Seaplane with retractable twin floats

Aeronautics and astronautics – Landing gear – Amphibian

Reexamination Certificate

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Reexamination Certificate

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06866224

ABSTRACT:
A twin float aircraft (1) which has a retractable float (4and5) for each side of a fuselage (3) providing buoyancy for the aircraft during take off and landing and reduced air resistance during flight with each of the floats (4and5) being articulated (12and13) to assist streamline alignment when retracted.

REFERENCES:
patent: 1639796 (1927-08-01), Congdon
patent: 2204457 (1940-06-01), Vogt
patent: 2207735 (1940-07-01), Herb
patent: 2285330 (1942-06-01), Dowden et al.
patent: 2320574 (1943-06-01), Dornier
patent: 2347841 (1944-05-01), Parker
patent: 2361293 (1944-10-01), Hugh
patent: 3790109 (1974-02-01), Fischer
patent: 6042052 (2000-03-01), Smith
patent: 6290174 (2001-09-01), Gioia
patent: 949988 (1956-09-01), None
patent: 154122 (1950-12-01), None
patent: 2083439 (1997-07-01), None
patent: 1200531 (1991-05-01), None
patent: WO-9505974 (1995-03-01), None

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