Actuator unit for operation of vertical stabilizer of aircraft, has two parallel working actuators supported in bodies at coupling points, respectively, where support of actuators is formed in hinged pendulum arrangement

摘要

The unit (3) has two parallel working actuators (30, 32) e.g. piston cylinder units, supported in bodies (1, 2) at coupling points (20, 22), respectively. A support (10) of the actuators is formed at the one of the bodies and in a hinged pendulum arrangement (4). The pendulum arrangement is formed by a pendulum lever (40), where one end of the pendulum arrangement is pivotally hinged to one of the bodies and mounted at an end of the actuators. The actuators on the other body are mounted on the coupling points, where the coupling points are located on two opposite sides of a pivot axis (X).