An actuator system for an actuatable door, the actuator system comprising a stiff hinge arm, the stiff hinge arm being adapted to pivotally support the actuatable door and to be pivotally mounted to an associated door mounting structure, wherein an actuator with a pneumatically operable actuating rod is provided, the actuating rod comprising a coupling rod joint that is connected to at least one coupling rod, the at least one coupling rod being mounted to at least one torque lever that is pivotally mounted in at least one hinge of the stiff hinge arm by means of at least one torsion bolt, the at least one torsion bolt being drivingly connectable to the actuatable door. The invention is further related to an aircraft having such an actuatable door.
ACTUATOR SYSTEM FOR AN ACTUATABLE DOOR AND AN AIRCRAFT HAVING SUCH AN ACTUATABLE DOOR
2016-03-24
Patent
Electronic Resource
English
ACTUATOR SYSTEM FOR ACTUATABLE DOOR AND AIRCRAFT HAVING SUCH ACTUATABLE DOOR
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