发明名称 PNEUMATIC RADIAL TIRE FOR AIRCRAFT
摘要 PROBLEM TO BE SOLVED: To provide a pneumatic radial tire for an aircraft capable of improving durability of a belt part by effectively restraining the propagation of a standing wave phenomenon to a shoulder part. SOLUTION: Strip materials S are constituted so as to be folded back while drawing a circular arc of the radius of a curvature R by both side belt ends x, x, the strip materials S are made to be accumulated in three to seven layers on both end parts of a belt body by setting the ratio R/BW of the radius of the curvature R and the width BW of the belt body as 2.0 to 3.0, and the relation of a distance SA of the end part of a belt layer 6 and the end part of a belt layer 7 and a strip material width SW 0<SA/SW<1.0 on the pneumatic radial tire for the aircraft constituted of the belt layer 6 made of two layers of strip material layers wound around the outside of a carcass layer by folding back the strip materials S at the both side belt ends x, x while inclining them relative to the tire peripheral direction T and the belt layer 7 formed by winding the strip material S in the tire peripheral direction so as to cover the belt layer 6.
申请公布号 JP2002211208(A) 申请公布日期 2002.07.31
申请号 JP20010055090 申请日期 2001.02.28
申请人 YOKOHAMA RUBBER CO LTD:THE 发明人 UNOKI TAKASHI;HAMAZAKI SUKEO
分类号 B60C9/20;B60C9/18;B60C9/26;B60C11/00;(IPC1-7):B60C9/20 主分类号 B60C9/20
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