COMPRESSOR

• Low Pressure Compressor - 8 Axial Flow Stages, Variable Inlet Guide Vanes
• High Pressure Compressor - 9 Axial Flow Stages
• Compression Ratio 13.7:1

COMBUSTOR

• Canular Reverse Flow with 10 Flame Tubes
• Two Igniters
• Natural Gas or Distillate Fuel

COMPRESSOR TURBINES

• One Axial Stage for each Rotor

COMPRESSOR ROTOR BEARING SYSTEMS

• Ball Radial/Thrust Bearing at the front and Radial Roller Bearing at the rear on LP Rotor
• Ball Radial/Thrust Bearing at the front and Radial Roller Bearing with Squeeze Film Dampers at the rear on HP Rotor

POWER TURBINE

• 3 Axial Stages (7,200 RPM Nominal), or 6 Axial Stages (3,000/3,600 RPM Nominal)
• Radial Roller Bearing at the front with Duplex Ball Radial/ Thrust Bearing Arrangement at the rear

DATA AT RATED POWER AND ISO 2314 CONDITIONS

• Mass Flow 30 kg/s (66.1 lbs/sec)
• Exhaust Temperature 405 ⁰C (761 ⁰F)
• Output Power: 6.7 MW at Shaft Flange
• Efficiency: 31.5%