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특허 상세정보

Turbofan case and method of making

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/02   
미국특허분류(USC) 060/226.1; 415/208.3; 415/209.4
출원번호 UP-0780609 (2007-07-20)
등록번호 US-7765787 (2010-08-24)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Ogilvy Renault LLP
인용정보 피인용 횟수 : 12  인용 특허 : 48
초록

A casing for a gas turbine includes a construction providing improved structural efficiency. Improved load paths and means for transmitting loads in the engine case are disclosed.

대표
청구항

We claim: 1. A casing for an aircraft turbofan bypass engine, the casing comprising: a case adapted to encircle the engine and having a plurality of engine mounts thereon adapted to mount the engine to an aircraft; an inner hub adapted to support at least one bearing supporting a main shaft of the engine, a airflow path through the engine defined by and between the inner hub and the case, the inner hub supported inside the case by a plurality of thin-walled struts each extending continuously from the inner hub to the case, the struts having a continuous...

이 특허에 인용된 특허 (48)

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