High performance amphibious airplane

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 4691881
SERIAL NO

06785470

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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An amphibious executive or business airplane, also having military application, possesses sponsons integrated with the airplane fuselage. The trailing end of the sponsons end in a sharp edge, thus eliminating the need for a hull or float step or venting. A channel is formed by the sponsons and the underside of the fuselage, which channel has a constant cross-section and produces a surface lift effect facilitating take-off and landing. A pair of keels beginning substantially aft of the center of gravity of the airplane provide directional stability on the water. The aircraft is preferably jet powered with the inlet of the engines disposed above the sponsons to eliminate water intake. Variable geometry wings of telescoping design maximize aerodynamic performance on take-off and landing and during the high altitude, high speed cruise regime of the flight.

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Gioia, G Leonard 255 Fortenberry Rd., A, Merritt Island, FL 32952 2 46

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