Door assemblies for aircraft interiors are described. Such door assemblies may comprise a door for opening and closing an aperture between zones of the aircraft interior and an interface configured to couple the door to the aircraft interior. A pressure-relief element may form at least a portion of the door wherein the pressure-relief element is retained by a magnetic force calibrated to permit release of the pressure-relief element upon presence of a predetermined pressure differential across the pressure-relief element. Components and mechanisms useful in reducing light bleed across doors for aircraft interiors are also disclosed.
DOOR ASSEMBLY FOR AIRCRAFT INTERIOR
TÜRANORDNUNG FÜR FLUGZEUGINNENRAUM
ENSEMBLE PORTE POUR L'INTÉRIEUR D'UN AVION
2019-04-17
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |