Invention Grant
- Patent Title: Turbine stage for a turbine engine
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Application No.: US14394355Application Date: 2013-04-17
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Publication No.: US09957841B2Publication Date: 2018-05-01
- Inventor: Alain Dominique Gendraud , Alberto Martin-Matos , Vincent Millier , Sebastien Jean Laurent Prestel
- 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: FR1253644 20120420
- International Application: PCT/FR2013/050843 WO 20130417
- International Announcement: WO2013/156734 WO 20131024
- Main IPC: F01D25/24
- IPC: F01D25/24 ; F01D9/04 ; F01D11/00

Abstract:
A turbine stage for a turbine engine, the stage including a nozzle and a wheel mounted inside a sectorized ring carried by a casing. The nozzle is attached to the casing and is retained axially downstream by bearing against an annular split ring. Each ring sector includes at its upstream end a member of C-shaped section that is engaged on the casing rail and that holds the split ring radially. A radially inner wall of the C-shaped member of each ring sector extends inside the split ring over an entire axial dimension thereof and its upstream end portion is engaged in at least one recess of the nozzle.
Public/Granted literature
- US20150118035A1 TURBINE STAGE FOR A TURBINE ENGINE Public/Granted day:2015-04-30
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