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Airplane tire having a casing reinforcement with improved endurance

机译:飞机轮胎具有改进耐久性的套管加固

摘要

A radial aircraft tire (1), defined in three main directions, circumferential (X), axial (Y) and radial (Z), comprises a crown (2) surmounted by a tread (3), two sidewalls (4), two beads (5), each sidewall (4) connecting each bead (5) to the crown (2), a carcass reinforcement (7) that is anchored in each of the beads (5) at at least one bead wire (6) and extends in the sidewalls (4) as far as the crown (2), a crown reinforcement or belt (10) that extends in the crown (2) in the circumferential direction (X) and is situated radially between the carcass reinforcement (7) and the tread (3), said carcass reinforcement (7) having at least one ply referred to as carcass ply in the form of a rubber matrix reinforced with radially oriented reinforcing elements, referred to as radial textile reinforcers, the latter being constituted entirely or partially by textile plied yarns of nylon comprising N multifilament strands twisted together to form a helix, characterized in that: N is greater than 2; the count of each strand is greater than 180 tex; the tenacity of each strand is greater than 75 cN/tex; the elongation at break of each strand is greater than 14%; the tenacity of each plied yarn is greater than 60 cN/tex; the elongation at break of each plied yarn is greater than 18%; and the helix angle of each plied yarn is greater than 20°.
机译:在三个主方向上定义的径向飞机轮胎( 1 ),周向(x),轴向(y)和径向(z),包括冠部( 2 )克服通过胎面( 3 ),两个侧壁( 4 ),两个珠子( 5 ),每个侧壁( 4 )将每个珠子( 5 )连接到冠部( 2 / b>),抵碎在每个珠子中的胎体增强件( 7 / b>) ( 5 )在至少一个胎圈( 6 )中延伸( 2 ),在圆周方向(x)中延伸在冠长(x)中延伸的冠加强件或皮带( 10 )并且位于胎体加强件( 7 )和胎面( 3 ),其具有至少一个帘布层的胎体帘布层用径向取向的增强元件加强的橡胶基质的形式,称为径向纺织品增强剂,后者通过纺织品完全或部分地构成尼龙的纱线包括n个复丝股,以形成螺旋,其特征在于:n大于2;每个股线的计数大于180 Tex;每条股的韧度大于75 cn / tex;每个股线的伸长率大于14%;每个镀纱的韧度大于60 CN / TEX;每个镀纱的断裂伸长率大于18%;每个镀纱的螺旋角度大于20°。

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