The invention relates to a method for managing an electric motor (6) intended to drive rotationally a wheel (4) of an aircraft (1), the method comprising the step of short-circuiting the phases of the electric motor (6) when the aircraft (1) is in a period of deactivation of the motor (6) during which it is envisaged not using the electric motor (6).
PROCÉDÉ DE GESTION D'UN MOTEUR ÉLECTRIQUE
METHOD FOR MANAGING AN ELECTRIC MOTOR
STEUERUNGSVERFAHREN EINES ELEKTROMOTORS
2023-05-10
Patent
Electronic Resource
French
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