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US Patent 9957972 Airfoil with an integrally stiffened composite cover
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Patent
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Date Filed
August 12, 2014
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Date of Patent
May 1, 2018
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Patent Applicant
United Technologies
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Patent Application Number
14913709
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Patent Citations Received
US Patent 11879355 Airfoil assembly with an internal reinforcement structure
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US Patent 12123322 Fibrous preform with stiffeners formed by unidirectional yarn layers
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US Patent 12110807 Altering structural response of two-piece hollow-vane assembly by changing the cover composition
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US Patent 11933194 Fan or propeller vane for an aircraft turbomachine and method for manufacturing same
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Patent Inventor Names
Larry Foster
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
9957972
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Patent Primary Examiner
Richard Edgar
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