The invention provides a rotary folding type unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles, the rotary folding type unmanned aerial vehicle comprises a fuselage, wings are arranged on the two sides of the fuselage, each wing comprises an inner wing section and an outer wing section, and the inner wing sections and the outer wing sections are connected through rotary folding mechanisms; the rotary folding mechanism comprises a first connecting part, a second connecting part, a pin shaft and a locking part, the first connecting part and the second connecting part are connected with the inner wing section and the outer wing section correspondingly, the second connecting part rotationally sleeves the outer side of the pin shaft and is rotationally connected with the first connecting part through the pin shaft, and the second connecting part can slide in the axial direction of the pin shaft; the outer wing section descends relative to the inner wing section, and the locking part can lock and position the first connecting part and the second connecting part when the wing is in an unfolded state; the problems that in the prior art, the wingspan of an unmanned aerial vehicle is large, and the requirement for the parking space of an airport hangar is high are solved.

    本发明提供一种旋转折叠式无人机,涉及无人机技术领域,包括:机身,机身的两侧设置有机翼,机翼包括内翼段和外翼段,内翼段与外翼段通过旋转折叠机构连接;旋转折叠机构包括第一连接部、第二连接部、销轴和锁紧部件,第一连接部和第二连接部分别与内翼段和外翼段连接,第二连接部转动套设在销轴的外侧并通过销轴与第一连接部转动连接,第二连接部能够沿销轴的轴向滑动,以使外翼段相对于内翼段下降,锁紧部件能够在机翼处于展开状态时对第一连接部和第二连接部锁紧定位;解决现有技术中的无人机翼展较大,对机场机库的停放空间要求较高的问题。


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    Titel :

    Rotary folding type unmanned aerial vehicle


    Weitere Titelangaben:

    一种旋转折叠式无人机


    Beteiligte:
    XIA ZHENFENG (Autor:in) / QIN HAN (Autor:in) / LI XILE (Autor:in) / YI ZHISHENG (Autor:in) / LI GUANGJIA (Autor:in)

    Erscheinungsdatum :

    01.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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