| 发明名称 |
REDUCED WEIGHT AIRCRAFT TIRE |
| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide an improved aircraft tire, capable of meeting high speed and high load, with reduced weight. <P>SOLUTION: A pneumatic tire has a carcass and a belt reinforcing structure. The belt reinforcing structure is a composite belt structure having at least one radially inner spiral layer and at least one zigzag belt reinforcing structure located radially outward of the spiral layer. The zigzag belt width is preferably wider than the spiral layer. <P>COPYRIGHT: (C)2012,JPO&INPIT |
| 申请公布号 |
JP2012041040(A) |
申请公布日期 |
2012.03.01 |
| 申请号 |
JP20110172588 |
申请日期 |
2011.08.08 |
| 申请人 |
GOODYEAR TIRE & RUBBER CO:THE |
发明人 |
UEYOKO KIYOSHI;BOEHLEFELD ROBERT JOHN |
| 分类号 |
B60C9/18;B60C9/00;B60C9/20 |
主分类号 |
B60C9/18 |
| 代理机构 |
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代理人 |
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| 地址 |
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