发明名称 PNEUMATIC TIRE FOR AIRCRAFT
摘要 An object is to make it make it possible to, before a protecting layer is exposed, visually recognize that a final stage of wear of a tread has been reached.;A pneumatic tire (10) for an aircraft has: a carcass ply (12) that spans between a pair of bead portions; a belt layer (14) that is provided at a tire radial direction outer side of a crown portion (12A) of the carcass ply (12); a protecting layer (16) that is provided at a tire radial direction outer side of the belt layer (14); a tread (18) that is provided at a tire radial direction outer side of the protecting layer (16), and at which ribs (30, 32, 34) are demarcated and formed by circumferential direction grooves; and filaments (20) that are provided between the protecting layer (16) and the tread (18), or within the tread (18), that extend in a tire axial direction, and that are disposed with an interval therebetween in a tire circumferential direction.
申请公布号 US2016068026(A1) 申请公布日期 2016.03.10
申请号 US201414784581 申请日期 2014.04.14
申请人 BRIDGESTONE CORPORATION 发明人 OKITA Yohei
分类号 B60C11/24 主分类号 B60C11/24
代理机构 代理人
主权项 1. A pneumatic tire for an aircraft, comprising: a carcass ply that spans between a pair of bead portions; a belt layer that is provided at a tire radial direction outer side of a crown portion of the carcass ply; a protecting layer that is provided at a tire radial direction outer side of the belt layer; a tread that is provided at a tire radial direction outer side of the protecting layer, and at which ribs are demarcated and formed by circumferential direction grooves; and filaments that are provided between the protecting layer and the tread, or within the tread, that extend in a tire axial direction, and that are disposed with an interval therebetween in a tire circumferential direction.
地址 Tokyo JP