According to the bionic landing mechanism of the fixed-wing unmanned aerial vehicle, in the mechanism, deformation areas on the left side and the right side of a wing are each composed of eight artificial feathers, namely wing plates, and the left side and the right side of a tail are each composed of four fan-shaped artificial feathers, namely tail plates; when the unmanned aerial vehicle flies quickly in the air, the corresponding wings and the tail are folded, so that the air resistance can be reduced when the fixed-wing unmanned aerial vehicle flies quickly; when the unmanned aerial vehicle prepares to land, the wings and the tail are unfolded, the air resistance is increased to reduce the flight speed, and after the claw-type landing mechanism makes contact with the ground, knee parts are bent to provide a buffering effect, reduce landing impact and achieve stable landing.

    本发明公开了一种固定翼无人机仿生降落机构,该机构中,机翼左右两侧的变形区各由八片人造羽毛即翼板组成,机尾左右各由四片扇形人造羽毛即尾板组成;当无人机在空中快速飞行时,相应的机翼和机尾均折起,能够使固定翼无人机在快速飞行时降低空气阻力;当无人机准备降落时,机翼和机尾均展开,增大空气阻力来降低飞行速度,再通过爪型降落机构接触地面后膝盖部分弯曲,提供缓冲作用,降低落地冲击,实现平稳着陆。


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    Titel :

    Bionic landing mechanism of fixed-wing unmanned aerial vehicle


    Weitere Titelangaben:

    一种固定翼无人机仿生降落机构


    Beteiligte:
    LIN DEFU (Autor:in) / WANG HEYANG (Autor:in) / DONG YIHAO (Autor:in) / GU XUECHEN (Autor:in) / QU JIAQI (Autor:in) / YU QIAN (Autor:in) / ZHANG FENGLIN (Autor:in) / YAN HAOMIN (Autor:in) / SHAN YUHANG (Autor:in)

    Erscheinungsdatum :

    2024-02-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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