- Patent Title: Method for heat treating a preform made of titanium alloy powder
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Application No.: US17193628Application Date: 2021-03-05
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Publication No.: US11440095B2Publication Date: 2022-09-13
- Inventor: Guillaume Fribourg , Jean-Claude Bihr , Clément Gillot
- Applicant: SAFRAN AIRCRAFT ENGINES , ALLIANCE
- Applicant Address: FR Paris; FR Saint-Vit
- Assignee: SAFRAN AIRCRAFT ENGINES,ALLIANCE
- Current Assignee: SAFRAN AIRCRAFT ENGINES,ALLIANCE
- Current Assignee Address: FR Paris; FR Saint-Vit
- Agency: Pillsbury Winthrop Shaw Pittman LLP
- Priority: FR1556375 20150706
- Main IPC: B22F3/10
- IPC: B22F3/10 ; C22C14/00 ; C22C16/00 ; F27D3/12 ; F27D5/00 ; B22F3/00 ; B22F7/02 ; B22F5/04

Abstract:
A method for heat treating a powder part preform including a titanium-based alloy, wherein the method includes the heat treatment of the preform in a furnace at a predetermined temperature, wherein the preform is on a holder during the heat treatment, wherein the holder includes a zirconium-based alloy having a zirconium content greater than or equal to 95% by weight, wherein the holder material has a melting temperature higher than the predefined temperature of the heat treatment, and wherein an anti-diffusion barrier is arranged between the preform and the holder in order to prevent welding of the preform to the holder.
Public/Granted literature
- US20210187609A1 METHOD FOR HEAT TREATING A PREFORM MADE OF TITANIUM ALLOY POWDER Public/Granted day:2021-06-24
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