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

摘要

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.