Invention Grant
- Patent Title: Sealing assembly for a turbine engine
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Application No.: US17995818Application Date: 2021-04-01
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Publication No.: US12031444B2Publication Date: 2024-07-09
- Inventor: Teddy Frederic Gilbert Chantrait , Antoine Robert Alain Brunet , Mael Thevenot , Gilles Jean-Luc Dessein , Jean-Yves Fernand Paris , Vincent Gilbert Alex Wagner
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: WOMBLE BOND DICKINSON (US) LLP
- Priority: FR 03636 2020.04.10
- International Application: PCT/FR2021/050577 2021.04.01
- International Announcement: WO2021/205099A 2021.10.14
- Date entered country: 2022-10-07
- Main IPC: F01D11/12
- IPC: F01D11/12

Abstract:
A sealing assembly (1) for a turbine engine comprising a first element (2) and a second element (3), the first and second elements (2, 3) being concentric and in relative rotational movement with respect to each other about an axis of rotation (X), the sealing assembly (1) comprising at least one first wiper (4a) and an abradable member (5), the first wiper (4a) being annular in shape and carried by the first element (2), the first wiper (4a) extending radially towards the abradable member (5) and continuously around the axis of rotation (X), the abradable member (5) being annular in shape and carried by the second element (3), the abradable member (5) extending tangentially opposite the first wiper (4a), the first wiper (4a) comprising primary angular portions (11), each extending tangentially along a primary angular sector (11′), the primary angular portions (11) each having, in cross-section, a first constant profile, characterised in that the first wiper (4a) comprises secondary angular portions (13) each extending tangentially along a secondary angular sector (13′), the secondary angular portions (13) each having, in cross-section, a second profile different from the first profile, the number of secondary angular portions (13) being equal to the number of primary angular portions (11), the secondary angular portions (13) being interposed between the primary angular portions (11).
Public/Granted literature
- US20230118871A1 SEALING ASSEMBLY FOR A TURBINE ENGINE Public/Granted day:2023-04-20
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