The invention relates to the technical field of aircraft manufacturing, and one embodiment of the invention provides a wing assembly turnover device which comprises a first turnover frame, the first turnover frame is provided with a plurality of limiting parts, a limiting space is formed among the limiting parts, a second turnover frame is arranged in a lifting and translation mode relative to the first turnover frame, and the first turnover frame is provided with a plurality of limiting parts. The second turnover frame moves into or out of the limiting space after moving relative to the first turnover frame, the third turnover frame is movably arranged relative to the second turnover frame, the adjusting frames are arranged in a lifting and swinging mode relative to the third turnover frame, and the multiple adjusting frames are used for bearing aircraft wings. By means of the technical scheme, the technical problem that in the prior art, a wing transfer device is poor in flexibility is solved.

    本公开涉及飞机制造技术领域,本公开的一个实施例提供了一种机翼组装周转装置,其包括第一周转架,第一周转架具有限位部,限位部为若干个,若干个限位部之间形成限位空间,第二周转架相对第一周转架升降且平移设置,第二周转架相对第一周转架移动后,移入或移出限位空间,第三周转架相对第二周转架移动设置,调节架相对第三周转架升降且摆动设置,调节架为若干个,用于承托飞机机翼。通过上述技术方案,解决了现有技术中机翼转运装置灵活性较差的技术问题。


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    Title :

    Wing assembly turnover device


    Additional title:

    一种机翼组装周转装置


    Contributors:
    ZHENG YI (author) / WANG LEI (author)

    Publication date :

    2025-04-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    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



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