Patent ID: 9630700
Date: 2017-04-25
CPC Classifications: B64C

Claim:
1. A device for opening an aircraft door provided on an aircraft fuselage, said device comprising: a support arm that is arranged in an articulated manner between the aircraft fuselage and the aircraft door; an opening system for opening the aircraft door by lifting the aircraft door from a closed position into an intermediate position and transferring the aircraft door from the intermediate position into an open position; a support arm cover substantially entirely covering the support arm in the closed position of the aircraft door, wherein the support arm cover has a cover element immovably arranged on the support arm, and a flap element which, when the aircraft door is opened, swivels between a state in which the flap element is substantially flush with the cover element, and a state in which the flap element overlaps the cover element; and a guide system for guiding the flap element when the aircraft door is opened, wherein the guide system has at least one guide arm, one end of which is joined in an articulated manner to the support arm, and the other end of which is joined to at least one guide element, wherein the guide element is guided along a guide track on an inner side of the flap element, when the aircraft door is opened.