Door panel assembly for an aircraft fuselage structure and method of making the fuselage structure

摘要

A door panel assembly for an aircraft fuselage structure (2) comprising a door panel (6) having an outer skin (12) and a rear frame structure (16) with at least one door frame (8), said door frame (8) having a door cutout (10) for receiving a door frame (8) Limited aircraft door, characterized in that a central portion (18) of the door cutout (10) between two not interrupted by the door panel fuselage (14c, 14d) of the fuselage structure (2) in the region of two adjacent, interrupted by the door panel (6) fuselage frames ( 14a, 14b) of the aircraft fuselage structure (2) is arranged, wherein the rear structure (16) integrally formed Spantanschlussprofile (20a-d) and stiffening elements (22a-d), and wherein the stiffening elements (22a-d) radiate on the door frame (8 ) and connected to at least one of the next two fuselage frames (14c, 14d) of the aircraft fuselage structure (2) which are not interrupted by the door panel.