The rotor and fixed wing separable composite unmanned aerial vehicle comprises a coaxial double-rotor system and a fixed wing system, the coaxial double-rotor system comprises rotors and a rotor body, the fixed wing system comprises wings, empennages and a fixed wing fuselage, the rotors are arranged at the front end of the rotor body, and the rotors can rotate to adjust the orientation; the rotor wing and fixed wing separable composite unmanned aerial vehicle can be folded and placed in the launching device and unfolded during flight; the wings and the empennage are connected to the fixed wing fuselage, and the fixed wing fuselage is connected to the rotor wing fuselage; the fixed wing fuselage can be separated from the rotor wing fuselage; the wings are rotationally connected to the fixed-wing fuselage and can be folded to be overlapped with the fixed-wing fuselage; the fixed wing fuselage is in sliding connection with the rotor wing fuselage, the fixed wing fuselage is fixed on the fuselage through an electric bolt, and the electric bolt is connected with a controller; the unmanned aerial vehicle is simple in structure and can prolong the sailing distance.

    本发明公开了一种旋翼固定翼可分离复合无人机,包括共轴双旋翼系统和固定翼系统,共轴双旋翼系统包括旋翼、旋翼机身,固定翼系统包括机翼、尾翼、固定翼机身,所述旋翼设置在旋翼机身前端,旋翼能转动调节朝向;旋翼固定翼可分离复合无人机能折叠置于发射装置中并在飞行时展开;机翼和尾翼连接在固定翼机身上,固定翼机身连接在旋翼机身上;固定翼机身能与旋翼机身分离;机翼转动连接在固定翼机身上能折叠至与固定翼机身重叠;固定翼机身与旋翼机身滑动连接,固定翼机身通过电动插销固定在机身上,电动插销连接有控制器;本无人机结构简单且能延长航行距离。


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    Title :

    Rotor wing and fixed wing separable composite unmanned aerial vehicle


    Additional title:

    旋翼固定翼可分离复合无人机


    Contributors:
    SONG YANGUO (author) / FENG BOHONG (author) / ZHANG HONG (author) / WANG HUANJIN (author) / WU PING (author) / WAN JUNMING (author) / GUO JIANDONG (author) / CHEN YONGHE (author)

    Publication date :

    2025-05-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



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