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. 06, 2022

Filed:

Sep. 29, 2020
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Clay Thomas Griffis, Greenville, SC (US);

Jonathan Dwight Berry, Simpsonville, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/02 (2006.01); F01D 5/18 (2006.01); B22F 3/10 (2006.01); B33Y 80/00 (2015.01); B33Y 10/00 (2015.01); B22F 10/28 (2021.01); B22F 10/40 (2021.01); B22F 10/00 (2021.01); B22F 5/04 (2006.01);
U.S. Cl.
CPC ...
F01D 9/02 (2013.01); B22F 5/04 (2013.01); B22F 10/00 (2021.01); F01D 5/18 (2013.01); B22F 2003/1042 (2013.01); B22F 2202/11 (2013.01); B33Y 10/00 (2014.12); B33Y 80/00 (2014.12); F05D 2230/31 (2013.01); F05D 2240/128 (2013.01); F05D 2240/35 (2013.01);
Abstract

Methods of fabricating a turbomachine component and turbomachine components are provided. The method includes irradiating a layer of powder in a powder bed to form a fused region. The powder is disposed on a build plate. The method further includes a step of providing a subsequent layer of powder over the powder bed by passing a recoater arm over the powder bed from a first side of the powder bed. The method further includes repeating the irradiating and providing steps until a turbine nozzle assembly is formed on the build plate. The turbine nozzle assembly includes the turbine nozzle and a plurality of heat fins disposed within the turbine nozzle. The plurality of heat fins transfer heat away from a thermally sensitive portion of the turbine nozzle.


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