发明申请
US20060060697A1 Device for assembly of a shroud placed between an aircraft engine air intake and a pylon 有权
用于组装放置在飞机发动机进气口和塔架之间的护罩的装置

  • 专利标题: Device for assembly of a shroud placed between an aircraft engine air intake and a pylon
  • 专利标题(中): 用于组装放置在飞机发动机进气口和塔架之间的护罩的装置
  • 申请号: US10954192
    申请日: 2004-10-01
  • 公开(公告)号: US20060060697A1
    公开(公告)日: 2006-03-23
  • 发明人: Jacques Beaufort
  • 申请人: Jacques Beaufort
  • 申请人地址: FR Toulouse
  • 专利权人: Airbus France
  • 当前专利权人: Airbus France
  • 当前专利权人地址: FR Toulouse
  • 优先权: FR0350715 20031022
  • 主分类号: B64D33/02
  • IPC分类号: B64D33/02
Device for assembly of a shroud placed between an aircraft engine air intake and a pylon
摘要:
The invention relates to a device (131) for assembly of a shroud (26) arranged between an air intake (22) and a pylon (2) fixed to the engine (4), the device comprising: stressed flexible means (130) provided with a first end (130a) and a second end (130b); first connection means connected to the air intake and to the end (130a); and second connection means connected to the shroud and to the end (130b). According to the invention, the second connection means comprise a primary assembly (140) fixed to the shroud and a secondary assembly (142) fixed to the second end (130b), and the primary and secondary assemblies (140,142) are connected to each other through a pivot connection (144).
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