- 专利标题: AIRCRAFT NACELLE INCLUDING A LINK BETWEEN A CONDUIT OF AN AIR INLET AND A CONDUIT OF AN ENGINE
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申请号: US15730954申请日: 2017-10-12
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公开(公告)号: US20180105281A1公开(公告)日: 2018-04-19
- 发明人: Alain PORTE , Frédéric 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
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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