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Gas turbine engine UGT 6000
Gas turbine engine UGT 6000

According to ISO 2314

Three-shaft gas turbine

Compressors: axial 8-stage LPC, 9-stage HPC

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

Compressor turbines are axial single stage LPT and HPT

Power turbine is an axial 2-, 3-, 4- or 6-stage engine (depending on modification)

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


The turbine

UGT6000

UGT6000R

71

71

71

71

71

Application

E

Power, kW

6360

6500

7350

7350

7350

Efficiency %

31,5

31,5

32,0

32,0

30,0

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

0,319

0,319

Specific fuel consumption

(Hu=10200kcal/kg), kg/(kW hr)

0,268

0,263

0,263

0,281

Summarized engine pressure ratio

13,5

14,0

14,5

14,5

15,0

Exhaust gas mass flow, kg/sec

30,5

31,0

32,0

32,0

32,5

Exhaust gas temperature,

425

430

440

440

470

Rotation speed of the turbine, rpm

3000

8200

7000

10000

4750

*E electric motor drivers

drive component for compressed gas pump

drive component for ship propellers

R reversing gas engine