发明名称 SOMMET POUR PNEUMATIQUE D'AVION
摘要 <p>A tire for an aeroplane and, in particular, to the crown of a tire for an aeroplane, having reduced dimensions and mass of the pieces of tread in the event of accidental tire tread separation, without the use of additional devices external to the tire and therefore without penalizing the payload of the aeroplane, including a tread intended to come into contact with the ground via a tread surface and comprised radially between a bottom surface and the tread surface, the tread comprising at least two circumferential ribs adjacent to at least one circumferential groove, each circumferential rib extending radially between the bottom surface and the tread surface and axially between two edge corners in the tread surface, and a crown reinforcement radially on the inside of the bottom surface, wherein a tread separation layer is arranged radially on the inside of at least one circumferential rib between the bottom surface and the crown reinforcement, axially between the two edge corners of the said circumferential rib, in the tread surface, and circumferentially over at least part of the circumference of the tire, and the radial distance (d1) between the tread separation layer and the bottom surface is at most equal to 1 mm.</p>
申请公布号 FR2984231(B1) 申请公布日期 2014.05.16
申请号 FR20110062025 申请日期 2011.12.20
申请人 SOCIETE DE TECHNOLOGIE MICHELIN;MICHELIN RECHERCHE ET TECHNIQUE S.A. 发明人 CHAMBRIARD FRANCOIS;ROCHE GILLES
分类号 B60C11/03 主分类号 B60C11/03
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