US Patent 8656722 Hybrid cooling of a gas turbine engine
Patent 8656722 was granted and assigned to United Technologies on February, 2014 by the United States Patent and Trademark Office.
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Patent abstract
A method for cooling components of a gas turbine engine, having first and second sets of components that require cooling, includes removing thermal energy from cooling air, directing the cooling air from which thermal energy has been removed to the first set of components of the gas turbine engine, and transferring thermal energy away from the second set of components of the gas turbine engine using a vaporization cycle of a vapor cooling assembly. Use of the vaporization cycle offsets thermal energy removed from the cooling air.
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Patent Inventor Names
Bernard J. Raver0
James D. Hill0
James W. Norris0
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Patent Citations Received
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Official Website
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Patent Citations Received
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US Patent 08656722 Hybrid cooling of a gas turbine engine US Patent 8656722 Hybrid cooling of a gas turbine engine
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Patent Number
086567220
Patent Number
86567220
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Current Assignee
Patent Jurisdiction
Patent Number
086567220
Date of Patent
February 25, 2014
0Patent Application Number
132430130
Date Filed
September 23, 2011
0Official Website
Patent Primary Examiner
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US Patent 08656722 Hybrid cooling of a gas turbine engine
Infobox
Is a
Current assignee
Patent jurisdiction
Patent number
08656722
Date of patent
February 25, 2014
Patent application number
13243013
Date Filed
September 23, 2011
Patent primary examiner
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