A wing rib structure of an aircraft wing box is a combined structure and comprises a wall type wing rib, a frame type wing rib, a reinforcing supporting column and a fuel oil tank, the wall type wing rib and the frame type wing rib are arranged in parallel and connected into an integral structure through the reinforcing supporting column, the reinforcing supporting column is located in the middle of the wall type wing rib and the middle of the frame type wing rib, and the fuel oil tank is connected with the wall type wing rib. The central axis of the reinforcing supporting column is perpendicular to the course of the aircraft, the front ends of the wall type wing rib and the frame type wing rib are fixed to the wing front beam, the rear ends of the wall type wing rib and the frame type wing rib are fixed to the wing rear beam, and the fuel oil tank is located between the wall type wing rib and the frame type wing rib.

    一种飞机机翼翼盒的翼肋结构,该翼肋结构是一种组合结构,含有墙式翼肋、框式翼肋、加强支柱和燃油舱,所述的墙式翼肋和框式翼肋平行布置,并通过加强支柱连接为整体结构,加强支柱位于墙式翼肋和框式翼肋中部,加强支柱的中心轴线垂直于飞机的航向,墙式翼肋和框式翼肋的前端分别固定在机翼前梁上,墙式翼肋和框式翼肋的后端分别固定在机翼后梁上,燃油舱位于墙式翼肋和框式翼肋之间。


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    Title :

    Wing rib structure of wing box of aircraft wing


    Additional title:

    一种飞机机翼翼盒的翼肋结构


    Contributors:
    LI ZHENBO (author) / TIAN SHIXIONG (author) / LI XINGFU (author) / WANG ZHENFA (author) / WEI TING (author)

    Publication date :

    2023-01-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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