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:
Nov. 26, 2019

Filed:

Jul. 20, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Brandon Wayne Miller, Cincinnati, OH (US);

Jeffrey Anthony Hamel, Maineville, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/12 (2006.01); F01D 9/06 (2006.01); F02C 7/16 (2006.01); F01D 5/08 (2006.01); F02C 3/30 (2006.01); F02C 7/14 (2006.01); F02C 3/10 (2006.01);
U.S. Cl.
CPC ...
F02C 7/16 (2013.01); F01D 5/081 (2013.01); F01D 9/065 (2013.01); F01D 25/12 (2013.01); F02C 3/10 (2013.01); F02C 3/30 (2013.01); F02C 7/14 (2013.01); F05D 2220/36 (2013.01); F05D 2260/212 (2013.01); Y02T 50/675 (2013.01);
Abstract

A gas turbine engine including a compressor section, a turbine section, and a combustion section positioned between the compressor section and the turbine section is provided. The gas turbine engine also includes a cooling system having a tank and one or more fluid lines in fluid communication with the tank. The one or more fluid lines are configured to carry a flow of consumable cooling liquid provide such consumable cooling liquid to one or more components of the compressor section, the turbine section, and/or the combustion section not directly exposed to a core air flowpath defined through the gas turbine engine.


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