The invention discloses an anti-vibration vertical take-off and landing aircraft, which comprises an aircraft body, an anti-vibration module and a sensor assembly are arranged in the aircraft body, and the anti-vibration module comprises a carrying table and a three-axis moving vibration buffering structure; the three-axis moving vibration buffering structure comprises an X-axis moving vibration buffering assembly and a Y-axis moving vibration buffering assembly, wherein the X-axis moving vibration buffering assembly is connected with the carrying table in a matched mode and enables the carrying table to move in the X-axis direction to achieve vibration buffering, and the Y-axis moving vibration buffering assembly is connected with the carrying table in a matched mode and enables the carrying table to move in the Y-axis direction to achieve vibration buffering. the Z-axis moving vibration buffering assembly is connected with the X-axis moving vibration buffering assembly and the Y-axis moving vibration buffering assembly in a matched mode and enables the X-axis moving vibration buffering assembly and the Y-axis moving vibration buffering assembly to move in the Z-axis direction so as to achieve vibration buffering. According to the anti-vibration vertical take-off and landing aircraft, the anti-vibration requirements of the aircraft in different working environments can be met, so that the situation of data deviation caused by vibration of the angle sensor and the acceleration sensor can be improved, and the accuracy of data detected by the angle sensor and the acceleration sensor can be improved.

    本发明公开了一种抗振垂直起降飞行器,包括飞行器本体,飞行器本体内设有抗振模块和传感器组件,抗振模块包括载台和三轴移动缓振结构;三轴移动缓振结构包括与载台配合连接并供载台沿X轴方向移动以实现缓振的X轴移动缓振组件、与载台配合连接并供载台沿Y轴方向移动以实现缓振的Y轴移动缓振组件、与X轴移动缓振组件和Y轴移动缓振组件配合连接并供X轴移动缓振组件和Y轴移动缓振组件沿Z轴方向移动以实现缓振的Z轴移动缓振组件。上述抗振垂直起降飞行器,可以满足飞行器在不同工作环境下的抗振要求,从而可以改善角度及加速度传感器由于受到振动而导致数据偏差的情况,有利于提高角度及加速度传感器检测数据的精确性。


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    Titel :

    Anti-vibration vertical take-off and landing aircraft


    Weitere Titelangaben:

    一种抗振垂直起降飞行器


    Beteiligte:
    XU KAIMING (Autor:in) / LI JIAPENG (Autor:in) / GAO DAPENG (Autor:in) / FENG GUOTAO (Autor:in) / XU KE (Autor:in) / WU ZHIGANG (Autor:in) / CHEN FUZHENG (Autor:in) / CHEN MIN (Autor:in) / YIN XINFAN (Autor:in) / SHI GUANGYI (Autor:in)

    Erscheinungsdatum :

    2021-09-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn