发明名称 CROWN FOR AEROPLANE TYRE
摘要 <p>Aeroplane tyre comprising a tread (1), a crown reinforcement (2) comprising at least one radially interior layer (21) having an axial width (L2) at least equal to two thirds of the maximum axial width (L1) of the tyre, and a carcass reinforcement (3) comprising at least one radially exterior layer (31), each of said layers comprising a concave portion, the axial limits (M2, M'2, M3, M'3) of which are the radially exterior points of the respective layer. The radial distance (d) between the aforementioned concave portions is at a maximum at the equatorial plane (XZ), and decreases continually up to the axial limits (M2, M'2), where the value is at a minimum (dM), said axial limits being axially closest to the equatorial plane.</p>
申请公布号 WO2013079351(A1) 申请公布日期 2013.06.06
申请号 WO2012EP73033 申请日期 2012.11.20
申请人 COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN;MICHELIN RECHERCHE ET TECHNIQUE S.A.;ESTENNE, VINCENT;CAFFEAU, CHARLOTTE 发明人 ESTENNE, VINCENT;CAFFEAU, CHARLOTTE
分类号 B60C9/28;B60C19/00 主分类号 B60C9/28
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