Modular experimental gyroplane float system

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 25/54 (2006.01)

Patent

CA 2537352

A lightweight modular floatation system designed to attach securely to the existing tricycle landing gear of any experimental aircraft. The float system is made up of three elongated sections, which are connected together to form a tri-hull shaped bottom surface. Each modular section of the embodiment of the float system is designed with pre-molded cavities within which the left, right and nose wheel will fit in their respective locations and be secured to the float. A series of clamps will be employed to secure each wheel in place and subsequent release of same allows quick removal of float system. Integral pockets are established within the float's port and starboard sections to receive a telescopic support structure designed to provide a bipod support both fore and aft for the main rotor blade. As well pre-molded compartments are built into each float to facilitate storage items.

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