An aircraft cabin partition system may include at least a first partition (112) with a partition cut-out and a first flange (202) with a first flange cut-out. The aircraft cabin partition system may include a first coupling assembly (200) configured to be inserted within the first flange cut-out, configured to be inserted within an opening of a seat rail (106) within a floor of an aircraft cabin, and configured to couple the at least the first partition to the seat rail when engaged. The aircraft cabin partition system may include at least a second partition with a second flange with a second flange cut-out. The aircraft cabin partition system may include a second coupling assembly configured to be inserted within the partition cut-out, configured to be inserted within the second flange cut-out, and configured to couple the at least the second partition to the at least the first partition when engaged.
AIRCRAFT CABIN PARTITION SYSTEM
TRENNWANDSYSTEM FÜR FLUGZEUGKABINEN
SYSTÈME DE SÉPARATION DE CABINE D'AÉRONEF
2023-11-15
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Partition element for an aircraft cabin and cabin arrangement
European Patent Office | 2015
|PARTITION ELEMENT FOR AN AIRCRAFT CABIN AND CABIN ARRANGEMENT
European Patent Office | 2015
|Partition element for an aircraft cabin and cabin arrangement
European Patent Office | 2017
|