The invention relates to a separation wall (10) for an aircraft cabin (1) with at least two cabin sections (2, 3) to be separated from each other, the cabin sections (2, 3) having an inner cabin contour (4), comprising a group of separate wall sections (20-24), including at least one static wall section (20), and at least one movable wall section (21-24). A separation wall (10) having the advantage of allowing for a passage through the aircraft cabin (1) with maximum space available to and minimal obstruction to the traversing passenger is characterised in that that the at least one static wall section (20) is connected to a first part of the inner cabin contour (4) of the cabin sections to stay in place during operation, and that the movable wall section is pivotably attached by a first pivotal connection (30) to the static wall section (20) and forming a foldable flap to set the separation wall into a folded position or into an unfolded position.
SEPARATION WALL FOR AN AIRCRAFT CABIN
TRENNWAND FÜR EINE FLUGZEUGKABINE
CLOISON DE SÉPARATION POUR UNE CABINE D'AVION
20.11.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Aircraft undercarriage cabin door separation mechanism
Europäisches Patentamt | 2025
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