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US Patent 10385777 Bifurcated inlet scoop for gas turbine engine
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Is a
Patent
Date Filed
June 25, 2013
Date of Patent
August 20, 2019
Patent Application Number
13926632
Patent Citations Received
US Patent 11767124 Aircraft propulsion system with variable area inlet
Patent Jurisdiction
United States Patent and Trademark Office
Patent Number
10385777
Patent Primary Examiner
Ninh H. Nguyen
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