| 摘要 |
An aircraft door in an aircraft fuselage (1), in particular a passenger door (2) for commercial aircraft, comprising a door leaf (3), a lever device (5, 7) for deflecting the weight of the door leaf (3) onto the aircraft fuselage (1), comprising two parallel control arms for parallel pivoting the door leaf (3) during opening and closing, in each case with a hinge (9; 13) on the door side and a hinge (11; 15) on the fuselage side, in each case comprising essentially vertical axes (27; 29), wherein the one hinge axis (29) on the fuselage side is arranged so as to be axially offset relative to the other hinge axis (27) on the fuselage side such that the connecting lines (6; 8) of the hinge axes, on the door side and on the fuselage side, of the respective control arm (5; 7) at no position of the door leaf (3) cover each other in a parallel manner during movement of said door leaf (3). |
