- Patent Title: Method of fabricating a turbine or compressor guide vane sector made of composite material for a turbine engine, and a turbine or a compressor incorporating such guide vane sectors
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Application No.: US14354239Application Date: 2012-10-23
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Publication No.: US09784113B2Publication Date: 2017-10-10
- Inventor: Eric Fremont , Antoine Beaujard , Romain Nunez
- Applicant: HERAKLES , SNECMA
- Applicant Address: FR Le Haillan FR Paris
- Assignee: HERAKLES,SNECMA
- Current Assignee: HERAKLES,SNECMA
- Current Assignee Address: FR Le Haillan FR Paris
- Agency: Workman Nydegger
- Priority: FR1159668 20111025
- International Application: PCT/FR2012/052422 WO 20121023
- International Announcement: WO2013/060977 WO 20130502
- Main IPC: F03B1/04
- IPC: F03B1/04 ; F01D9/04 ; F01D5/28 ; B23K1/00 ; B29D99/00 ; F01D25/24 ; F04D29/40 ; B29C70/22 ; B29C70/24 ; B29L31/08

Abstract:
Single-airfoil vanes each having an inner platform, an outer platform, and an airfoil are obtained by three-dimensionally weaving a fiber blank in a single piece, by shaping the fiber blank to obtain a single-piece fiber preform, and by densifying the preform with a matrix to obtain a vane of composite material forming a single piece with inner and outer platforms incorporated therein. A plurality of vanes is assembled together at an intermediate stage of densification to form a multi-airfoil composite material guide vane sector for a turbine nozzle or a compressor diffuser and the assembled-together vanes are bonded together.
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