An aerial vehicle system including a vertical takeoff and landing apparatus, a wing assembly removably coupled to the vertical takeoff and landing apparatus, and a rotor guard interchangeable with the wing assembly and removably coupleable to the vertical takeoff and landing apparatus. The vertical takeoff and landing apparatus can include a frame, a control module carried by the frame, and a plurality of thrust assemblies carried by the frame.


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    Titel :

    MODULAR UNMANNED AERIAL VEHICLE WITH ADJUSTABLE CENTER OF GRAVITY


    Beteiligte:

    Erscheinungsdatum :

    15.08.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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