Gas turbine engine GTE-8RM

GTD-6RM and GTD-8RM are twin-shaft gas turbines for driving electric generators as part of thermal power plants of small and medium capacity (from 6 to 64 MW and above).

Design Features:

- 11-stage compressor
- tube-and-ring combustion chamber (12 flame tubes)
- 2-stage compressor turbine
- 4-stage power turbine

Benefits:

- high reliability of GTE-6/8RM is ensured by the reliability and operating experience of D-30KU/KP family aircraft engines
- total operating time of GTE-6/8RM in operation, as part of GTA and GTPP, is more than 3.5 million hours
- possibility of operation on different types of fuel: gaseous (natural gas, associated petroleum gas) and liquid (paraffin, diesel fuel)
- reduction of capital and operating costs due to unification of gas turbines GTD-6/8RM with aircraft engines D-30KU/KP.