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US Patent 8292227 Aircraft wings having continuously tailored structural strength
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Patent
Date Filed
July 12, 2008
Date of Patent
October 23, 2012
Patent Application Number
12172230
Patent Citations Received
US Patent 12014712 Corrugated acoustic stiffening devices and methods
0
US Patent 11780179 Thermoplastic composite panel with corrugated peaks and troughs stiffening systems and methods
US Patent 11993388 Corrugated stiffening devices utilizing peaks and valleys and methods of manufacture
0
Patent Jurisdiction
United States Patent and Trademark Office
Patent Number
8292227
Patent Primary Examiner
Joseph W Sanderson
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