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Gas turbine engine UGT 15000
Gas turbine engine UGT 15000

According to ISO 2314

Three-shaft gas turbine

Compressors: axial 9-stage LPC, 10-stage HPC


Combustion chamber is a  can-annular 16-liner counterflow chamber


Compressor turbines are axial single-stage engines

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

The turbine start up is fulfilled by means of the rotor spinning with two AC electric starters of 30kW continuous power

 

UGT15000

UGT15000R

90

90

90

090

Application

E*

*

*

Power, kW

16900

16700

17650

14700

Efficiency  %

35,0

35,0

35,4

32,0

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

0,287

0,287

Specific fuel consumption (Hu = 10200 kcal/kg), kg/(kW hr)

0,241

0,238

0,263

Summarized engine pressure ratio

19,5

19,5

20,0

18,0

Exhaust gas mass flow,  kg/sec

71,0

71,0

73,0

70,0

Exhaust gas temperature,

420

420

430

430

Rotation speed of the turbine, rpm

3000

5200

5300

4400

* E electric motor drivers
   drive component for compressed gas pump
  drive component for ship propellers
  R reversing gas engine