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
26.04.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Pressure bulkhead for an aircraft fuselage, and an aircraft comprising such a pressure bulkhead
Europäisches Patentamt | 2019
|PRESSURE BULKHEAD FOR AN AIRCRAFT FUSELAGE, AND AN AIRCRAFT COMPRISING SUCH A PRESSURE BULKHEAD
Europäisches Patentamt | 2016
|