US Patent 8936071 Hybrid cooling system for aircraft applications
Patent 8936071 was granted and assigned to Hamilton Sundstrand on January, 2015 by the United States Patent and Trademark Office.
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Patent abstract
An aircraft cooling system includes a refrigerant cycle including a first heat exchanger. A liquid cycle passes a liquid through the first heat exchanger, at which it is cooled by a refrigerant in the refrigerant cycle. An air cycle compresses air and delivers the compressed air into a second heat exchanger. The liquid passes through the second heat exchanger at a location downstream of the first heat exchanger. The liquid cools the air in the second heat exchanger. Air downstream of the second heat exchanger passes to be utilized by a use on an aircraft.
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US Patent 08936071 Hybrid cooling system for aircraft applications US Patent 8936071 Hybrid cooling system for aircraft applications
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Patent Number
0893607100
Patent Number
893607100
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Is a
Current Assignee
Patent Jurisdiction
Patent Number
089360710
Date of Patent
January 20, 2015
0Patent Application Number
126156560
Date Filed
November 10, 2009
0Official Website
Patent Primary Examiner
Edits on 23 Sep, 2022
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Infobox
Is a
Current Assignee
Patent Jurisdiction
Patent Number
089360710
Date of Patent
January 20, 2015
0Patent Application Number
126156560
Date Filed
November 10, 2009
0Official Website
Patent Primary Examiner
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US Patent 08936071 Hybrid cooling system for aircraft applications
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
08936071
Date of patent
January 20, 2015
Patent application number
12615656
Date Filed
November 10, 2009
Patent primary examiner
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