- Patent Title: Metal structural reinforcement for a composite turbine engine blade
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Application No.: US14397730Application Date: 2013-04-25
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Publication No.: US09598966B2Publication Date: 2017-03-21
- Inventor: Gilles Charles Casimir Klein , Jean-Michel Patrick Maurice Franchet , Dominique Magnaudeix , Gilbert Michel Marin Leconte
- 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: FR1253977 20120430
- International Application: PCT/FR2013/050917 WO 20130425
- International Announcement: WO2013/164532 WO 20131107
- Main IPC: F01D5/28
- IPC: F01D5/28 ; F04D29/02 ; F04D29/32

Abstract:
In structural reinforcement for a composite blade of a turbine engine, the reinforcement being for adhesively bonding to a leading edge of the blade and presenting over its full height a section that is substantially V-shaped, having a base that is extended by two lateral flanks, there is provided an assembly of a plurality of fiber bundles that is mounted in at least one housing in the base, which assembly defines fiber content that varies along the full height of the housing.
Public/Granted literature
- US20150086378A1 METAL STRUCTURAL REINFORCEMENT FOR A COMPOSITE TURBINE ENGINE BLADE Public/Granted day:2015-03-26
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