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:
Jul. 16, 2024

Filed:

Jan. 21, 2022
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Honggang Wang, Clifton Park, NY (US);

Michael Anthony Benjamin, Cincinnati, OH (US);

Seung-Hyuck Hong, Clifton Park, NY (US);

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

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2024.01); B64D 27/10 (2006.01); F02C 7/26 (2006.01); H01M 8/04111 (2016.01); H01M 8/04223 (2016.01); H01M 8/04225 (2016.01); H01M 8/04701 (2016.01); B64D 27/02 (2006.01); B64D 41/00 (2006.01); F02C 1/10 (2006.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64D 27/10 (2013.01); F02C 7/26 (2013.01); H01M 8/04111 (2013.01); H01M 8/04225 (2016.02); H01M 8/04231 (2013.01); H01M 8/04708 (2013.01); H01M 8/04738 (2013.01); B64D 27/026 (2024.01); B64D 2041/005 (2013.01); F02C 1/10 (2013.01); H01M 2250/20 (2013.01);
Abstract

A method for operating a propulsion system for an aircraft, the propulsion system including a gas turbine engine and a fuel cell assembly, the fuel cell assembly comprising a fuel cell stack having a fuel cell defining an outlet positioned to remove output products from the fuel cell during operation, the method including: executing a startup sequence for the gas turbine engine, wherein executing the startup sequence comprises initiating the startup sequence for the gas turbine engine; executing a startup sequence for the fuel cell assembly concurrently with, or subsequent to, initiating the startup sequence for the gas turbine engine; and operating the fuel cell assembly to provide output products to a combustion section of the gas turbine engine.


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