The invention discloses a subdivision device and method for a non-adhesive smooth wall surface boundary. Comprising a partition plate supporting seat (1), the partition plate supporting seat (1) is in sliding connection with an airtight partition plate (2) in the vertical direction, an airtight clamping groove (8) is formed in the outer edge of the airtight partition plate (2), an airtight belt (3) is arranged in the airtight clamping groove (8), and the outline of the outer edge of the top of the airtight partition plate (2) is parallel to the outline of a subdivision interface (7). According to the invention, the problems of cabin loading uniformity and structural rigidity are solved.

    本发明公开了一种非粘接式光滑壁面边界的分舱装置及方法。包括隔板支撑座(1),隔板支撑座(1)与气密隔板(2)沿竖向滑动连接,沿气密隔板(2)外缘设有气密卡槽(8),气密卡槽(8)内设有气密带(3),气密隔板(2)顶部外缘轮廓与分舱界面轮廓(7)平行。本发明解决了分舱加载均匀性和结构刚度的问题。


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    Title :

    Non-adhesive smooth wall surface boundary subdivision device and method


    Additional title:

    一种非粘接式光滑壁面边界的分舱装置及方法


    Contributors:
    YANG KONGJIA (author) / LI XIANG (author) / WANG MINGHAI (author) / CHEN ZHUO (author) / WEI ZIXIANG (author) / GAO XUDONG (author)

    Publication date :

    2025-04-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / 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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