B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/14 (2006.01) E05D 3/06 (2006.01) E05D 15/34 (2006.01)
Patent
CA 2368542
Articulation device for an aircraft door panel and an aircraft door integrating such a device. An aircraft door panel is articulated on the jamb by a device (20) that defines an approximately elliptical opening and closing trajectory, in which the major axis is approximately perpendicular to the panel. The device (20) comprises in particular a main arm (30), a secondary arm (32) articulated at the end of the main arm and a control lever (34) connecting the secondary arm (32) to the jamb, by articulation axes (A4, A5) close to the articulation axes of the main arm (30) on the jamb and the secondary arm (32) on the main arm. This arrangement makes it possible to fit a more voluminous emergency exit chute into the door panel.
Un dispositif de rotation destiné au panneau de porte d'un aéronef et la porte d'un aéronef intégrant ce dispositif. Le panneau de porte d'un aéronef est articulé dans son embrasure à l'aide d'un dispositif (20) qui définit une trajectoire d'ouverture et de fermeture quasi elliptique et dans lequel l'axe principal est quasi perpendiculaire au panneau. Le dispositif (20) comprend entre autres un bras principal (30), un bras auxiliaire (32) articulé situé à l'extrémité du bras principal (30) et un levier de commande (34) reliant le bras auxiliaire (32) à l'huisserie de la porte à l'aide d'axes de rotation (A4, A5) situés à proximité des axes de rotation du bras principal (30) sur l'huisserie et au bras principal (30). Cette configuration permet d'installer une chute de sortie d'urgence de plus grande taille.
Dazet Francis
Rouyre Francois
Airbus France
Airbus Operations Sas
Goudreau Gage Dubuc
LandOfFree
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