Device for limiting deflection of door arranged in fuselage cabin of aircraft, particularly hatch or cargo gate, has retaining element arranged preferably in area of door jamb or in area of door sheet edge
摘要
<p>The device has a retaining element (5) arranged preferably in the area of a door jamb (4) or in the area of a door sheet edge (7). The retaining element is brought into engagement with a counter bearing (6) arranged in the area of the door sheet edge or the door jamb in the case of a sufficient differential pressure between an inner pressure (p-i) existing in a fuselage cabin (3) and the outer air pressure p-a dominating outside the fuselage cabin.</p>
