发明申请
- 专利标题： BYPASS TURBOJET ENGINE NACELLE
- 专利标题（中）： 旁路涡轮发动机NACELLE
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申请号： US12445421申请日： 2007-10-05
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公开(公告)号： US20100040466A1公开(公告)日： 2010-02-18
- 发明人: Guy Bernard Vauchel , Jerome Collier , Patrice Dhainault , Francois Conte , Nicolas Hillereau , Pierre-Alain Chouard , Guillaume Lefort
- 申请人： Guy Bernard Vauchel , Jerome Collier , Patrice Dhainault , Francois Conte , Nicolas Hillereau , Pierre-Alain Chouard , Guillaume Lefort
- 申请人地址： FR GONFREVILLE L'ORCHER
- 专利权人： AIRCELLE
- 当前专利权人： AIRCELLE
- 当前专利权人地址： FR GONFREVILLE L'ORCHER
- 优先权： FR06/08892 20061011; FR07/01899 20070316
- 国际申请： PCT/FR07/01633 WO 20071005
- 主分类号： F01D25/28
- IPC分类号： F01D25/28 ; F16M13/00 ; F02K3/02
摘要：
The nacelle (1) comprises an air intake (5) upstream of the turbojet engine (2), a middle section (6) an internal casing (6a) of which is intended to surround a fan (3) of the turbojet engine (2), and a downstream section (7) comprising an external structure (7a)which is rigidly connected to a downstream part of the casing (6a) of the fan (3) so as to support the turbojet engine (2) and has means of attachment to a strut (12) intended to be connected to a fixed structure (13) of an aeroplane.
公开/授权文献
- US08523516B2 Bypass turbojet engine nacelle 公开/授权日：2013-09-03
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