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US Patent 11859820 Gas turbine combustion section having an integrated fuel cell assembly

Patent 11859820 was granted and assigned to General Electric on January, 2024 by the United States Patent and Trademark Office.

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Contents

Is a
Patent
Patent
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Patent attributes

Patent Applicant
General Electric
General Electric
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Current Assignee
General Electric
General Electric
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
118598200
Patent Inventor Names
Andrew Wickersham0
Anil Raj Duggal0
Michael Anthony Benjamin0
Narendra Digamber Joshi0
Richard L. Hart0
Seung-Hyuck Hong0
Honggang Wang0
Date of Patent
January 2, 2024
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Patent Application Number
179846690
Date Filed
November 10, 2022
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Patent Citations
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US Patent 7470477 Cascaded fuel cell stacks for fast start-up and anode coking control
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US Patent 7513119 Systems and methods for starting aircraft engines
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US Patent 7578136 Integrated power and pressurization system
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US Patent 7659021 Power generating apparatus using solid oxide fuel cell
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US Patent 7709118 Recuperated atmospheric SOFC/gas turbine hybrid cycle
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US Patent 7743499 Reactor manufacturing method for a fuel cell processor
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US Patent 7781115 Recuperated atmosphere SOFC/gas turbine hybrid cycle
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US Patent 7854582 Operation of an aircraft engine after emergency shutdown
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Patent Primary Examiner
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Todd E. Manahan
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CPC Code
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F02C 3/20
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H01M 8/04089
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H01M 8/2457
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F23R 3/28
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H01M 2250/20
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H01M 8/04761
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F23R 3/002
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H01M 2250/407
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Patent abstract

A combustion section defines an axial direction, a radial direction, and a circumferential direction. The combustion section includes a casing that defines a diffusion chamber. A combustion liner is disposed within the diffusion chamber and defines a combustion chamber. The combustion liner is spaced apart from the casing such that a passageway is defined between the combustion liner and the casing. A fuel cell assembly is disposed in the passageway. The fuel cell assembly includes a fuel cell stack that has a plurality of fuel cells each extending between an inlet end and an outlet end. The inlet end receives a flow of air and fuel and the outlet end provides output products to the combustion chamber. The outlet end of the plurality of fuel cells extends through the combustion liner and partially defines the combustion chamber.

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