FIELD: power engineering. SUBSTANCE: method of decreasing pressure fluctuations in combustion chamber of gas turbine engine caused by burning of fuel and air in chamber provides for combustion of fuel-air mixture in combustion chamber downwards along technological line from plane of outlet section of fuel nozzle in such a way that zones of recirculation formed by fuel nozzle are remote from plane of outlet section, and combustion products are separated from fuel and air in zone of mixing at all modes of engine operation. EFFECT: reduced noises and pressure fluctuations. 3 cl, 3 dwg
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