Door assemblies for aircraft interiors are described. Such door assemblies may comprise a door (18) for opening and closing an aperture (20) between zones (12, 14) of the aircraft interior and an interface (40) configured to couple the door (18) to the aircraft interior. A pressure-relief element (36) may form at least a portion of the door (36) wherein the pressure-relief element (36) is retained by a magnetic force calibrated to permit release of the pressure-relief element (36) upon presence of a predetermined pressure differential across the pressure-relief element (36). Components and mechanisms useful in reducing light bleed across doors (18) for aircraft interiors are also disclosed.
Door assembly for aircraft interior
2015-04-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |