Aircraft fuselage section

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

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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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Beschreibung
Zusammenfassung: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 longitudinal structure of a lifting surface (1). Additionally the central element (3) and the two lateral extensions (4) being configured as an integrated piece.