The invention provides a five-wing bionic ornithopter which comprises a fuselage skeleton, and wing units, a control unit, leg units and an empennage unit are sequentially mounted on the fuselage skeleton; the wing unit comprises a wing flapping mechanism fixedly installed at the front end of the fuselage framework and a folding driving mechanism fixedly installed in the middle of the fuselage framework, forelimb deformation mechanisms are hinged to the two sides of the wing flapping mechanism and the two sides of the folding driving mechanism correspondingly, the forelimb deformation mechanisms are symmetrically arranged, and feather mechanisms are rotationally connected to the forelimb deformation mechanisms; the feather mechanism is hinged with an elastic energy storage mechanism; the leg unit comprises leg deformation driving mechanisms symmetrically and fixedly connected to the tail of the fuselage framework, bionic leg mechanisms are rotationally connected to the leg deformation driving mechanisms, and feather pieces are hinged to the bionic leg mechanisms; the wing flapping mechanism, the folding driving mechanism, the leg deformation driving mechanism and the empennage unit are electrically connected with the control unit.

    本发明提供一种五翼仿生扑翼飞行器,包括机身骨架,机身骨架上依次安装有翅膀单元、控制单元、腿部单元以及尾翼单元;翅膀单元包括固定安装在机身骨架前端的翅膀扑动机构以及固定安装在机身骨架中部的折叠驱动机构,翅膀扑动机构与折叠驱动机构的两侧分别铰接有前肢变形机构,前肢变形机构对称设置,前肢变形机构上转动连接有羽毛机构,羽毛机构铰接有弹性储能机构;腿部单元包括对称固接在机身骨架尾部的腿部变形驱动机构,腿部变形驱动机构上转动连接有仿生腿机构,仿生腿机构上铰接有羽毛片;翅膀扑动机构、折叠驱动机构、腿部变形驱动机构以及尾翼单元分别与控制单元电性连接。


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    Titel :

    Five-wing bionic flapping wing aircraft


    Weitere Titelangaben:

    一种五翼仿生扑翼飞行器


    Beteiligte:
    ZHAO JINGSHAN (Autor:in) / LEE KYUNG-HO (Autor:in)

    Erscheinungsdatum :

    13.02.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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