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특허 상세정보

Structure for eliminating lift load bending in engine core of turbofan

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-027/00   
미국특허분류(USC) 244/54 ; 248/554 ; 60/3931
출원번호 US-0765804 (1991-09-26)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 50  인용 특허 : 0
초록

A structure for removing bending caused by an inlet lift load in the engine core of an aircraft having a support frame which is attached to a frame mount which connects to the pylon floor. The frame mount is located between a forward mount and a rear mount and to the front of the engine core. As a result of the frame mount, the moment created by the inlet lift load is not reacted through the engine core so engine performance is not affected.

대표
청구항

A mounting structure for securing a turbofan engine assembly to an aircraft, said turbofan engine assembly including an engine core section, said mounting structure comprising: auxiliary mounting means for removing bending in the engine core section, said auxiliary mounting means being located between a forward mount location and a rear mount location, said auxiliary mounting means being located in a direction forward of the engine core section; an outer nacelle connected to said auxiliary mounting means said auxiliary mounting means comprising a frame s...

이 특허를 인용한 특허 피인용횟수: 50

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