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US Patent 10978723 Fuel cell secondary power and thermal management systems

Patent 10978723 was granted and assigned to Honeywell on April, 2021 by the United States Patent and Trademark Office.

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Contents

Patent abstractTimelineTable: Further ResourcesReferences
Is a
Patent
Patent

Patent attributes

Patent Applicant
Honeywell
Honeywell
Current Assignee
Honeywell
Honeywell
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
10978723
Date of Patent
April 13, 2021
Patent Application Number
16122256
Date Filed
September 5, 2018
Patent Citations Received
‌
US Patent 12129789 Systems and method of operating a fuel cell assembly, a gas turbine engine, or both
3
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US Patent 12074350 Solid oxide fuel cell assembly
4
‌
US Patent 12078350 Gas turbine combustion section having an integrated fuel cell assembly
5
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US Patent 12123361 Systems and methods for providing output products to a combustion chamber of a gas turbine engine
6
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US Patent 11804607 Cooling of a fuel cell assembly
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US Patent 11859820 Gas turbine combustion section having an integrated fuel cell assembly
7
‌
US Patent 11912416 Hydrogen systems for environmental control systems onboard aircraft
8
‌
US Patent 11923586 Gas turbine combustion section having an integrated fuel cell assembly
9
...
Patent Primary Examiner
‌
Claude J Brown
Patent abstract

A fuel cell secondary power and thermal management system includes a compressor, a turbine, a first heat exchanger, a proton exchange membrane fuel cell, and a second heat exchanger. The first heat exchanger has first and second air flow circuits and transfers heat between the first and second air flow circuits. The proton exchange membrane fuel cell includes a cathode air flow circuit and an anode hydrogen flow circuit. The cathode air flow circuit receives air from the first air flow circuit. The second heat exchanger has a third and fourth air flow circuits and is configured to transfer heat between the third and fourth air flow circuits. The third air flow circuit receives air from the second air flow circuit outlet. The fourth air flow circuit receives the air discharged from the cathode air flow circuit and supplies air to the turbine.

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