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특허 상세정보

Method and system for controlling fuel supply in a combustion turbine engine

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-009/28    F02C-009/00   
미국특허분류(USC) 060/773; 060/039.281; 060/746
출원번호 US-0954085 (2004-09-30)
우선권정보 GB-0323255.0(2003-10-04)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Manelli Denison & Selter PLLC
인용정보 피인용 횟수 : 91  인용 특허 : 6
초록

In order to regulate fuel flow to the combustor (36) of the combustion turbine engine (10) having a primary combustion zone (64) and at least one further combustion zone, the temperature of the inlet and outlet of the combustor (36) are determined, as are first and second values representing first and second properties, with the first property being one of: the total enthalpy rise in the combustor (36), the equivalence ratio of the combustor ( 36), the fuel/air ratio of said combustor (36), the fuel flow through the combustor, and the second property bei...

대표
청구항

We claim: 1. A method of regulating fuel flow to a combustion turbine engine, said engine having a combustor including an inlet, an outlet, a primary combustion zone and at least one further combustion zone, the total fuel supplied to the combustor being divided between primary fuel supplied to said primary combustion zone and other fuel supplied to said at least one further combustion zone, the resulting of the fuel comprising regulating the fuel ratio of said primary fuel to said total fuel by the steps of a) determining the inlet and outlet temperatu...

이 특허를 인용한 특허 피인용횟수: 91

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