| 摘要 |
A fuel supply control unit for a gas turbine includes a fuel supply system for sending fuel in a fuel reservoir to a plurality of gas turbine combustors, a heater provided for the fuel supply system for heating the fuel, a pressure reducing valve and an inlet fuel cutoff valve disposed on a downstream side of the heater, and a pressure reducing valve controller which detects an inlet fuel pressure of the inlet fuel cutoff valve and which supplies a pressure reduction control signal to the pressure reducing valve if a detected fuel pressure is higher than a required fuel pressure of the gas turbine.
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