Invention Grant
- Patent Title: Turbomachine stator element
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Application No.: US17055054Application Date: 2019-05-13
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Publication No.: US11236627B2Publication Date: 2022-02-01
- Inventor: Alexis Maxime Germain , Jean-Marc Claude Perrollaz , Pierre Grégoire Anton
- 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: FR1854134 20180517
- International Application: PCT/FR2019/051068 WO 20190513
- International Announcement: WO2019/220042 WO 20191121
- Main IPC: F01D9/04
- IPC: F01D9/04 ; F01D11/00

Abstract:
A turbomachine stator element extends around a longitudinal axis and includes a first stator vane and a second stator vane circumferentially adjacent to the first stator vane. Each of the first and second stator vanes include a platform and a blade extending radially from the platform. The stator element also comprising at least one inter-platform seal, arranged between the platform of the first stator vane and the platform of the second stator vane. The inter-platform seal has a flat support provided with an upper surface on which there extends a fin.
Public/Granted literature
- US20210215055A1 TURBOMACHINE STATOR ELEMENT Public/Granted day:2021-07-15
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