Automated tuning of gas turbine combustion systems

Details Automated tuning of gas turbine combustion systems Automated tuning of gas turbine combustion systems

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 9/28 (2006.01) F02C 9/34 (2006.01) F02D 43/00 (2006.01)

Patent

CA 2701322

A system for tuning the operation of a gas turbine is provided based on measuring operational parameters of the turbine and directing adjustment of operational controls for various operational elements of the turbine. A controller is provided for communicating with sensors and controls within the system. The controller receiving operational data from the sensors and comparing the data to stored operational standards to determining if turbine operation conforms to the standards. The controller then communicates selected adjustment in an operational parameter of the turbine. The controller then receives additional operational data from the sensors to determine if an additional adjustment is desired or is adjustment is desired of a further selected operational parameter.

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