Gas turbine engine UGT 8000

According to ISO 2314

 

Three-shaft gas turbine

Compressors: axial 8-stage LPC, 9-stage HPC

Combustion chamber is a can-annular 10-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 continious power.

  

 

 

UGT 8000

(70)

Application

*

Turbine power, kW

8300

Efficiency  %

33,2

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

0,303

Summarized engine pressure ratio

16,6

Exhaust gas mass flow, kg/sec

33,0

Exhaust  gas temperature,

470

Rotation speed of the turbine, rpm

8200

 

* Gas charger drive