An assembly (70) for mounting an aircraft engine (10) to an aircraft includes an engine casing flange having a first annular wall extending radially to terminate at an annular rim. A second flange of an additional engine component mounted aft of the engine casing (30) includes a second annular wall. An aft mount bracket (50) has an annular body (51) extending uninterrupted about the center axis (11) and a spigot (55) extending axially from the annular body (51), the spigot (55) extending circumferentially about an entire circumference of the annular body (51). The aft mount bracket (50) is axially disposed between the engine casing flange and the additional engine component, with corresponding holes (46, 54, 57, 64) in the first annular wall, second annular wall and aft mount bracket (50) being circumferentially aligned, and the spigot (55) radially abutting the annular rim of the engine casing flange.
AFT ENGINE MOUNT RING WITH SPIGOT
HINTERER MOTORLAGERRING MIT ZAPFEN
ANNEAU DE SUPPORT DE MOTEUR ARRIÈRE AVEC ERGOT
2023-02-08
Patent
Electronic Resource
English
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