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
23.10.2024
Patent
Elektronische Ressource
Französisch
Europäisches Patentamt | 2025
|