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:
Oct. 27, 2020

Filed:

Jan. 25, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Anthony B. Swift, Waterboro, ME (US);

Ken F. Blaney, Middleton, NH (US);

Paul M. Lutjen, Kennebunkport, ME (US);

Neil L. Tatman, Brentwood, NH (US);

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

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/12 (2006.01); B22C 9/10 (2006.01); F01D 5/18 (2006.01); F01D 5/14 (2006.01); F01D 9/04 (2006.01); F01D 11/08 (2006.01); F02C 7/12 (2006.01);
U.S. Cl.
CPC ...
F01D 25/12 (2013.01); B22C 9/103 (2013.01); F01D 5/14 (2013.01); F01D 5/187 (2013.01); F01D 9/041 (2013.01); F01D 11/08 (2013.01); F02C 7/12 (2013.01); F05D 2220/32 (2013.01); F05D 2230/10 (2013.01); F05D 2230/211 (2013.01); F05D 2230/30 (2013.01); F05D 2240/11 (2013.01); F05D 2250/323 (2013.01); F05D 2250/324 (2013.01); F05D 2260/202 (2013.01);
Abstract

A gas turbine engine component has a body extending between two circumferential sides, and between a leading edge and a trailing edge. A refractory metal core within the body forms at least one cooling circuit to utilize fluid to cool the body. When the refractory metal core is removed from the body, the at least one cooling circuit includes an inlet, an outlet, and a passage that varies in cross-sectional area between the inlet and outlet. A method of manufacturing a gas turbine engine, a method of manufacturing a core, and a refractory metal core are also disclosed.


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