| 摘要 |
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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