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특허 상세정보

Hybrid combustor with staged injection of pre-mixed fuel

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-007/22   
미국특허분류(USC) 60/733 ; 60/737 ; 60/746 ; 60/753 ; 431/10
출원번호 US-0784754 (1977-04-05)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Winans, F. A.
인용정보 피인용 횟수 : 112  인용 특허 : 2
초록

A combustor for a gas turbine engine which includes a fuel nozzle at the head end of the combustor, to provide a diffusion flame, and downstream inlet means at a plurality of axial dimensions of the combustor to inject pre-mixed lean fuel/air into the combustor for admission downstream from the diffusion flame resulting in a series of low temperature premixed flames to provide relatively high turbine inlet temperatures from the combustor with a minimum of thermally formed NOx compounds.

대표청구항이 없습니다

이 특허를 인용한 특허 피인용횟수: 112

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