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Variable Geometry Aerodynamic Winglet System for Reduced Drag in Commercial Aircraft

Patent #US11989234B2

Public record:Verify on Google Patents

A winglet design capable of adjusting its curvature and angle of attack based on airspeed and flight phase. This system enhances fuel efficiency by dynamically optimizing the aircraft lift-to-drag ratio.

Issue Date

5/5/2026

Inventor

Amelia Vance

Seller Location

United States

Price on request

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