FIELD: engines and pumps.
SUBSTANCE: group of inventions relates to the field of control of the operation of gas turbine engines and can be used to control the supply of fuel to the gas turbine engine and the guiding devices of the compressor. In the method for controlling the gas turbine engine, a predetermined value of the rate of change in the rotor speed of the turbocharger is formed, depending on the pressure behind the compressor and the reduced speed of the turbocharger and limit the rate of change in the rotor speed of the turbocharger. Set value of the ramp is corrected depending on the actual position of the compressor guiding devices. Control system of a gas turbine engine is also described.
EFFECT: stabilization of the acceleration time and provision of gas-dynamic stability reserves of the gas generator in all flight conditions.
2 cl, 4 dwg
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