Aircraft tire with composite cables

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

Reexamination Certificate

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Details

C152S451000, C152S533000, C152S536000, C152S556000, C152S557000

Reexamination Certificate

active

07905265

ABSTRACT:
An aircraft tire inflated to high pressure and including a tread and a crown reinforcement in the form of composite textile cables which form at least one twin ply of two layers of crossed elements obtained by winding, in a zigzag around a cylindrical support and from one edge of the crown reinforcement to the other, a strip of at least one reinforcement until the two layers of crossed elements form angles of opposing directions of between 8° and 30° with the circumferential direction.

REFERENCES:
patent: 4155394 (1979-05-01), Shepherd et al.
patent: 4244414 (1981-01-01), Uemura et al.
patent: 4865098 (1989-09-01), Majerus
patent: 4893665 (1990-01-01), Reuter et al.
patent: 4914902 (1990-04-01), Keefe, Jr.
patent: 5285835 (1994-02-01), Ueyoko et al.
patent: 5427167 (1995-06-01), Watanabe et al.
patent: 5476129 (1995-12-01), Shoyama
patent: 5522443 (1996-06-01), Ueyoko et al.
patent: 6273163 (2001-08-01), Materne et al.
patent: 6601626 (2003-08-01), Royer et al.
patent: 0 335 588 (1989-10-01), None

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