A pressure bulkhead for an aircraft includes a wall assembly 22. The wall assembly includes a first wall section 24 which extends in a direction nonparallel to a length of the aircraft. The wall assembly further includes a second wall section 26 secured to the first wall section wherein the second wall section includes a curved shape 32. The curved shape includes a convex portion 34 which extends further along the length of the aircraft in a direction toward the aft end of the aircraft than the first wall section. A method for assembling a pressure bulkhead is also provided.
PRESSURIZED BULKHEAD
DRUCKSCHOTT
CLOISON SOUS PRESSION
2020-05-20
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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