Invention Grant
- Patent Title: Turbomachine rotor blade
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Application No.: US14372841Application Date: 2013-01-16
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Publication No.: US10196907B2Publication Date: 2019-02-05
- Inventor: Slim Bensalah , Arnaud Negri , Sebastien Digard Brou De Cuissart , Guillaume Klein , Ba-Phuc Tang , David Mathieu , Sibylle Doremus
- 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: FR1250435 20120117; FR1255586 20120614
- International Application: PCT/FR2013/050096 WO 20130116
- International Announcement: WO2013/107982 WO 20130725
- Main IPC: F01D5/22
- IPC: F01D5/22 ; F01D5/28 ; F01D5/30

Abstract:
A turbomachine rotor blade includes an outer part at its distal end. The outer part includes a platform defining an outside surface of a passage for gas passing through a turbomachine and presenting first and second opposite side edges; and upstream and downstream sealing wipers extending outwards from the platform, each wiper extending between two lateral faces situated respectively at the first and second side edges. The two lateral faces of the upstream or the downstream wiper are covered at least in part in an anti-wear material.
Public/Granted literature
- US20150023793A1 TURBOMACHINE ROTOR BLADE Public/Granted day:2015-01-22
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