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SPACE PATENTS BY
Aerospace Assignees
Aerospace Inventors
Time Lines

Wingtip and sponson interaction on an amphibious aircraft

Invented by: Jon Karkow
Tehachapi, CA

Krik Hawkins
Los Angeles, CA

Matthew Gionta
Tehachapi, CA

Steen Strand
Los Angeles, CA

Originally Assigned to: Icon Aircraft, Inc.
Los Angeles, CA
[Now assigned to . . .]

Issued:2012-10-16
Filed:2012-02-13
Application No:13372150
Examined by:Collins; Timothy D

A system for enhanced lateral stability of an amphibious aircraft includes a buoyancy system laterally displaced from opposite sides of the fuselage of the aircraft and wingtip system having a hydrodynamic planing surface associated with each wingtip. The hydrodynamic planing surface on each wingtip prevents the submersion of an associated buoyancy structure. By supplementing the lateral stability of the buoyancy structures using hydrodynamic planing surfaces, the combined lateral width of the fuselage and buoyancy structures can be reduced without detrimentally impacting operational performance. This reduced lateral width enables the amphibious aircraft to be configured for storage and transportation on a trailer or shipping container.

[pdf] U.S. Pat. No. 8,286,912

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This information is part of a study by Oasis Global, Inc. of all space inventions filed at the United States Patent and Trademark Office, and is provided for informational purposes only. It is not an endorsement of any particular assignee, inventor or invention. Although Peter A. Koziol represents inventors and assignees of space inventions he does not represent all of the inventors and assignees listed. The prosecuting attorney agent or firm for each patent is identified by the United States Patent and Trademark Office in the patent specfication, which can be viewed by clicking on the patent image or downloading the patent document. For more information regarding Mr. Koziol's background and experience, or to learn more about space inventions, please contact Mr. Koziol.

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