FIELD: machine building.
SUBSTANCE: invention relates to the field of automatic control of a gas-turbine engine, namely to a control system of operation modes of an afterburner combustion chamber. Afterburner combustion chamber control system comprises series-augmented pump, nozzle and afterburner regulator, afterburner fuel distributor, and N fuel collectors. Inputs of fuel manifolds are combined and connected to output of up-down fuel distributor, and outlets are output of system. Gas flow temperature transducer arranged at the outlet of afterburner combustion chamber and control valve of fuel distribution manifold valve arranged on afterburner fuel distributor case is additionally introduced. Output of fuel manifold control valve of fuel manifolds is connected to second input of afterburner distributor.
EFFECT: invention allows increasing completeness of fuel combustion in afterburner combustion chamber.
1 cl, 3 dwg
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