An aircraft door including a door leaf, a door frame, a support arm assembly, and first and second connecting elements. The first connecting element connects the support arm assembly with the door leaf and includes a first adjustment unit that is adapted for adjusting the position of the door leaf relative to the door frame along a first axis (x-axis). The second connecting element connects the support arm assembly with the door frame and includes a second adjustment unit that is adapted for adjusting the position of the door leaf relative to the door frame along a second axis (z-axis) that is perpendicular to the first axis (x-axis).
AIRCRAFT DOOR WITH AN ADJUSTMENT SYSTEM FOR ADJUSTING THE POSITION OF THE DOOR LEAF RELATIVE TO THE DOOR FRAME
2024-06-20
Patent
Electronic Resource
English
European Patent Office | 2024
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