This relates to a fuselage section comprising an inner surface with a non-circular contour and a pressure bulkhead comprising a non-circular outer edge. The non-circular outer edge of the pressure bulkhead is aligned with the non-circular contour of the inner surface of the fuselage section when the pressure bulkhead is attached to the fuselage section. This further relates to an aircraft with a fuselage section and a method for manufacturing a fuselage section.
PRESSURE BULKHEAD ADAPTED TO NON-CIRULAR FUSELAGE SECTION
2016-09-08
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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