A hydraulic assembly for an aircraft engine includes a pump with a housing and a rotor arranged inside the housing. The housing has at least one hydraulic line configured for the passage of a fluid; and a hydraulic transfer unit comprising: a hydraulic transfer block attached to the housing and comprising an internal fluid passage channel which communicates with the hydraulic line, and a casing which covers the transfer block and which is guided in rotation about an axis of revolution (Y) and about the transfer block, the casing having a fluid outlet port that communicates with the internal channel.
ENSEMBLE HYDRAULIQUE POUR UN MOTEUR D'AERONEF
HYDRAULIC ASSEMBLY FOR AN AIRCRAFT ENGINE
HYDRAULIKBAUGRUPPE FÜR EIN FLUGZEUGTRIEBWERK
2024-10-23
Patent
Electronic Resource
French
European Patent Office | 2025
|