CPC B64D 45/0026 (2019.08) [B64C 1/1469 (2013.01); E05B 43/00 (2013.01); E05B 65/0085 (2013.01); E05B 83/00 (2013.01)] | 16 Claims |
1. A device for preventing access to an area of an aircraft, said device comprising:
a first vertical frame post designed for attachment to a structure of the aircraft;
a second vertical frame post designed for attachment to a structure of the aircraft;
a barrier element displaceably connected to the first frame post and including a latching element for detachable connection of the barrier element to the second frame post;
a delay unit arranged in the second frame post and including a spring-loaded damping cylinder displaceable into a damping position by a locking movement in opposition to a spring force, said delay unit designed to release the latching element after a time delay;
a closure body arranged for displacement in the second frame post in a longitudinal direction of the second frame post and Including an actuating element to move the closure body manually, said delay unit being connected to the closure body; and
a locking element acting between the closure body and the second frame post and designed to lock the closure body in a locking position.
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