US Patent 8651431 Aircraft with movable winglets and method of control
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Patent abstract
A method and apparatus for improved aircraft control through the use of adjustable winglets. The adjustable winglets are located at the terminal ends of an aircraft's wings and may pivot about an axis parallel to the yaw axis of the aircraft. The adjustable winglets may also include outboard ailerons for improved control of the aircraft.
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US Patent 08651431 Aircraft with movable winglets and method of control US Patent 8651431 Aircraft with movable winglets and method of control
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Patent Number
0865143100
Patent Number
865143100
Edits on 18 May, 2023
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Patent Jurisdiction
Patent Number
086514310
Date of Patent
February 18, 2014
0Patent Application Number
132063170
Date Filed
August 9, 2011
0Official Website
Patent Primary Examiner
Edits on 27 Sep, 2022
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Is a
Patent Jurisdiction
Patent Number
086514310
Date of Patent
February 18, 2014
0Patent Application Number
132063170
Date Filed
August 9, 2011
0Official Website
Patent Primary Examiner
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US Patent 08651431 Aircraft with movable winglets and method of control
Infobox
Is a
Patent jurisdiction
Patent number
08651431
Date of patent
February 18, 2014
Patent application number
13206317
Date Filed
August 9, 2011
Patent primary examiner
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