The invention relates to the field of tires, and discloses an aircraft tire, the inner contour of the cross section of the aircraft tire comprises a crown circular arc, two first side circular arcs, two first transition circular arcs, two second side circular arcs, two tire bead circular arcs and two second transition circular arcs, the two first side arcs are connected with the two ends of the crown arc through the two first transition arcs respectively, the two second side arcs are connected with the two first side arcs respectively, and the two tire bead arcs are connected with the two second side arcs through the two second transition arcs respectively. According to the aircraft tire, the long and soft tire side is designed, so that in the landing impact process of the tire, the stress on the tire side is reduced, the tire side can better adapt to the working condition of large deformation, and the fault problems of bulging, delaminating, blasting and the like are not prone to occurring.

    本发明涉及轮胎领域,公开一种航空轮胎,该航空轮胎的横截面内轮廓包括冠部圆弧、两个第一侧部圆弧、两个第一过渡圆弧、两个第二侧部圆弧、两个胎圈圆弧以及两个第二过渡圆弧,两个第一侧部圆弧分别通过两个第一过渡圆弧分别与冠部圆弧的两端相连,两个第二侧部圆弧分别与两个第一侧部圆弧相连接,两个胎圈圆弧分别通过两个第二过渡圆弧分别与两个第二侧部圆弧相连。该航空轮胎,设计了较长且柔软的胎侧,轮胎着陆冲击过程中,胎侧受力减少,胎侧可以更好地适应大变形工况,不容易出现鼓包、脱层、爆破等故障问题。


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    Title :

    Aircraft tire


    Additional title:

    一种航空轮胎


    Contributors:

    Publication date :

    2023-04-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B60C VEHICLE TYRES , Fahrzeugreifen



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