US Patent 8991768 Highly efficient transonic laminar flow wing
Patent 8991768 was granted and assigned to Aerion corporation on March, 2015 by the United States Patent and Trademark Office.
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Patent abstract
Improved supersonic laminar flow wing structure, on a supersonic aircraft, having strake extending forwardly of the wing inboard extent, and reversed fillet at strake junction with the wing leading edge.
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Patent Inventor Names
James D. Chase0
Michael Henderson0
Sturdza Peter0
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Patent Citations Received
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US Patent 08991768 Highly efficient transonic laminar flow wing US Patent 8991768 Highly efficient transonic laminar flow wing
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Patent Number
08991768
Patent Number
8991768
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US Patent 08991768 Highly efficient transonic laminar flow wing
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Is a
Current assignee
Patent jurisdiction
Patent number
08991768
Date of patent
March 31, 2015
Patent application number
13068774
Date Filed
May 18, 2011
Patent primary examiner
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