发明授权
US07818958B2 Jet engine nacelle for an aircraft and aircraft comprising such a nacelle
有权
用于包括这种机舱的飞机和飞机的喷气发动机机舱
- 专利标题: Jet engine nacelle for an aircraft and aircraft comprising such a nacelle
- 专利标题(中): 用于包括这种机舱的飞机和飞机的喷气发动机机舱
-
申请号: US12443343申请日: 2007-09-28
-
公开(公告)号: US07818958B2公开(公告)日: 2010-10-26
- 发明人: Guillaume Bulin , Patrick Oberle , Thierry Surply
- 申请人: Guillaume Bulin , Patrick Oberle , Thierry Surply
- 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
- 代理机构: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- 优先权: FR0608547 20060929
- 国际申请: PCT/FR2007/001595 WO 20070928
- 国际公布: WO2008/040869 WO 20080410
- 主分类号: F02K3/04
- IPC分类号: F02K3/04
摘要:
A nacelle for an aircraft high-bypass jet engine, in which a jet engine having a longitudinal axis is mounted, the nacelle including a wall concentrically and at least partially surrounding the jet engine and defining with the latter an annular duct for fluid inner flow, including at the downstream end of the nacelle wall a passage section of a flow outlet. The nacelle includes a displacement mechanism displacing on request a portion of the nacelle wall to modify the passage section of the flow outlet through which a major portion of the flow escapes, the displacement forming in the nacelle wall at least one opening through which a small portion of a leak flow, naturally escapes. The nacelle further includes a fluid device that uses a fluid for compelling the leak flow to flow along the outer face of the portion of the nacelle wall located downstream relative to the at least one opening.
公开/授权文献
信息查询