发明名称 RADIAL TIRE FOR AIRPLANE
摘要 PURPOSE:To relax the compressive stress of a crown shoulder section in the cross-sectional direction by forming a stress relaxing groove between the respective ground contact ends under the normal operating load in a crown section and under the larger load than the normal operating load just by a specific rate. CONSTITUTION:At least two circumferential belt layers in are arranged the crown section of a tire 10 and the maximum width of these belt layers is set to the width of approximately 100-140% of the ground width under the normal operating conditions of the crown section. For example, the tire is provided with a carcass layer 11 made of cords arranged at a right angle with the circumferential direction and the belt structure 12 containing a number of circumferential belt layers made of cords arranged almost inparallel to the circumferential direction and a number of circumferential grooves 13 are formed on the ground contact surface of the crown section. In this case, a stress relaxing groove 16 stretching in the circumferential direction is formed between a ground contact end 14 under the normal operating load of the crown section and a ground contact end 15 under the load of approximately 150% of the normal operating load.
申请公布号 JPS61241203(A) 申请公布日期 1986.10.27
申请号 JP19850080268 申请日期 1985.04.17
申请人 BRIDGESTONE CORP 发明人 TANIGUCHI MOTOAKI;TAKAHASHI MASANOBU;YAMADA SHIGEKI;KATO KENSHIRO;ENDO KAZUYUKI
分类号 B60C9/18;B60C9/08;B60C11/01;B60C11/04 主分类号 B60C9/18
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