Invention Grant
- Patent Title: Vaned ring for turbomachine stator having vanes connected to an outer shell by conical seating and frangible pin
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Application No.: US16271991Application Date: 2019-02-11
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Publication No.: US10907489B2Publication Date: 2021-02-02
- Inventor: Thierry Georges Paul Papin , Kaelig Merwen Orieux , Jean-Marc Claude Perrollaz
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1851347 20180216
- Main IPC: F01D9/04
- IPC: F01D9/04

Abstract:
A vaned ring for a turbomachine stator includes an outer shell, a vane having a vane head, and two platforms arranged circumferentially on either side of the vane head, and fixed on a radially inner face of the outer shell by detachable fasteners. The vane head has first conical seatings bearing on respective second conical seatings of the two platforms so as to prevent a displacement of the vane radially inwards and along the circumferential direction. The vaned ring includes a frangible pin including a base mounted on the outer shell and a head projecting radially inwards with respect to the outer shell and having a head surface forming, vis-à-vis a top surface of the vane head, a stop opposing a displacement of the vane radially outwards.
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