Invention Grant
US08579078B2 Acoustic panel for a turbojet engine nacelle, with in-built fasteners
失效
用于涡轮喷气发动机机舱的隔音板，内置紧固件
- Patent Title: Acoustic panel for a turbojet engine nacelle, with in-built fasteners
- Patent Title (中): 用于涡轮喷气发动机机舱的隔音板，内置紧固件
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Application No.: US13749215Application Date: 2013-01-24
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Publication No.: US08579078B2Publication Date: 2013-11-12
- Inventor: Herve Hurlin , Nicolas Dezeustre , Wouter Balk , Bertrand Desjoyeaux
- Applicant: Aircelle
- Applicant Address: FR Gonfreville l'Orcher
- Assignee: Aircelle
- Current Assignee: Aircelle
- Current Assignee Address: FR Gonfreville l'Orcher
- Agency: Brinks Hofer Gilson & Lione
- Priority: FR1056136 20100727
- Main IPC: E04B1/82
- IPC: E04B1/82
Abstract:
An acoustic panel is provided that includes at least one cellular core arranged between at least an internal skin and an external skin, wherein the external skin incorporates at least one fastener able to collaborate in a disconnectable fashion with a complementary fastener associated with a structure to which it is to be attached.
Public/Granted literature
- US20130133977A1 ACOUSTIC PANEL FOR A TURBOJET ENGINE NACELLE, WITH IN-BUILT FASTENERS Public/Granted day:2013-05-30
Information query
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