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US Patent 9446842 Hybrid power rotary wing aircraft
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Patent
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Date Filed
December 28, 2015
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Date of Patent
September 20, 2016
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Patent Application Number
14979704
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Patent Citations Received
US Patent 11932125 Rotor break effect by using electric distributed anti-torque generators and opposing electric motor thrust to slow a main rotor
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US Patent 12091182 Aircraft hybrid electric propulsion architecture with generator-motor fail mode
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US Patent 12091179 Aircrafts, systems, and methods for providing constant torque on takeoff
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US Patent 11655022 Anti-torque control using fixed blade pitch motors
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US Patent 12006049 Flying body
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Patent Inventor Names
Leo J. Luyks
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
9446842
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Patent Primary Examiner
J. Woodrow Eldred
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