DOOR ASSEMBLY FOR AIRCRAFT INTERIOR

摘要

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.

主权项

1. A door assembly for an aircraft interior, the door assembly comprising:
a door for opening and closing an aperture between zones of the aircraft interior, a pressure-relief element forming at least a portion of the door, the pressure-relief element being 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; and an interface configured to couple the door to the aircraft interior.