AIRCRAFT FUSELAGE FRAME

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: COLMAGRO JEROME, MARTINO GONZALEZ ESTEBAN, GUILLEMAUT JULIEN, BOUCHET ERIC, FOLCH CORTES DIEGO, GOYA ABAURREA PABLO, PASCUAL FUERTES ANGEL, LINARES MENDOZA SANDRA, BLANC JONATHAN
Format: Patent
Sprache:eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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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.