COMPRESSOR

• Low Pressure Compressor - 9 Axial Flow Stages (1st Stage is Supersonic),
  Variable IGV, Stage 1 and 2 Stator Vanes
• High Pressure Compressor - 9 Axial Flow Stages
• Compression Ratio 21.8:1

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 Turbine Blades and Stator Segments

COMPRESSOR ROTOR BEARING SYSTEMS

• Ball Radial/Thrust Bearing  at the front and Roller Radial Bearing arrangement at the rear on LP and HP Rotors, both with Squeeze Film Dampers
• Squeeze Film Dampers are used to reduce the dynamic bearing loads and casing vibration level

POWER TURBINE

• 4 Axial Stages (Electrical Generator Drive)
• 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 88 kg/s (194 lbs/sec)
• Exhaust Temperature 475 ⁰C (887 ⁰F)
• Output Power: 27.5 MW at Shaft Flange
• Efficiency: 36.0%