FIELD: motors and pumps.
SUBSTANCE: invention relates to the field of a gas turbine engine (GTE) automatic control, namely, to the afterburner combustion chamber with adaptive fuel supply system operation control methods. Afterburner combustion chamber control method, in which additionally measuring the gas stream total pressure at the afterburner combustion chamber outlet and controlling the fuel manifold position in the afterburner combustion chamber.
EFFECT: increase in the combustion chamber operation process control efficiency due to the gas flow total pressure measuring at the afterburner combustion chamber outlet and controlling the fuel manifold position before the flame stabilizer.
1 cl, 3 dwg
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