发明名称 Pneumatic tire for airplanes
摘要 A pneumatic tire for airplanes which can reduce a ratio of the load subjected to a tread center zone of the tire to the load subjected to two shoulder zones thereof and improve a high speed durability of the tire without sacrificing a wear resistance thereof is disclosed. The tire comprises a pair of circumferentially extending grooves each arranged at a shoulder portion of the tire and substantially symmetrically and equally spaced apart from a crown center of the tire. A distance between the circumferentially extending grooves is from 50% to 95%, preferably 55% to 80% of a tread width and serves to divide a tread portion of the tire into a center zone and two shoulder zones. The outer surfaces of the shoulder zones are protruded from the circumferentially extending grooves toward the outside thereof by a step having a level difference from 0.5 mm to 6 mm.
申请公布号 US4044810(A) 申请公布日期 1977.08.30
申请号 US19750618860 申请日期 1975.10.02
申请人 BRIDGESTONE TIRE COMPANY LIMITED 发明人 TANIGUCHI, MOTOAKI;IWATA, TOYOMI
分类号 B60C11/04;B29D30/00;B60C3/00;B60C9/06;B60C11/00;B60C11/01;B60C19/00;(IPC1-7):B60C11/06 主分类号 B60C11/04
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