首页> 外国专利> Assembly part for assembling composite panels with each other, has plate stiffener comprising longitudinal sides secured with interior surface of wing and extended according to longitudinal direction from part over entire length of wing

Assembly part for assembling composite panels with each other, has plate stiffener comprising longitudinal sides secured with interior surface of wing and extended according to longitudinal direction from part over entire length of wing

机译:用于彼此组装复合面板的组装部件具有板加强件,该板加强件包括固定在机翼内表面上并沿纵向从机翼的整个长度上沿纵向延伸的纵向侧面

摘要

The part (200) has two wings (201, 202) connected with each other at respective longitudinal edges by a junction zone. Each wing comprises an external surface intended to prepare itself in front of one of two structural elements (103, 104) to be assembled, and an opposite interior surface (208). A rigid plate stiffener (203) comprises two opposite longitudinal sides (210, 211) that are secured with the interior surface of the wing. The stiffener is extended according to a longitudinal direction from the part over entire length of the wings.
机译:部件(200)具有两个翼(201、202),两个翼(201、202)在各个纵向边缘处通过接合区域彼此连接。每个机翼包括旨在在要组装的两个结构元件(103、104)之一的前面准备自身的外表面,以及相对的内表面(208)。刚性板加强件(203)包括两个相对的纵向侧面(210、211),其与机翼的内表面固定在一起。加强件沿纵向方向从该部分在翼的整个长度上延伸。

著录项

  • 公开/公告号FR2983264A1

    专利类型

  • 公开/公告日2013-05-31

    原文格式PDF

  • 申请/专利权人 MECANO I.D.;

    申请/专利号FR20110060922

  • 发明设计人 BONNES LIONEL;MESNIER DIDIER;

    申请日2011-11-29

  • 分类号F16B5;F16B11;

  • 国家 FR

  • 入库时间 2022-08-21 16:21:02

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