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Patent Searching and Data


Title:
RADIAL TIRE FOR AIRPLANE
Document Type and Number:
Japanese Patent JPH06156028
Kind Code:
A
Abstract:

PURPOSE: To prevent the occurrence of separation around a carcass up-ply end section and a drop in the durability of a carcass dot-ply section in the long-term use of a tire under a heavy load.

CONSTITUTION: The end of each up-ply 26 is dispersed and laid at both sides of a zone enclosed with the first perpendicular (m) orthogonal with the intermediate section of the up-ply 26 via an oppositional point 34 in a condition where internal pressure is fully applied and no load is acting, and the second perpendicular (n) orthogonal with the intermediate section of the up-ply 26 in a condition where internal pressure is fully applied and no load is acting, via such an oppositional point 36 as appearing in a case where internal pressure is fully applied and a load equal to 20% of a standard load is acting. Furthermore, the end of the up-ply 26 positioned at the radial outside of the zone is kept away from the internal end of a tire by a distance equal to 1.7 times or more of rim flange height H, and laid at the end of the tire inner than the third perpendicular P orthogonal with the intermediate section of the up-ply 26 via the maximum breadth position of the tire in a condition where internal pressure is fully applied and no load is acting.


Inventors:
SHOYAMA YOSHINOBU
Application Number:
JP31348492A
Publication Date:
June 03, 1994
Filing Date:
November 24, 1992
Export Citation:
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Assignee:
BRIDGESTONE CORP
International Classes:
B60C9/08; B60C15/00; B60C15/06; B64C25/36; (IPC1-7): B60C15/06; B60C9/08; B64C25/36
Attorney, Agent or Firm:
Atsushi Nakajima (2 outside)