The invention provides a wing hoisting and fixing structure of civil aircraft, which comprises a main body and a hoisting rope, a sliding block is connected to the top end of the middle of the main body and moves left and right along the top end of the middle of the main body, and the hoisting rope is connected to the bottom end of the sliding block to suspend aircraft wings; and multiple limiting assemblies arranged around the bottom end part of the hoisting rope in a penetrating, sleeving and embedding manner. By means of the limiting assemblies arranged on the device, when the wings are suspended through the hoisting rope, deflection blocks on the two sides of the limiting assemblies are made to deflect, extend and move out through abutting of the weight of the bottom ends of the wings, so that the deflection blocks can abut against the surface of the bottom ends of the wings, therefore, the contact area and distance between the hoisting rope and the bottom ends of the wings are increased, and the hoisting rope is not prone to inclination when hoisting the wings.

    本发明提供了一种民用飞机机翼吊装固定结构,包括:主体和吊装绳索,主体中部顶端连接有滑块沿着其主体中部顶端左右移动,滑块底端连接有吊装绳索来对飞机机翼进行悬吊;限定组件,限定组件为若干贯穿套接嵌合设置于在吊装绳索底端部分周围。通过该装置设置的限定组件能够在通过吊装绳索来对机翼进行悬吊的时候,通过机翼底端重量的抵靠来让限定组件两侧的偏斜块偏斜延伸移出,使得能够让偏斜块抵住到机翼的底端表面,以此来增加吊装绳索于机翼底端的接触面积和距离,使得吊装绳索在对机翼进行吊装的时候不会轻易的发生倾斜。


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    Title :

    Wing hoisting and fixing structure of civil aircraft


    Additional title:

    一种民用飞机机翼吊装固定结构


    Contributors:
    LI JIAO (author)

    Publication date :

    2021-05-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B66C Krane , CRANES / 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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