The invention relates to a catapulting method for a folding unmanned aerial vehicle, belongs to the technical field of unmanned aerial vehicle launching, and solves the problems that in the prior art, folding unmanned aerial vehicle launching needs electric power or pneumatic driving, the requirement for launching conditions is high, and the environmental adaptability is poor. The ejection method comprises the following steps that S1, a thrust guide plate is installed in an ejection cylinder, the thrust guide plate is locked through an ejection mechanism, and meanwhile the thrust guide plate is connected with an elastic rubber band; s2, pulling a launching mechanism and a thrust guide plate to a launching position, and loading the folding unmanned aerial vehicle to be launched; s3, the launching mechanism is driven to unlock the thrust guide plate; the thrust guide plate slides along the launching barrel under the elastic action of the elastic rubber band, and meanwhile the folding type unmanned aerial vehicle is pushed to be ejected out of the barrel. According to the invention, catapult launching of the folding unmanned aerial vehicle is realized.

    本发明涉及一种用于折叠无人机的弹射方法,属于无人机发射技术领域,解决了现有技术中折叠无人机发射需要电力或气压驱动对发射条件要求高环境适应性差的问题。本发明的弹射方法包括以下步骤:步骤S1:将推力导板装入发射筒内,通过发射机构将推力导板锁定,同时将推力导板与弹力皮筋连接;步骤S2:拉动发射机构和推力导板至发射位,装入待发射的折叠式无人机;步骤S3:驱动发射机构解锁推力导板;推力导板在弹力皮筋的弹力作用下沿发射筒滑移,同时推动折叠式无人机弹射出筒。本发明实现了对折叠式无人机的弹射发射。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Ejection method for folding unmanned aerial vehicle


    Weitere Titelangaben:

    一种用于折叠无人机的弹射方法


    Beteiligte:
    WANG DONG (Autor:in) / SONG HAIPING (Autor:in) / LI HAO (Autor:in) / NAN LIJUN (Autor:in) / WANG YONGSHAN (Autor:in) / ZHOU HEJIA (Autor:in) / YANG SHUAI (Autor:in)

    Erscheinungsdatum :

    2023-11-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    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



    Ejection device, unmanned aerial vehicle and ejection method

    KOMINAMI ATSUSHI / ARAKI SOJI | Europäisches Patentamt | 2021

    Freier Zugriff

    Unmanned aerial vehicle ejection method

    NIE YONGBIN / LIU YAFENG / LIU ZEFENG et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    EJECTION DEVICE, UNMANNED AERIAL VEHICLE AND EJECTION METHOD

    KOMINAMI ATSUSHI / ARAKI SOUJI | Europäisches Patentamt | 2021

    Freier Zugriff

    Ejection type unmanned aerial vehicle

    DAI PENG | Europäisches Patentamt | 2021

    Freier Zugriff

    Folding unmanned aerial vehicle

    SONG WENHAO / BIAN HAO / LIU HUIYING | Europäisches Patentamt | 2023

    Freier Zugriff