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US 2015/0028160 A1Published application
Wingtip for a general aviation aircraft
OwnerJohn Gregory Ronczinventor
Life of this patent
Estimating the term…
Abstract
A wingtip for extending a wing of an aircraft having a NACA 23012 airfoil. The wingtip has an airfoil design for directing and associated wingtip vortex outward and upward to thereby increase the effective wingspan of the aircraft and to reduce induced drag. The wingtip is preferably molded and comprises a fuel tank bay, internal antenna, landing light and navigation light.
Claims1
A wingtip for extending a wing of an aircraft having a NACA 23012 airfoil, the wing tip has an airfoil design which directs an associated wingtip vortex outward and upward to thereby increase the effective wingspan of the aircraft to reduce induced drag
Dependencies are inferred from the claim text.