FIELD: gas turbine engine engineering.
SUBSTANCE: system comprises hollow tubular structure (41) for flowing the fuel-air mixture to combustion chamber (12), means (38) for fuel injection arranged at the front end of the hollow tubular structure, means (28) and (32) for blowing air arranged downstream of means (38) for fuel injection, means (42) for generating cold plasma and mounted downstream of means (28) for air blowing, and means for control of the means (42) for generating cold plasma depending on the regime of operation of the gas turbine engine.
EFFECT: reduced toxicity of gas emission.
16 cl, 5 dwg
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