A pressure bulkhead of an aircraft and an associated method of installation are disclosed. The pressure bulkhead comprises an upper bulkhead portion sealingly separating a first pressurized compartment disposed above a floor of the aircraft from an unpressurized zone of the aircraft, and a lower bulkhead portion sealingly separating a second pressurized compartment disposed below the floor of the aircraft from the unpressurized zone of the aircraft. The method of installation can comprise installing the lower bulkhead portion before the upper bulkhead portion in order to facilitate the installation of other components.
PRESSURE BULKHEAD AND METHOD OF INSTALLATION
23.01.2020
Patent
Elektronische Ressource
Englisch
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