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:
Mar. 29, 2016

Filed:

Apr. 24, 2012
Applicants:

Tracy A. Propheter-hinckley, Manchester, CT (US);

Mark F. Zelesky, Bolton, CT (US);

Dominic J. Mongillo, Jr., West Hartford, CT (US);

Matthew A. Devore, Cromwell, CT (US);

Steven Bruce Gautschi, Naugatuck, CT (US);

Benjamin T. Fisk, East Granby, CT (US);

Inventors:

Tracy A. Propheter-Hinckley, Manchester, CT (US);

Mark F. Zelesky, Bolton, CT (US);

Dominic J. Mongillo, Jr., West Hartford, CT (US);

Matthew A. Devore, Cromwell, CT (US);

Steven Bruce Gautschi, Naugatuck, CT (US);

Benjamin T. Fisk, East Granby, CT (US);

Assignee:

UNITED TECHNOLOGIES CORPORATION, Hartford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); B22C 9/04 (2006.01); B22C 9/10 (2006.01); B22F 5/04 (2006.01); B22F 3/105 (2006.01);
U.S. Cl.
CPC ...
B22C 9/04 (2013.01); B22C 9/10 (2013.01); B22F 3/1055 (2013.01); B22F 5/04 (2013.01); F01D 5/187 (2013.01); F05D 2240/303 (2013.01); F05D 2260/201 (2013.01); F05D 2260/202 (2013.01); F05D 2260/205 (2013.01);
Abstract

An airfoil has a body that includes leading and trailing edges joined by spaced apart pressure and suction sides to provide an exterior airfoil surface. A leading edge wall provides the exterior airfoil surface at the leading edge. An impingement wall is integrally formed with the leading edge wall to provide an impingement cavity between the leading edge wall and the impingement wall and multiple impingement holes are provided in the impingement wall. The impingement holes are spaced laterally across the impingement wall. A method of manufacturing an airfoil includes the steps of depositing multiple layers of powdered metal onto one another, joining the layers to one another with reference to CAD data relating to a particular cross-section of an airfoil, and producing the airfoil.


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