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:
Jul. 07, 2020

Filed:

Feb. 22, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Gregory Terrence Garay, West Chester, OH (US);

Mark Kevin Meyer, Cincinnati, OH (US);

Douglas Gerard Konitzer, West Chester, OH (US);

William Thomas Carter, Niskayuna, NY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/00 (2006.01); B22F 5/04 (2006.01); B23K 20/22 (2006.01); F01D 5/14 (2006.01); B22F 7/06 (2006.01); B22C 9/24 (2006.01); B22D 29/00 (2006.01); B23P 15/04 (2006.01); B33Y 80/00 (2015.01); B23K 26/34 (2014.01); B22F 3/105 (2006.01); B23P 6/04 (2006.01); B23P 6/00 (2006.01); B23K 35/02 (2006.01); B23K 26/0622 (2014.01); B22F 7/08 (2006.01); B22C 9/04 (2006.01); B23K 101/00 (2006.01); B23K 103/08 (2006.01); B23K 103/18 (2006.01);
U.S. Cl.
CPC ...
B23P 6/045 (2013.01); B22C 9/04 (2013.01); B22C 9/24 (2013.01); B22D 29/00 (2013.01); B22F 5/04 (2013.01); B22F 7/062 (2013.01); B22F 7/08 (2013.01); B23K 20/22 (2013.01); B23K 26/0624 (2015.10); B23K 35/0244 (2013.01); B23P 6/007 (2013.01); B23P 15/04 (2013.01); B33Y 80/00 (2014.12); F01D 5/005 (2013.01); F01D 5/147 (2013.01); B22F 3/105 (2013.01); B22F 3/1055 (2013.01); B22F 2998/10 (2013.01); B23K 26/34 (2013.01); B23K 2101/001 (2018.08); B23K 2103/08 (2018.08); B23K 2103/26 (2018.08); F05D 2230/211 (2013.01); F05D 2230/31 (2013.01); F05D 2230/80 (2013.01); F05D 2300/175 (2013.01);
Abstract

Methods of manufacturing or repairing a turbine blade or vane are described. The airfoil portions of these turbine components are typically manufactured by casting in a ceramic mold, and a surface made up of the cast airfoil and at the least the ceramic core serves as a build surface for a subsequent process of additively manufacturing the tip portions. The build surface is created by removing a top portion of the airfoil and the core, or by placing an ultra-thin shim on top of the airfoil and the core. The overhang projected by the shim is subsequently removed. These methods are not limited to turbine engine applications, but can be applied to any metallic object that can benefit from casting and additive manufacturing processes. The present disclosure also relates to finished and intermediate products prepared by these methods.


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