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METHOD FOR MANUFACTURING A STIFFENER IN COMPOSITE MATERIAL WITH AN OMEGA SECTION

机译:在带有欧姆部分的复合材料中制造硬挺剂的方法

摘要

The object of the invention is a method of manufacturing a stiffener composite material comprising a central portion with on both sides of the wings such that when the wings are in abutment against an element to strengthen said central portion is removed said element to be reinforced, said method consisting of producing a flat strip (16) comprising at least one layer of fibers, to arrange it on a mold (26) comprising at least one recessed shape corresponding to the central part of the stiffener to be produced , heating said strip (16) and deforming it so as to make it conform to the shapes of said mold (26), characterized in that it consists in exerting transverse traction on the strip (16) during the deformation of said bandaged.
机译:本发明的目的是一种制造加劲肋复合材料的方法,该复合材料包括在翼的两侧具有中心部分的中央部分,使得当翼与用于增强所述中心部分的元件邻接时,将所述待增强的元件去除。该方法包括以下步骤:制造包括至少一层纤维的扁平条带(16),将其布置在模具(26)上,该模具包括至少一个与待制造的加强件的中央部分相对应的凹入形状,加热所述条带(16) )并使其变形以使其符合所述模具(26)的形状,其特征在于,它在于在所述绷带的变形过程中在条带(16)上施加横向牵引力。

著录项

  • 公开/公告号FR2960470A1

    专利类型

  • 公开/公告日2011-12-02

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS;

    申请/专利号FR20100054218

  • 发明设计人 DENIS DE MATTIA;

    申请日2010-05-31

  • 分类号B29C70/42;B29C70/54;B64C1/06;

  • 国家 FR

  • 入库时间 2022-08-21 17:04:12

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