PRESSURE FUSELAGE OF AN AIRCRAFT WITH A FUSELAGE SHELL AND A PRESSURE BULKHEAD DISPOSED THEREIN

摘要

The invention relates to a pressure bulkhead of an aircraft with a fuselage shell (2) and a pressure bulkhead (3) disposed therein preferably in the rear region (1) for forming a fuselage-internal pressure region (a), which pressure bulkhead (3) is attached on the edge in the interior of the fuselage shell (2), wherein the pressure bulkhead (3) has a lenticular cross-section and a sandwich construction that comprises a foam core (6) sandwiched between two opposing exterior shells (5a, 5b).