The invention discloses a box-type launching device based on an inclined nozzle rocket boosting unmanned aerial vehicle, which comprises a framework, skins, a guide rail, an unmanned aerial vehicle releasing mechanism, a rocket tightening mechanism, a first butt joint mechanism and a second butt joint mechanism, the framework is an integral force bearing structure of the launching box device, and four side surfaces of the framework cover the skins; the guide rails are fixed to the inner side areas of the two sides of the framework, the unmanned aerial vehicle releasing mechanism is installed above the rear side of the framework, the rocket tightening mechanism is installed below the rear side of the framework, and the first butt-joint mechanism and the second butt-joint mechanism are installed on the upper edge and the lower edge of the two sides of the framework and used for stacking and fixing box type launching devices. During boxing, the unmanned aerial vehicle is pushed into the box type launching device along the guide rail, and the unmanned aerial vehicle releasing mechanism fixes the unmanned aerial vehicle in the launching box; in the launching stage, the unmanned aerial vehicle releasing mechanism is separated from the unmanned aerial vehicle, and the rocket tightening mechanism abuts against the lower fulcrum of the inclined nozzle rocket. The problems that in the prior art, the occupied space of a cluster launching site is large, the guarantee difficulty is high, and position transfer is inconvenient are solved.

    本发明公开了一种基于斜喷管火箭助推无人机的箱式发射装置,包括骨架、蒙皮、导轨、无人机释放机构、火箭加紧机构、第一对接机构和第二对接机构,所述骨架为发射箱装置的整体承力结构,骨架的四个侧面覆盖蒙皮,导轨固定在骨架两侧内侧区域,所述无人机释放机构安装在骨架后侧上方,火箭加紧机构安装在骨架后侧下方,第一对接机构、第二对接机构安装在骨架两侧上下棱边上,用于箱式发射装置的堆码固定;装箱时,无人机沿导轨推入箱式发射装置,无人机释放机构使无人机在发射箱内固定;发射阶段,无人机释放机构与无人机分离,火箭加紧机构顶紧斜喷管火箭的下支点。本发明解决了现有技术中集群发射场地占用大、保障难度高、阵地转移不便等问题。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Box-type launching device based on inclined nozzle rocket boosting unmanned aerial vehicle


    Weitere Titelangaben:

    一种基于斜喷管火箭助推无人机的箱式发射装置


    Beteiligte:
    XIAO JIE (Autor:in) / YAO LIN (Autor:in) / ZHANG XIAOMU (Autor:in) / JIANG QIYONG (Autor:in) / WANG BING (Autor:in) / ZHANG CHENGCHENG (Autor:in)

    Erscheinungsdatum :

    2024-03-12


    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



    Rocket boosting launching thrust axis design of unmanned aerial vehicle

    RAO XIBO / WANG DONGLI / XUE YING | Europäisches Patentamt | 2023

    Freier Zugriff

    Unmanned aerial vehicle boosting launching device

    ZHONG FUJIAN / DENG JINGYONG / HAN CAIGUAN et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Booster rocket launching type unmanned aerial vehicle

    ZHOU TAO / GAO YAJING / YANG BIN et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Rapid matching method for rocket boosting launching parameters of unmanned aerial vehicle

    CHEN JIE / TONG CHAO / LEI LIMING et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Front-axle rotary type double-rocket booster unmanned aerial vehicle launching device

    WANG XIAODONG / YAO LIN / DU HONGLI et al. | Europäisches Patentamt | 2024

    Freier Zugriff