Aircraft tire

Details Aircraft tire Aircraft tire

B - Operations, Transporting

60

C

B60C 9/08 (2006.01) B60C 9/09 (2006.01) B60C 15/00 (2006.01) B60C 15/06 (2006.01)

Patent

CA 2125202

An improved aircraft tire 10 is described. The tire 10 has at least two circumferentially extending reinforcement inserts. At least one pair of reinforced inserts 90 is located on each side of the tire. Each insert 90 preferably has two cord reinforced members 91,92 having bias angled cords. The cords are equal but opposite in orientation relative to the cords of the adjacent member. The pairs of reinforced members 91,92 extend from the bead portion 18,20 and terminate in a radially upper portion of the sidewall 14A,16A. Each pair of reinforcement members 91,92 is interposed between a pair of carcass plies 36,37,38,39,40,41,42,43 on the ply side of the tire 10. This structure can increase tire durability while at the same time achieve a significant weight reduction.

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