Safran Aircraft Engines

Théodore Magne

Loïc Pora

Petar Tomov

Device () for testing a hydraulic part () for a turbomachine, the device comprising a closed loop for circulation of a working fluid, the loop comprising at least one recirculation pump () configured to circulate the working fluid in the loop according to a direction of circulation, at least one valve () for regulating the flow rate of a working fluid, at least one reservoir (A) configured to store the working fluid, a test section () configured to accommodate the hydraulic part (), the device () further comprising a gas injection means () configured to inject and dissolve, at atmospheric pressure, a gas in the working fluid stored in the reservoir (A).

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Moissy-Cramayel, France

Théodore Magne