A pressure bulkhead for the pressure-tight axial closure of a pressurized fuselage of an aircraft or spacecraft that is capable of being put under internal pressure includes dome segments, having an integrated reinforcement, in particular a peripheral reinforcement, which are in each case made integrally from a fiber-reinforced thermoplastic plastics material, and are joined to one another so as to form a pressure dome.
PRESSURE BULKHEAD FOR AN AIRCRAFT
2019-09-05
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Pressure bulkhead for an aircraft fuselage, and an aircraft comprising such a pressure bulkhead
European Patent Office | 2019
|PRESSURE BULKHEAD FOR AN AIRCRAFT FUSELAGE, AND AN AIRCRAFT COMPRISING SUCH A PRESSURE BULKHEAD
European Patent Office | 2016
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