A rotor for a motor of an electric aircraft is provided. The rotor may include a hub, which includes a plurality of magnets fixed to an inner surface of the hub that are configured to interact with a stator of the motor to rotate rotor. The rotor also includes redial spokes that extend from the hub and provide structural support to the rotor. The rotor may also include a hoop, which provides balance for rotor during operation of motor and may include an integrated fan that provides cooling to various components of the motor.


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    Titel :

    Rotor for an electric aircraft motor comprising a plurality of magnets


    Beteiligte:

    Erscheinungsdatum :

    01.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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