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
2015-07-30
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / E06B Feste oder bewegliche Abschlüsse für Öffnungen in Bauwerken, Fahrzeugen, Zäunen oder ähnlichen Einfriedungen allgemein, z.B. Türen, Fenster, Läden, Tore , FIXED OR MOVABLE CLOSURES FOR OPENINGS IN BUILDINGS, VEHICLES, FENCES, OR LIKE ENCLOSURES, IN GENERAL, e.g. DOORS, WINDOWS, BLINDS, GATES |