The invention relates to the technical field of aircraft wing riveting assembly, in particular to an aircraft wing riveting assembly hoisting auxiliary device. The aircraft wing riveting, assembling and hoisting auxiliary device provided by the invention can perform small-amplitude fine adjustment on the butt joint position of the wing and improve the assembly and butt joint accuracy of the wing. An aircraft wing riveting assembly hoisting auxiliary device comprises supporting plates, connecting plates, mounting plates, hoisting mechanisms and moving mechanisms, the number of the supporting plates is two, the connecting plates are connected between the tops of the supporting plates, the upper sides of the front portions and the rear portions of the supporting plates are connected with the mounting plates through bolts, the hoisting mechanisms are arranged on the supporting plates, and the moving mechanisms are arranged on the connecting plates. A hydraulic cylinder telescopic rod drives a first connecting frame to move, so that a fixing frame drives a supporting plate to conduct small-amplitude position adjustment, then the position of a wing is finely adjusted, and the wing can be in butt joint more accurately.

    本发明涉及飞机机翼铆接装配技术领域,尤其涉及一种飞机机翼铆接装配吊装辅助装置。本发明提供一种能够对机翼对接位置进行小幅度微调,提高机翼装配对接精准度的飞机机翼铆接装配吊装辅助装置。一种飞机机翼铆接装配吊装辅助装置,包括有支撑板、连接板、安装板、吊装机构和移动机构,支撑板共有两块,支撑板顶部之间连接有多个连接板,支撑板前后两部上侧均通过螺栓连接安装板,支撑板上设有吊装机构,连接板上设有移动机构。本发明通过液压缸伸缩杆带动第一连接架进行运动,从而使得固定架带动支撑板进行小幅度位置调整,进而对机翼的位置进行微调,使得机翼能够对接的更加精准。


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    Titel :

    Auxiliary device for riveting, assembling and hoisting aircraft wings


    Weitere Titelangaben:

    一种飞机机翼铆接装配吊装辅助装置


    Beteiligte:
    WU DI (Autor:in) / HAN GUIJUN (Autor:in) / TAN JUN (Autor:in) / XU WENMING (Autor:in) / GAO XIAOLONG (Autor:in) / ZHANG XINXIN (Autor:in)

    Erscheinungsdatum :

    09.05.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B66C Krane , CRANES / B66D Haspeln , CAPSTANS



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