An aircraft engine assembly including an attachment mechanism of a turbojet onto a rigid structure of a mounting strut, including a first, second, and third forward engine attachment for taking up thrust loads brought onto the fan frame, and arranged such that the third attachment passes through a first diametrical plane of the turbojet, the first and second attachments being disposed on one side and another of the first plane. The first and second forward engine attachments are respectively brought to the fan frame at two points, situated beyond the second diametrical plane of the turbojet, orthogonal to the first diametrical plane, with respect to the third attachment.
ENSEMBLE MOTEUR POUR AERONEF COMPRENANT DES ATTACHES MOTEUR DEPORTEES VERS LE BAS SUR LE CARTER DE SOUFFLANTE
AIRCRAFT ENGINE ASSEMBLY COMPRISING DOWNWARDLY OFFSET ENGINE MOUNTS ON THE FAN CASING
FLUGZEUGTRIEBWERKANORDNUNG MIT ABWÄRTS VERSETZTEN TRIEBWERKHALTERUNGEN AUF DEM LÜFTERGEHÄUSE
2019-01-09
Patent
Electronic Resource
French
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