Redundant trip solenoid valve shut-off for gas turbine fuel system
AssigneeGeneral Electric Company
InventorsHenry G. Chu, George Hubschmitt, Brian P. Ray, Scott V. Annin
Life of this patent
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AssigneeGeneral Electric Company
InventorsHenry G. Chu, George Hubschmitt, Brian P. Ray, Scott V. Annin
Estimating the term…
A trip oil system automatically controls the fuel shut-off valves in an industrial gas turbine. The trip oil system applies hydraulic pressure to actuate and hold open a fuel shut-off valve so that fuel flows to the combustor of the gas turbine. When the trip oil system relieves the hydraulic pressure, the fuel shut-off valve closes and stops the fuel flow to the combustor. A bank of three solenoid valves controls the application of hydraulic pressure to each fuel shut-off valve. Hydraulic fluid conduits interconnect the three solenoid valves such that no single valve by itself can relieve the hydraulic pressure applied to the fuel shut-off valve. During normal operation of the gas turbine, all three redundant solenoid valves are activated. For the trip oil system to cause the fuel shut-off valve to close, at least two of the solenoid valves must de-energize to relieve pressure to the fuel shut-off valve.
In a fuel supply coupled to a combustor in a gas turbine, a trip oil system comprising:
A method for controlling the flow of fuel to a gas turbine having a fuel supply conduit with a fuel valve, a controller, and a trip oil system including an actuator coupled to the fuel valve, a fluid conduit connected to the actuator and three interconnected trip oil valves disposed in the fluid conduit, said method comprising the steps of:
In a fuel supply coupled to a gas turbine, a trip oil system comprising:
Dependencies are inferred from the claim text.