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특허 상세정보

Resilient pivot type aircraft mounting

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-027/00   
미국특허분류(USC) 244/54 ; 244/131 ; 60/3931 ; 248/557
출원번호 US-0770058 (1991-09-30)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 41  인용 특허 : 0
초록

A pivot type aircraft mounting for resiliently connecting a structure to an aircraft engine which uses a pivoting and siding joint on a beam at the engine attachment point, a vertically stiff and laterally soft intermediate pivot joint on the beam, and a resilient compression section near the end of the beam for reacting the engine loads into the structure and providing the desired spring rates in the vertical and lateral direction. The invention can utilize low friction pivoting and sliding joints such as nylon lines bearings or elastomeric bearings. Th...

대표
청구항

A resilient engine mounting for flexibly attaching an aircraft engine to a structure, comprising: (a) a first pivot means slidably receiving a first portion of a beam for connecting said beam to said engine about said first portion of said beam and accommodating pivoting motion and sliding motion of said beam relative to said engine; (b) spring means attached at a second portion of said beam spaced along said beam from said first portion, said spring means reacting engine loads into a housing; (c) a second pivot means located in said housing at a third p...

이 특허를 인용한 특허 피인용횟수: 41

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