Invention Grant
- Patent Title: Turbomachine sealing ring
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Application No.: US17642019Application Date: 2020-09-11
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Publication No.: US11952901B2Publication Date: 2024-04-09
- Inventor: Etienne Gérard Joseph Canelle , Jacques Marcel Arthur Bunel , Bruno Giardini
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: CHRISTENSEN O'CONNOR JOHNSON KINDNESS PLLC
- Priority: FR 10134 2019.09.13
- International Application: PCT/FR2020/051570 2020.09.11
- International Announcement: WO2021/048505A 2021.03.18
- Date entered country: 2022-03-10
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F01D11/12

Abstract:
A turbomachine sealing ring has an axis of revolution and includes an annular support, an annular coating made of abradable material which is carried by the support, and an annular thermal protection plate which is carried by the support. The ring is divided into sectors and has a plurality of ring sectors disposed circumferentially next to one another about the axis. Each ring sector has a support sector, a coating sector, and a plate sector. Each plate sector ling includes a flat tab that is pressed against a face of the corresponding support sector and is fixed to this face by brazing. The tab is inserted into a through-slot in the support sector in order to improve its integrity in operation.
Public/Granted literature
- US20230175412A1 TURBOMACHINE SEALING RING Public/Granted day:2023-06-08
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