|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/773; 060/039.281; 060/746|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 91 인용 특허 : 6|
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...
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...