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특허 상세정보

Aircraft bleed air and engine starter systems and related methods

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/27    F02C-006/08   
출원번호 US-0744398 (2015-06-19)
등록번호 US-10100744 (2018-10-16)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Hanley, Flight & Zimmerman, LLC
인용정보 피인용 횟수 : 0  인용 특허 : 48

Example bleed air and engine starter systems are described herein that employ a shaft-driven compressor to start an aircraft engine and/or to supply pressurized air to one or more systems of an aircraft. An example compressor includes a housing and an impeller disposed within a cavity of the housing. The impeller is operatively coupled to a drive shaft. The compressor includes a first port in the housing to direct onto the impeller to rotate the impeller when the compressor is operating in a first mode. In the first mode, the impeller is to drive the dri...


1. A compressor comprising: a housing;an impeller disposed within a cavity of the housing, the impeller operatively coupled to a drive shaft;a first port in the housing oriented to provide air to the impeller when the impeller is operating in a first mode, wherein in the first mode the drive shaft is to rotate the impeller to draw the air from the first port and increase a pressure of the air; anda second port in the housing to direct air onto the impeller to rotate the impeller when the compressor is operating in a second mode, wherein in the second mod...

이 특허에 인용된 특허 (48)

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