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Gas turbine engine UGT 10000
Gas turbine engine UGT 10000

According to ISO 2314

Three-shaft gas turbine

Compressors: axial 9-stage LPC, 9-stage HPC

Combustion chamber is a can-annular 10-liner counterflow chamber

Compressor turbines are axial single stage engines

Power turbine is an axial 3- or 4-stage engine

The turbine start up is fulfilled by means of the rotor spinning with one AC electric starter of 30kW continious power.

The turbine

UGT10000

70

70

Application

*

Power, kW

10500

10500

Efficiency %

36,0

36,0

Specific gas discharge (Hu=8555kcal/nm3), nm3/(kW hr)

0,279

0,279

Summarized engine pressure ratio

19,0

19,0

Exhaust gas mass flow, kg/sec

36,0

36,0

Exhaust gas temperature,

490

490

Rotation speed of the turbine, rpm

4800

6500

* Gas charger drive