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US Patent 11834154 Shockwave mitigation system for supersonic aircraft
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Patent
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Date Filed
March 9, 2020
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Date of Patent
December 5, 2023
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Patent Application Number
16813718
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Patent Citations
US Patent 10618638 Shockwave mitigation system for supersonic aircraft
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US Patent 10793266 Commercial supersonic aircraft and associated systems and methods
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US Patent 7631836 Jet engine nacelle for a supersonic aircraft
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US Patent 7837142 Supersonic aircraft jet engine
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US Patent 7861966 Supersonic aircraft footprint spreading control system and method
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US Patent 7967241 Supersonic aircraft jet engine installation
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US Patent 8083171 Supersonic aircraft for reducing sonic boom effects at ground level
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US Patent 9482155 Isentropic compression inlet for supersonic aircraft
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US Patent 9884688 Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system
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Patent Inventor Names
John B. Schlaerth, Jr.
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
11834154
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Patent Primary Examiner
Joseph W Sanderson
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CPC Code
B64C 23/04
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B64C 30/00
0
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