Abstract An aeronautical vehicle that rights itself from an inverted state to an upright state has a self righting frame assembly has a protrusion extending upwardly from a central vertical axis. The protrusion provides an initial instability to begin a self-righting process when the aeronautical vehicle is inverted on a surface. A propulsion system, such as rotor driven by a motor can be mounted in a central void of the self-righting frame assembly and oriented to provide a lifting force. A power supply is mounted in the central void of the self-righting frame assembly and operationally connected to the at least one rotor for rotatably powering the rotor. An electronics assembly is also mounted in the central void of the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a surface. - -


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Self-righting frame and aeronautical vehicle


    Beteiligte:
    YAN GAOFEI (Autor:in) / DEES JAMES (Autor:in)

    Erscheinungsdatum :

    27.04.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    SELF-RIGHTING FRAME AND AERONAUTICAL VEHICLE

    YAN GAOFEI / DEES JAMES | Europäisches Patentamt | 2016

    Freier Zugriff

    Self-righting frame and aeronautical vehicle

    YAN GAOFEI / DEES JAMES | Europäisches Patentamt | 2016

    Freier Zugriff

    Self-righting frame and aeronautical vehicle

    YAN GAOFEI / DEES JAMES | Europäisches Patentamt | 2015

    Freier Zugriff

    SELF-RIGHTING FRAME AND AERONAUTICAL VEHICLE

    YAN GAOFEI / DEES JAMES | Europäisches Patentamt | 2019

    Freier Zugriff

    SELF-RIGHTING FRAME AND AERONAUTICAL VEHICLE

    YAN GAOFEI / DEES JAMES | Europäisches Patentamt | 2015

    Freier Zugriff