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    • 16. 发明公开
    • ARMATURE DE SOMMET DE PNEUMATIQUE POUR AVION
    • EP3131761A1
    • 2017-02-22
    • EP15716070.6
    • 2015-04-17
    • Compagnie Générale des Etablissements MichelinMichelin Recherche et Technique S.A.
    • ESTENNE, VincentJOULIN, Emmanuel
    • B60C9/26B60C9/20
    • B60C9/263B60C9/0007B60C9/0042B60C9/1807B60C9/2009B60C9/28B60C2009/0021B60C2009/2032B60C2200/02
    • The invention relates to a tyre (1) for an airplane, which includes a tread (3), a working reinforcement (2) including at least one working bilayer (21) which has the largest axial width (L
      T ) and includes two axial ends (E), a carcass reinforcement (4) including at least one carcass layer (41), and a binding reinforcement (7) including at least one binding layer (71), which is radially inside the working bilayer (21) and has an axial width (L
      F ) which is at least 0.8 times the axial width (L
      T ). The distance D between an axial end (E) of the working bilayer (21) and the orthogonal projection (I) thereof onto the radially outermost carcass layer (41) is at least 7 mm and the distance D' between the point (F) of the working bilayer (21), located axially inside the axial end (E) at a distance L of 25 mm, and the orthogonal projection (J) thereof onto the carcass layer (41) at least 4 mm and no greater than the distance D.
    • 本发明涉及一种用于飞机的轮胎(1),其包括胎面(3),包括至少一个具有最大轴向宽度(LT)的工作双层(21)并包括两个轴向端部 (E),包括至少一个胎体层(41)的胎体增强件(4)以及包括至少一个结合层(71)的结合加强件(7),所述结合层位于所述工作双层(21)的径向内侧并且具有 轴向宽度(LF)至少为轴向宽度(LT)的0.8倍。 工作双层(21)的轴向端部(E)与其正交投影(I)之间在径向最外侧胎体层(41)上的距离D至少为7mm,点(F) (21)的轴向端部(E)以25mm的距离L定位,并且其正交投影(J)在所述胎体层(41)上至少4mm并且不大于所述距离L D.