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Aircraft tire having a casing reinforcement member with improved durability

机译:具有具有增强的耐久性的壳体增强构件的飞机轮胎

摘要

The radial tire for an aircraft (1) defines three main directions of circumferential direction (X), axial direction (Y) and radial direction (Z), and a crown (2) on which the tread (3) is placed; It comprises two side walls (4) and two beads (5), each of the side walls (4) connecting the bead (5) to the crown (2) and further beading at the at least one bead wire (6) A carcass reinforcing member (7) fixed in each of (5) and extending in the side wall (4) to the crown (2); and extending in the circumferential direction (X) in the crown (2) and carcass A carcass reinforcing member (7), which is referred to as a radial carcass reinforcing member, comprising a crown reinforcing member or a belt (10) radially arranged between the reinforcing member (7) and the tread (3), N multi forming a helical structure Rubber reinforced by a substantially radially oriented reinforcing element, called a radial fabric reinforcer, consisting wholly or partly of nylon woven plied yarn (30) comprising yarn strands (20a, 20b, 20c) With at least one ply, referred to as carcass ply, in the form of a matrix or composition, -N is greater than 2,-count number indicated by Ti of each strand is greater than 180 tex,-indicated by Te1 of each strand The tensile strength is greater than 75 cN / tex, the breaking elongation of each strand shown by Ar 1 is greater than 14%, the tensile strength shown by Te 2 of each ply yarn is greater than 60 cN / tex, each Elongation at break indicated by Ar2 of ply yarn is greater than 18%,-helical angle indicated by α of each ply yarn Is characterized by greater than 20 degrees. [Selected figure] Figure 1
机译:用于飞机的子午线轮胎(1)限定了圆周方向(X),轴向方向(Y)和径向方向(Z)的三个主要方向,以及在其上放置胎面(3)的胎冠(2)。它包括两个侧壁(4)和两个胎圈(5),每个侧壁(4)将胎圈(5)连接到胎冠(2),并在至少一根胎圈钢丝(6)处进一步胎圈化。加强件(7)固定在(5)的每一个中,并在侧壁(4)中延伸至胎冠(2);胎体增强件(7),被称为径向胎体增强件,其包括胎冠增强件或沿径向布置在胎冠之间的带束层(10),胎冠增强件(7)被称为径向胎体增强件。增强构件(7)和胎面(3),N多重形成螺旋结构,通过被称为径向织物增强剂的基本上径向取向的增强元件增强的橡胶,该增强元件全部或部分地由包含纱线股的尼龙编织合股纱线(30)组成(20a,20b,20c)在具有基质或组合物形式的至少一层称为胎体帘布层的情况下,-N大于2,-每根链的Ti表示的数量大于180 tex, -由每根股线的Te1表示拉伸强度大于75 cN / tex,由Ar 1表示的每根股线的断裂伸长率大于14%,由每层帘线的Te 2表示的拉伸强度大于60 cN / tex,每个断裂伸长率表示帘线的Ar 2的Δθ大于18%,每条帘线的由α表示的螺旋角的特征在于大于20度。 [选定图]图1

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