These turbines are fuel-flexible, and can operate on natural gas, liquefied natural gas (LNG), distillate and treated residual oil in a variety of applications including: mechanical drive for large compressor trains; simple cycle and combined cycle; base load and peaking power generation; industrial and cogeneration. They all feature a 17-stage compressor with stacked disk design, reverse flow combustion system, three-stage turbine with air-cooled 1st and 2nd stage nozzles and buckets, and two or three bearing rotor supports.

The MS6001B is a single-shaft, heavy-duty gas turbine which has a high-efficiency axial compressor and a combustor with 10 chambers, each with individual fuel nozzles. The machine has a three-stage impulse turbine with air-cooled buckets and stationary nozzles on the first two stages to achieve higher firing temperatures and higher efficiency without compromising hot section component life.

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Parameter Power Generation Mechanical Drive
Power Output  42.100 MW  43. 530 MW
Efficiency 32.1% 33.3%
Heat Rate 11,230 kJ/kWh 10,820 kJ/kWh
Pressure Ratio 12.2 12.2
Exhaust Mass Flow 141.1 kg/s  140.0 kg/s
Exhaust Temperature 548 °C 544 °C
Turbine Speed 5,163 rpm 5,111 rpm
  • Single Shaft engine
  • 17 compressor stages
  • 10 cannular combustion chambers
  • 3 turbine stages
  • Approximate weight:
    • 96,000 kg (including auxiliary skid)
  • Approximate dimensions:
    • 15.9×3.2×3.8 m3 (including auxiliary skid)




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