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:
May. 12, 2015

Filed:

Jun. 23, 2011
Applicants:

Christine Hottier, La Celle Saint Cloud, FR;

Bertrand Lamaison, Issy les Moulineaux, FR;

Jacques Abousefian, Achères, FR;

Inventors:

Christine Hottier, La Celle Saint Cloud, FR;

Bertrand Lamaison, Issy les Moulineaux, FR;

Jacques Abousefian, Achères, FR;

Assignee:

Snecma, Paris, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B21K 1/74 (2006.01); B21K 3/04 (2006.01); B23P 15/04 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01); F04D 29/02 (2006.01); F04D 29/32 (2006.01); F01D 5/00 (2006.01); B29C 65/00 (2006.01); B29L 31/08 (2006.01); B29C 65/48 (2006.01);
U.S. Cl.
CPC ...
B21K 3/04 (2013.01); B23P 15/04 (2013.01); F01D 5/147 (2013.01); F01D 5/282 (2013.01); F01D 5/286 (2013.01); F04D 29/023 (2013.01); F04D 29/324 (2013.01); Y02T 50/672 (2013.01); Y02T 50/673 (2013.01); B29C 66/12461 (2013.01); B29C 66/12463 (2013.01); B29C 66/301 (2013.01); B29C 66/53 (2013.01); B29C 66/721 (2013.01); B29C 66/742 (2013.01); B29L 2031/08 (2013.01); B29L 2031/082 (2013.01); F01D 5/00 (2013.01); F05D 2230/25 (2013.01); F05D 2230/24 (2013.01); B29C 65/484 (2013.01); B29C 65/48 (2013.01); B29C 65/483 (2013.01);
Abstract

A method for producing a solid component which in succession includes deforming a metal bar by forging using two dies in order to obtain an intermediate component including two fins one on each side of a solid part capable of forming the base of the metal reinforcement, the two fins being at a divergent angle α; deforming the two fins of the intermediate component, altering the divergent angle α, so as to obtain the final shape of the turbomachine blade leading edge or trailing edge metal reinforcement.


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