METHOD OF STARTUP CONTROL FOR GAS TURBINE SYSTEM OPERATING IN FIRED DECELERATION SHUTDOWN MODE

摘要

PROBLEM TO BE SOLVED: To provide a method of startup control for a gas turbine system operating in a fired deceleration shutdown mode.SOLUTION: A method of startup control for a gas turbine system that is operating in a fired deceleration shutdown process mode is provided. The method includes determining whether the combustor flame is in a lit state. Also included is increasing a fuel flow to the gas turbine system if the combustor is determined to be in the lit state. Further included is initiating a starter system to the gas turbine system.