the turbofan gas turbine engine. The first mounting point on the aircraft structure is connected to all of the three mounting points on the fan casing by three links. The second mounting point on the aircraft structure is connected to the second mounting point and the third mounting point on the fan casing by two links. The third mounting poi...

대표
청구항

[ We claim:] [1.] A mounting for coupling a turbofan gas turbine engine to an aircraft structure, the turbofan gas turbine engine having an axis and comprising a core engine and a fan, the core engine having compressor means, combustion means, turbine means and a core casing, the fan operating within a fan duct defined in part by a fan casing, the fan casing extending from a fan duct intake to a fan duct nozzle,the aircraft structure having three mounting points on the aircraft structure, the three mounting points being arranged at the vertices of a firs...

이 특허를 인용한 특허 피인용횟수: 94

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