Invention Grant
- Patent Title: Vibration damper for a turbomachine rotor vane
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Application No.: US16771048Application Date: 2017-12-12
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Publication No.: US11333027B2Publication Date: 2022-05-17
- Inventor: Laetitia Pollet
- Applicant: SAFRAN HELICOPTER ENGINES
- Applicant Address: FR Bordes
- Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee: SAFRAN HELICOPTER ENGINES
- Current Assignee Address: FR Bordes
- Agency: Christensen O'Connor Johnson Kindness PLLC
- International Application: PCT/FR2017/053529 WO 20171212
- International Announcement: WO2019/115886 WO 20190620
- Main IPC: F01D5/26
- IPC: F01D5/26 ; F01D5/16 ; F01D5/22 ; F01D5/30 ; F01D25/06 ; F01D5/10 ; F16F7/01

Abstract:
A turbomachine rotor has a disk carrying vanes, each vane having a blade linked by a platform to a root. For at least one vane, a recess is defined between the platform and the disk, and a vibration damper is mounted in the recess. The vibration damper includes a first structural portion configured to contact the platform of which the vibrations are to be dampened, and a second mass portion configured to dampen these vibrations. The second mass portion is a powder and the first structural portion is a box containing the powder.
Public/Granted literature
- US20210180460A1 VIBRATION DAMPER FOR A TURBOMACHINE ROTOR VANE Public/Granted day:2021-06-17
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