The invention relates to a module (3) having a longitudinal axis (X) and comprising a hydraulic actuator (46), and a pump (54) for supplying the hydraulic actuator (46) with fluid, the pump comprising axial pistons (54c) intended to be movable so as to rotate about the longitudinal axis (X) and are configured to transfer the fluid to the hydraulic actuator (46), a connecting plate (54g) connected to the axial pistons (54c) and engaging with an annular main plate (54e) centred on the longitudinal axis (X) intended to be rotated about the longitudinal axis (X) and tilted relative to the longitudinal axis (X), the connecting plate (54g) being arranged between the main plate (54e) and the axial pistons (54c), the axial pistons (54c) being movable so as to rotate in a direction (D) parallel to the longitudinal axis (X), the tilting of the main plate (54e) resulting in the movement of the axial pistons (54c) in the direction (D).
MODULE POUR UNE TURBOMACHINE D'AERONEF
MODULE FOR AN AIRCRAFT TURBINE ENGINE
MODUL FÜR EIN FLUGZEUGTURBINENTRIEBWERK
19.02.2025
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge / F04B Verdrängerkraft- und Verdrängerarbeitsmaschinen für Flüssigkeiten , POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS |