Patent Leaderboard
USPTO Patent Rankings Data through Dec 31, 2025
Home › Wingtip vortex device for induced drag reduction and vortex cancellation

Wingtip vortex device for induced drag reduction and vortex cancellation

US Patent 5934612 · Granted Aug 10, 1999

Estimated economic value: $5,843,000 ⓘ

Assignee

Inventors

View full patent text on Google Patents →

More Patents by These Inventors

Linear motion wind driven power plant1999
Aircraft with variable forward-sweep wing1999
Wingtip vortex impeller device for reducing drag and vortex cancellation1999
Laminar supersonic transport aircraft1998
Linear motion wind driven power plant1998
Linear turbine propulsion system1997
Linear turbine propulsion system1996
Supersonic natural laminar flow wing1996
Aircraft1995
Skewed hinge control surface1995
Paddle wheel rotorcraft1993
Aircraft outboard control1992