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특허 상세정보

MyON담기
내보내기 페이스북 공유 카카오톡 공유

ATR full ring sliding nacelle

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-025/24    B64D-029/06    F01D-025/28    F01D-009/02   
출원번호 US-0187021 (2014-02-21)
등록번호 US-9617009 (2017-04-11)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Kinney & Lange, P.A.
인용정보 피인용 횟수 : 0  인용 특허 : 50
초록
▼

A gas turbine engine includes a core, a first annular portion, a rail, and a second annular portion. The first annular portion is stationary and adapted for partially surrounding an engine core. The first annular portion includes a fore pylon connecting portion, and a fore bi-fi. The rail is coupled to the fore pylon portion and extending in the aft direction from the stationary portion. The second annular portion is arranged aft of the first portion and coupled to the rail. The second annular portion is movable along an engine core centerline between a ...

대표
청구항
▼

1. A gas turbine engine comprising: a first annular portion that is stationary and adapted for partially surrounding an engine core, wherein the first annular portion includes: a fore pylon connecting portion; anda fore bi-fi comprising an upper fore portion located radially above the engine core, and a lower fore portion located radially below the engine core;a rail coupled to the fore pylon portion and extending in the aft direction from the stationary portion; anda second annular portion, aft of the first portion and coupled to the rail, the second an...

이 특허에 인용된 특허 (50)

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  9. Jannetta, Thomas J.; Peters, Frederick H.. Converging nozzle thrust reverser. USP2003056568172.
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  50. Bubello Robert (Meriden CT) Ream Jeffrey L. (Tollano CT). Ventilation system for a nacelle. USP1989054825644.

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