Gas turbine engine UGT 2500

According to ISO 2314

Single-shaft gas turbine with integrated gearbox

Axial-centrifugal compressor, 9 axial stages, 1centrifugal stage

Double-tube external combustion chamber

Three-stage axial turbine

The turbine start up is fulfilled by means of the turbo compressors rotor spinning with two electric alternate current starters of 55kW continuous power each

UGT2500

(049)

Application

E*

Power, KW

2850

Efficiency, %

28,5

Specific gas discharge (Hu=8555ccal/nm3), nm3/(KW/h)

0,353

Engine pressure ratio

12,8:1

Exhaust gas mass flow, kg/sec

16,5

Exhaust gas temperature,

460

Output speed of the engine, rpm

14000

Output speed of the reduction gear, rpm

1500, 1800,
3000, 3600

*E electric motor driver