The invention relates to a fixed-wing drone capable of realizing vertical take-off and landing and an implementation method thereof. The fixed-wing drone capable of realizing vertical take-off and landing at least comprises a control part, a fuselage and wings; the wings are fixedly connected with the fuselage, the top end of the fuselage is fixedly connected with a nose fairing, a first control surface, a second control surface, a third control surface and a fourth control surface are hinged to four side surfaces of the fuselage at the lower end of the nose fairing respectively; an undercarriage mechanism is fixedly connected to the tail of the fuselage, and a coaxial double-propeller power source is arranged below the fuselage. According to the method, the course of an airplane is controlled by operating different control surface unfolding angles. The fixed-wing drone capable of realizing vertical take-off and landing has the advantages of being good in stability, high in aircraft maneuverability, low in cost, good in manufacturability and capable of achieving vertical take-off and landing.

    本发明涉及一种可实现垂直起降的固定翼无人机及实现方法,该可实现垂直起降的固定翼无人机,至少包括:控制部件、机身、机翼,机翼与机身固连在一起,所述的机身顶端固定连接有机头整流罩,在机头整流罩下端的机身四个侧面分别铰接有第一操纵舵面、第二操纵舵面、第三操纵舵面和第四操纵舵面;机身的尾部固连有起落架机构,机身下方设置有共轴双桨动力源。本发明的方法通过分别操作不同操纵舵面展开角度,来控制飞机航向。本发明具有稳定性好、飞机机动性强、成本低、工艺性好的可实现垂直起降的特点。


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    Titel :

    Fixed-wing drone capable of realizing vertical take-off and landing and implementation method thereof


    Weitere Titelangaben:

    一种可实现垂直起降的固定翼无人机及实现方法


    Beteiligte:
    YANG KE (Autor:in)

    Erscheinungsdatum :

    24.11.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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