发明名称 REDUCED WEIGHT AIRCRAFT TIRE
摘要 <P>PROBLEM TO BE SOLVED: To provide a lightweight and efficient tire structure, without causing a crack in a chafer of a bead, with excellent durability. <P>SOLUTION: This pneumatic tire 10 includes a carcass 22 and a belt reinforcing structure 40, and the carcass has at least two inside carcass plies 1-4. At least the two inside carcass plies are wound around an annular bead member toward the outside in the axial direction from the inside in the axial direction of the annular bead member 14, extend toward a crown outward the radial direction, and constitute respective turnup parts. At least one of the inside carcass plies is not wound around the annular bead member, and has end parts 1'-4' having a radial directional position in an area C determined by a first plane 28 and a second plane 29 and being inside in the radial direction more than the first plane and outside in the axial direction more than the second plane. <P>COPYRIGHT: (C)2012,JPO&INPIT
申请公布号 JP2012091778(A) 申请公布日期 2012.05.17
申请号 JP20110225493 申请日期 2011.10.13
申请人 GOODYEAR TIRE & RUBBER CO:THE 发明人 UEYOKO KIYOSHI;DAS BADAL
分类号 B60C9/02;B60C9/00;B60C9/08;B60C15/00 主分类号 B60C9/02
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