The disclosure herein relates to an aircraft fuselage stiffener including a heel, a flange, and a web connecting the heel and the flange, this stiffener comprising a folded sheet extending along the length of the heel, the web and the flange. In addition, to improve the mechanical behaviour of the stiffener, the folded sheet includes on the one hand a main portion extending along the length of the heel, the web and the flange, and on the other hand at least one folded-over portion forming a lining of the main portion over at least part of the web and/or the heel and/or the flange.
AIRCRAFT FUSELAGE STIFFENER FORMED FROM A SHEET FOLDED OVER ONTO ITSELF
2015-12-24
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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