A stator with cooling system for an electric motor of an electric aircraft and a method of manufacturing a stator of an electric motor for an electric aircraft with cooling system are disclosed. The stator may include a winding configured to provide magnetic flux and comprising an electrically conductive material. The stator may further include a soft magnet configured to hold the winding. The stator may further include a passive heat sink in thermal communication with the winding and comprising a phase change material.


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    Titel :

    STATOR WITH COOLING SYSTEM FOR AN ELECTRIC MOTOR OF AN ELECTRIC AIRCRAFT


    Beteiligte:
    LIN CHENJIE (Autor:in)

    Erscheinungsdatum :

    25.04.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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