The invention discloses a flapping-wing robot in the technical field of aircrafts. The flapping-wing robot comprises a robot body, a wing module, a posture adjusting module and a power module. Wherein the wing module comprises a wing main body, a wing driving joint and a wing driving electrode, the posture adjusting module comprises a posture adjusting sheet and a posture adjusting driving electrode, and the wing driving electrode and the posture adjusting driving electrode are both electrically connected with the power supply module. The wing driving joints and the posture adjusting pieces are made of IPMC (ionic polymer metal composite). According to the flapping-wing robot, the transmission mode and the driving mode are integrally designed, and the size and the weight of the flapping-wing robot are greatly reduced.

    本发明公开了飞行器技术领域的一种扑翼机器人,包括:机器人主体、翅翼模块、姿态调节模块和电源模块;其中,所述翅翼模块包括翅翼主体、翅翼驱动关节和翅翼驱动电极,所述姿态调节模块包括姿态调节片和姿态调节驱动电极,所述翅翼驱动电极与所述姿态调节驱动电极均与电源模块电连接,所述翅翼驱动关节和姿态调节片使用的材料均为离子聚合物金属复合材料IPMC。本发明提供的扑翼机器人对传动与驱动模式一体化设计,大大缩减了扑翼机器人的尺寸及重量。


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    Titel :

    Flapping-wing robot


    Weitere Titelangaben:

    一种扑翼机器人


    Beteiligte:
    WANG YANJIE (Autor:in) / JIANG MINGFEI (Autor:in) / TANG GANGQIANG (Autor:in)

    Erscheinungsdatum :

    21.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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