The invention discloses a tailstock type vertical take-off and landing solar unmanned aerial vehicle which comprises a fuselage; wings which are connected with the vehicle body, wherein the tip ends of the wings incline towards the upper part of the fuselage; a solar cell panel which is arranged on the upper surface of the wings; a power structure which is arranged on the wingtip of the wings; undercarriages which arranged at the tail part of the power structure and the tail part of the fuselage; vertical take-off and landing can be carried out through the design of the power structure without depending on an airport runway, spot hovering can be carried out above a target, and long-distance long-endurance flight can be achieved.

    本发明公开了一种尾坐式垂直起降太阳能无人机,包括:机身;机翼,与机身连接,机翼的翼尖端向机身的上方倾斜;太阳能电池板,设置于机翼的上表面;动力结构,设置于机翼的翼尖上;起落架,设置在动力结构的尾部和机身的尾部;既能不依赖于机场跑道通过动力结构的设计进行垂直起降,又能在目标上空定点悬停,还能远距离长航时飞行。


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    Titel :

    Tailstock type vertical take-off and landing solar unmanned aerial vehicle


    Weitere Titelangaben:

    一种尾坐式垂直起降太阳能无人机


    Beteiligte:
    ZHANG KAI (Autor:in) / SONG JING (Autor:in) / ZOU YUXIANG (Autor:in) / LI GUANGJIA (Autor:in) / LI XINJUN (Autor:in) / XUE HAICHAO (Autor:in)

    Erscheinungsdatum :

    2021-12-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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