The invention discloses a mass center control system for a flapping rotor aircraft, and the mass center control system comprises a counterweight sliding block and a sliding block driving assembly which is used for driving the counterweight sliding block to move on a sliding plane so as to adjust the position, the sliding block driving assembly comprises a first driving mechanism capable of driving the balance weight sliding block to move in the first direction and a second driving mechanism capable of driving the balance weight sliding block to move in the second direction, and the straight line where the first direction is located does not coincide with the straight line where the second direction is located. The invention further discloses a flapping rotor aircraft. The flapping rotor aircraft comprises the mass center control system. The mass center control system and the flapping rotor aircraft have the advantages of being simple in structure, light in weight, good in environmental adaptability, high in control efficiency, high in reliability, free of a reaction torque mechanism and the like, and flexible flight in multiple directions can be achieved.

    本发明公开了一种用于扑旋翼飞行器的质心控制系统,所述质心控制系统包括配重滑块和用于带动所述配重滑块在滑动平面上移动以调整位置的滑块驱动组件,所述滑块驱动组件包括可带动配重滑块沿第一方向移动的第一驱动机构和可带动配重滑块沿第二方向移动的第二驱动机构,所述第一方向所在的直线与所述第二方向所在的直线互不重合。本发明还公开了一种扑旋翼飞行器,所述扑旋翼飞行器包括上述的质心控制系统。本发明的质心控制系统及扑旋翼飞行器具有结构简单、重量轻、环境适应性好、控制效率高、可靠性强、无需反扭矩机构等优点,并可实现多个方向的灵活飞行。


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    Title :

    Mass center control system for flapping-rotor aircraft and flapping-rotor aircraft


    Additional title:

    一种用于扑旋翼飞行器的质心控制系统及扑旋翼飞行器


    Contributors:
    WANG DOU (author) / LIU QINGHAO (author) / DAI JIAN (author)

    Publication date :

    2022-04-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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