A high-efficiency, high specific power electric motor/generator for aircraft use provides a cantilevered external rotor removed from load thrust. and vibration by an isolator and hearing set between the rotor and stator reducing material demands and weight otherwise required for stiffness to preserve close rotor/stator proximity.


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    Titel :

    External Rotor Aircraft Motor Having Force Isolated Cantilevered Rotor


    Beteiligte:
    XIAO JIANQIAO (Autor:in) / HARAN KIRUBA S (Autor:in)

    Erscheinungsdatum :

    2023-03-16


    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 / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F16C SHAFTS , Wellen



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