PRESSURIZED FUSELAGE OF AN AIRCRAFT, WITH A FUSELAGE STRUCTURE AND A PRESSURE BULKHEAD SPECIALLY MOUNTED THEREIN

摘要

The invention relates to a pressurized fuselage of an aircraft, with a fuselage structure (2) and a pressure bulkhead (3) mounted therein for forming a fuselage-internal pressure region (a), which pressure bulkhead (3) is attached on the edge region, by way of mounting means, to the inside of the fuselage structure (2), wherein the mounting means comprise at least one pivoting socket arrangement (5), arranged on the edge side (4) of the pressure bulkhead (3), which edge side (4) faces away from the pressure region (a), and interacting with the fuselage structure (2), as well as a supporting frame element (7), arranged on the opposite edge side (6) and supporting itself on the fuselage structure (2).