A device for attaching an aircraft engine to a pylon secured to the aircraft, the attachment device comprising a beam secured to the pylon and a first clevis mount comprising two cheeks connected to one another by a first clevis pin. A second clevis mount is secured to the engine and comprises two cheeks connected to one another by a second clevis pin. A shackle is rotatably connected to the first and second pins by first and second spherical joints. The attachment device further comprises at least one pair of washers positioned around one of the pins, one washer on each side of the shackle, and separating the shackle from the cheeks of the clevis mount bearing the one of the pins. The shackle, in its extreme positions of rotation about the one of the pins passing through the two spherical joints, coming into contact with the washers.
DISPOSITIF DE FIXATION D'UN MOTEUR D'AÉRONEF, ET AÉRONEF CORRESPONDANT
DEVICE FOR ATTACHING AN AIRCRAFT ENGINE, AND CORRESPONDING AIRCRAFT
BEFESTIGUNGSVORRICHTUNG FÜR EINEN MOTOR EINES LUFTFAHRZEUGS, UND ENTSPRECHENDES LUFTFAHRZEUG
2017-07-26
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
DISPOSITIF DE FIXATION D'UN MOTEUR D'AERONEF, ET AERONEF CORRESPONDANT
Europäisches Patentamt | 2016
|DISPOSITIF DE COMMANDE D'UN AERONEF, AERONEF CORRESPONDANT ET METHODE DE PILOTAGE D'UN AERONEF
Europäisches Patentamt | 2018
|Europäisches Patentamt | 2023
|