Invention Grant
- Patent Title: Turbine engine part forming a compressor stator or a turbine nozzle, and method for fabricating same
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Application No.: US14127989Application Date: 2012-06-20
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Publication No.: US09708917B2Publication Date: 2017-07-18
- Inventor: Olivier Belmonte , Julien Foll
- Applicant: Olivier Belmonte , Julien Foll
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1155430 20110621
- International Application: PCT/FR2012/051387 WO 20120620
- International Announcement: WO2012/175867 WO 20121227
- Main IPC: F01D5/22
- IPC: F01D5/22 ; F01D5/28 ; F01D9/02 ; F04D29/54 ; F01D9/04 ; C04B35/563 ; C04B35/565 ; C04B35/571 ; C04B35/628 ; C04B35/80 ; B29C70/24 ; B29B11/16

Abstract:
A turbine engine part forming a compressor stator or a turbine nozzle and including an inner shroud, an outer shroud, and vanes extending substantially radially between the inner and outer shrouds and being secured thereto. The part is made of composite material and is obtained by densifying a fiber preform with a matrix. The fiber preform includes a set of yarns extending continuously along a path passing longitudinally along the preform portions of at least two consecutive vanes by passing through the inner shroud preform portion and the outer shroud preform portion, and the woven fiber reinforcement yarns extends continuously in the circumferential direction along an inner shroud segment and along an outer shroud segment between which the consecutive vanes extend.
Public/Granted literature
- US20140133989A1 TURBINE ENGINE PART FORMING A COMPRESSOR STATOR OR A TURBINE NOZZLE, AND METHOD FOR FABRICATING SAME Public/Granted day:2014-05-15
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