A pressurized aircraft fuselage, comprising a pressure bulkhead (1) installed on a fuselage structure (2), which forms a barrier between an internal pressurized cabin area (3) and an outside area (4), wherein the edge of the pressure bulkhead (1) is circumferentially attached to the fuselage structure (2) by fastening means, wherein the fastening means comprise a pair of ring-shaped attachment frames (5a;5b) made of an open or hollow profile, which are disposed at each side of the pressure bulkhead (1) respectively, in order to form a clamping connection for the pressure bulkhead towards the fuselage structure (2).
A pressurized airplane fuselage, comprising a pressure bulkhead
Druckfester Flugzeugrumpf mit einem Druckschott
Fuselage d'avion sous pression comprenant une cloison de pressurisation
2020-11-04
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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