Fabric inserts for filament wound aircraft tires
    1.
    发明授权
    Fabric inserts for filament wound aircraft tires 失效
    用于FILAMENT FAIL飞机轮胎的织物插件

    公开(公告)号:US3613762A

    公开(公告)日:1971-10-19

    申请号:US3613762D

    申请日:1969-11-26

    CPC classification number: B60C3/02 B60C15/0233 B60C2200/02 Y10T152/10873

    Abstract: A filament wound aircraft tire of the toroidal type which includes annular fabric strips positioned between the circular piles of the carcass in the heel or rim area, reinforcing the heel and adjacent rim edge increasing the strength and modulus of the tire carcass in this flexure area, and preventing flexure and compression fatigue failures of the carcass piles in these highly stressed areas. This invention constitutes an important improvement on my invention disclosed in my (T. J. Reinhart, Jr.) U.S. Pat. No. 3,171,462 for Toroidal Pneumatic Tire, dated Mar. 2, 1965, and having for an object the provision of means to increase the strength and modulus of the toroidal tire carcass in the area of the reinforcing ring or heel bead, adjacent the outer edges of the split rim or wheel.

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