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US Patent 11041443 Multi-spool gas turbine engine architecture
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Patent
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Date Filed
September 26, 2019
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Date of Patent
June 22, 2021
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Patent Application Number
16583896
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Patent Citations
US Patent 10113482 Gearbox for gas turbine engine
US Patent 10125722 Turbine engine with a turbo-compressor
US Patent 10054001 V-shaped gearbox for driving turbomachine equipment
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US Patent 10072570 Reverse flow gas turbine engine core
US Patent 10082080 Fan rotor for a turbo machine such as a multiple flow turbojet engine driven by a reduction gear
US Patent 10087761 Devices and methods for balancing a high-pressure spool of a gas turbine engine
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US Patent 10094295 Gas turbine engine with transmission
Patent Citations Received
US Patent 11668253 System and method for providing in-flight reverse thrust for an aircraft
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Patent Inventor Names
Martin Poulin
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Jean Dubreuil
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Keith Morgan
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Lazar Mitrovic
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Eric Durocher
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
11041443
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Patent Primary Examiner
Ehud Halberstam
0
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