Sidewall and bead reinforcing structure for a pneumatic aircraft

Resilient tires and wheels – Tires – resilient – Pneumatic tire or inner tube

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Details

152546, 152554, 152555, B60C 300, B60C 1506

Patent

active

047903643

ABSTRACT:
A tire structure that is especially advantageous for an aircraft tire has a pair of annular elastomeric members (40,41) disposed axially inwardly of the carcass plies (13,14) to maintain the carcass plies in a desired configuration. A preferred arrangement of bead reinforcing strips (32,33,34,35) is disclosed for use in tires that are intended for mounting on H-type aircraft rims.

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