| 摘要 |
The invention relates to a device (1) for opening an aircraft door (2) provided in an aircraft fuselage (4), said device comprising: a support arm (3) that can be arranged in an articulated manner between the aircraft fuselage (4) and the aircraft door (2); an opening system (5) for opening the aircraft door (2) by lifting the aircraft door (2) from a closed position into an intermediate position and swivelling the aircraft door (2) from the intermediate position into an open position; a support arm cover (10) substantially entirely covering the support arm (3) in the closed position of the aircraft door (2), wherein the support arm cover (10) has a cover element (11) immovably arranged on the support arm (3), and a flap element (12) which, when the aircraft door (2) is opened, can swivel between a state in which said flap element is substantially flush with the cover element (11), and a state in which said flap element overlaps the cover element (11); and a guide system (13) for guiding the flap element (12) when the aircraft door (2) is opened, wherein the guide system (13) has at least one guide arm (14), one end of which is joined in an articulated manner to the support arm (3), and the other end of which is joined to at least one guide element (17), which guide element can be guided along a guide track (18) on the inner side of the flap element (12), when the aircraft door (2) is opened. |
