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The Facility

GE Aerospace

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in our facility
The Cold Flow Turbine Test Facility is the most modern laboratory of its kind worldwide and is used to carry out testing of new-generation engine turbine prototypes as well as technological demonstrators used in the construction of aeroengines.
Here the main key parameters of the Cold Flow Turbine Test Facility “Polonia Aero”: 
  • Max External Diameter of Test Article: 1900 mm,
  • Max Weight of Test Rig: 50 kN,
  • Max Flow Rate: 80 kg/s,
  • Max Inlet Total Pressure: 750 kPa,
  • Min Exit Total Pressure: 24 kPa,
  • Max Inlet Total Temperature: 650 K,
  • Max Turbine Shaft Power: 16 MW,
  • Max Torque: 67 kNm,
  • Max Axial Thrust: 75 kN,
  • Max Shaft Speed: 5000 rpm (10000 rpm after installation of gearbox).