A rear engine fastener for an aircraft connecting a primary structure and an engine of an aircraft, the rear engine fastener comprising a support configured to be connected to the primary structure, at least one main shackle connected to the support by first and second support link pins, which are symmetrical relative to a vertical longitudinal plane, and to the engine by a first lateral engine link pin and by a central engine link pin, and at least one secondary shackle connected to the engine by a second lateral engine link pin and to the main shackle by a secondary link pin.
ATTACHE MOTEUR ARRIÈRE D'UN AÉRONEF PRÉSENTANT UN ENCOMBREMENT RÉDUIT EN LARGEUR ET AÉRONEF COMPRENANT AU MOINS UNE TELLE ATTACHE MOTEUR ARRIÈRE
REAR ENGINE MOUNT FOR AN AIRCRAFT HAVING A REDUCED WIDTH AND AIRCRAFT COMPRISING AT LEAST ONE SUCH REAR ENGINE MOUNT
HINTERE MOTORHALTERUNG MIT REDUZIERTER BREITE FÜR EIN FLUGZEUG UND FLUGZEUG MIT MINDESTENS EINER SOLCHEN HINTEREN MOTORHALTERUNG
2022-02-23
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2020
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