The invention discloses a vertical take-off and landing fixed-wing unmanned aerial vehicle convenient to disassemble and assemble, and belongs to the field of unmanned aerial vehicles. Comprising a fuselage, two main wings installed on the two sides of the fuselage respectively, a traction assembly installed on the front portion of the fuselage, an empennage installed on the tail portion of the fuselage, an avionics system installed in the fuselage and a main power source used for supplying power to the avionics system, the traction assembly and steering engines on the empennage. Vertical take-off and landing mechanisms are detachably and fixedly connected to the two main wings, and each vertical take-off and landing mechanism comprises a machine arm and two lift force assemblies installed at the two ends of the machine arm correspondingly; the two ends of the vehicle arms extend to the front and the rear of the main wings correspondingly, and secondary power sources are further mounted on the vehicle arms and electrically connected with the two lift assemblies through wires; the lift assemblies on the arms and the secondary power supplies are in communication connection with the avionics system through control cables. The vertical take-off and landing mechanism can be added to the fixed-wing unmanned aerial vehicle as required, so that the fixed-wing unmanned aerial vehicle has the flight advantages of two unmanned aerial vehicles at the same time.

    本发明公开了一种便于拆装的垂直起降固定翼无人机,属于无人机领域,包括机身、两个分别安装在机身的两侧的主翼、安装在机身的前部的牵引组件、安装在机身的尾部的尾翼、安装在机身内的航电系统和用于为航电系统、牵引组件以及尾翼上的舵机供电的主电源,两个主翼上均可拆卸固定连接有垂直起降机构,垂直起降机构包括机臂以及两个分别安装在机臂的两端上的升力组件;机臂的两端分别延伸到主翼的前方和后方,机臂上还安装有次级电源,次级电源通过导线与两个升力组件电性连接;各机臂上的升力组件以及次级电源分别通过控制线缆与航电系统通信连接。本发明能够根据需要为固定翼无人机增加垂直起降机构,从而同时具备两种无人机的飞行优势。


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    Title :

    Vertical take-off and landing fixed-wing unmanned aerial vehicle convenient to disassemble and assemble


    Additional title:

    一种便于拆装的垂直起降固定翼无人机


    Contributors:
    GONG BANGMIN (author) / AI JIANLIANG (author)

    Publication date :

    2022-07-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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