According to the foldable flapping micro aircraft provided by the invention, the integral transmission system control mechanism is used for controlling the flapping of the flapping-wing micro aircraft and can automatically complete wing unfolding and wing folding actions before taking off and after landing, so that the wing unfolding and wing folding actions can be effectively completed, the exposed area of wings is reduced, and the folding flapping micro aircraft is convenient to recycle and carry; flapping and folding of the wings of the aircraft can share one transmission device, the structure of an aircraft body is greatly simplified, meanwhile, the unfolding state of the wings of the aircraft can be adjusted in real time according to needs, and the operability of the aircraft is improved.

    本发明提供一种可折叠的扑动微型飞行器,其整体式传动系统控制机构用于控制扑翼微飞行器的扑动以及在起飞前和降落后可自动完成展翼和收翼动作,可以有效的完成展翼和收翼动作,减少了机翼暴露的面积,便于回收和携带;本发明可以使飞行器机翼的扑动和折叠共用一套传动装置,大大简化了飞行器机体的结构,同时可以使飞行器根据需要实时调整机翼的展开状态,提高了飞行器的操作性。


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    Titel :

    Foldable flapping miniature aircraft


    Weitere Titelangaben:

    一种可折叠的扑动微型飞行器


    Beteiligte:
    SUN JIYU (Autor:in) / WANG WENZHE (Autor:in) / LIU XIAOFENG (Autor:in) / SONG FA (Autor:in) / XU NUO (Autor:in) / YAN YONGWEI (Autor:in) / ZHU HAOCHEN (Autor:in) / ZHANG ZHIJUN (Autor:in)

    Erscheinungsdatum :

    28.07.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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