Secondary airfoil apparatus, system, and method for improving lift and aerodynamic performance of a floatplane
AssigneeComp Air Solutions, LLC
InventorsRonald A. Lueck, Michael Ryan
Life of this patent
Estimating the term…
Loading patent…
AssigneeComp Air Solutions, LLC
InventorsRonald A. Lueck, Michael Ryan
Estimating the term…
The present disclosure relates to a secondary airfoil apparatus, system and method for improving lift, takeoff, landing and aerodynamic performance of a floatplane. The secondary airfoil is itself of sufficient structural rigidity to withstand any and all forces added by the airfoil during floatplane operation, and is fixedly attached between the floats of the floatplane. The secondary airfoil can be arranged at an optimal angle of incidence and vertical lift position relative to the primary airfoil, or wing of the aircraft, and relative to the floats center of gravity and drag for optimal maneuverability of the floatplane.
A secondary airfoil apparatus for use on a floatplane, the floatplane including one or more primary airfoils and a pair of floats, the secondary airfoil apparatus comprising:
A system for improving lift and aerodynamic performance of a floatplane, the system comprising:
A method for improving lift and aerodynamic performance of a floatplane, the floatplane including a primary airfoil, a first float, and a second float, the method comprising:
Dependencies are inferred from the claim text.