| GE10GasTurbine |
 |
| SPECIFICATIONS |
| Axial Compressor |
• 11-Stage Axial Flow |
| • 15.5:1 Pressure Ratio |
| Combustion Chamber |
• Single Can Combustor |
| • Pollution prevention:• Pollution prevention: |
| DLN Dual Fuel Available |
| Turbine |
| GE 10-1 |
• 3-Stage HP Turbine-11000rpm |
| 　/TD> |
| GE 10-2 |
• 2-Stage LP Turbine-7900rpm |
| • LP Turbine: Variable 1st Stage Nozzle |
| • 2-Stage LP Turbine-11000rpm |
|
Nominal Rating - ISO |
At 15 °C, Sea Level, No External |
|
Pressure Losses, Relative Humidity |
|
60%, Natural Gas Fuel with |
|
LHV = 32 to 44 MJ/Nm3, |
| THERMAL EFFICIENCY (%) ..................................................................- 32.6 |
| ELECTRICAL OUTPUT POWER (kW) .................................................11250 11690 |
| ELECTRICAL EFFICIENCY (%) ........................................................... 31.4 - |
| EXHAUST FLOW (kg/sec) .......................................................................47 47 |
| EXHAUST TEMPERATURE (°C) ..........................................................490 490 |
GE Power Systems Oil& Gas
| GE10GasTurbine |
|
| Performance Curves |
Effect of Compressor Inlet Temperature on Exhaust Temperature and Exhaust Flow
Base Load with zero inlet and zero exhaust pressure drops at Sea Level, 60% RH - Natural Gas |
Effect of Compressor Inlet Temperature on Output and Heat Rate
Base Load with zero inlet and zero exhaust pressure drops at Sea Level, 60% RH - Natural Gas |
|
