The invention discloses a wing body butt joint quick release mechanism which comprises an upper plate, a lower plate, a plug pin assembly and a pair of limiting assemblies. The upper plate piece and the lower plate piece are connected through a plate piece connecting piece, and sliding ways are formed in the upper plate piece and the lower plate piece; one end of the bolt assembly is located in the slide way, and the bolt assembly slides in the slide way, so that opening and closing operation of the wing body butt joint quick-release mechanism can be achieved, and shearing force and bending moment transmitted by the wing body butt joint lug piece are transmitted to the fuselage butt joint lug piece; the limiting assemblies are located on the two sides of the plug pin assembly. Compared with the prior art, tools are not needed, quick disassembly and assembly can be achieved, opening and closing operation can be completed only by pushing and pulling the corresponding plug pin assemblies and the limiting assemblies by hands, the tools are not needed, the quick disassembly and assembly function can be achieved, and the use requirement is met; according to the invention, the technical difficulty of butt joint and quick disassembly of the wing body of the large unmanned aerial vehicle is well solved, and the device has the advantages of no need of tools, quick disassembly and assembly, anti-vibration and high reliability.

    本发明公开了一种翼身对接快卸机构,包括上板件、下板件、插销组件和一对限位组件;所述上板件与下板件之间通过板件连接件相连接,所述上板件与下板件上均开设有滑道;所述插销组件一端位于滑道内部,通过所述插销组件在滑道内部滑动能够实现翼身对接快卸机构的打开、关闭操作,并将翼身对接耳片传来的剪力与弯矩传给机身对接耳片;一对所述限位组件位于插销组件的两侧。与现有技术相比,本发明无需工具、可快速拆装,仅靠人手推拉相应插销组件、限位组件就能完成打开、关闭操作,无需使用工具,可实现快速拆装功能,满足使用需求;本发明很好的解决了大型无人机翼身对接快卸的技术难点,具有无需工具、快速拆装、防振脱、可靠性高的优点。


    Access

    Download


    Export, share and cite



    Title :

    Wing body butt joint quick release mechanism and manufacturing method thereof


    Additional title:

    一种翼身对接快卸机构及其制造方法


    Contributors:
    GONG RUIJUN (author) / LIU DUANNA (author) / JU XIAOBIN (author) / GUO LEI (author) / WANG GUOPING (author)

    Publication date :

    2024-12-13


    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



    Aircraft wing body butt joint method

    QI ZHENCHAO / SUN GUANYU / LI WEI et al. | European Patent Office | 2024

    Free access

    Aircraft wing body butt joint adjusting method

    LIU GUOXIN / ZHANG SHANGAN / LIU YING et al. | European Patent Office | 2024

    Free access

    Quick butt joint mechanism for special emergency vehicle

    YU XINWEI / LI XUEWEI / LI GUIZHU et al. | European Patent Office | 2020

    Free access

    Quick butt joint locking device

    ZHANG HENGMING | European Patent Office | 2021

    Free access

    Quick-release fishing rod butt section

    HUANG REX H | European Patent Office | 2023

    Free access