发明名称 REDUCED WEIGHT AIRCRAFT TIRE
摘要 <P>PROBLEM TO BE SOLVED: To provide a reduced weight aircraft tire compatible with a high speed and high load. <P>SOLUTION: A pneumatic tire having a carcass and a belt reinforcing structure is disclosed. The belt reinforcing structure is a composite belt structure, which includes a first belt layer 50 and a second belt layer 60 having a plurality of cords arranged at an angle of 5 degrees or less with respect to the centerplane of the tire, and at least one zigzag belt reinforcing structure 70 located radially outward of the first belt layer 50. The first belt layer 50 is wider than the zigzag belt reinforcing structure 70, and the second belt layer 60 is narrower than the zigzag belt reinforcing structure 70. <P>COPYRIGHT: (C)2012,JPO&INPIT
申请公布号 JP2012001206(A) 申请公布日期 2012.01.05
申请号 JP20110130298 申请日期 2011.06.10
申请人 GOODYEAR TIRE & RUBBER CO:THE 发明人 UEYOKO KIYOSHI
分类号 B60C9/18;B60C9/20;B60C9/22 主分类号 B60C9/18
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