Convertiplane

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 27/28 (2006.01) B64C 29/00 (2006.01) B64D 35/08 (2006.01)

Patent

CA 2327081

A convertiplane having a wing in turn having two half-wings, each defined by a fixed portion adjacent to the fuselage, and by a movable portion rotating, with respect to the fixed portion, about a beam element extending the full length of the wing; the beam element supports, integrally, rotors located at respective ends of the wing, and engines connected to the rotors by a transmission, and is rotated about a respective axis by actuators to change the position of the rotors from a vertical-axis position wherein the convertiplane operates in helicopter mode, to a horizontal-axis position wherein the convertiplane operates in airplane mode.

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