Mounting and adjustment device for an adjustment element of an aircraft, in particular for a control surface, wing tip or door of an aircraft

Abstract

The disclosure relates to a mounting and adjustment device for an adjustment element of an aircraft, for example for a control surface, pivotable wing tip or door of an aircraft, said mounting and adjustment device comprising a hydraulic cylinder arrangement for performing a linear movement, and a crank mechanism for converting the linear movement into a rotational movement in order to move the adjustment element accordingly. The hydraulic cylinder arrangement comprises a double-acting hydraulic cylinder.

Dependencies are inferred from the claim text.