Gas Turbine power unit of the Ural-2500 Hydroelectric power Station
(Equipment / Material)
Model Number: Урал-2500
Condition: New
Location or Storage Country: Russia
Service Engineering Support: Yes
Warranty: Yes
Price: Call for price
Description:
The power unit is based on the GTU-2.5P with a nominal capacity of 2.5 MW, developed on the basis of the gas generator of the most reliable engine in the history of the domestic aviation industry, the D-30, created for mainline passenger aircraft such as the Tu-134. It is used to produce electrical and thermal energy. It operates as the main and backup power source; in the basic, semi-peak and peak use classes, autonomously and in parallel with other sources of electrical energy and power systems.
Overview:
| Nominal power at generator terminals | 2.6 MW |
| Nominal frequency of electric current | 50 Hz |
| Gas temperature behind the power turbine at the exhaust | 361 °C |
| Gas flow behind the power turbine at the exhaust | 25.6 kg/s |
| Thermal power according to the utilization scheme | 5.8 Gcal/h |
| Fuel heat utilization coefficient at t out = 110 °C | 76.9% |
| Fuel gas parameters before the gas turbine power plant: pressure (excess) | 10...12 kgf/cm2 |
| Fuel gas parameters before the gas turbine power plant: temperature range | +5...+90 °С |
| Equivalent sound level during maintenance | no more than 80 dBA |
| Resource before major repairs | 30000 h |
| Resource assigned | 120000 h |
JSC "UDK"
Locations: Yaroslavl region, Rybinsk, Tolbukhina st., 16
Main Products/Services: Power equipment