FIELD: fuel combustion devices.
SUBSTANCE: gas fuel is fed to the main burners at switching the combustion in the auxiliary burner from burning oil to burning gas and gas starts to burn in the main burners. Then gas fuel is supplied to the auxiliary burner and gas starts to be burned in the auxiliary burner.
EFFECT: task of manufacturing the combustion chamber of a gas turbine and method of operation thereof is to reduce the visibility of the exhaust gas of a gas turbine when switching the gas turbine fuel from oil fuel to gas fuel to a minimum.
4 cl, 6 dwg
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