The invention discloses a bionic flapping wing device and an aircraft, relates to the technical field of aircrafts, and aims to solve the problems that an existing flapping wing aircraft is more in component parts, high in assembly difficulty and low in stability. The bionic flapping wing device comprises a first rotation driving mechanism, a transmission gear, a linear driving mechanism and a flapping wing mechanism, the driving end of the first rotation driving mechanism is in transmission connection with the transmission gear, the linear driving mechanism is arranged on the transmission gear, and the flapping wing mechanism is rotationally connected with the driving end of the linear driving mechanism. The aircraft comprises the bionic flapping wing device. The bionic flapping wing device and the aircraft provided by the invention are used for reducing the assembly difficulty of the flapping wing aircraft, reasonably balancing the weight and improving the motion stability of the flapping wing aircraft.

    本发明公开一种仿生扑翼装置及飞行器,涉及飞行器技术领域,以解决现有的扑翼飞行器组成零部件较多,装配难度大,稳定性不高的问题。该仿生扑翼装置包括:第一转动驱动机构、传动齿轮、直线驱动机构以及扑翼机构,第一转动驱动机构的驱动端与传动齿轮传动连接,直线驱动机构设在传动齿轮上,扑翼机构与直线驱动机构的驱动端转动连接。该飞行器包括该仿生扑翼装置。本发明提供的仿生扑翼装置和飞行器用于用于降低扑翼飞行器的装配难度,合理配重,提高了扑翼飞行器的运动稳定性。


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    Titel :

    Bionic flapping wing device and aircraft


    Weitere Titelangaben:

    一种仿生扑翼装置及飞行器


    Beteiligte:
    PAN TIANYU (Autor:in) / LIANG JINZE (Autor:in) / ZHENG MENGZONG (Autor:in) / PENG LIANSONG (Autor:in) / SU GUANTING (Autor:in)

    Erscheinungsdatum :

    2023-05-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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