The invention discloses a foldable composite configuration vertical take-off and landing unmanned aerial vehicle which comprises a fuselage, a front wing, a rear wing, a control plane, an execution mechanism, a rotor wing motor and a propeller, the front wing and the rear wing are connected with the fuselage through a front folding mechanism and a rear folding mechanism respectively, and the front wing and the rear wing are in an X-shaped layout after being unfolded. Rotor motors and propellers are installed on the front wings, control surfaces and execution mechanisms are installed on the rear wings, and the front wings and the rear wings can be folded to be attached to the fuselage. According to the unmanned aerial vehicle, only one power system is used, the unmanned aerial vehicle has the vertical take-off and landing capacity and high flexibility of a multi-rotor unmanned aerial vehicle and the low-energy-consumption cruising and high-speed flying capacity of a fixed-wing aircraft at the same time, the wings can be folded to be attached to the fuselage, the outer contour is cylindrical after folding, and the unmanned aerial vehicle is compact in structure and more convenient to store, transport and carry; in addition, the device can support the modes of barrel type launching, ground takeoff, handheld takeoff, high-altitude spreading and the like for deployment.

    本发明公开了一种可折叠复合构型垂直起降无人机,包括机身、前机翼、后机翼、控制舵面及执行机构、旋翼电机和螺旋桨,前机翼和后机翼分别通过前折叠机构和后折叠机构连接机身,前机翼和后机翼展开后均为X型布局,前机翼上安装有旋翼电机和螺旋桨,后机翼上安装控制舵面及执行机构,前机翼和后机翼可折叠至与机身贴合。本发明仅使用一套动力系统,使无人机同时具备多旋翼无人机垂直起降能力、高灵活性和固定翼飞机低能耗巡航、高速飞行的能力,并且机翼可折叠收拢至贴合机身,折叠后外轮廓为圆柱状,结构紧凑,更便于存储、运输和携行;另外可支持筒式发射、地面起飞、手持起飞、高空布撒等方式进行部署。


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    Titel :

    Foldable composite configuration vertical take-off and landing unmanned aerial vehicle


    Weitere Titelangaben:

    一种可折叠复合构型垂直起降无人机


    Beteiligte:
    XU XIANRUI (Autor:in) / LIN YU (Autor:in) / LU BEN (Autor:in) / MEI XINYI (Autor:in) / ZHANG SIYU (Autor:in) / LI XIAOLONG (Autor:in)

    Erscheinungsdatum :

    03.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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