A device for attaching an aircraft engine including a thrust force take-up device that includes a main fitting to be fixed to an engine mounting beam fixed to a box structure, an additional fitting fixed to the main fitting, and two load reacting link rods connected to the main fitting by a balance beam, each of the link rods being connected to the balance beam by a first longitudinal end by a first mechanical connection that has at least one axis of rotation, each of the link rods being connected to the additional fitting by a second longitudinal end by a second mechanical connection that has at least one axis of rotation, the second mechanical connection having play, the first and second mechanical connections having at least one axis of rotation in common.
DISPOSITIF D'ACCROCHAGE DE MOTEUR D'AERONEF ET AERONEF COMPORTANT AU MOINS UN TEL DISPOSITIF
DEVICE FOR ATTACHING AN AIRCRAFT ENGINE AND AIRCRAFT COMPRISING AT LEAST ONE SUCH DEVICE
VORRICHTUNG ZUR BEFESTIGUNG EINES FLUGZEUGTRIEBWERKS UND FLUGZEUG MIT MINDESTENS EINER DERARTIGEN VORRICHTUNG
2017-05-31
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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