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. 24, 2026

Filed:

Jan. 04, 2024
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Honggang Wang, Clifton Park, NY (US);

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

Michael Anthony Benjamin, Cincinnati, OH (US);

Richard L. Hart, Broadalbin, NY (US);

Randy M. Vondrell, Cincinnati, OH (US);

Ryan St. Pierre, Jacksonville, FL (US);

Assignee:

General Electric Company, Evendale, OH (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/232 (2006.01); H01M 8/04014 (2016.01); H01M 8/04089 (2016.01); H01M 8/04111 (2016.01); H01M 8/0612 (2016.01); H01M 8/12 (2016.01);
U.S. Cl.
CPC ...
F02C 7/232 (2013.01); H01M 8/04014 (2013.01); H01M 8/04097 (2013.01); H01M 8/04111 (2013.01); H01M 8/0618 (2013.01); H01M 2008/1293 (2013.01); H01M 2250/20 (2013.01);
Abstract

A gas turbine engine is provided. The gas turbine engine includes a turbomachine having a turbomachine having a compressor section, a combustor, and a turbine section arranged in serial flow order, the turbomachine further including an outer casing; and a fuel cell assembly positioned within the outer casing of the turbomachine, the fuel cell assembly including a fuel cell, an inlet line in fluid communication with an inlet of the fuel cell, and an output products line in fluid communication with an outlet of the fuel cell for receiving output products from the fuel cell, wherein the inlet line is positioned to be in thermal communication with the output products during operation of the gas turbine engine.


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