首页> 外国专利> Lower aft pylon fairing for engine mounting structure inserted between wing and turbojet engine of aircraft, has extension traversing inner cross stiffening rib and fixed on spar, where extension and bracket are formed as single piece

Lower aft pylon fairing for engine mounting structure inserted between wing and turbojet engine of aircraft, has extension traversing inner cross stiffening rib and fixed on spar, where extension and bracket are formed as single piece

机译:用于飞机的机翼和涡轮喷气发动机之间的发动机安装结构的下部后挂架整流罩,具有延伸的横穿内部横向加强肋并固定在翼梁上,其中延伸和支架形成为单件

摘要

The fairing (30) has an anchoring unit including an attachment (60) permitting withdrawal of efforts along a longitudinal direction, where the fairing is in the form of caisson. The attachment has a bracket (62) that is fixed and is plated against a face of an inner cross stiffening rib (46). The attachment has a triangular bracket extension (70) that extends along the longitudinal direction. The extension and the bracket are formed as a single piece. The extension traverses the inner cross stiffening rib, and is fixed on a closing spar (41).
机译:整流罩(30)具有包括附接件(60)的锚固单元,该附件允许沿纵向撤回作用,其中整流罩为沉箱形式。附件具有固定的支架(62),并被固定在内部横向加强肋(46)的表面上。该附件具有沿着纵向方向延伸的三角形支架延伸部(70)。延伸部和支架形成为一体。该延伸部横穿内部的横向加强肋,并固定在闭合的梁(41)上。

著录项

  • 公开/公告号FR2964947A1

    专利类型

  • 公开/公告日2012-03-23

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS;

    申请/专利号FR20100057614

  • 发明设计人 DUMONT JEAN FRANCOIS;FOYER LAURENT;

    申请日2010-09-22

  • 分类号B64D29/06;B64C7/02;

  • 国家 FR

  • 入库时间 2022-08-21 17:04:09

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