Invention Application
- Patent Title: TURBINE RING ASSEMBLY MADE FROM CERAMIC MATRIX COMPOSITE MATERIAL
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Application No.: US15558856Application Date: 2016-03-15
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Publication No.: US20180073398A1Publication Date: 2018-03-15
- Inventor: Lucien Henri Jacques QUENNEHEN , Gaël Frédéric Claude Cyrille EVAIN , David Mathieu Paul MARSAL , Thierry Guy Xavier TESSON
- Applicant: SAFRAN AIRCRAFT ENGINES , SAFRAN CERAMICS
- Priority: FR1552145 20150316
- International Application: PCT/FR2016/050567 WO 20160315
- Main IPC: F01D25/28
- IPC: F01D25/28 ; F01D11/12

Abstract:
A turbine ring assembly includes ring sectors made as a single piece of ceramic matrix composite material and being for mounting on a metal ring support structure, the ring support structure having two tabs extending radially towards a gas flow passage, each ring sector having a first portion forming an annular base with a radially inside face defining the inside face of the turbine ring and an outside face from which there extend two tab-forming portions, the ring sectors having a section that is substantially r shaped. The tabs of each ring sector fit axially over the tabs of the ring support structure with contact between the tabs of the ring support structure and the tabs of each ring sector when cold. The tabs of each ring sector are held to the ring support structure by pegs passing through holes formed in the tabs of each ring sector.
Public/Granted literature
- US10590803B2 Turbine ring assembly made from ceramic matrix composite material Public/Granted day:2020-03-17
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