发明名称 Pneumatic tire for airplane with reinforcing layer having two or more joint portions in the circumferential direction
摘要 In a pneumatic tire for an airplane of the present invention, a reinforcing layer, which is disposed at an outer side, in the radial direction of the tire, of a belt, includes plural cords, the cords being provided such that the longitudinal direction thereof forms an angle of substantially 15° or less with respect to a tire circumferential direction. The reinforcing layer has two or more joint portions in the circumferential direction of the tire. In accordance with the present invention, a length of the cords forming the reinforcing layer in the tire circumferential direction can be made short, whereby a size (length) of tread pieces formed at a time when the tire is damaged can be made small and damage caused to an airplane can be reduced.
申请公布号 US6843294(B2) 申请公布日期 2005.01.18
申请号 US20010948538 申请日期 2001.09.10
申请人 BRIDGESTONE CORPORATION 发明人 TOGO HIROYUKI
分类号 B60C9/18;B60C9/20;B60C9/22;B60C19/00;(IPC1-7):B60C9/18 主分类号 B60C9/18
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