Aircraft fuselage frame

An aircraft fuselage frame including a central element adapted to be located within the perimeter of the fuselage, and two lateral extensions projecting outside the perimeter of the fuselage from both sides of the central element that are a portion of a longitudinal structure of a lifting surface. T...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Goya Abaurrea, Pablo, Blanc, Jonathan, Bouchet, Eric, Pascual Fuertes, Angel, Linares Mendoza, Sandra, Folch Cortes, Diego, Martino Gonzalez, Esteban, Guillemaut, Julien, Colmagro, Jerome
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:An aircraft fuselage frame including a central element adapted to be located within the perimeter of the fuselage, and two lateral extensions projecting outside the perimeter of the fuselage from both sides of the central element that are a portion of a longitudinal structure of a lifting surface. The central element and the two lateral extensions are configured as an integrated piece.