US Patent 10947929 Integrated aircraft propulsion system
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Patent abstract
An integrated propulsion system comprising at least two gas turbine engines, at least one fan, and a transmission assembly coupling the at least two gas turbine engines to the at least one fan wherein the at least two gas turbine engines are disposed within a main body of an airframe comprising the main body and a pair of wings, and wherein the number of gas turbine engines is greater than the number of fans.
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Patent Number
109479290
Date of Patent
March 16, 2021
0Patent Application Number
160176470
Date Filed
June 25, 2018
0Official Website
Patent Citations
Patent Primary Examiner
Edits on 25 Sep, 2022
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Patent Jurisdiction
Patent Number
109479290
Date of Patent
March 16, 2021
0Patent Application Number
160176470
Date Filed
June 25, 2018
0Official Website
Patent Citations
Patent Primary Examiner
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US Patent 10947929 Integrated aircraft propulsion system
Infobox
Is a
Patent jurisdiction
Patent number
10947929
Date of patent
March 16, 2021
Patent application number
16017647
Date Filed
June 25, 2018
Patent citations
Patent primary examiner
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