Method of and device for controlling fuel for gas turbine

Details Method of and device for controlling fuel for gas turbine Method of and device for controlling fuel for gas turbine

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/22 (2006.01) F02C 9/28 (2006.01) F02C 9/32 (2006.01)

Patent

CA 2408704

Values such as a pressure for supplying fuel gas to a gas turbine, a pressure in a combustor casing of the gas turbine, an output of a generator connected to the gas turbine, and a controlled output for a flow rate control valve are detected by sensors. The detected values are input into a control device. A differential pressure across the flow rate control valve and a target value of the differential pressure are also input into the control device. The control device performs a desired arithmetic operation based on these input value, to output a lift instruction for a pressure control valve.

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