• 专利标题: AIRCRAFT NACELLE INCLUDING A LINK BETWEEN A CONDUIT OF AN AIR INLET AND A CONDUIT OF AN ENGINE
  • 申请号: US15730954
    申请日: 2017-10-12
  • 公开(公告)号: US20180105281A1
    公开(公告)日: 2018-04-19
  • 发明人: Alain PORTEFrédéric VINCHES
  • 申请人: Airbus Operations SAS
  • 优先权: FR1659895 20161013; FR1659899 20161013
  • 主分类号: B64D33/02
  • IPC分类号: B64D33/02 B64C7/02
AIRCRAFT NACELLE INCLUDING A LINK BETWEEN A CONDUIT OF AN AIR INLET AND A CONDUIT OF AN ENGINE
摘要:
An aircraft nacelle including a conduit rigidly connected to an air inlet and a conduit rigidly connected to an engine, a link between the conduit rigidly connected to the air inlet and the conduit rigidly connected to the engine. The link includes a sleeve that receives one end of a first conduit and is rigidly connected to a second conduit, and linking elements that link the sleeve and the first conduit and that are distributed about the entire circumference of the nacelle, each linking element having a threaded stem oriented in a radial direction and being configured to enable tightening from inside the first conduit.
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