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특허 상세정보

Aircraft gas turbine engine thrust mount

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/20   
미국특허분류(USC) 60/3931 ; 248/554 ; 244/54
출원번호 US-0116621 (1993-09-07)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 63  인용 특허 : 0
초록

An engine mount assembly includes an axially pivotable engine support and a thrust mount with a three or four bar linkage which includes a thrust bar, as the first bar, pivotably joined to a forward axial position on the engine structure at the forward end of the first bar. The line of action of the thrust bar intersects the engine centerline at a forward vertical mount plane, which is generally perpendicular to the engine centerline and through which a forward pivotal support mount of the engine support acts to support the engine, substantially at the a...

대표
청구항

A mount assembly for mounting an aircraft gas turbine engine to an aircraft by its engine structure which supports the engine rotor assembly about an engine centerline, said mount assembly comprising; a pivotable engine support for suspending the engine from the aircraft including a forward support mount and an aft support mount which permit at least limited axial movement of the engine such that a thrust bar of a thrust mount system transmits substantially all of the thrust from the engine to the aircraft, said thrust mount system having a linkage with ...

이 특허를 인용한 특허 피인용횟수: 63

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