The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
May. 12, 2026

Filed:

Aug. 22, 2023
Applicants:

Ronald A. Lueck, Merritt Island, FL (US);

Michael Ryan, Jefferson City, MO (US);

Inventors:

Ronald A. Lueck, Merritt Island, FL (US);

Michael Ryan, Jefferson City, MO (US);

Assignee:

Other;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 35/00 (2006.01); B64C 3/26 (2006.01); B64C 3/34 (2006.01); B64C 25/54 (2006.01); B64D 37/16 (2006.01);
U.S. Cl.
CPC ...
B64C 35/007 (2013.01); B64C 3/26 (2013.01); B64C 3/34 (2013.01); B64C 25/54 (2013.01); B64C 35/001 (2013.01); B64C 35/006 (2013.01); B64C 35/008 (2013.01); B64D 37/16 (2013.01);
Abstract

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.


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