Invention Grant
- Patent Title: Turbine ring assembly mounted on a cross-member
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Application No.: US17604904Application Date: 2020-04-03
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Publication No.: US12158079B2Publication Date: 2024-12-03
- Inventor: Lucien Henri Jacques Quennehen , Antoine Claude Michel Etienne Danis , Clément Jean Pierre Duffau , Clément Jarrossay , Nicolas Paul Tableau
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Pillsbury Winthrop Shaw Pittman LLP
- Priority: FR1904663 20190503
- International Application: PCT/EP2020/059592 WO 20200403
- International Announcement: WO2020/224891 WO 20201112
- Main IPC: F01D25/28
- IPC: F01D25/28 ; F01D25/12 ; F01D25/24

Abstract:
A turbine ring assembly extending about an axis, includes 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 lug and a downstream lug spaced axially from each other extend radially outwardly, the ring support structure including a spacer having a clamp against which the downstream lug of the ring sectors is held, a first upstream flange against which the upstream lug of the ring sectors is held, and upstream of the first upstream flange, a second upstream flange for absorbing forces against which the first upstream flange is held.
Public/Granted literature
- US20220195894A1 TURBINE RING ASSEMBLY MOUNTED ON A CROSS-MEMBER Public/Granted day:2022-06-23
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