The invention relates to an environment-adaptive landing mechanism for a flapping-wing flying robot, which is arranged on the flapping-wing flying robot and comprises a left mechanical claw and a right mechanical claw which are transversely and symmetrically arranged at the gravity center position of the flapping-wing flying robot; the left mechanical claw and the right mechanical claw are the same in structure and each comprise a base frame, and landing wheels are arranged on the two sides of each base frame. The rotating mechanism is arranged on the base frame and comprises a first rotating mechanism and a second rotating mechanism, and the second rotating mechanism is connected with the first rotating mechanism; and the clamping jaw assembly comprises a left hook claw, a right hook claw and an opening and closing control mechanism, the opening and closing control mechanism is arranged on the base frame, and the left hook claw and the right hook claw are both connected with the opening and closing control mechanism. The lifting mechanism has two form conversion modes of a claw type and a wheel type, combines the advantages of two lifting mechanisms, can realize stable lifting on different surfaces through the form conversion of the mechanisms according to different lifting surface conditions, effectively improves the environment adaptability of lifting, and increases the application scenarios.

    本发明涉及一种用于扑翼飞行机器人的环境适应性起落机构,设置在扑翼飞行机器人上,包括左机械爪和右机械爪,横向对称设置在扑翼飞行机器人的重心位置;左机械爪和右机械爪结构相同,均包括:基座框架,基座框架的两侧设有起落轮;旋转机构设置在基座框架上,其包括第一旋转机构和第二旋转机构,第二驱动旋转机构与第一驱动旋转机构连接;夹爪组件,包括左钩爪、右钩爪和开合控制机构,开合控制机构设置在基座框架上,左钩爪和右钩爪均与开合控制机构连接。本发明拥有爪式和轮式两种形态变换模式,结合两种起落机构的优点,可根据不同的起落面情况,通过机构的形态变换,在不同的表面实现平稳起落,有效提高了起落的环境适应性,增加了应用场景。


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    Titel :

    Environmentally adaptive landing mechanism for flapping-wing flying robot


    Weitere Titelangaben:

    一种用于扑翼飞行机器人的环境适应性起落机构


    Beteiligte:
    LIU CHAO (Autor:in) / SHI JUNYI (Autor:in) / FENG HAOZHE (Autor:in) / SHEN TIANYU (Autor:in) / CHI WENZHENG (Autor:in) / CHEN GUODONG (Autor:in) / SUN LINING (Autor:in)

    Erscheinungsdatum :

    04.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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