Fuel supply apparatus for gas turbine and control unit for the s

Power plants – Combustion products used as motive fluid – Combustion products generator

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60734, 60 39465, F02C 322, F02C 7224

Patent

active

058990739

ABSTRACT:
A fuel supply apparatus for a gas turbine comprises 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 for reducing a pressure of the fuel, which has been heated, according to a required fuel pressure of a gas turbine, and a surge tank absorbing a change of the fuel pressure after the pressure reduction. A fuel supply control unit for a gas turbine comprises 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 a gas turbine combustor inlet fuel cutoff valve disposed downstream of the heater, and a pressure reducing valve controller which detects an inlet fuel pressure of the gas turbine combustor inlet fuel cutoff valve and applies a pressure reduction control signal to the pressure reducing valve if a detected pressure is higher than a required fuel pressure of the gas turbine.

REFERENCES:
patent: 3552134 (1971-01-01), Arenson
patent: 3720057 (1973-03-01), Arenson
patent: 4505124 (1985-03-01), Mayer
patent: 4612766 (1986-09-01), Eder

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