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    • 103. 发明授权
    • TIRE FOR VEHICLES
    • 轮胎车辆
    • EP1701854B1
    • 2008-04-09
    • EP03819231.6
    • 2003-12-30
    • PIRELLI TYRE S.p.A.
    • BOIOCCHI, Maurizio, Pirelli Pneumatici S.p.A.MATRASCIA, Giuseppe, Pirelli Pneumatici S.p.A.
    • B60C11/18
    • B60C11/00B60C11/0058B60C11/1346B60C11/18
    • A pneumatic tire (1) is described comprising: a carcass structure (2) having at least one carcass ply (2a), and at least one annular reinforcing structure (3) associated to said carcass ply (2a), a pair of axially opposite side walls (7, 8) on the carcass structure (2), a belt structure (5) arranged at a radially outer position with respect to the carcass structure (2) and a tread band (6), arranged at a radially outer position with respect to the belt structure (5), and generally consisting of a first elastomeric material incorporating at least one portion substantially consisting of a second elastomeric material; wherein the tread band (6) comprises at least one groove (11) defined in the at least one portion substantially consisting of the second elastomeric material; wherein the ratio between the modulus of elasticity (E') under compression at 100°C of the second elastomeric material and the modulus of elasticity (E') under compression at 100°C of the first elastomeric material is not lower than about 1.30; and wherein the ratio between the IRHD hardness at 100°C of the second elastomeric material, measured in accordance with standard ISO 48, and the IRHD hardness at 100°C of the first elastomeric material, measured in accordance with standard ISO 48, is lower than about 1.10.
    • 105. 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。