METHOD FOR FUEL SPLIT CONTROL TO A GAS TURBINE USING A MODIFIED TURBINE FIRING TEMPERATURE

摘要

A method for controlling fuel splits to a controller is provided that includes comparing a combustor operating parameter to a predefined combustor operating parameter range. If the combustor operating parameter is outside its respective range, then a modified turbine firing temperature is calculated. The modified turbine firing temperature may then be used to determine the fuel splits to the combustor using a nominal fuel splits lookup table.