Invention Grant
- Patent Title: Jet engine nacelle having dampers for half-shells
- Patent Title (中): 喷气发动机机舱具有半壳的阻尼器
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Application No.: US12673933Application Date: 2008-07-25
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Publication No.: US08800299B2Publication Date: 2014-08-12
- Inventor: Fabrice Provost
- Applicant: Fabrice Provost
- Applicant Address: FR Gonfreville l'Orcher
- Assignee: Aircelle
- Current Assignee: Aircelle
- Current Assignee Address: FR Gonfreville l'Orcher
- Agency: Brinks Gilson & Lione
- Priority: FR0705939 20070820
- International Application: PCT/EP2008/059760 WO 20080725
- International Announcement: WO2009/024428 WO 20090226
- Main IPC: F02C7/20
- IPC: F02C7/20 ; B64D27/00

Abstract:
A jet engine nacelle includes an air intake section, a middle section, and an aft section. The aft section is formed from two half-shells rotatably mounted such that they can each be deployed between a working position and a maintenance position under the action of a jack and a telescopic connecting rod each respectively having a first end fastened on the jet engine and a second end fastened in the corresponding half-shell. In particular, the nacelle includes at least one damping member arranged between each telescopic connecting rod and the corresponding half-shell, and the damping member is designed so as to be in a prestressed state when the corresponding half-shell is in the working position and can reduce vibration in the half-shell.
Public/Granted literature
- US20110173949A1 JET ENGINE NACELLE HAVING DAMPERS FOR HALF-SHELLS Public/Granted day:2011-07-21
Information query
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