Invention Grant
- Patent Title: Bypass turbojet engine nacelle
- Patent Title (中): 旁路涡轮喷气发动机舱
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Application No.: US12445421Application Date: 2007-10-05
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Publication No.: US08523516B2Publication Date: 2013-09-03
- Inventor: Guy Bernard Vauchel , Jerome Collier , Patrice Dhainault , Francois Conte , Nicolas Hillereau , Pierre-Alain Chouard , Guillaume Lefort
- Applicant: Guy Bernard Vauchel , Jerome Collier , Patrice Dhainault , Francois Conte , Nicolas Hillereau , Pierre-Alain Chouard , Guillaume Lefort
- Applicant Address: FR Gonfreville L'Orcher
- Assignee: Aircelle
- Current Assignee: Aircelle
- Current Assignee Address: FR Gonfreville L'Orcher
- Agency: Brinks Hofer Gilson & Lione
- Priority: FR0608892 20061011; FR0701899 20070316
- International Application: PCT/FR2007/001633 WO 20071005
- International Announcement: WO2008/043903 WO 20080417
- Main IPC: F03B11/08
- IPC: F03B11/08 ; F03B1/00 ; F01D5/00 ; F01D25/28 ; F04D29/44
Abstract:
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.
Public/Granted literature
- US20100040466A1 BYPASS TURBOJET ENGINE NACELLE Public/Granted day:2010-02-18
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