Aircraft tire having an improved bead

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

Reexamination Certificate

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Details

C152S526000, C152S539000, C152S543000, C152S544000, C152S547000, C152S550000

Reexamination Certificate

active

06951234

ABSTRACT:
An aircraft tire, the inflation pressure of which is greater than 12 bar, comprises a crown, two sidewalls and two beads, a carcass reinforcement anchored in the two beads and a crown reinforcement. The carcass reinforcement comprises at least two circumferential alignments of first reinforcing threads of high elasticity modulus. The means for anchoring the first reinforcing threads within each bead comprises second reinforcing threads oriented circumferentially and axially bordering the circumferential alignments of the first reinforcing threads, the first reinforcing threads and second reinforcing threads being separated by a layer of mix of very high elasticity modulus.

REFERENCES:
patent: 2002/0170647 (2002-11-01), Pereira et al.
patent: 2003/0062107 (2003-04-01), Leblond et al.
patent: 0242840 (1987-10-01), None
patent: 0329592 (1989-08-01), None
patent: 0582196 (1994-02-01), None
patent: 0664232 (1995-07-01), None
patent: 0718090 (1996-06-01), None
patent: 0822047 (1998-02-01), None
patent: 2771050 (1999-05-01), None
patent: 9747463 (1997-12-01), None
patent: 9854006 (1998-12-01), None
patent: 0136219 (2001-05-01), None
First two pages of parent PCT/EP01/07223 published as WO 02/00456 A2 and preliminary examination report for parent PCT/EP01/07223.

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