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US Patent 9410451 Gas turbine engine with integrated bottoming cycle system

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Patent Citations Received
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US Patent 11885260 Gas turbine engines having cryogenic fuel systems
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Patent abstract

The present application provides an integrated bottoming cycle system for use with a gas turbine engine. The integrated bottoming cycle system described herein may include a compressor/pump, a cooling circuit downstream of the compressor/pump, a bottoming cycle heat exchanger, a heating circuit downstream of the bottoming cycle heat exchanger, and a number of turbine components in communication with the cooling circuit and/or the heating circuit to maximize the overall plant efficiency and economics.

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Patent Inventor Names
Charles Michael Booth0
Donald Gordon Laing0
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Patent Citations Received
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US Patent 11689080 Supercritical CO2 cooled electrical machine
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Official Website
https://pdfpiw.uspto.gov/.piw?Docid=094104510
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US Patent 09410451 Gas turbine engine with integrated bottoming cycle system US Patent 9410451 Gas turbine engine with integrated bottoming cycle system

Infobox
Patent Number
094104510
Patent Number
94104510
Edits on 28 Sep, 2022
"Entity importer update"
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Infobox
Is a
Patent
Patent
0
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
0
Patent Number
094104510
Date of Patent
August 9, 2016
0
Patent Application Number
136931130
Date Filed
December 4, 2012
0
Official Website
https://pdfpiw.uspto.gov/.piw?Docid=094104510
Patent Primary Examiner
‌
Carlos A Rivera
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Website URL
https://pdfpiw.uspto.gov/.piw?Docid=09410451
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 US Patent 09410451 Gas turbine engine with integrated bottoming cycle system

Infobox
Is a
Patent
Patent
Patent jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent number
09410451
Date of patent
August 9, 2016
Patent application number
13693113
Date Filed
December 4, 2012
Patent primary examiner
‌
Carlos A Rivera

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