FIELD: engineering.
SUBSTANCE: described is a controller (50) for a gas turbine configured to supply a load L. The gas turbine is comprised of a fuel supply tool configured to supply fuel with a fuel flow FF into the combustion chamber. The fuel supply tool is comprised of a first fuel supply tool and a second fuel supply tool. The controller (50) is configured to control the proportion P of the fuel flow FF supplied by means of the first fuel supply tool based at least partially on the fuel flow FF. Described are a gas turbine containing such a controller (50) and a method for controlling such a gas turbine.
EFFECT: proposed is a gas turbine controller, a gas turbine containing such a controller and a method for operation thereof.
16 cl, 8 dwg
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