Control lever assembly for a tilt-rotor aircraft
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United States of America Patent
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-
Sep 25, 2012
Grant Date -
Nov 19, 2009
app pub date -
May 15, 2009
filing date -
May 15, 2008
priority date (Note) -
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Abstract
A control lever assembly for a tilt-rotor aircraft, comprises at least one control lever which is movable relative to a control lever support. The control lever support has a rotational position that varies in correspondence with the tilt of the rotor of the aircraft. For example, the control lever support is movable by an actuator 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.
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