The invention relates to an assembly (1) of an electric motor (2) for propelling an aircraft and a control device (5), the electric motor (2) comprising a stator (21) and a rotor (22) and at least one cooling channel (CR) configured to be supplied with a heat transfer fluid (F), the control device (5) being configured to issue a control command (01) in order to control the rotation of the rotor (22), the control device (5) also being configured to issue a heating command configured to generate a heating current in the stator (21) in order to heat the heat transfer fluid (F), the heating current comprising a non-zero DC component and a substantially zero quadratic component so as to limit the rotation of the rotor (22) during heating.
ENSEMBLE D'UN MOTEUR ÉLECTRIQUE ET D'UN DISPOSITIF DE COMMANDE DU MOTEUR ÉLECTRIQUE, PROCÉDÉ DE CONTRÔLE D'UN TEL ENSEMBLE
ASSEMBLY OF AN ELECTRIC MOTOR AND A DEVICE FOR CONTROLLING THE ELECTRIC MOTOR, AND METHOD FOR CONTROLLING SUCH AN ASSEMBLY
ANORDNUNG EINES ELEKTROMOTORS UND VORRICHTUNG ZUR STEUERUNG DES ELEKTROMOTORS SOWIE VERFAHREN ZUR STEUERUNG EINER SOLCHEN ANORDNUNG
2025-07-02
Patent
Electronic Resource
French
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