An asymmetric folding unmanned aerial vehicle comprises a fuselage, a left wing, a right wing, a V-shaped empennage and an unfolding actuating device, the unfolding actuating device is arranged in the fuselage and comprises a wing unfolding actuator and an empennage unfolding actuator, and the left wing, the right wing and the V-shaped empennage of the folding unmanned aerial vehicle are controlled by the unfolding actuating device, so that the unmanned aerial vehicle has two states. In the folding state, the unmanned aerial vehicle is cylindrical, the left wing and the right wing are attached to the upper surface and the lower surface of the fuselage, and the V-shaped empennage is attached to the two side faces of the fuselage; in the unfolded state, the unmanned aerial vehicle is in a single-wing aerodynamic layout, and the left wing and the right wing have a height difference.

    一种非对称折叠无人机,含有机身、左机翼、右机翼、V型尾翼及展开作动装置,所述的展开作动装置设置在机身内,包含机翼展开作动器和尾翼展开作动器,折叠无人机的左机翼、右机翼、V型尾翼受展开作动装置的控制,使无人机有两种状态,分别为折叠状态和展开状态,折叠状态时无人机呈筒状,左机翼、右机翼贴合在机身的上表面和下表面,V型尾翼贴合在机身的两侧面;展开状态时无人机为单翼机气动布局,左机翼和右机翼具有高度差。


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    Titel :

    Asymmetric folding unmanned aerial vehicle


    Weitere Titelangaben:

    一种非对称折叠无人机


    Beteiligte:
    SUN JIANGTONG (Autor:in) / LI CHUANGCHUANG (Autor:in) / LEI YANJUN (Autor:in)

    Erscheinungsdatum :

    06.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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