The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Sep. 01, 2020

Filed:

May. 26, 2016
Applicants:

Safran Aircraft Engines, Paris, FR;

Safran, Paris, FR;

Inventors:

Gilbert Leconte, Moissy-Cramayel, FR;

Jean-Michel Franchet, Moissy-Cramayel, FR;

Pierre Sallot, Moissy-Cramayel, FR;

Assignees:

SAFRAN AIRCRAFT ENGINES, Paris, FR;

SAFRAN, Paris, FR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B23P 15/02 (2006.01); B21C 23/00 (2006.01); B22F 3/17 (2006.01); B22F 3/20 (2006.01); B21C 23/16 (2006.01); B22F 5/04 (2006.01); B21C 35/02 (2006.01); B23P 13/02 (2006.01); B21C 23/14 (2006.01); B21K 3/04 (2006.01); F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
B21C 23/002 (2013.01); B21C 23/142 (2013.01); B21C 23/16 (2013.01); B21C 35/023 (2013.01); B21K 3/04 (2013.01); B22F 3/17 (2013.01); B22F 3/20 (2013.01); B22F 5/04 (2013.01); B23P 13/02 (2013.01); B23P 15/02 (2013.01); F01D 5/14 (2013.01); B22F 2998/10 (2013.01); F05D 2230/10 (2013.01); F05D 2230/24 (2013.01); F05D 2230/25 (2013.01); F05D 2240/24 (2013.01); F05D 2300/174 (2013.01);
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.


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