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US Patent 12017754 Download reducing wingtips

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Date Filed
March 12, 2020
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Date of Patent
June 25, 2024
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Patent Application Number
16816577
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Patent Citations
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US Patent 8376266 Method of controlling a hybrid helicopter in yaw, and a hybrid helicopter provided with a yaw control device suitable for implementing said method
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US Patent 8820673 Rotary-wing and fixed-wing aircraft
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US Patent 9266607 Compound helicopter with tail booms
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US Patent 9302761 High-lift device of flight vehicle
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US Patent 9714080 Wing tip device having configurations for flight and ground-based operations
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US Patent 9738379 Removable lift assembly for a rotorcraft, and a rotorcraft
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US Patent 9868516 Adhesive panels of microvane arrays for reducing effects of wingtip vortices
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US Patent 10005550 Compound aircraft having an additional anti-torque device
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US Patent 10071798 Hypersonic laminar flow control
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US Patent 10266252 Wing extension winglets for tiltrotor aircraft
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•••
Patent Inventor Names
Kent E. Donaldson
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Kyle Smolarek
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Phillip A. Kendrick
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
12017754
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Patent Primary Examiner
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Nicholas McFall
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CPC Code
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B64C 2003/148
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B64C 27/26
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B64C 23/065
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B64C 21/10
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