A door assembly (10), particularly for doors of passenger aircraft, includes a door frame, a door having a door body (1), a guiding rail (15) mounted at a side beam of the door frame and extending vertically along the door frame, and a linkage mechanism (17) coupled between the door frame and the guiding rail. The linkage mechanism is configured to retract and extend the guiding rail perpendicular to the vertical extension of the guiding rail along the door frame.
AIRCRAFT DOOR ASSEMBLY
FLUGZEUGTÜRANORDNUNG
ENSEMBLE PORTE D'AÉRONEF
2017-05-10
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |