FIELD: gas turbine units.
SUBSTANCE: invention relates to a method for controlling a gas turbine unit (T), comprising an electric motor (ME), forming a device for supplying torque to a high-pressure rotating shaft (22), wherein the method determines the fuel consumption setpoint QCMD and the torque setpoint TRQCMD directed to the electric motor (ME), wherein the control method comprises: the step of using the first fuel control circuit to determine the fuel consumption setpoint QCMD, the step of using the second cond torque control circuit to determine the torque setpoint TRQCMD, including: i) the stage of determining the amount of correction of ΔTRQCMD torque based on transition speed setpoint NHTrajAccelCons, NHTrajDecelCons, and ii) the stage of determining torque setpoint TRQCMD based on amount of correction of ΔTRQCMD torque.
EFFECT: gas turbine unit and an electronic control unit are also presented.
8 cl, 9 dwg
