| 摘要 |
The invention is related to an actuator system 1 for an actuatable door, said actuator system 1 comprising a stiff hinge arm 2, said stiff hinge arm 2 being adapted to pivotally support said actuatable door and to be pivotally mounted to an associated door mounting structure, wherein an actuator 7 with a pneumatically operatable actuating rod 8 is provided, said actuating rod 8 comprising a coupling rod joint 12a that is connected to at least one coupling rod 12, said at least one coupling rod 12 being mounted to at least one torque lever 14a, 14b that is pivotally mounted in at least one hinge 16a, 16b of said stiff hinge arm 2 by means of at least one torsion bolt 13a, 13b, said at least one torsion bolt being drivingly connectable to said actuatable door. The invention is further related to an aircraft having such an actuatable door. |
