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US Patent 10843807 System and method for aircraft noise mitigation

OverviewStructured DataIssuesContributors
Is a
Patent
Patent
0
Date Filed
June 3, 2019
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Date of Patent
November 24, 2020
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Patent Application Number
16430163
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Patent Citations
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US Patent 10183746 Aircraft with independently controllable propulsion assemblies
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US Patent 10144503 Fixed wing aircraft with trailing rotors
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US Patent 10046855 Impact resistant propeller system, fast response electric propulsion system and lightweight vertical take-off and landing aircraft using same
Patent Citations Received
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US Patent 12071234 Hybrid power systems for different modes of flight
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US Patent 11787537 Hybrid power systems for different modes of flight
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US Patent 11414184 Electric distributed propulsion with different rotor rotational speeds
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US Patent 12071233 Battery systems with power optimized energy source and energy storage optimized source
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US Patent 10988249 Tilting mechanism with telescoping actuator
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US Patent 11247773 Pylon mounted tilt rotor
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US Patent 11639219 Pylon mounted tilt rotor
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US Patent 11639218 Tilting mechanism with telescoping actuator
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US Patent 11655024 Battery systems with power optimized energy source and energy storage optimized source
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US Patent 11698032 Systems and methods for controlling noise in aircraft powered by hybrid-electric gas turbine engines
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•••
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
10843807
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Patent Primary Examiner
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Assres H Woldemaryam
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