发明名称 Tire for an aircraft and method for producing the same
摘要 <p>There is provided a tire for an aircraft capable of enhancing abrasion resistance and effectively preventing a progress of peeling of the non-extensible cords of the main belt layers even when the tire suffers external injury reaching the main belt layers. A tire comprises a pair of bead cores 4, a carcass 5 toroidaly extending between the bead cores, a main belt 6 disposed on an outer peripheral side of a crown area of the carcass 5 and consisting of main belt layers having a spirally-wound structure of a non-extensible cord, and a sub belt 7 disposed on the outer peripheral side of the main belt 6 and consisting of sub belt layers 7a, 7b having an organic fiber cord extending in a circumferential direction of the tire in a zigzag pattern, wherein the sub belt layers 7a, 7b are formed in such a manner that the organic fiber cord in a zigzag pattern is wound several times in the circumferential direction of the tire, and that a crossing angle of the organic fiber cord with respect to an equatorial plane of the tire is within a range between 45 degrees and 90 degrees.</p>
申请公布号 EP1847408(B1) 申请公布日期 2010.05.12
申请号 EP20070251589 申请日期 2007.04.13
申请人 BRIDGESTONE CORPORATION 发明人 ITAMI, DAISUKE
分类号 B60C9/22;B60C9/26;B60C19/00 主分类号 B60C9/22
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