发明名称 AIRCRAFT TIRE
摘要 PROBLEM TO BE SOLVED: To increase durability of a tire by accelerating radiation of heat from a circumferential groove of a tread of the aircraft tire.SOLUTION: A plurality of circumferential grooves (a central-side circumferential groove 14 and an end-side circumferential groove 16) elongated in a circumferential direction of a tire are formed on a tread 12. In a cross-section in the circumferential direction of the tire, a groove bottom 18 of the at least one circumferential groove has a wave shape having an amplitude in the radial direction of the tire.
申请公布号 JP2014205423(A) 申请公布日期 2014.10.30
申请号 JP20130084210 申请日期 2013.04.12
申请人 BRIDGESTONE CORP 发明人 YANO TAKESHI
分类号 B60C11/04;B60C11/13 主分类号 B60C11/04
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