Fuel supply control unit for gas turbine

Details Fuel supply control unit for gas turbine Fuel supply control unit for gas turbine

1999-02-26

2000-07-04

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Using special fuel or oxidizer

60734, F02C 322

Patent

active

060820950

ABSTRACT:
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.

REFERENCES:
patent: 2599480 (1952-06-01), Phenninger
patent: 4087961 (1978-05-01), Avery
patent: 5609016 (1997-03-01), Yamada

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