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A door assembly, particularly for doors of passenger aircraft, includes a door frame, a door having a door body hingedly installed in the door frame, at least one hooking pintle (4) attached to the door frame or an edge of the door body extending along a pintle axis, and at least one door latch (2) connected to an edge of the door body or the door frame, respectively, the door latch having a substantially C-shaped latch body (2a) configured to rotate around an axis parallel to the pintle axis of the hooking pintle (4). The door assembly further includes a bistable latch and hook mechanism configured to catch the door latch (2) in hooking engagement with the hooking pintle (4) and to retain the door latch (2) in a direction perpendicular to the door body in an overcenter position.
A door assembly, particularly for doors of passenger aircraft, includes a door frame, a door having a door body hingedly installed in the door frame, at least one hooking pintle (4) attached to the door frame or an edge of the door body extending along a pintle axis, and at least one door latch (2) connected to an edge of the door body or the door frame, respectively, the door latch having a substantially C-shaped latch body (2a) configured to rotate around an axis parallel to the pintle axis of the hooking pintle (4). The door assembly further includes a bistable latch and hook mechanism configured to catch the door latch (2) in hooking engagement with the hooking pintle (4) and to retain the door latch (2) in a direction perpendicular to the door body in an overcenter position.
AIRCRAFT DOOR ASSEMBLY
FLUGZEUGTÜRANORDNUNG
ENSEMBLE PORTE D'AÉRONEF
ERBEN JOHANN KONRAD (author)
2018-06-06
Patent
Electronic Resource
English