Aircraft fuselage section

The invention refers to an aircraft fuselage frame (2) that comprises a central element (3) adapted to be located within the perimeter of the fuselage, and two lateral extensions (4) projecting outside the perimeter of the fuselage from both sides of the central element (3) that are a portion of a l...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Goya Abaurrea, Pablo, Gillemaut, Julien, Blanc, Jonathan, Bouchet, Eric, Colmagro, Jérôme, Liñares Mendoza, Sandra, Folch Cortés, Diego, Martino González, Esteban, Pascual Fuertes, Ángel
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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