A door assembly (10), particularly for doors of passenger aircraft, includes a door frame, a guiding rail (15) mounted at a side edge of the door frame and extending vertically along the door frame, a door having a door body (1), and a latch lever (3). The latch lever (3) has a guiding member (6) attached to a first end portion of the latch lever (3) at a first revolute joint (R1) and a latch lever fulcrum (4) attached to a second end portion of the latch lever at a second revolute joint (R2). The guiding member (6) is received in the guiding rail (15) in a prismatic joint (P1), while the latch lever fulcrum (4) is fixedly connected to the door body (1).
AIRCRAFT DOOR ASSEMBLY
FLUGZEUGTÜRANORDNUNG
ENSEMBLE PORTE D'AÉRONEF
2017-05-10
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |