Invention Grant
- Patent Title: CMC guide vane for a turbomachine turbine
-
Application No.: US17997628Application Date: 2021-04-28
-
Publication No.: US11965433B2Publication Date: 2024-04-23
- Inventor: Antoine Claude Michel Etienne Danis , Clément Jarrossay , Lucien Henri Jacques Quennehen , Nicolas Paul Tableau , Matthieu Arnaud Gimat
- Applicant: SAFRAN AIRCRAFT ENGINES , SAFRAN CERAMICS
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES,SAFRAN CERAMICS
- Current Assignee: SAFRAN AIRCRAFT ENGINES,SAFRAN CERAMICS
- Current Assignee Address: FR Paris; FR Le Haillan
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR 04494 2020.05.06
- International Application: PCT/FR2021/050733 2021.04.28
- International Announcement: WO2021/224565A 2021.11.11
- Date entered country: 2022-10-31
- Main IPC: F01D9/06
- IPC: F01D9/06 ; F01D5/28 ; F01D25/12

Abstract:
A turbomachine turbine nozzle extending around a central axis, including at least one radially outer shroud, at least one radially inner shroud, and at least one blade made of ceramic matrix composite material, distinct from the radially inner shroud and from the radially outer shroud, and extending radially between the radially inner shroud and the radially outer shroud, the blade being hollow and including a cavity opening at a radially inner end and at a radially outer end of the blade, the nozzle including at least one tubular mast arranged in the cavity of the blade and allowing routing the ventilation air passing through the cavity of the blade, the mast including a radially outer end attached to the radially outer shroud, and a radially inner end cooperating with a radial flange for positioning the radially inner shroud.
Public/Granted literature
- US20230212952A1 IMPROVED CMC GUIDE VANE FOR A TURBOMACHINE TURBINE Public/Granted day:2023-07-06
Information query