发明名称 CROWN REINFORCEMENT FOR AIRCRAFT TYRE
摘要 Working layer (5) comprises a circumferential zigzag winding of a strip (6) on a cylindrical surface having as its axis the axis of rotation of the tire (1), with a periodic curve (7), the peak-to-peak amplitude of which defines the axial width L of the working layer (5) between a first and a second axial end (I, I′). The working layer (5) is made up, in any meridian plane (YZ) containing the axis of rotation of the tire (1), of an arrangement of portions of strip (6) extending axially from the first axial end (I) to the second axial end (I′) of the working layer (5), such that two consecutive portions of strip (6) overlap, at least in part, over a width of overlap e. The width of overlap e between two consecutive portions of strip (6) is constant over the entire axial width L of the working layer (5).
申请公布号 EP3063020(A1) 申请公布日期 2016.09.07
申请号 EP20140796003 申请日期 2014.10.29
申请人 COMPAGNIE GÉNÉRALE DES ETABLISSEMENTS MICHELIN;MICHELIN RECHERCHE ET TECHNIQUE S.A. 发明人 ROMERO DE LA OSA, MARC;DELACROIX, SERGE
分类号 B60C9/26;B60C9/28 主分类号 B60C9/26
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