The invention relates to an unmanned flight system with an automatic ejection function and an ejection method thereof, belongs to the technical field of unmanned aerial vehicles, and solves the problems that wings need to be manually unfolded when an existing folding unmanned aerial vehicle is launched and the unmanned aerial vehicle is slow in lift-off response. Comprising an unmanned aerial vehicle and an automatic ejection mechanism. The unmanned aerial vehicle is a folding unmanned aerial vehicle; the automatic ejection mechanism comprises an energy storage cavity, an ejection cabin and an unmanned aerial vehicle bracket; the energy storage cavity is used for providing power required by ejection; the ejection cabin is cylindrical and is used for filling the folded unmanned aerial vehicle; the unmanned aerial vehicle bracket is arranged in the ejection cabin and located above the energy storage cavity. The energy storage cavity can push the unmanned aerial vehicle bracket to slide along the ejection cabin; the unmanned aerial vehicle bracket is used for pushing the unmanned aerial vehicle to pop out of the ejection cabin. Ejection lift-off of the folding type unmanned aerial vehicle is achieved, the unmanned aerial vehicle is automatically unfolded and enters a flight state after being launched, and the task state of quick response, lift-off and flight of the unmanned aerial vehicle can be achieved.

    本发明涉及一种自动弹射的无人飞行系统及其弹射方法,属于无人飞行器技术领域,解决现有折叠式无人机发射时需要手动展开机翼以及无人机升空响应慢的问题。包括:无人机和自动弹射机构;无人机为折叠式无人机;自动弹射机构包括:蓄能腔、弹射舱和无人机托架;蓄能腔用于提供弹射所需的动力;弹射舱为筒形,用于装填折叠后的无人机;无人机托架设置在弹射舱内部,且位于蓄能腔的上方;蓄能腔能够推动无人机托架沿弹射舱滑移;无人机托架用于推动无人机从弹射舱内部弹出。本发明实现了折叠式无人机的弹射升空,无人机发射后自动展开并进入飞行状态,可以实现无人机的快速响应、升空并达到飞行的任务状态。


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    Titel :

    Automatic ejection unmanned flight system and ejection method thereof


    Weitere Titelangaben:

    一种自动弹射的无人飞行系统及其弹射方法


    Beteiligte:
    ZHANG SHAOQUN (Autor:in) / ZHAO XIAOCHUAN (Autor:in) / WANG XINGQUAN (Autor:in) / KANG LE (Autor:in) / LIU YING (Autor:in) / HONG TIANGE (Autor:in) / DONG SHIPENG (Autor:in) / SHAO JIAXING (Autor:in) / WANG ZICHE (Autor:in)

    Erscheinungsdatum :

    11.11.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    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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