Patent ID: 9682765
Date: 2017-06-20
CPC Classifications: B64C,E06B

Claim:
1. An aircraft door, comprising: an outer shell with an exterior and an interior; a stiffening structure arranged on the interior of the outer shell; and at least one door seal arranged on the interior of the outer shell, which door seal is circumferential in an edge region, wherein in the edge region between the outer shell and the door seal at least one circumferential stiffening component is arranged that is connected to the stiffening structure, wherein the stiffening structure in a region in close proximity to the edge comprises an outwards-extending profile limb that is situated on the interior of the outer shell, and wherein each circumferential stiffening component comprises two limbs that are arranged parallel to each other and comprise a shoulder, wherein a first limb is fastened to the interior of the outer shell, and a second limb rests against the profile limb of the stiffening structure.