Seaplane with retractable twin floats

Details Seaplane with retractable twin floats Seaplane with retractable twin floats

B - Operations, Transporting

64

C

B64C 35/00 (2006.01) B64C 25/12 (2006.01) B64C 25/16 (2006.01) B64C 25/54 (2006.01) B64C 25/66 (2006.01) B64C 37/00 (2006.01)

Patent

CA 2420106

A twin float aircraft (1) which has a retractable float (4 and 5) 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 (4 and 5) being articulated (12 and 13) to assist streamline alignment when retracted.

L'invention concerne un hydravion à deux flotteurs (1) comportant un flotteur rétractable (4, 5) sur chaque côté de son fuselage (3). Ces flotteurs confèrent à cet hydravion une flottabilité positive pendant le décollage et l'atterrissage, et permettent de réduire la résistance à l'air en cours de vol, lesdits flotteurs (4, 5) étant tous deux articulés (12, 13) de façon à s'aligner aérodynamiquement lors d'une rétraction.

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