Patent ID: 7278457
Filing Date: 2007-10-09
Classification: B60C,Y10T

Abstract:
1. 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 carcass reinforcement elements and in which the carcass reinforcement elements are anchored within each bead by circumferentially oriented reinforcement elements axially bordering said at least one circumferential alignment of said carcass reinforcement elements, said carcass reinforcement elements and said circumferentially oriented reinforcement elements being separated by a bonding rubber mix of very high elasticity modulus, wherein said circumferentially oriented reinforcement elements are cables, wherein said cables have a penetrability of between 80 and 100%, wherein the breaking load of the cables is greater than 150 daN and wherein said cables have an elongation at break greater than 4%.