There is disclosed an emergency door positionable in an exit opening of an aircraft. The door has door supports mountable to the lower wall and each having a pivot point. A first pivot axis is defined between the pivot points. A block is mountable to the lower wall and is offset from a center of the lower wall. A door body is mountable within the opening to the door supporting structure and pivotally mountable to the door supports. The door body is pivotable about the first pivot axis from an initial position in which the door body is within the opening, until the door body is disengaged from the door supports. A bottom portion of the door body abuts against the block to define a removal pivot point. The door body is pivotable about the removal pivot point to remove the door body from the exit opening.
AIRCRAFT DOOR AND METHOD OF OPERATING THE SAME
FLUGZEUGTÜR UND VERFAHREN ZUM BETRIEB DAVON
PORTE D'AÉRONEF ET PROCÉDÉ DE FONCTIONNEMENT ASSOCIÉ
01.04.2020
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT EMERGENCY DOOR AND METHOD OF OPERATING THE SAME
Europäisches Patentamt | 2020
|AIRCRAFT EMERGENCY DOOR AND METHOD OF OPERATING THE SAME
Europäisches Patentamt | 2020
|