FIELD: power engineering; combustion chambers of gas turbines. SUBSTANCE: method involves air admission through one air inlet port and fuel, through several burners. Each burner is adjusted to respective delay time upon whose expiration acoustic pulse in combustion chamber generates heat pulse in burning fuel supplied through this burner. In the process fuel feed is controlled so that delay time greatly differs for each respective burner. EFFECT: enhanced reliability of suppressing fluctuations in combustion process. 17 cl, 3 dwg
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