In order to reduce the width of the attachment between the rear portion of an aircraft engine and its attachment pylon, an engine assembly attachment include an assembly of rear engine attachments comprising a first connecting rod laid out in a longitudinal and median vertical plane, a second connecting rod substantially laid out tangentially to the inter-turbine case, and a rear engine attachment for transversely spreading the loads, axially shifted rearwards relatively to the first and second connecting rods, and comprising a shear pin oriented along a vertical direction of the engine assembly.
ENSEMBLE MOTEUR POUR AERONEF COMPRENANT AU MOINS DEUX ATTACHES MOTEUR ARRIERE DECALEES AXIALEMENT L'UNE DE L'AUTRE
2017-12-15
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
ENSEMBLE MOTEUR POUR AERONEF COMPRENANT DES ATTACHES MOTEUR ARRIERE SOUS FORME DE MANILLES
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