The invention relates to the technical field of aircrafts, in particular to a modular unmanned aerial vehicle which comprises a front fuselage section, a rotating base, paddle modules, a rear fuselage section and wing modules, the rear fuselage section is connected to the axial direction of the front fuselage section, and the unmanned aerial vehicle can form an axis type structure through the front fuselage section and the rear fuselage section. The rotating base is arranged on the front-section fuselage in a sleeving mode and is rotationally connected with the front-section fuselage, the paddle module is arranged in the circumferential direction of the rotating base and contracts to the rotating base, the wing module is connected to the rear-section fuselage and contracts to the rear-section fuselage, and the paddle module and the wing module are connected to the rear-section fuselage through being contracted to the rotating base and the rear-section fuselage correspondingly. The unmanned aerial vehicle actually forms a static rod-shaped structure and can be conveniently filled into tubular objects such as rocket launchers or artillery, so that the unmanned aerial vehicle can be effectively matched with battlefield launching and launching of the rocket launchers, the artillery and fighters, and the unmanned aerial vehicle can reach a preset battlefield in time.

    本发明涉及飞行器技术领域,尤其涉及一种模块化无人机,包括前段机身、旋转基座、桨叶模块、后段机身和机翼模块,后段机身连接于前段机身的轴向方向上,无人机可通过前段机身和后段机身形成轴线型结构,旋转基座套设于所述前段机身并与前段机身转动连接,桨叶模块设置于旋转基座的圆周方向并收缩于旋转基座,机翼模块连接于后段机身并收缩于后段机身,桨叶模块和机翼模块分别通过收缩于旋转基座和后段机身,使得无人机实际形成静态棒状结构,便于填入诸如火箭炮或者火炮等管状器物内,进而使得无人机可有效配合火箭炮、火炮和战机的战场发射与投放,使无人机能够即时到达预设战位。


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    Title :

    Modular unmanned aerial vehicle


    Additional title:

    模块化无人机


    Contributors:
    LI XINSHENG (author) / TAN XUETONG (author) / TANG YUFEI (author)

    Publication date :

    2024-12-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



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