Patent ID: 8702035

Claim:
A method of operating an apparatus for use on an aircraft, wherein the apparatus comprises a landing gear; an actuator arranged to move the landing gear between a first position and a second position, net load from external forces acting on the landing gear tending to drive the landing gear towards the first position, wherein the actuator comprises a threaded screw; a threaded nut; a main prime mover arranged to rotate the screw or the nut in order to impart relative linear motion between the screw and the nut; an emergency prime mover arranged to rotate the screw or the nut in order to impart relative linear motion between the screw and the nut; a normal control system configured to energize the main prime mover under normal operating conditions so that the main power mover applies torque to the screw or nut acting in opposition to the net load; and an emergency control system configured to energize the emergency prime mover under emergency operating conditions so that the emergency power mover applies torque to the screw or nut acting in the same sense as the net load thereby driving the landing gear to the first position, wherein the emergency control system is configured so that under the normal operating conditions the emergency prime mover is not energized by the emergency control system to apply torque to the screw or nut, the method comprising: applying a first torque to the nut or screw with the main prime mover when the landing gear moves from the second position to the first position under normal operating conditions, the first torque acting opposite to the net load to decelerate the landing gear; applying a second torque to the nut or screw with the main prime mover when the landing gear moves from the first position to the second position under normal operating conditions, the second torque acting opposite to the net load to accelerate the landing gear; and applying a third torque to the nut or screw with the emergency prime mover to drive the landing gear from the second position to the first position under emergency operating conditions in which the interface between the nut and the screw has become partially jammed to the extent that the frictional forces are greater than the net load and that the landing gear cannot be moved to the first position by operation of the net load alone, the third torque acting in the same direction as the net load.