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US Patent 11618550 Foldable rotor assembly for fixed-wing VTOL aircraft

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Patent Inventor Names
Matthew S. Stauffer0
Michael J. Duffy0
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 US Patent 11618550 Foldable rotor assembly for fixed-wing VTOL aircraft

Article

A rotor assembly for a fixed-wing VTOL aircraft. The rotor assembly is configured to provide vertical flight for the fixed-wing VTOL aircraft. In one embodiment, the rotor assembly includes a hub assembly, a first rotor blade affixed to the hub assembly, and a second rotor blade affixed to the hub assembly. The hub assembly orients the second rotor blade in relation to the first rotor blade about an axis of rotation of the hub assembly with the first rotor blade and the second rotor blade vertically stacked when the hub assembly is stopped for wing-borne flight.

Infobox
Is a
Patent
Patent
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
116185500
Date of Patent
April 4, 2023
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Patent Application Number
172200970
Date Filed
April 1, 2021
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Patent Citations
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US Patent 10112698 Deployment mechanism
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US Patent 10392104 Shaft-mounted operators for folding and opening propeller blades
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US Patent 10399666 Aerial vehicle propulsion mechanism with coaxially aligned and independently rotatable propellers
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US Patent 10494088 Deployable propeller blades for aerial vehicles
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US Patent 10669869 Independently rotatable propeller blade mounts
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US Patent 10994836 Feathering propeller clutch mechanisms
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Patent Primary Examiner
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Philip J Bonzell
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CPC Code
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B64C 29/0025
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B64C 27/50
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B64C 27/30
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B64C 27/26
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B64C 11/28
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