A VTOL (vertical take-off and landing) aerial flying vehicle comprising an inner frame, a gimbal system and an outer frame, the inner frame comprising a propulsion system and a control system. The propulsion system being able to generate a lift force. The VTOL may also include a decoupling mechanism having either a linear or non-linear beam coupled to a ring. The beam may optionally include sliders at ends thereof that provide an additional rotation freedom to the inner frame.


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    Titel :

    Vertical take-off and landing aerial vehicle


    Beteiligte:
    DALER LUDOVIC (Autor:in) / GARNIER ARNAUD (Autor:in) / BRIOD ADRIEN (Autor:in)

    Erscheinungsdatum :

    2017-08-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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