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특허 상세정보

Translating independently mounted air inlet system for aircraft turbofan jet engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64D-029/00   
미국특허분류(USC) 244/053B; 244/054
출원번호 US-0580900 (2000-05-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    James M. Rashid
인용정보 피인용 횟수 : 93  인용 특허 : 4
초록

An arrangement for an aircraft propulsion system to determinably reduce or eliminate inlet cowl induced bending of a turbofan aircraft jet engine case during certain flight conditions. The arrangement includes a turbofan aircraft jet engine having an engine case with a fan case portion, a nacelle structure housing the engine and having a forward nacelle portion and a rearward nacelle portion, and a pylon structure to support the engine and the nacelle structure while permitting the forward nacelle structure to be translated forwardly from an operational ...

대표
청구항

1. An aircraft propulsion system arrangement to determinably reduce or eliminate inlet cowl induced bending of an aircraft jet engine case during certain flight conditions, which arrangement comprises a turbofan aircraft jet engine having an engine case with a fan case portion, a nacelle structure housing the engine and having a forward generally cylindrical nacelle portion and a rearward nacelle portion, and a pylon structure to support the engine and the nacelle structure while permitting relative movement between the forward and rearward nacelle porti...

이 특허를 인용한 특허 피인용횟수: 93

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