The invention discloses an unmanned aerial vehicle launch frame and provides an unmanned aerial vehicle launch frame which is simple in structure and capable of improving launch reliability. The unmanned aerial vehicle launch frame comprises a base, a track platform, an angle controller and a launch assembly, wherein the track platform is arranged in the middle of the base; the tail end of the track platform is hinged to the tail end of the base; the angle controller is fixedly arranged between the tail end of the track platform and the tail end of the base; three walking passages are formed in the top surface of the track platform and are arranged in parallel at intervals; the launch assembly is arranged on the tail end of the track platform. According to the unmanned aerial vehicle launch frame, an unmanned aerial vehicle is arranged on the base, is connected with the base by the launch assembly and is subjected to launch; the control on an angle is realized by the angle controller, so that different launch requirements can be met. When the unmanned aerial vehicle takes off, the unmanned aerial vehicle advances along the walking passages in the track platform, so the reliability is improved; and since an upward transition section is arranged on the head end, the unmanned aerial vehicle is assisted in taking off. The unmanned aerial vehicle launch frame is convenient to disassemble, assembly and carry.


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    Titel :

    Unmanned aerial vehicle launch frame


    Beteiligte:
    LYU ZHONGGUANG (Autor:in)

    Erscheinungsdatum :

    2015-07-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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