FIELD: continuous combustion chambers using different fuels. SUBSTANCE: method involves preliminary supplying liquid fuel mainly consisting of ignition gas into nozzle components; igniting liquid fuel by firing member; generating flame around nozzle components, wherein firing member activating results in appearance of separate priming fire, which fires ignition gas for flame generation; deactivating firing element, which is performed by means of priming fire suppression after flame appeared about each nozzle member; suppressing flame around at least one nozzle member; feeding liquid fuel into nozzle members having un-extinguished flame around thereof which results in gas turbine primary accelerating; stopping ignition gas feeding into nozzle members; supplying liquid fuel into nozzle members which were closed before. EFFECT: increased safety and reliability of fuel ignition. 4 cl, 2 dwg
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