The invention discloses an unmanned flight system. The system comprises a launch canister; the piston assembly is arranged in the launching cylinder in a sliding manner; the foldable unmanned aerial vehicle is located in the launching cylinder, and the piston assembly can slide till the foldable unmanned aerial vehicle is pushed out of the launching cylinder; the launching device is used for driving the piston assembly to move; the foldable unmanned aerial vehicle comprises a fuselage; the cantilever is movably arranged on the machine body and can move to be close to the machine body; the propeller hub is rotationally arranged at the tail end, away from the fuselage, of the cantilever; the paddle assembly is movably arranged on the propeller hub, and the paddle assembly can move to be close to the cantilever; the driving device is used for driving the propeller hub to rotate; the reset device is used for driving the cantilever to be away from the fuselage and driving the paddle assembly to be away from the cantilever; by applying the system, the deployment efficiency can be effectively improved.

    本发明公开一种无人飞行系统,包括:发射筒;活塞组件,滑动设置在发射筒当中;可折叠无人机,位于发射筒当中,活塞组件能够滑动至将可折叠无人机推出发射筒;发射装置,用于驱动活塞组件移动;可折叠无人机包括:机身;悬臂,可移动设置在机身上,悬臂能够移动至靠近机身;桨毂,转动设置在悬臂远离机身的末端;桨叶组件,可移动设置在桨毂上,桨叶组件能够移动至靠近悬臂;驱动装置,用于驱动桨毂转动;复位装置,用于驱动悬臂远离机身,以及驱动桨叶组件远离悬臂;应用上述系统能够有效提高部署效率。


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    Title :

    Unmanned flight system and control method


    Additional title:

    一种无人飞行系统及控制方法


    Contributors:
    HE JUN (author) / YANG BONING (author) / DENG DENGBAO (author) / LIU SHIYAO (author)

    Publication date :

    2023-08-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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