A pressure bulkhead (12) of an aircraft (10) and an associated method of installation are disclosed. The pressure bulkhead (12) comprises an upper bulkhead portion (12U) sealingly separating a first pressurized compartment (22A) disposed above a floor (30) of the aircraft (10) from an unpressurized zone (24) of the aircraft, and a lower bulkhead portion (12L) sealingly separating a second pressurized compartment (22B) disposed below the floor (30) of the aircraft (10) from the unpressurized zone (24) of the aircraft (10). The method of installation can comprise installing the lower bulkhead portion (12L) before the upper bulkhead portion (12U) in order to facilitate the installation of other components.
PRESSURE BULKHEAD AND METHOD OF INSTALLATION
DRUCKSCHOTT UND VERFAHREN ZUR INSTALLATION
CLOISON DE PRESSURISATION ET PROCÉDÉ D'INSTALLATION
22.01.2020
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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