发明名称 AIRCRAFT TIRE
摘要 In order to suppress an excessive increase in the temperature of a tread section, a tire includes: a first land portion that is formed at a tread section by providing a plurality of circumferential direction grooves extending around a tire circumferential direction at an interval in a tire width direction, and that includes a plurality of first recesses provided in the tire circumferential direction of a wall face of the first land portion; and a second land portion that is formed by the circumferential direction grooves provided at the tread section, that has a wider width than the first land portion, and that includes a greater number of second recesses than a number of the first recesses, the second recesses being provided in the tire circumferential direction of a wall face of the second land portion.
申请公布号 EP2990232(A4) 申请公布日期 2016.03.16
申请号 EP20140788818 申请日期 2014.04.15
申请人 BRIDGESTONE CORPORATION 发明人 SAKIYAMA, TOMOTAKA;OKITA, YOHEI
分类号 B60C11/04;B60C11/03;B60C11/13 主分类号 B60C11/04
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