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. 19, 2020

Filed:

Jul. 26, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Sandip Dutta, Greenville, SC (US);

Benjamin Paul Lacy, Greer, SC (US);

Gary Michael Itzel, Simpsonville, SC (US);

Joseph Anthony Weber, Simpsonville, SC (US);

David Edward Schick, Greenville, SC (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); B22F 5/04 (2006.01); B33Y 80/00 (2015.01); F01D 9/04 (2006.01); F01D 25/12 (2006.01); B22F 3/105 (2006.01);
U.S. Cl.
CPC ...
F01D 5/189 (2013.01); B22F 5/04 (2013.01); B33Y 80/00 (2014.12); F01D 9/041 (2013.01); F01D 25/12 (2013.01); B22F 3/1055 (2013.01); F05D 2230/22 (2013.01); F05D 2230/232 (2013.01); F05D 2230/30 (2013.01); F05D 2240/128 (2013.01); F05D 2240/30 (2013.01); F05D 2250/292 (2013.01); F05D 2260/201 (2013.01); F05D 2260/202 (2013.01); F05D 2300/171 (2013.01); Y02P 10/295 (2015.11);
Abstract

Turbine components are disclosed including a component wall defining a constrained portion, a manifold having an impingement wall, and a post-impingement cavity disposed between the manifold and the component wall. The impingement wall includes a wall thickness and defines a plenum and a tapered portion. The tapered portion tapers toward the constrained portion and includes a plurality of impingement apertures and a wall inflection. The wall inflection is disposed proximal to the constrained portion, and the tapered portion is integrally formed as a single, continuous object. The wall inflection may include an inflection radius of less than about 3 times the wall thickness of the impingement wall, or the tapered portion may include a consolidated portion with the impingement wall extending across the plenum. A method for forming the turbine component is also disclosed, including forming the tapered portion as a single, continuous tapered portion by an additive manufacturing technique.


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