COMPRESSOR
- Low Pressure Compressor - 9 Axial Flow Stages, Variable Inlet Guide Vanes
- High Pressure Compressor - 10 Axial Flow Stages, Variable Inlet Guide Vanes
- Compression Ratio 20:1
COMBUSTOR
- Canular Reverse Flow with 16 Flame Tubes
- Two Igniters
- Natural Gas or Distillate Fuel
COMPRESSOR TURBINES
- One Axial Stage for each Rotor
- Air-Cooled HP Turbine Blades and LP and HP Stator Segments
COMPRESSOR ROTOR
BEARING SYSTEMS
- Ball Radial/Thrust Bearing with Squeeze Film Damper at the front and Roller Radial Bearing arrangement at the rear on LP and HP Rotors
- Squeeze Film Dampers are used to reduce the dynamic bearing loads and casing vibration level
POWER TURBINE (5200 RPM NOMINAL)
- 3 Axial Stages
- Radial Roller Bearing at the front and Radial Ball and Ball Radial/Thrust Bearing arrangement at the rear
POWER TURBINE (3000/3600 RPM NOMINAL)
- 4 Axial Stages
- Radial Roller Bearing at the front and Radial Ball and Oil Film Thrust Bearing arrangement at the rear
DATA AT RATED POWER
AND ISO 2314 CONDITIONS
- Mass Flow 70 kg/s (154.3 lbs/sec)
- Exhaust Temperature 420
