Rubber/fabric wear strips for aircraft tires

B - Operations – Transporting – 60 – C

Patent

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Details

B60C 9/18 (2006.01) B60C 9/20 (2006.01)

Patent

CA 2264740

A pneumatic tire (10) for use in aircraft landing applications is provided. The tire includes a breaker assembly (20, 20A, 20B) having circumferentially extending layers of cord fabric and wear strips to enhance performance. In one embodiment, the wear strips are rubber and are provided as central portions (26, 44) of breaker layers (24, 40) with cord fabric extensions (30, 48) on either side. In a second embodiment, the wear strips are thin, narrow rubber strips (72) imposed between adjacent cord fabric breaker layers (56, 60, 64, 68). In a third embodiment, the wear strips are narrow cord fabric strips (92) imposed between adjacent cord fabric layers (80, 84, 88).

L'invention concerne un pneu (10) destiné à être utilisé dans des applications d'atterrissage pour avion. Le pneu comprend un ensemble nappe sommet (20, 20A, 20B) présentant des couches circonférentielles de bandelettes de tissu câblé et d'usure afin d'améliorer le rendement. Dans un mode de réalisation, les bandelettes d'usure sont en caoutchouc et se présentent sous la forme de parties centrales (26, 44) de couches de nappe sommet (24, 40) avec des prolongements en tissu câblé (30, 48) de chaque côté. Dans un second mode de réalisation, les bandelettes d'usure sont des bandelettes en caoutchouc minces et étroites (72) placées entre des couches de nappe sommet en tissu câblé adjacentes (56, 60, 64, 68). Dans un troisième mode de réalisation, les bandelettes d'usure sont des bandelettes en tissu câblé étroites (92) placées entre des couches adjacentes (80, 84, 88) de tissus câblé.

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