A rotor of an aircraft electric motor includesa shaft made of a first material, anda skin made of a second material different from the first material. The skin includes two half-shells welded together,each half-shell of the two half-shells including a chamfer,and the chamfers assembling the two half-shells together. The shaft includes a shoulder portion the skin being fixed on the shoulder portion. The rotor further includesan interpenetration layer of the first material and of the second material, the interpenetration layer including an alloy of the first material and an alloy of the second material,the interpenetration layer being between the shaft and the skin.


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    Titel :

    ELECTRIC MOTOR ROTOR


    Beteiligte:
    SERGHINE CAMEL (Autor:in) / KLONOWSKI THOMAS (Autor:in)

    Erscheinungsdatum :

    07.11.2024


    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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