초록 ▼

A fuel supply amount is controlled while the load of a gas turbine is changed so that the fuel supply amount is shifted to a fuel supply amount in accordance with the changed load. A fuel supply control valve is operated at high speed during an initial stage and operated at a lower speed as the fuel

A fuel supply amount is controlled while the load of a gas turbine is changed so that the fuel supply amount is shifted to a fuel supply amount in accordance with the changed load. A fuel supply control valve is operated at high speed during an initial stage and operated at a lower speed as the fuel supply amount necessary for the changed load is reached. Therefore flameout of a combustor is prevented without increasing the number of revolutions of the gas turbine over a certain upper limit.

대표청구항 ▼

An apparatus for controlling fuel of a gas turbine having a fuel controlling function during a time period of a load rejection with an arithmetic unit comprising a fuel flow rate control system of the gas turbine, said apparatus comprising: a fuel control valve for controlling a fuel flow rate of th

An apparatus for controlling fuel of a gas turbine having a fuel controlling function during a time period of a load rejection with an arithmetic unit comprising a fuel flow rate control system of the gas turbine, said apparatus comprising: a fuel control valve for controlling a fuel flow rate of the gas turbine; a pressure control valve for controlling an inlet pressure of said fuel control valve; a revolution detecting means for detecting a number of revolutions of the gas turbine to produce a first signal; a first arithmetic unit converting an output request for the gas turbine to a second signal of a desired number of revolutions; a second arithmetic unit for setting a desired opening value for said fuel control valve based on a deviation between said first signal of detected number of revolutions of the gas turbine and said second signal of the desired number of revolutions; a limiter arithmetic unit for setting a minimum value of said desired opening value for the fuel control valve based on the number of revolutions of the ga turbine and atmospheric temperature; and a corrective arithmetic unit for setting a correction value for the minimum value of said desired opening value for the fuel control valve, wherein said correction value is set during a time period from occurrence of the load rejection to a time when the number of revolutions of the gas turbine reaches the maximum value after the load rejection, and said corrective arithmetic unit sets the correction value in accordance with one of a signal corresponding to a measured opening of said fuel flow rate control valve and a load signal.