Method for controlling a hybrid turbomachine incorporating a torque meter, associated hybrid turbomachine and aircraft comprising such a turbomachine.

Abstract

The invention relates to a method for controlling a hybrid turbomachine comprising a drive shaft, an electric machine, and a mechanical transmission line between the shaft and the electric machine. This mechanical transmission line includes a torque meter and a control device for the electric machine. The method involves the following steps: a) applying a torque command to the electric machine via the control device; b) providing a measurement of the mechanical torque at the electric machine to the control device; c) calculating the torque difference between the torque command and the mechanical torque measurement; d) using the torque difference calculated in step c) providing a corrected torque command with a controller equipped with a proportional-integral function and a phase-advance function. Figure 2 is shown in the abstract.