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).
PROCEDE DE GESTION D'UN MOTEUR ELECTRIQUE
2016-10-21
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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