Gas turbine engine UGT 60000 (UGT 45 000)

According to ISO 2314

Single-shaft gas turbine with integrated gearbox

Compressor: axial 15-stage

Combustion chamber is a can-annular 20-liner counterflow chamber

Turbine axial 4-stage

The turbine start up is fulfilled by means of standard electric power generator by thyristor frequency-to-current converter

UGT60000

 (-60)

 UGT45000

 (-45)

Application

      E*

     E

Power, kW

63500

47700

Efficiency  %

38,8

36,1

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

0,259

          0,278

Engine pressure ratio

18,0

14,0

Exhaust gas mass flow,  kg/sec

174,5

138,5

Exhaust gas temperature,

520

550

Turbine output speed, rpm

4320

3960

Gearbox output speed, rpm

3000

3000

 *E electric motor drivers