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US Patent 11440671 Adjustable motor fairings for aerial vehicles

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Contents

Is a
Patent
Patent

Patent attributes

Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
11440671
Date of Patent
September 13, 2022
Patent Application Number
16256279
Date Filed
January 24, 2019
Patent Citations
‌
US Patent 10214285 Aircraft having autonomous and remote flight control capabilities
‌
US Patent 10011351 Passenger pod assembly transportation system
‌
US Patent 10029785 Aircraft capable of vertical takeoff
‌
US Patent 10183746 Aircraft with independently controllable propulsion assemblies
‌
US Patent 10315761 Aircraft propulsion assembly
‌
US Patent 10329014 Aircraft having M-wings
‌
US Patent 10364024 Multicopter with angled rotors
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US Patent 10468545 Airfoil body including a moveable section of an outer surface carrying an array of transducer elements
...
Patent Citations Received
0
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US Patent 11597489 Aerial vehicle airframe design and manufacturing
0
Patent Primary Examiner
‌
Medhat Badawi
CPC Code
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B64C 23/02
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B64C 2201/086
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B64C 2201/104
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B64C 2201/165
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B64C 29/0016
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B64C 29/0033
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B64C 29/0075
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B64C 2201/027
...

Systems and methods to reduce aerodynamic drag and/or affect flight characteristics of an aerial vehicle may include adjustable fairings associated with one or more components of the aerial vehicle. The adjustable fairings may be coupled to and at least partially surround a motor, propulsion mechanism, motor arm, strut, or other component of an aerial vehicle. In addition, the adjustable fairings may be passively movable between two or more positions responsive to airflow around the fairings, and/or the adjustable fairings may be actively moved between two more positions to affect flight characteristics. Further, the adjustable fairings may include actuatable elements to alter a portion of an outer surface of the fairings to thereby affect flight characteristics. In this manner, adjustable fairings associated with various components of an aerial vehicle may reduce aerodynamic drag and/or may improve control and safety of an aerial vehicle.

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