Brochure

6 GE Gas Turbines
Turbine
The two-shaft version of the GE10 is optimized for mechanical drive applications.
It consists of two air-cooled high pressure reaction stages and two low pressure reaction stages
coupled to the power shaft.
To optimize the behavior at partial speed/load a variable geometry Nozzle Guide Vane (NGV) is
installed between the HP and LP sections.
GE10-2 Gas Turbines
GENERAL SPECIFICATIONS
Axial Compressor
- 11-Stage Axial Flow
- 15.5:1 Pressure Ratio
Combustion Chamber
- Single Can Combustor
- Emission Control:
- DLN Gas Fuel at 25 ppmvd NOx
- DLN Gas Fuel at 15 ppmvd NOx
- DLN Dual Fuel Gas Fuel at 25 ppmvd NOx
- DLN Dual Fuel Liquid Fuel at 85 ppmvd NOx
Turbine
- 2-Stage HPT (11000 rpm) + 2-Stage LPT (7900 rpm)