KG2 is a single-shaft, all-radial gas turbine with a single can tangential combustor. These basic design features result in several important technical advantages. Customers benefit by reliability, operational flexibility and a reduction in overall installation costs.

Model Designations

  • KG2-3C
  • KG2-3E
  • Starting reliability higher than 99%
  • 0.15% frequency stability
  • Designed and built specifically for marine and other arduous environment
  • Low fuel gas pressure
  • Robustness
  • Designed for ease of operation and maintenance

Exceptional Electrical Response curves

TURBINE SPECIFICATIONS

  KG2-3C KG2-3E

 

Base Load Stand By Base Load Stand By
ISO (15°C) shaft output (kW) 1530 1890 1934 2250
Output shaft speed (rpm) 1500/1800 1500/1800 1500/1800 1500/1800
Fuel type Natural gas, diesel fuel or equal
Fuel flow, full load (MJ/sec) 9,32 10,96 11,54 12,76
Exhaust gas temperature (°C) 570 623 549 604
Exhaust mass flow (kg/sec.) 12,8 13,5 15,0 14,9
Heat loss, lube oil approx. (kW) 75 75 90 90
Heat loss, radiation approx. (kW) 30 35 35 40
Starting time to full load approx. (sec.) 35 – 55 seconds
depending on type of start system
Weight, turbine/gear (kg) 1810 1810 1925 1925
 

 

 

© Dresser-Rand 2008 All Rights Reserved. Privacy Policy & Terms of Use