The method and system controller to tune the operation of a gas turbine, method for the determination of the situation of the combustion system of a gas turbine and method for automated control of inlet temperature of fuel of a gas turbine

摘要

System, method and controller to tune the operation of a gas turbine, method for the determination of the situation of the combustion system of a gas turbine and method for automated control of inlet temperature of fuel of a gas turbine.The present invention relates to a system to tune the operation of a gas turbine that is fomecido based on measurement of the operational parameters of the turbine and directing the adjustment of operational controls for various operational elements of the turbine. A controller is fomecido for communication with sensors and controls within the system.The controller receives operational data of the sensors and compares the data with the stored operating standards to determine whether the operation of the turbine is in accordance with the standards. The controller then communicates the selected adjustment in an operational parameter of the turbine.The controller then receives operational data from additional sensors to determine if additional adjustment is desirable, or if the adjustment of a selected additional operational parameter is desirable.