Patent attributes
The invention relates to an aircraft seat comprising an adjusting device, the aircraft seat comprising at least one adjustable seat element. The seat element has an adjustable state and a locked state, the seat element being adjustable by means of manual force application and/or force application by a spring element and/or force application due to the weight of parts of the aircraft seat only in the adjustable state. The adjusting device comprises at least one control element and at least one locking element, the locking element being movable by means of the control element between a locking position in which the seat element is locked, and a neutral position in which the seat element is adjustable. The control element is an electronic and/or electric switch, and the locking element can be moved between the locking position and the neutral position by means of an electrically operated actuator which can be actuated by means of signals from the switch.
