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Gas Turbine Engine UGT 6000+
Gas Turbine Engine UGT 6000+

 

Three-shaft gas turbine

Compressors axial, eight-stage LPC, nine-stage HPC

Combustion chamber can-annular reverse flow with 10 combustion liners

Compressor turbines axial, single-stage

Power turbine axial, three-stage

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

 

UGT6000+

(79)

UGT6000R+

(77)

Application

*

Power of gas turbine engine, kW

8800

8800

Efficiency of gas turbine engine, %

33.0

31.0

Liquid fuel consumption. (Hu = 10200 kcal/kg), kg/(kW h)

0.255

0.272

Compressor overall pressure ratio

16.0

16.5

Exhaust gas flow, kg/s

34.0

34.5

Exhaust temperature,

470

500

Power turbine speed, rpm

7000

7300

 * drive for ship propellers

  R reversing gas engine