FIELD: power engineering.
SUBSTANCE: invention relates to power engineering. The method of control of working point of gas turbine comprising compressor, combustion chamber and turbine. The method includes the estimation of the reference curve of temperature of exhaust gas of the turbine as a function of pressure ratio of the turbine, controlling the distribution parameter of fuel. A controller for controlling the working point of the gas turbine is offered as well.
EFFECT: invention allows to ensure more accurate control of combustion temperature, burning parameters, emission of exhaust gas.
13 cl, 21 dwg, 1 tbl
