RACCORDEMENT DES CADRES DE RAIDISSAGE ENTRE UN FUSELAGE D'AERONEF ET UN CAISSON DE VOILURE

RACCORDEMENT DES CADRES DE RAIDISSAGE ENTRE UN FUSELAGE D'AERONEF ET UN CAISSON DE VOILURE

The structure has a rib (3) extending a fuselage and provided for a wing box. An upper panel (5) of the box is connected to the fuselage and the rib. Stiffening frames (14) of the fuselage are respectively extended in transverse sections of an aircraft. The frames extend continuously via notches in...

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Bibliographische Detailangaben
Hauptverfasser: COLMAGRO JEROME, GUILLEMAUT JULIEN, LOYANT FRANCOIS, DURAND JEAN MARC, CABANAC JEAN PIERRE, FOURNIE LUDOVIC
Format: Patent
Sprache:fre
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The structure has a rib (3) extending a fuselage and provided for a wing box. An upper panel (5) of the box is connected to the fuselage and the rib. Stiffening frames (14) of the fuselage are respectively extended in transverse sections of an aircraft. The frames extend continuously via notches in the panel and include lower ends that stiffen the rib. The notches are oriented toward the sections to allow passage of cores (16) of the frames. Notch heels are oriented in an axial direction of the aircraft to free passage for base plates (18) of the frames on the fuselage and the rib.