Gas Turbine Engine UGT 5000

According to ISO 2314

 

Single-shaft gas turbine with integral reduction gear

Compressor: axial/centrifugal with 10 axial stages and 1 centrifugal stage

Combustion chamber is an 8-liner external chamber

Compressor turbines are axial single stage LPT and HPT

Power turbine is an axial 3-stage engine

The turbine start up is fulfilled by means of the rotor spinning with two AC electric starters of 132 kW continious power each.

  

Application

E

Power, kW

5250

Efficiency, %

32,0

Specific gas discharge

(Hu = 8555 kcal/nm3), nm3/(kW hr)

0,314

Engine pressure ratio

14,0:1

Gas flow rate at the outlet, kg/sec

21,5

Gas temperature at the outlet,

480

Rotation speed of the gas turbine engine output shaft,  rpm

12840

Rotation speed of the reducing gear output shaft, rpm

1500, 1800, 3000, 3600


E* Electric generator drivers