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특허 상세정보

Gas turbine combustor

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-001/00   
미국특허분류(USC) 60/733 ; 60/737 ; 60/738 ; 60/747 ; 60/748
출원번호 US-0593087 (1996-01-29)
우선권정보 JP-0012304 (1995-01-30)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Fay, Sharpe, Beall, Fagan, Minnich & McKee
인용정보 피인용 횟수 : 106  인용 특허 : 3
초록

A gas turbine combustor includes a diffusion combustor arranged at an axis portion of a combustion chamber for effecting diffusion combustion, a plurality of first premixing combustors arranged at an outer periphery of the diffusion combustor for effecting premixed combustion, each of the plurality of first premixing combustors being formed so that a mixture outlet end thereof projects more downstream than a fuel outlet end of the diffusion combustor, and a plurality of second premixing combustors each formed so that a mixture outlet thereof projects mor...

대표
청구항

[ What is claimed is:] [1.] A gas turbine combustor comprising:a diffusion combustor arranged at an axis portion of a combustion chamber for injecting fuel and effecting diffusion combustion;a plurality of first premixing combustors arranged at an outer periphery of said diffusion combustor for injecting a mixture of air and fuel and effecting premixed combustion, each of said plurality of first premixing combustors being formed so that a mixture outlet end thereof projects more downstream than a fuel outlet end of said diffusion combustor;a plurality of...

이 특허를 인용한 특허 피인용횟수: 106

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