| 摘要 |
The door has a panel (14) formed of two parts (14a, 14b), where the part (14a) is coupled to a structure of an aircraft by a pivoting axle (20). An actuator (22) is interposed between the structure and the panel. A support plate is articulated inside the part (14b) at its edge parallel to an articulation axle. The plate is coupled to a kinematic control unit (26) to automatically open the door, when preset force is applied to the plate.
|
