Invention Grant
- Patent Title: Method of manufacturing a leading edge shield
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Application No.: US15512140Application Date: 2015-09-18
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Publication No.: US10576578B2Publication Date: 2020-03-03
- Inventor: Gilles Charles Casimir Klein , Jean-Michel Patrick Maurice Franchet , Dominique Michel Serge Magnaudeix
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1458855 20140919
- International Application: PCT/FR2015/052507 WO 20150918
- International Announcement: WO2016/042275 WO 20160324
- Main IPC: B23K20/02
- IPC: B23K20/02 ; F04D29/32 ; F01D5/28 ; F04D29/02 ; B23P15/04 ; F01D5/14 ; B23K101/00 ; B21D53/78

Abstract:
A field of rotary blades, and more particularly to a method of fabricating a leading edge shield for protecting such a blade. The method includes at least steps of performing initial plastic deformation on at least one sheet from a pressure side sheet and a suction side sheet, using additive fabrication to add a reinforcement with a fiber insert on at least one of the pressure and suction side sheets, closing the pressure and suction side sheets around a core after the initial plastic deformation and after adding the reinforcement, performing subsequent plastic deformation by pressing the pressure and suction side sheets against an outside surface of the core after the sheets have been closed around the core, and extracting the core.
Public/Granted literature
- US20170274470A1 METHOD OF MANUFACTURING A LEADING EDGE SHIELD Public/Granted day:2017-09-28
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