Invention Grant
- Patent Title: Method for manufacturing a TiAl blade of a turbine engine
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Application No.: US15576783Application Date: 2016-05-26
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Publication No.: US10758957B2Publication Date: 2020-09-01
- Inventor: Gilbert Leconte , Jean-Michel Franchet , Pierre Sallot
- Applicant: SAFRAN AIRCRAFT ENGINES , SAFRAN
- Applicant Address: FR Paris FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES,SAFRAN
- Current Assignee: SAFRAN AIRCRAFT ENGINES,SAFRAN
- Current Assignee Address: FR Paris FR Paris
- Agency: Oblon, McClelland, Maier & Neustadt, L.L.P.
- Priority: com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@597eacc7
- International Application: PCT/FR2016/051244 WO 20160526
- International Announcement: WO2016/189254 WO 20161201
- Main IPC: B23P15/02
- IPC: B23P15/02 ; B21C23/00 ; B22F3/17 ; B22F3/20 ; B21C23/16 ; B22F5/04 ; B21C35/02 ; B23P13/02 ; B21C23/14 ; B21K3/04 ; F01D5/14

Abstract:
A method for manufacturing a titanium aluminide blade of a turbine engine, including production of a titanium aluminide ingot, extrusion of the ingot through an opening in a die having one main arm and at least one side arm, such as to obtain a extruded ingot having the shape of a bar with a cross-section having one main arm and at least one side arm substantially perpendicular to the main arm, transverse cutting of the extruded ingot such as to obtain sections of extruded ingot, forging of each section of extruded ingot such as to obtain a turbine engine blade.
Public/Granted literature
- US20180304329A1 METHOD FOR MANUFACTURING A TiAl BLADE OF A TURBINE ENGINE Public/Granted day:2018-10-25
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