A static aircraft seat privacy panel (102) may include a body (106). At least a portion of a surface of the body (106) may be shaped to at least partially conform with at least a portion of an aircraft seat. A lower edge (108) of the body may be configured to couple to a floor via a set of floor-mounted components (300). The set of floor-mounted components (300) may be within the floor separate from a set of seat tracks of an aircraft seat compliant with 16G force requirements for aviation transport. An upper edge (120) of the body may be configured to be offset a selected distance from a surface of one or more overhead structures (116) of the aircraft cabin when the body (106) is coupled to one or more structures positioned proximate to a ceiling of the aircraft cabin. The static aircraft seat privacy panel (102) may be compliant with 9G force requirements for aviation transport.
STATIC AIRCRAFT SEAT PRIVACY PANELS
STATISCHE SICHTSCHUTZPANEELE FÜR FLUGZEUGSITZE
PANNEAUX DE CONFIDENTIALITÉ STATIQUES POUR SIÈGE D'AVION
2025-05-14
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |