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특허 상세정보

Forward compartment baffle arrangement for a geared turbofan engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-025/18    F01D-025/24    F02K-003/06    F02C-007/06    F02C-007/36   
출원번호 US-0709153 (2012-12-10)
등록번호 US-9896968 (2018-02-20)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Bachman & LaPointe, P.C.
인용정보 피인용 횟수 : 0  인용 특허 : 40
초록

A baffle within a gas turbine engine includes a cylindrical flange with a multiple of holes at least partially therearound.

대표
청구항

1. An engine case assembly within a gas turbine engine comprising: a baffle located radially inboard of an annular core flow path of the gas turbine engine, said baffle defined around an engine central longitudinal axis, wherein said baffle defines an axial length approximately 70%+25%/−30% of an axial length of said front center body from a forward most inner diameter bolt flange to an aft most inner diameter bolt flange, said baffle having a cylindrical flange with a multiple of holes at least partially therearound. 2. The assembly as recited in claim ...

이 특허에 인용된 특허 (40)

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