An aircraft door mounted in a fuselage in a reference frame X, Y, Z, having a casing, a door leaf and a support arm enabling the door leaf to be installed and the position thereof to be adjusted relative to the fuselage by a pair of fasteners. Each fastener (10, 40) includes a pivot (16, 46) rotatable about a common axis parallel to the axis Z, a base (13, 43) fastened to the casing (3), and a trolley (14, 44) movable on this base (13, 43), the base (13, 43) and the trolley (14, 44) of each fastener (10, 40) forming two translational adjustment links in directions parallel to the X and Y axes, these directions determining adjustment axes (11, 12; 41, 42) secant in a plane parallel to the plane XY.
PORTE D'AÉRONEF ÉQUIPÉE D'UN SYSTÈME DE RÉGLAGE EN POSITION ET PROCÉDÉ D'INSTALLATION D'UNE TELLE PORTE
AIRCRAFT DOOR EQUIPPED WITH A SYSTEM FOR ADJUSTMENT IN POSITION AND METHOD FOR INSTALLING SUCH A DOOR
FLUGZEUGTÜR MIT EINEM SYSTEM ZUR POSITIONSEINSTELLUNG UND VERFAHREN ZUR INSTALLATION SOLCH EINER TÜR
2025-01-01
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2022
|European Patent Office | 2022
|European Patent Office | 2025
|European Patent Office | 2019
|European Patent Office | 2021
|