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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 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+

91

Application

*

Power, kW

20000

Efficiency  %

36,0

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

0,234

Summarized engine pressure ratio

20,0

Exhaust gas mass flow,  kg/sec

76,5

Exhaust gas temperature,

450

Rotation speed of the turbine, rpm

3500

* drive component for ship propellers