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    • 102. 发明公开
    • Pneumatic radial tire for airplanes
    • Pneumatischer Radialflugzeugififen
    • EP1800905A2
    • 2007-06-27
    • EP06256065.1
    • 2006-11-28
    • Bridgestone Corporation
    • Itai, Seiji c/o Bridgestone Corp. Technical Center
    • B60C9/28B60C3/00
    • B60C11/0083B60C9/2204B60C9/263B60C11/00B60C11/0306B60C11/0332B60C11/04B60C2200/02
    • A pneumatic radial tire for an airplane comprises a pair of bead cores, a carcass comprised of at least one carcass ply, a main belt comprised of at least two belt layers, an auxiliary belt comprised of plural layers, and a tread, wherein the main belt has a lamination thickness satisfying 0.2 ≤ G 1 /G 0 ≤ 0.8 as a relation between a lamination thickness at the widthwise center of the tire (Go) and a lamination thickness at a position corresponding to 2/3 of a maximum width (G 1 ), and the tread satisfies 0.85 ≤ D S /D C ≤ 1.1 as a relation between a tread thickness at a widthwise center position of the tire (D C ) and a tread thickness at a position of a width corresponding to 80% of a maximum width of the main belt (D S ), and has a radius of curvature on an outer surface of the tread formed by filling a normal internal pressure satisfying 0.4 ≤ R 2 /R 1 ≤ 3.0 as a relation between a radius of curvature in a central region including the widthwise center of the tire (R 1 ) and a radius of curvature forming a widthwise side region outward from the central region (R 2 ) being connected to each other at a position corresponding to 40-60% of the maximum width of the main belt.
    • 一种用于飞机的充气子午线轮胎包括一对胎圈芯,包括至少一个胎体帘布层的胎体,由至少两个带束层组成的主带,由多层构成的辅助带和胎面,其中主体 作为轮胎宽度方向中心处的层叠厚度(Go)与对应于最大宽度(G)的2/3的位置的层叠厚度之间的关系,具有满足0.2‰G 1 / G 0‰0.8的层压厚度 1),并且胎面满足0.85‰DS / DC‰1.1作为轮胎(DC)的宽度方向中心位置处的胎面厚度与宽度对应于最大宽度的80%的位置处的胎面厚度之间的关系 ,并且在通过填充满足0.4‰R 2 / R 1‰3.0的正常内部压力的胎面外表面上具有曲率半径作为中心区域的曲率半径之间的关系 包括轮胎的宽度方向中心(R 1) 并且形成从中心区域(R 2)向外的横向侧区域的曲率半径在对应于主带的最大宽度的40-60%的位置处彼此连接。
    • 110. 发明公开
    • PNEUMATIC TIRE FOR AIRCRAFT
    • LUFTREIFENFÜRFLUGZEUG
    • EP1714801A1
    • 2006-10-25
    • EP05709868.3
    • 2005-02-08
    • Bridgestone Corporation
    • ONUMA, S., c/o Bridgestone Corp. Tech. CenterSUZUKI, T., c/o Bridgestone Corp. Tech. Center
    • B60C11/00
    • B60C11/00B60C11/005B60C11/0075B60C2200/02
    • An aircraft pneumatic tire that has deeper grooves without causing deterioration in the heat resistance of a top tread and thereby can increase the number of landings per tread is provided.
      At least part of a top tread 2 in the width direction of the tire has a two-layer structure consisting of a base tread layer 11 and a cap tread layer 12 stacked in the radial outward direction in this order. At least one circumferential groove 4a to 4d is provided in the surface of the top tread 2. The base tread layer 11 and the cap tread layer 12 satisfy the relationships expressed by the following formulas (1) and (2): 1.05 M ( 50 ) b / M ( 50 ) c ≤ 1.30 1.04 R b / R c ≤ 1.20 (wherein M(50) b and M(50) c denote 50% moduli of the base tread rubber and the cap tread rubber, respectively, and R b and R c denote the resiliences of the base tread rubber and the cap tread rubber, respectively).
    • 具有更深的凹槽而不会导致顶部胎面的耐热性劣化并因此可以增加每个胎面的着陆数量的飞机充气轮胎。 轮胎宽度方向上的顶部胎面2的至少一部分具有由沿着径向向外的方向依次层叠的基底胎面层11和胎面覆盖层12构成的两层结构。 至少一个圆周槽4a至4d设置在顶部胎面2的表面中。基底胎面层11和胎面花纹层12满足由下式(1)和(2)表示的关系:1.05