The disclosed embodiments relate to an aircraft having an interior door with a self-adjusting door jamb. The self-adjusting door jamb includes a door jamb configured to receive the interior door and a bias mechanism coupled to the door jamb and facilitating movement of the door jamb along an axis. Additionally, an angular translating mechanism coupled to the bias mechanism and facilitating angular displacement of the door jamb relative to the axis.
SELF-ADJUSTING DOOR JAMB FOR AN AIRCRAFT DOOR
2017-01-12
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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