An engine assembly for an aircraft rigid structure comprising a mounting pylon comprising a central box and a box extension connected to a reducing gear case of the turboreactor. The box extension includes two parts bearing the front engine attachments, these pieces each comprising a structure forming a reinforcing rib of the central box, as well as two parts of horseshoe shape surrounding the reducing gear case.
ENSEMBLE MOTEUR POUR AERONEF COMPRENANT UNE STRUCTURE PRIMAIRE DE MAT D'ACCROCHAGE EQUIPEE D'UNE EXTENSION DE CAISSON COMPRENANT DEUX PARTIES EN FORME GLOBALE D'ARCEAU
2017-08-11
Patent
Electronic Resource
French
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