Invention Grant
- Patent Title: Removable acoustic panels for turbojet engine casing
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Application No.: US14648745Application Date: 2013-12-12
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Publication No.: US09932897B2Publication Date: 2018-04-03
- Inventor: Georges Jean Xavier Riou , Norman Bruno Andre Jodet , Jacky Novi Mardjono
- Applicant: SNECMA
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1262150 20121217
- International Application: PCT/FR2013/053053 WO 20131212
- International Announcement: WO2014/096634 WO 20140626
- Main IPC: F01D25/04
- IPC: F01D25/04 ; F02C7/045 ; F01D25/24 ; F02K1/82 ; B64D33/02

Abstract:
An acoustic panel intended to be fixed internally to a fan casing of a turbojet engine, including an exterior face and an interior face which are curved about an axis, and two axially opposed transverse faces, the exterior curved face having at least one first recess on the side of a first transverse face and at least one second recess on the side of the opposite transverse face, said recesses each an attachment, in which said recesses do not open onto the interior curved face of the panel. Also covered are the turbojet engine including these panels and the method of mounting them.
Public/Granted literature
- US20150292407A1 REMOVABLE ACOUSTIC PANELS FOR TURBOJET ENGINE CASING Public/Granted day:2015-10-15
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