| 摘要 |
The invention relates to an aircraft tire, the inflation pressure of which is greater than 9 bar and the deflection of which is greater than 30%, comprising a crown, two sidewalls and two beads, a carcass reinforcement anchored in the two beads and a crown reinforcement, in which the carcass reinforcement comprises at least one circumferential alignment of reinforcement elements and in which the means for anchoring said reinforcement elements within each bead comprise circumferentially oriented reinforcement elements axially bordering said circumferential aligmnents of said reinforcement elements of the carcass reinforcement, said reinforcement elements of the carcass reinforcement and said circumferentially oriented reinforcement elements being separated by a bonding rubber mix of very high elasticity modulus. According to the invention, said circumferentially oriented reinforcement elements are cables having a penetrability of between 80 and 100%, the breaking load of the cables being greater than 150 daN and said cables having an elongation at break greater than 4%.
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