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:
Oct. 06, 2020

Filed:

Mar. 15, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventor:

Eric W. Malmborg, Amston, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B33Y 10/00 (2015.01); F01D 5/14 (2006.01); F01D 5/16 (2006.01); F01D 5/20 (2006.01); C23C 4/134 (2016.01); B23K 10/02 (2006.01); B23P 15/02 (2006.01); C23C 4/08 (2016.01); F01D 5/28 (2006.01); B33Y 80/00 (2015.01); B23K 101/04 (2006.01);
U.S. Cl.
CPC ...
C23C 4/134 (2016.01); B23K 10/027 (2013.01); B23P 15/02 (2013.01); C23C 4/08 (2013.01); F01D 5/147 (2013.01); F01D 5/28 (2013.01); B23K 2101/04 (2018.08); B33Y 10/00 (2014.12); B33Y 80/00 (2014.12); F05D 2230/30 (2013.01); F05D 2230/312 (2013.01); F05D 2230/42 (2013.01); F05D 2250/291 (2013.01); F05D 2300/133 (2013.01);
Abstract

A method of producing a gas turbine engine fan blade having a geometric configuration is provided. The method includes: plastically deforming an initial substrate comprised of a first metallic material into a formed substrate; depositing a second metallic material onto the formed substrate using an additive manufacturing process to produce a blade blank, which depositing includes: additively depositing second metallic material to at least one of the first face surface or the second face surface of the formed substrate adjacent the first end surface, to form a root portion; additively depositing second metallic material to at least one of the first face surface or the second face surface of the formed substrate between the root portion and the second end surface to form an airfoil portion; and shaping the blade blank into the geometric configuration.


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