FIELD: fuel combustion methods and devices.
SUBSTANCE: invention relates to the gas turbine plant operation method with step and / or sequential combustion, in which the second stage or the second combustion chamber burners are separately and sequentially turning on during the load and turning off during unloading. Fuel total mass flow rate and the compressor adjustable inlet guide vanes are adjusted simultaneously to enable control of the gas turbine plant operating temperatures and engine power relative to the required CO emission rate.
EFFECT: higher combustion efficiency.
14 cl, 3 dwg
