| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a method for controlling fuel splits to a combustor of a gas turbine. <P>SOLUTION: The methods includes determining a combustion reference temperature of the gas turbine (202), measuring a biasing parameter of the gas turbine (204), determining at least one fuel split biasing value based on the combustion reference temperature and the biasing parameter (206) and adjusting a nominal fuel split schedule based on the at least one fuel split biasing value (208). <P>COPYRIGHT: (C)2012,JPO&INPIT |
