US Patent 9759130 Gas turbine engine with cooling system
Patent 9759130 was granted and assigned to Rolls-Royce on September, 2017 by the United States Patent and Trademark Office.
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Patent abstract
A cooling system for a gas turbine engine. The system includes a fuel air heat exchanger with a fuel passage that is in thermal contact with an engine cooling air passage. The system further includes a fuel deoxygenator located upstream of the fuel air heat exchanger and configured to deliver deoxygenated fuel to the fuel air heat exchanger fuel passage. The system also includes a valve configured to moderate engine cooling air flow to the engine cooling air passage.
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Patent Inventor Names
Ajith Appukuttan0
Andrew Martin Rolt0
Anthony John Moran0
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US Patent 09759130 Gas turbine engine with cooling system US Patent 9759130 Gas turbine engine with cooling system
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Patent Number
097591300
Patent Number
97591300
Edits on 28 Mar, 2023
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Is a
Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
097591300
Date of Patent
September 12, 2017
0Patent Application Number
140338780
Date Filed
September 23, 2013
0Patent Primary Examiner
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US Patent 09759130 Gas turbine engine with cooling system
Infobox
Is a
Patent applicant
Current assignee
Patent jurisdiction
Patent number
09759130
Date of patent
September 12, 2017
Patent application number
14033878
Date Filed
September 23, 2013
Patent primary examiner
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