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:
Jun. 01, 2021

Filed:

Jan. 04, 2018
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Daniel Alan Niergarth, Norwood, OH (US);

Brandon Wayne Miller, Liberty Township, OH (US);

Raymond Floyd Martell, Wyoming, OH (US);

Jeffrey Douglas Rambo, Mason, OH (US);

Ryan James Matthys, South Lebanon, OH (US);

Joel Francis Kirk, Monroe, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/143 (2006.01); F01D 5/14 (2006.01); F02C 7/18 (2006.01); F01D 25/12 (2006.01); F02C 7/12 (2006.01); F01D 5/08 (2006.01); F02C 3/06 (2006.01); F23R 3/28 (2006.01); F01D 9/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/143 (2013.01); F01D 5/142 (2013.01); F01D 5/085 (2013.01); F01D 9/065 (2013.01); F01D 25/12 (2013.01); F02C 3/06 (2013.01); F02C 7/12 (2013.01); F02C 7/185 (2013.01); F05D 2220/3216 (2013.01); F05D 2240/12 (2013.01); F05D 2260/213 (2013.01); F23R 3/283 (2013.01);
Abstract

A gas turbine engine includes a turbomachine including a compressor section, a combustion section, a turbine section, and an exhaust section arranged in serial flow order and together defining at least in part a core air flowpath. The gas turbine engine also includes a thermal management system including a flowpath heat exchanger coupled to, or integrated into, one or more components of the compressor section, the combustion section, the turbine section, or the exhaust section such that the flowpath heat exchanger is directly thermally coupled to an airflow through the core air flowpath.


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