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특허 상세정보

Methods and systems for operating oxidizer systems

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02K-003/00    F02K-007/00    F02K-009/00    F02K-099/00   
미국특허분류(USC) 060/224; 060/785
출원번호 US-0994709 (2004-11-22)
등록번호 US-8127527 (2012-03-06)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Clement, Esq., David J.
인용정보 피인용 횟수 : 0  인용 특허 : 17
초록

A method and system for operating a gas turbine engine is provided. The system includes in serial flow arrangement, at least one compressor, a combustor, and at least one turbine. The method includes compressing atmospheric air in the gas turbine engine, channeling at least a portion of the compressed air from the turbine engine flowpath to an oxidizer supply system, and channeling an oxygen-depleted flow of the compressed air from the oxidizer supply system to the gas turbine engine flowpath.

대표
청구항

1. A method of operating an auxiliary gas turbine engine on an aircraft having a propulsion engine, said method comprising: providing an auxiliary gas turbine engine that is configured to be non-propulsive and includes, in serial flow arrangement, at least one compressor, a combustor, and at least one turbine;channeling ambient air into the auxiliary gas turbine engine during proper operation of the propulsion engine;compressing the ambient air in the auxiliary gas turbine engine;channeling at least a portion of the compressed air from the auxiliary gas ...

이 특허에 인용된 특허 (17)

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