首页> 外国专利> Aircraft assembly, has engine mounting structure with rigid structure forming shell with rear closing element, and rigid structure mounted on wing element so that wing element is supported against front longeron

Aircraft assembly, has engine mounting structure with rigid structure forming shell with rear closing element, and rigid structure mounted on wing element so that wing element is supported against front longeron

机译:飞机组件,具有发动机安装结构,该发动机安装结构具有形成带有后关闭元件的壳体的刚性结构,以及安装在机翼元件上的刚性结构,使得机翼元件被支撑在前纵梁上

摘要

The assembly has an engine mounting structure (4) below a wing element (2). The structure (4) has a rigid structure (6) forming a shell with a rear closing element (28). The element (2) with a front longeron (34) extends parallel to a leading edge (30) of the element (2). A rigid structure (6) is mounted on the element (2) so that the element (28) is supported against the longeron. The element (28) is in support against a support bracket (52).
机译:该组件在机翼元件(2)下方具有发动机安装结构(4)。结构(4)具有刚性结构(6),该刚性结构(6)形成具有后封闭元件(28)的壳体。具有前纵梁(34)的元件(2)平行于元件(2)的前缘(30)延伸。刚性结构(6)安装在元件(2)上,使得元件(28)支撑在纵梁上。元件(28)支撑在支撑托架(52)上。

著录项

  • 公开/公告号FR2891247A1

    专利类型

  • 公开/公告日2007-03-30

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE SOCIETE PAR ACTIONS SIMPLIFIEE;

    申请/专利号FR20050052870

  • 发明设计人 LAFONT LAURENT;

    申请日2005-09-26

  • 分类号B64D27/26;

  • 国家 FR

  • 入库时间 2022-08-21 20:26:55

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