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특허 상세정보

Bleed air systems for use with aircraft and related methods

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-006/08    F02C-007/047    F02K-003/02    F02C-007/32    F02C-007/36    F02C-009/18    F02C-007/141    B64D-013/06   
출원번호 US-0242493 (2014-04-01)
등록번호 US-10054051 (2018-08-21)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Hanley, Flight & Zimmerman, LLC
인용정보 피인용 횟수 : 0  인용 특허 : 47
초록

Bleed air systems for use with aircraft and related methods are disclosed. An example apparatus includes a compressor having a compressor inlet and a compressor outlet. The compressor is to be driven by a drive shaft extending from an engine of an aircraft. The example apparatus also includes a first passageway to fluidly couple a first low-pressure bleed air port from the engine to the compressor inlet and a second passageway to fluidly couple the compressor outlet to a system of the aircraft.

대표
청구항

1. An apparatus comprising: a shaft-driven compressor system comprising: a compressor having a compressor inlet and a compressor outlet, the compressor to be driven by a drive shaft extending from an engine of an aircraft;a first passageway to fluidly couple a first bleed air port of a low-pressure compressor of the engine to the compressor inlet;a second passageway to fluidly couple the compressor outlet to a system of the aircraft; anda first flow control member operable between a first position to enable the shaft-driven compressor system to supply bl...

이 특허에 인용된 특허 (47)

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