Invention Grant
- Patent Title: Nozzle for a turbomachine turbine
- Patent Title (中): 涡轮机涡轮喷嘴
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Application No.: US12922461Application Date: 2009-03-13
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Publication No.: US08662835B2Publication Date: 2014-03-04
- Inventor: Thierry Fachat , Patrick Joseph Marie Girard , Jean-Luc Soupizon
- Applicant: Thierry Fachat , Patrick Joseph Marie Girard , Jean-Luc Soupizon
- Applicant Address: FR Paris
- Assignee: SNECMA
- Current Assignee: SNECMA
- Current Assignee Address: FR Paris
- Agency: Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR0801502 20080319
- International Application: PCT/FR2009/000268 WO 20090313
- International Announcement: WO2009/118490 WO 20091001
- Main IPC: F04D29/08
- IPC: F04D29/08

Abstract:
A turbine nozzle for a turbomachine, including inner and outer annular platforms connected together by vanes, the inner platform carrying annular elements of abradable material co-operating with annular wipers of a rotor of the turbomachine to form a labyrinth seal, these elements of abradable material being carried by annular sheet-metal sectors of substantially L-, S-, or C-shaped section that are fastened by brazing or welding at their outer peripheries to the inner platform and at their inner peripheries to the elements of abradable material.
Public/Granted literature
- US20110127352A1 NOZZLE FOR A TURBOMACHINE TURBINE Public/Granted day:2011-06-02
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