A door assembly for an aircraft includes a partition panel disposed laterally within a fuselage of the aircraft and a descender panel moveably secured to a lower end of the partition panel for selectively closing an aisle opening defined below the partition panel. The door assembly further includes a handle disposed on the partition panel that is operatively connected to the descender panel through a link mechanism such that rotation of the handle is translated into movement of the descender panel to move the descender panel between a retracted position and a deployed position.
AIRCRAFT DOOR MECHANISM WITH HANDLE ACTUATED DESCENDER
FLUGZEUGTÜRMECHANISMUS MIT EINEM DURCH EINEN GRIFF ZU BETÄTIGENDEN ABSENKBAREN PANEL
MÉCANISME DE PORTE D'AÉRONEF AYANT UN PANNEAU ABAISSABLE ACTIONNÉ PAR UN MANCHE
2018-05-30
Patent
Electronic Resource
English