| 摘要 |
<p>A control lever assembly (4) for a tilt-rotor aircraft (1), comprises at least one control lever (5) which is movable relative to a control lever support (6). The control lever support has a rotational position that varies in correspondence with the tilt of the rotor (2) of the aircraft. For example, the control lever support is movable by an actuator (9) between a first position, in the airplane mode of the aircraft, in which the control lever moves substantially horizontally and a second position, in the helicopter mode of the aircraft, in which the control lever moves substantially vertically.</p> |
