A pressurized aircraft fuselage includes a pressure bulkhead installed on a fuselage structure, which forms a barrier between an internal pressurized cabin area and an outside area. The edge of the pressure bulkhead is circumferentially attached to the fuselage structure. In particular, at least one clamping element is arranged inside a mounting bracket having an open trapezoidal-shaped channel formed by a base section of the mounting bracket and non-parallel sides of the mounting bracket. An edge of the pressure bulkhead is inserted in the trapezoidal shaped mounting bracket, in order to form a clamping connection for the pressure bulkhead towards the fuselage structure.
Pressurized aircraft fuselage comprising a pressure bulkhead movably fixed to the fuselage
27.12.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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