Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
DOOR ARRANGEMENT FOR THE INTERIOR OF AN AIRCRAFT AND AIRCRAFT COMPRISING SUCH A DOOR ARRANGEMENT
The invention relates to a door arrangement for the interior of an aircraft and to an aircraft comprising such a door arrangement. The door arrangement (1) comprises a frame portion and a door blade (2) hinged to the frame portion to be pivotable about a pivot axis (4) between a closed position, in which the door blade (2) closes a door opening (5) defined by the frame portion, and an open position, in which the door blade (2) is positioned to allow access through the door opening (5). The door arrangement (1) further comprises a lever arm (9), and an actuator (6) mounted to the frame portion and operable to selectively move the door blade (2) between the open position and the closed position via the lever arm (9) engaging the door blade (2) and the actuator (6). The actuator (6) is movable into a first actuator position, in which the lever arm (9) is in a first lever arm position and the door blade (2) is in the open position, and into a second actuator position, in which the lever arm (9) is in a second lever arm position and the door blade (2) is in the closed position. The actuator (6) is movable into the second actuator position such that the door blade (2) is able to move from the closed position towards the open position independent of the actuator (6) while the actuator (6) remains in the second actuator position.
DOOR ARRANGEMENT FOR THE INTERIOR OF AN AIRCRAFT AND AIRCRAFT COMPRISING SUCH A DOOR ARRANGEMENT
The invention relates to a door arrangement for the interior of an aircraft and to an aircraft comprising such a door arrangement. The door arrangement (1) comprises a frame portion and a door blade (2) hinged to the frame portion to be pivotable about a pivot axis (4) between a closed position, in which the door blade (2) closes a door opening (5) defined by the frame portion, and an open position, in which the door blade (2) is positioned to allow access through the door opening (5). The door arrangement (1) further comprises a lever arm (9), and an actuator (6) mounted to the frame portion and operable to selectively move the door blade (2) between the open position and the closed position via the lever arm (9) engaging the door blade (2) and the actuator (6). The actuator (6) is movable into a first actuator position, in which the lever arm (9) is in a first lever arm position and the door blade (2) is in the open position, and into a second actuator position, in which the lever arm (9) is in a second lever arm position and the door blade (2) is in the closed position. The actuator (6) is movable into the second actuator position such that the door blade (2) is able to move from the closed position towards the open position independent of the actuator (6) while the actuator (6) remains in the second actuator position.
DOOR ARRANGEMENT FOR THE INTERIOR OF AN AIRCRAFT AND AIRCRAFT COMPRISING SUCH A DOOR ARRANGEMENT
TÜRANORDNUNG FÜR DEN INNENRAUM EINES FLUGZEUGS UND FLUGZEUG MIT SOLCH EINER TÜRANORDNUNG
SYSTÈME DE PORTE POUR L'INTÉRIEUR D'UN AÉRONEF ET AÉRONEF COMPORTANT UN TEL SYSTÈME
BUTTELMANN MAIK (Autor:in)
11.04.2018
Patent
Elektronische Ressource
Englisch
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