US Patent 10247108 Turbojet engine with offset fans with a differential system
Patent 10247108 was granted and assigned to Safran on April, 2019 by the United States Patent and Trademark Office.
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Patent abstract
A propulsion unit of an aircraft including a turbine (15), at least one fan (10) with an axis offset relative to the axis of the turbine and a power transmission mechanism between the turbine and the fan. The power transmission mechanism includes a speed reducing gear (20) with an input and a movement output, the input being in the extension of the axis (16) of the turbine and the output connected to the fan.
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Patent Inventor Names
Augustin Marc Michel Curlier0
Sebastien Courtois0
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Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
102471080
Date of Patent
April 2, 2019
0Patent Application Number
152843290
Date Filed
October 3, 2016
0Patent Primary Examiner
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US Patent 10247108 Turbojet engine with offset fans with a differential system
Infobox
Is a
Patent applicant
Current assignee
Patent jurisdiction
Patent number
10247108
Date of patent
April 2, 2019
Patent application number
15284329
Date Filed
October 3, 2016
Patent primary examiner
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