US Patent 10352274 Direct drive aft fan engine
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Patent abstract
An aircraft engine includes a gas powered turbine core. A first fan is connected to the turbine core via a shaft. The fan is positioned aft of the turbine. A second fan is connected to the first fan via a geared connection.
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Patent Inventor Names
Gabriel L. Suciu0
Jesse M. Chandler0
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Patent Number
103522740
Date of Patent
July 16, 2019
0Patent Application Number
152401040
Date Filed
August 18, 2016
0Official Website
Patent Citations Received
Patent Primary Examiner
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US Patent 10352274 Direct drive aft fan engine
Infobox
Is a
Patent jurisdiction
Patent number
10352274
Date of patent
July 16, 2019
Patent application number
15240104
Date Filed
August 18, 2016
Patent primary examiner
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