Invention Grant
- Patent Title: Assembly for turbine engine for measuring vibrations sustained by a rotating blade
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Application No.: US15107533Application Date: 2014-12-22
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Publication No.: US10921179B2Publication Date: 2021-02-16
- Inventor: Arnaud Talon , Gilbert Arrouge , Jean-Yves Cazaux , Julien Garnier
- Applicant: SAFRAN HELICOPTER ENGINES
- Applicant Address: FR Bordes
- Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee Address: FR Bordes
- Agency: Obion, McClelland, Maier & Neustadt, L.L.P.
- Priority: FR1363471 20131223
- International Application: PCT/FR2014/053515 WO 20141222
- International Announcement: WO2015/097399 WO 20150702
- Main IPC: G01H1/00
- IPC: G01H1/00 ; G01P3/487 ; F01D5/02 ; F01D5/12 ; F01D21/00 ; F01D25/24

Abstract:
An assembly for a turbine engine, the assembly including a casing and an impeller rotatably movable inside the casing, the impeller including at least one blade having a tip edge opposite the casing, wherein the tip edge includes a magnet and wherein the casing includes an electrical conductor suitable for generating between the terminals thereof an electric voltage induced by the magnet of the tip edge opposite same and representing vibrations sustained by the tip edge of the blade when the impeller is rotated.
Public/Granted literature
- US20160320230A1 ASSEMBLY FOR TURBINE ENGINE FOR MEASURING VIBRATIONS SUSTAINED BY A ROTATING BLADE Public/Granted day:2016-11-03
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