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TIRE OF AIRCRAFT WITH CIRCUMFERENTIAL REINFORCEMENTS

机译:带有航空加强件的飞机轮胎

摘要

P The tire (10) is of the type comprising a tread (12), two flank portions (14, 16), two bead portions (18, 20), spaced from one another and comprising at least one bead wire (50, 52, 54) inextensible, the rods being disposed side by side and spaced axially, and a plurality of carcass plies extending circumferentially around the tire, from one bead portion to the other bead portion, each web having a web side extending between the bead webs (50, 52, 54) of opposing bead portions. br/ [0013] According to the invention there is provided at least one inserted part. reinforcing member (90) extending circumferentially and disposed on at least one side of the tire, the at least one reinforcement insert extending from the bead portion and terminating in a radially upper portion of the sidewall, each insert reinforcement being arranged radially towards the exterior to the carcass plies and being interposed between the sidewall (14, 16) and the carcass plies. / P
机译:轮胎(10)的类型包括胎面(12),两个侧面部分(14、16),两个胎圈部分(18、20),它们彼此间隔开并且包括至少一根胎圈钢丝(50)。 ,52、54)是不可延伸的,杆并排设置并且轴向间隔开,并且多个胎体帘布层围绕轮胎从一个胎圈部分延伸到另一胎圈部分,每个腹板的腹板侧在胎圈之间延伸相对的胎圈部分的腹板(50、52、54)。
[0013]根据本发明,提供了至少一个插入部分。加强件(90)沿周向延伸并设置在轮胎的至少一侧上,该至少一个加强插入件从胎圈部分延伸并终止于胎侧的径向上部,每个插入件加强件沿径向朝向外部布置。胎体帘布层并插入在侧壁(14、16)和胎体帘布层之间。

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