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US Patent 9611034 Wide fuselage aircraft with increased boundary layer ingestion
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Patent
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Date Filed
November 3, 2015
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Date of Patent
April 4, 2017
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Patent Applicant
United Technologies
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Patent Application Number
14930712
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Patent Citations Received
US Patent 11772771 Vehicle configuration with aerodynamic shaping to reduce drag, and vehicle and method for the same
US Patent 11964772 Boundary layer ducted fan propulsion system
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Patent Inventor Names
Jesse M. Chandler
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Gabriel L. Suciu
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Wesley K. Lord
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
9611034
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Patent Primary Examiner
Joseph W Sanderson
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