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:
Jan. 18, 2022

Filed:

Aug. 13, 2019
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Thomas Earl Dyson, Niskayuna, NY (US);

Lyndsay Marie Kibler, Cincinnati, OH (US);

Brendon James Leary, Simpsonville, SC (US);

David Vincent Bucci, Greenville, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C23C 4/01 (2016.01); B33Y 10/00 (2015.01); B33Y 80/00 (2015.01); F01D 5/18 (2006.01); F01D 5/28 (2006.01); B23P 15/02 (2006.01); B23P 15/04 (2006.01);
U.S. Cl.
CPC ...
C23C 4/01 (2016.01); B23P 15/02 (2013.01); B23P 15/04 (2013.01); B33Y 10/00 (2014.12); B33Y 80/00 (2014.12); F01D 5/186 (2013.01); F01D 5/288 (2013.01); F05D 2220/30 (2013.01); F05D 2230/90 (2013.01); F05D 2240/24 (2013.01); F05D 2260/202 (2013.01);
Abstract

A method of depositing a coating on a component of a turbine engine. The method includes forming a turbine component including at least one cooling flow passage in fluid communication with an aperture on a surface of the turbine component. A protective shield is formed on an inner surface of the at least one cooling flow passage and extending to an exterior of the turbine component via the aperture. During a coating process, the protective shield is configured to block the coating from being deposited in the at least one cooling flow passage via the aperture. Subsequent to coating, at least a portion of the protective shield is removed to provide for passage of a cooling fluid flow in the at least one cooling flow passage. The cooling fluid flow exits the turbine component through the aperture. A turbine component employing user of the protective shield is also disclosed.


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