Twin-shaft gas turbines GTD-6/8RM
GTD-6RM and GTD-8RM are twin-shaft gas turbines for driving electric generators as part of thermal power plants of low and medium power (from 6 to 64 MW and above).
Technical characteristics
| Power (ISO 2314), MW | GTD-6RM - 6.38 | GTD-8RM - 8.44 |
| Efficiency (ISO 2314), % | GTD-6RM - 24.8 | GTD-8RM - 25.5 |
| N output shaft, rpm | 3000 |
| Fuel used | gas / diesel |
| Fuel consumption (at nominal mode), kg/hour | GTD-6RM - 1,853 / 2,136 | GTD-8RM 2 385 / 3 465 |
| Outlet gas temperature, °C | GTD-6RM - 460 | GTD-8RM - 520 |
| Outlet gas flow, kg/s | GTD-6RM - 46.2 | GTD-8RM - 51.0 |
| Dimensions (L x B x H), m | 3.4 x 2.3 x 2.5 |
| Weight (on frame), tons | 5.62 |
Advantages
- high reliability indicators of the GTD-6/8RM are ensured by the reliability and operating experience of aircraft engines of the D-30KU/KP family
- the total operating time of GTD-6/8RM in operation, as part of gas turbine units and gas turbine power plants, amounts to more than 3.5 million hours
- possibility of working on various types of fuel: gaseous (natural gas, associated petroleum gas) and liquid (kerosene, diesel fuel)
- reduction of capital and operating costs due to the unification of gas turbines GTD-6/8RM with aircraft engines D-30KU/KP
Application
GTD-6/8RM is the basis of power gas turbine units GTA-6/8RM, used as part of gas turbine thermal power plants GTES-12/24/other. low and medium power (from 6 to 64 MW and above), intended for the generation of thermal and electrical energy in simple, combined and cogeneration cycles.
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