In order to reduce the time and the cost of manufacturing an aircraft fuselage, the subject matter disclosed herein provide an aircraft fuselage frame element comprising a core provided with at least one through-opening intended for the passing of a fuselage stiffener, and further comprising, associated with each opening, a tab for the fastening of the frame element onto the fuselage stiffener, with the tab being a single piece with the core and connected to the latter by a fold that delimits the opening.
Aircraft fuselage frame element integrating tabs for the fastening of stiffeners
2017-08-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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