FIELD: machine building.
SUBSTANCE: disclosed is controller (50) for gas turbine. Gas turbine is configured to feed load L. Gas turbine (600) comprises fuel feed means (60) configured to supply fuel with fuel flow rate FF to combustion chamber (70), wherein fuel supply means comprises first fuel supply means (61) and second fuel supply means (62). Controller (50) is configured to determine one or more ratios R of one or more operating parameters of combustion chamber COP at load L to respective reference operating parameters of combustion chamber COPR at reference load LR. Controller (50) is further configured to control the fuel flow rate ratio FF supplied by the first fuel feed means based at least in part on the determined one or more ratios R. Also disclosed is gas turbine (600) and a control method of the gas turbine.
EFFECT: broader functional capabilities.
16 cl, 11 dwg
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