A connecting mechanism between an aircraft door and a structure of the aircraft, a related aircraft and method are provided. The connecting mechanism includes an arm intended to be hinged on to the structure, a rotating connection between the door and the arm. The rotating connection may be disengaged from a connection configuration for connecting the door with the arm in an open position of the door, into an uncoupling configuration for uncoupling of the door from the arm, in a closed door position of the door.
MÉCANISME DE LIAISON ENTRE UNE PORTE D'AÉRONEF ET UNE STRUCTURE DE L'AÉRONEF, AÉRONEF ET PROCÉDÉ ASSOCIÉS
CONNECTING MECHANISM BETWEEN AN AIRCRAFT DOOR AND A STRUCTURE OF THE AIRCRAFT, RELATED AIRCRAFT AND METHOD
VERBINDUNGSMECHANISMUS ZWISCHEN EINER LUFTFAHRZEUGTÜR UND EINER STRUKTUR DES LUFTFAHRZEUGS, ENTSPRECHENDES LUFTFAHRZEUG UND VERFAHREN
2020-04-08
Patent
Electronic Resource
French
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