The invention relates to a four-shaft eight-rotor unmanned aerial vehicle with tiltable rotor shafts, and belongs to the technical field of aircraft design, the four-shaft eight-rotor unmanned aerial vehicle is composed of a fuselage assembly, a connecting assembly group, a tilting driving assembly group, a detection assembly, an undercarriage group, a GPS module and a camera, and the design of the connecting assembly and the tilting driving assembly enables the rotor shafts to realize omnidirectional tilting in space; the rotor wings are driven to generate flexible and variable lift force directions in the space, and the loaded expansion assembly can expand the application scene of the four-shaft eight-rotor-wing unmanned aerial vehicle with the tiltable rotor wing shafts. Compared with a traditional unmanned aerial vehicle, the unmanned aerial vehicle has more motion freedom degrees, the position and the posture of the unmanned aerial vehicle can be independently controlled, the advantages of operability, high reliability and the like of the traditional unmanned aerial vehicle are reserved, and meanwhile the maneuverability, the flexibility and the wind disturbance resistance of the unmanned aerial vehicle can be improved.

    一种可倾转旋翼轴的四轴八旋翼无人机属飞行器设计技术领域,本发明由机身组件、连接组件组、倾转驱动组件组、探测组件、起落架组、GPS模块和摄像头组成,连接组件以及倾转驱动组件的设计使旋翼轴可在空间中实现全向倾转,带动旋翼在空间中产生灵活可变的升力方向,装载的扩展组件可拓展本发明的可倾转旋翼轴的四轴八旋翼无人机的应用场景。相较于传统无人机,拥有更多的运动自由度,可以独立控制其位置与姿态,保留传统无人机的易操作性、高可靠性等优点的同时,能提高无人机的机动性、灵活性以及抗风扰能力。


    Access

    Download


    Export, share and cite



    Title :

    Four-shaft eight-rotor unmanned aerial vehicle with tiltable rotor shafts


    Additional title:

    一种可倾转旋翼轴的四轴八旋翼无人机


    Contributors:
    ZHU HANG (author) / ZHANG JIAKUO (author) / LIN DEKAI (author) / LIU SHUBIN (author)

    Publication date :

    2024-11-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



    Deformation tiltable four-rotor unmanned aerial vehicle

    HU DANDAN / FENG KUNHUI / GUAN RUOQIAO et al. | European Patent Office | 2021

    Free access

    Rotor wing tiltable unmanned aerial vehicle control system

    ZHANG JUNQI | European Patent Office | 2024

    Free access

    Tiltable rotor unmanned aerial vehicle and using method thereof

    XIE ZHONGLIANG / WANG XUERUI / CHEN JIAPING et al. | European Patent Office | 2020

    Free access

    Tilting component of tilting rotor unmanned aerial vehicle, tiltable rotor unmanned aerial vehicle and using method

    XIE ZHONGLIANG / WANG XUERUI / CHEN JIAPING et al. | European Patent Office | 2020

    Free access

    Multirotor aerial vehicle with tiltable rotor

    WANG XI | European Patent Office | 2024

    Free access