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특허 상세정보

Turbofan mounting arrangement

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-025/28    F04D-029/60    B64D-027/26    B64D-027/20    F01D-025/16    F02K-003/06   
미국특허분류(USC) 415/213.1; 248/554; 248/555; 060/226.1; 060/796
출원번호 US-0289067 (2011-11-04)
등록번호 US-8979491 (2015-03-17)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Norton Rose Fulbright Canada LLP
인용정보 피인용 횟수 : 3  인용 특허 : 45
초록

A gas turbine engine has a rear mounting structure incorporating a mounting apparatus attached to a bypass duct wall with a link device of six rods for transferring core portion related inertia-induced loads, from an inner case of the core portion in a short circuit across an annular bypass air passage to the bypass duct wall.

대표
청구항

1. A turbofan gas turbine engine comprising: a front mounting structure attached to an annular bypass duct wall at a front axial position adjacent an inlet of a bypass air passage, the bypass air passage defined by and radially between the bypass duct wall and an inner case of a core portion of the engine, the front mounting structure supporting the core portion within the bypass duct wall;a rear mounting structure having a mounting apparatus attached to the bypass duct wall at a rear axial position adjacent to an outlet of the bypass air passage, the re...

이 특허에 인용된 특허 (45)

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