Gas turbine engine UGT 16000

According to ISO 2314

Three-shaft gas turbine

Compressors: axial 7-stage LPC, 9-stage HPC

Combustion chamber is a  can-annular 10-liner straight-flow chamber

Compressor turbines are axial 2-stage engines

Power turbine is an axial 2-, 3-stage engine

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

 

 

UGT16000

UGT16000R

 

593

592

59

Application

 

*

*

*

Power, kW

 

15900

16700

16550

Efficiency  %

 

31,4

32,0

30,0

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

 

0,320

0,314

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

 

0,269

0,281

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

 

12,5

13,0

13,5

Exhaust gas mass flow,  kg/sec

 

96,0

98,0

100,0

Exhaust gas temperature,

 

350

360

380

Rotation speed of the turbine, rpm

 

3000

5300

3600

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