Rotary drive system linkage for use in aircraft wing, has attached unit drive displaceably mounted on multiple guides and movable during operation on pivotal axis such that shaft executes movement on drive hinge half

摘要

The linkage has a displaceable shaft (1) for a power-operated hinge to pivot a hinge. An attached unit drive i.e. servomotor, is displaceably mounted on multiple guides and movable during operation on a pivotal axis (14) such that the shaft executes a movement on a drive hinge half (12). A two-piece carriage slides on the guides with the unit drive and the shaft, where the guides form a frame together with a rod and a cage. The carriage is reinforced by a bridge. A bend part (10) of the bent shaft lies over the pivotal axis of the hinge.