Gas turbine control system having optimized ignition air...

F - Mech Eng,Light,Heat,Weapons – 02 – C

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F02C 6/00 (2006.01) F02C 9/28 (2006.01) F02C 9/40 (2006.01) F02C 9/54 (2006.01)

Patent

CA 2029258

Abstract of the Invention Method and apparatus for controlling fuel flow in a combustion turbine, wherein a speed reference signal is given and wherein an actual speed signal is given, is shown to include a fuel flow regulator for regulating the flow of fuel in response to a control signal, a controller for generating a control signal representative of the difference between the actual speed signal and the speed reference signal, a first adjustment member for modifying the speed reference signal to account for droop prior to generation of the control signal, and a second adjustment means for modifying the speed reference signal to account for speed error also prior to generating the control signal. A load condition specifically envisioned for use with the present invention is the point of closure of the generator breaker.

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