| 摘要 |
An aircraft seat (3) comprising – a first and a second seat element (1, 2), wherein – the second seat element (2) is mounted adjustably in relation to the first seat element (1), wherein – a spring element (4) moving the second seat element (2) in relation to the first seat element (1) is provided, wherein – the force acting on the second seat element (2) by means of the spring element (4) can be released by means of an actuator (5), and therefore, in a first switching position of the actuator (5), the spring element (4) is deactivated, and, in a second switching position of the actuator (5), the spring element (4) is activated, wherein – a force-limiting element (6) is provided with which the force acting on the second seat element (2) by means of the spring element (4) can be limited to a predefined value, and therefore intermediate states between the first and the second switching position can also be set. |
