Invention Publication
- Patent Title: TURBINE RING ASSEMBLY MOUNTED ON A CROSS-MEMBER
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Application No.: US18555801Application Date: 2022-04-12
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Publication No.: US20240093619A1Publication Date: 2024-03-21
- Inventor: Jérôme Claude George LEMONNIER , Franck Davy BOISNAULT , Florian Armand Gabriel GAUDRY , Kévin Claude Luc BAUDY , Marion France CHAMBRE
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Priority: FR 2104149 2021.04.21
- International Application: PCT/FR2022/050688 2022.04.12
- Date entered country: 2023-10-17
- Main IPC: F01D25/24
- IPC: F01D25/24 ; F01D11/12

Abstract:
A turbine ring assembly extending around an axis, including a plurality of ring sectors made of ceramic matrix composite material forming a turbine ring and a ring support structure held by a turbine casing, each ring sector including a base from which an upstream tab and a downstream tab extend radially outward, spaced axially from one another, wherein the assembly also includes a cross-member mechanically connected to the ring support and including a first radial flange bearing against the upstream latching tabs of the ring sectors, and, for each ring sector, at least two transverse pins and a radial spring, each transverse pin passing through the upstream latching tab and the downstream latching tab of the ring sector and the ring support to hold the ring sector and the ring support secured to one another.
Public/Granted literature
- US12055061B2 Turbine ring assembly mounted on a cross-member Public/Granted day:2024-08-06
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