The invention provides a pressure bulkhead (1) for an aircraft comprising a pressurized zone, the pressure bulkhead (1) made of a composite material and comprising a front panel (2), which is intended to be faced towards the pressurized zone; and a rear panel (3), which is substantially parallel to the front panel (2) and is intended to be located farther from the pressurized zone than the front panel (2). The pressure bulkhead (1) further comprises a plurality of longerons (41) located between the front panel (2) and the rear panel (3), each one of them being attached to the front panel (2) and to the rear panel (3); and a plurality of stiffeners (43) some of them being attached to the front panel (2) and the rest of them being attached to the rear panel (3).
PRESSURE BULKHEAD FOR AN AIRCRAFT
DRUCKSCHOTT FÜR EIN FLUGZEUG
CLOISON DE PRESSURISATION POUR UN AVION
2019-12-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Pressure bulkhead for an aircraft fuselage, and an aircraft comprising such a pressure bulkhead
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