| 摘要 |
The invention relates to a method for actuating at least one regulating flap on each wing of an aircraft, which is actuated by at least two flap coupling devices (11, 12, 13, 14), each having one servo drive device (30), wherein at least one braking device per regulating flap is disposed at a servo drive device (30). By actuating the braking device, an adjusted state of the respective servo drive device (30) can be locked in position. The method comprises the following steps: actuating each braking device of a regulating flap individually; subsequently actuating the servo drive device by means of the drive motor; once the adjusted state of the regulating flap has been changed by a specified amount, the actuation of said regulating flap is concluded. The invention also relates to a system for implementing the method. |
