Pressurized cabin of an aircraft, with a fuselage shell and a arranged therein, a pressure bulkhead

摘要

The present invention relates to a pressurized cabin of an aircraft, with a fuselage shell (2) and a preferably in the rear area (1) a pressure bulkhead (3) arranged for the formation of a hull internal pressure range (a), which at the edge on the inside on the fuselage shell (2) is mounted, wherein the pressure bulkhead (3) has a lens-shaped cross section and a sandwich structure having a between two mutually opposite outer shells (5a, 5b) enclosed foam core (6) comprises.