An aerial vehicle has a fuselage, at least one wing, propulsion means for forward flight and at least two pairs of arms. Each arm supports at least one rotor powered for vertical take-off and landing (VTOL) and each arm is in a deployed position for vertical take-off or hovering and transitions to a retracted position for forward flight using the at least one wing, and the arms re-transition to a deployed position for vertical landing or hovering.


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    Titel :

    AERIAL VEHICLES


    Beteiligte:
    VON BERTOUCH MICHAEL (Autor:in) / KELLY ADAM (Autor:in)

    Erscheinungsdatum :

    09.11.2023


    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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