首页> 外国专利> Sealing joint for use between rear secondary structure and aft pylon fairing of e.g. turbojet engine mounting structure of aircraft, has junction zone with section shrunk with respect to connection zone section to permit folding of joint

Sealing joint for use between rear secondary structure and aft pylon fairing of e.g. turbojet engine mounting structure of aircraft, has junction zone with section shrunk with respect to connection zone section to permit folding of joint

机译:后部二级结构和后塔整流罩之间使用的密封接头,例如飞机的涡轮喷气发动机安装结构,具有相对于连接区部分收缩的连接区,以允许接头折叠

摘要

The joint (60) has a lip (62) and a base (64) for establishing a sealed contact with corresponding a rear secondary structure and an aft pylon fairing of a mounting structure of an engine of an aircraft. The lip and the base have respective connection zones (68, 72) that are connected together by a junction zone (74) along a longitudinal direction (X) of the joint. The junction zone has a shrunk section (Sr) shrunk with respect to a section of each of the connection zones, along any plane orthogonal to the direction, to permit folding of the joint along the junction zone.
机译:接头(60)具有唇部(62)和基座(64),用于与飞机的发动机的安装结构的相应的后部二级结构和后塔整流罩建立密封接触。唇部和基部具有各自的连接区域(68、72),该连接区域通过接合区域(74)沿着接头的纵向(X)连接在一起。接合区域具有沿着每个正交于该方向的平面相对于每个连接区域的截面收缩的收缩部分(Sr),以允许接头沿着接合区域折叠。

著录项

  • 公开/公告号FR2966803A1

    专利类型

  • 公开/公告日2012-05-04

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS;

    申请/专利号FR20100058951

  • 申请日2010-10-29

  • 分类号B64D29/06;F16J15/06;

  • 国家 FR

  • 入库时间 2022-08-21 17:04:08

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