The invention discloses a folding wing unmanned aerial vehicle aerial cluster throwing device, and belongs to the field of unmanned aerial vehicle throwing devices.The folding wing unmanned aerial vehicle aerial cluster throwing device comprises a carrier, a load assembly, a fixing frame, a rotating frame, a rotating driving assembly and a locking assembly, a first throwing opening is formed in the bottom of the carrier, and the load assembly comprises a throwing cylinder and a brake parachute which are connected; the throwing barrel is used for loading and launching the folding wing unmanned aerial vehicle, the fixing frame is installed in the carrier, a second throwing opening is formed in the bottom of the fixing frame, the rotating frame is rotationally connected into the fixing frame, and a plurality of third containing cavities used for loading the load assemblies are formed in the rotating frame around the axis of the rotating frame in an annular array mode. The rotating driving assembly is used for driving the rotating frame to rotate so that the open end of the third containing cavity can face the second throwing opening, and the locking assembly is used for opening or closing the second throwing opening. The problems of short voyage, limited air launching quantity and the like of the folding-wing unmanned aerial vehicle can be effectively solved, and the purpose that the folding-wing unmanned aerial vehicle cluster remotely reconnaissance or strikes ground targets is achieved.

    本发明公开了一种折叠翼无人机空中集群投放装置,属于无人机投放装置领域,包括载机、载荷组件、固定架、转动架、转动驱动组件和锁定组件,载机的底部设置有第一投放口,载荷组件包括相连接的投放筒和减速伞,投放筒用于装载和发射折叠翼无人机,固定架安装在载机内,固定架的底部设置有第二投放口,转动架转动连接在固定架内,转动架上绕转动架的轴线环形阵列设置有多个用于装载载荷组件的第三容置腔,转动驱动组件用于带动转动架转动以使第三容置腔的敞口端朝向第二投放口,锁定组件用于打开或关闭第二投放口。可有效解决折叠翼无人机航程短、空中发射数量局限等问题,实现折叠翼无人机集群远距离侦察或打击地面目标的目的。


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    Titel :

    Folding-wing unmanned aerial vehicle aerial cluster launching device


    Weitere Titelangaben:

    一种折叠翼无人机空中集群投放装置


    Beteiligte:
    LU YAFEI (Autor:in) / WANG PENG (Autor:in) / WANG YUJIE (Autor:in) / CHEN QINGYANG (Autor:in) / GUO ZHENG (Autor:in) / JIA GAOWEI (Autor:in) / LIU DUONENG (Autor:in)

    Erscheinungsdatum :

    03.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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