The present invention provides a rear pressure bulkhead comprising a dome-shaped structure (1.1), and a set of built-in extension components (1.2) ("petals") homogeneously distributed along the periphery of said dome-shaped structure (1.1), so that the dome-shaped structure (1.1) is secured to a frame of the aircraft (2.1), whilst the extension components (1.2) are secured to longitudinal structures (3) of the aircraft. The invention further provides an aircraft rear fuselage comprising such rear pressure bulkhead so that the available cabin space, i.e. pressurized space, can be extended without enlarging the fuselage.
PRESSURE BULKHEAD
DRUCKSCHOTT
CLOISON DE PRESSURISATION
2021-12-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |