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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|