An electric propulsion system including a stationary rotor hub assembly and a rotating system mounted to the stationary rotor hub assembly. The rotating system is rotatable about an axis. An electric motor including a stator assembly is associated with the rotor hub assembly and a rotor assembly of the electric motor is associated with the rotating system. A swashplate assembly having a dynamic component is integrated into the rotor hub assembly.


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    Titel :

    Electric powered direct drive rotor motor with integrated mechanical flight control


    Beteiligte:

    Erscheinungsdatum :

    2021-02-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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