COMPRESSOR

• 9 Axial Flow Stages (Variable Inlet Guide Vanes) plus one Centrifugal Stage
• Compression Ratio 12:1

COMBUSTOR

• Two Tubular Radial Flame Tubes (each with an Igniter)
• Natural Gas or Distillate Fuel

TURBINE

• Three Axial Stages

ROTOR

• Speed: 14,000 RPM
• Tilt Pad Thrust & Journal Bearings at the front and Radial Roller Bearing at the rear
• Integral Epicyclic Speed Reduction Gearbox

DATA AT RATED POWER
AND ISO 2314 CONDITIONS

• Mass Flow 15 kg/s (33 lbs/sec)
• Exhaust Temperature 435 ⁰C (815 ⁰F)
• Output Power: 2.85 MW at Shaft Flange
• Efficiency: 28.5%