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:
Apr. 07, 2020

Filed:

Oct. 27, 2015
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Thomas N. Slavens, Vernon, CT (US);

Brooks E. Snyder, Glastonbury, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F23R 3/00 (2006.01); F01D 5/14 (2006.01);
U.S. Cl.
CPC ...
F01D 5/187 (2013.01); F01D 5/143 (2013.01); F23R 3/002 (2013.01); F05D 2200/263 (2013.01); F05D 2230/21 (2013.01); F05D 2240/81 (2013.01); F05D 2250/322 (2013.01); F05D 2250/71 (2013.01); F05D 2260/202 (2013.01); Y02T 50/673 (2013.01); Y02T 50/676 (2013.01);
Abstract

A cooling circuit for a gas turbine engine comprises a gas turbine engine component having a first portion connected to a second portion via a curved surface. An inlet is formed in or near one of the first and second portions to receive a cooling air flow. An outlet is formed in or near the other of the first and second portions to direct cooling flow along a surface of the gas turbine engine component. At least one cooling path extends between the inlet and the outlet and has at least one cooling path portion that conforms in shape to the curved surface. A gas turbine engine and a method of forming a cooling circuit for a gas turbine engine are also disclosed.


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