Invention Grant
US08800299B2 Jet engine nacelle having dampers for half-shells 有权
喷气发动机机舱具有半壳的阻尼器

  • 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
  • Application No.: US12673933
    Application Date: 2008-07-25
  • Publication No.: US08800299B2
    Publication 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
Jet engine nacelle having dampers for half-shells
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.
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