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특허 상세정보

Mounting for gas turbine powerplant

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/20    B64D-027/20   
미국특허분류(USC) 244/54 ; 60/226R ; 248/554
출원번호 US-0124735 (1980-02-26)
우선권정보 GB-0008516 (1979-03-10)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 58  인용 특허 : 2
초록

A gas turbine powerplant has an inner casing (4A) containing a gas turbine engine, an outer casing (5) surrounding the inner casing, a fan driven by the engine and driving air through an annular duct defined between the casings. The powerplant is connected to an aircraft fuselage (1) by a front mounting (9,9A,9B,9C) and by a rear mounting (8,10,17,18). The front and rear mountings react lateral forces on the powerplant. The powerplant includes a thrust reverser (11) situated rearwards of the rear mounting and supported by a ring (18) lying in the annulus...

대표
청구항

A mounting for a gas turbine powerplant which comprises an inner annular casing containing a gas turbine engine, an outer annular casing surrounding the inner casing, a compressor connected to be driven by the engine and adapted to drive air through an annular duct defined between the casings, and a thrust reverser means at the outer casing for reversing the flow therethrough; the mounting comprising front and rear structural means arranged respectively at a front and rear location of the powerplant for supporting the powerplant laterally on a support si...

이 특허를 인용한 특허 피인용횟수: 58

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  29. Norris, James W.; Nordeen, Craig A.. Plurality of individually controlled inlet guide vanes in a turbofan engine and corresponding controlling method. USP2014028641367.
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  35. Heyerman, Jeffrey Bernard; Olver, Bryan W.. Support links with lockable adjustment feature. USP2016029267435.
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