Invention Grant
- Patent Title: Turbomachine stator
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Application No.: US17278903Application Date: 2019-09-06
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Publication No.: US11408292B2Publication Date: 2022-08-09
- Inventor: Hugo Louis Rousseaux , Pamela Jessica Benevent , Léna Jeffroy
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Bookoff McAndrews, PLLC.
- Priority: FR1858804 20180926
- International Application: PCT/FR2019/052057 WO 20190906
- International Announcement: WO2020/065161 WO 20200402
- Main IPC: F01D9/02
- IPC: F01D9/02 ; F01D11/00

Abstract:
Turbine nozzle for a turbomachine extending about an axis, the nozzle including a plurality of sectors each having at least one vane which extends radially between an internal platform and an external platform, the nozzle including at least two sealing strips each including a main portion configured to ensure the sealing between the nozzle and an element of the turbomachine which is adjacent to the nozzle, and a first portion folded relative to the main portion, the first folded portion being in contact with an outer face of at least one platform, each strip being held to the at least one platform by a clamping device configured to clamp the first folded portion between the outer face of the platform and the clamping device.
Information query