The present technology relates to an aircraft door 200. The aircraft door 200 includes a door leaf 210, a door frame 610, a support arm assembly 220, and first and second connecting elements 380, 680. The first connecting element 380 connects the support arm assembly 220 with the door leaf 210 and includes a first adjustment unit 300 that is adapted for adjusting the position of the door leaf 210 relative to the door frame 610 along a first axis (x-axis). The second connecting element 680 connects the support arm assembly 220 with the door frame and includes a second adjustment unit 600 that is adapted for adjusting the position of the door leaf 210 relative to the door frame 610 along a second axis (z-axis) that is perpendicular to the first axis (x-axis).
AN AIRCRAFT DOOR WITH AN ADJUSTMENT SYSTEM FOR ADJUSTING THE POSITION OF THE DOOR LEAF RELATIVE TO THE DOOR FRAME
FLUGZEUGTÜR MIT EINER VERSTELLVORRICHTUNG ZUR VERSTELLUNG DER POSITION DES TÜRBLATTS IN BEZUG AUF DEN TÜRRAHMENN
PORTE D'AÉRONEF AVEC UN SYSTÈME DE RÉGLAGE POUR RÉGLER LA POSITION DU BATTANT DE PORTE PAR RAPPORT AU CADRE DE PORTE
2024-06-26
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Europäisches Patentamt | 2024
|DOOR LEAF FRAME, DOOR LEAF, AND METHOD OF MANUFACTURING THE DOOR LEAF FRAME
Europäisches Patentamt | 2021
|DOOR LEAF FRAME, DOOR LEAF, AND METHOD OF MANUFACTURING THE DOOR LEAF FRAME
Europäisches Patentamt | 2021
|DOOR LEAF FRAME, DOOR LEAF, AND METHOD OF MANUFACTURING THE DOOR LEAF FRAME
Europäisches Patentamt | 2021
|FRAME BODY FOR DOOR LEAF, DOOR LEAF, AND METHOD FOR MANUFACTURING FRAME BODY FOR DOOR LEAF
Europäisches Patentamt | 2021
|