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Gas turbine engine UGT 3000
Gas turbine engine UGT 3000

According to ISO 2314

Three-shaft gas turbine
Compressors: axial 8-stage LPC, 9-stage HPC
Combustion chamber is a can-annular
9-liner counterflow chamber
Compressor turbines are axial single-stage engines

Power turbine is an axial 3-stage engine

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

UGT3000

(76)

UGT3000R

(76)

Application

H, M*

M

Power, kW

3360

3360

Efficiency %

31,0

29,0

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

0,324

-

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

0,272

0,291

Summarized engine pressure ratio

13,5

14,0

Exhaust gas mass flow, kg/sec

15,5

16,0

Exhaust gas temperature,

440

470

Rotation speed of the turbine, rpm

9700

8800

* drive component for compressed gas pump

drive component for ship propellers