Aircraft fuselage stiffener formed from a sheet folded over onto itself

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 behavior of the st...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Lieven Patrick, Rodrigo Philippe, Mialhe Christophe
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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