FIELD: machine building.
SUBSTANCE: invention relates to the field of automatic control of a gas-turbine engine, namely to a method for controlling operation modes of an afterburner combustion chamber. Proposed method comprises measurement of engine control lever position, measurement of total air pressure behind compressor, measurement of air temperature at engine inlet, and control of fuel feed to afterburner combustion chamber. Temperature of the gas flow at the outlet of the afterburner combustion chamber is additionally measured and the position of the distribution valve of the fuel manifolds is controlled.
EFFECT: invention allows increasing completeness of fuel combustion in afterburner combustion chamber.
1 cl, 3 dwg
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Authors
Dates
2019-09-04—Published
2018-02-05—Filed