D-30STU

Having a power turbine, the D-30STU industrial gas-turbine engine is intended for operation as the power source for a compressor test bench.

It provides for tests of high and low pressure compressors, including those with inlet air preheating and variable rotation direction. The change of rotation direction is carried out by reduction gearbox.

Main specifications of the engine:

Version I :

  • rotation direction : clockwise (view from output shaft);
  • working speed range ï = 5 000 ... 11 500 rev/min;
  • transmission capacity Nå=18700 kW at maximum speed.

Version II :

  • rotation direction : clockwise (view from output shaft);
  • working speed range ï=6 000 ... 14 000 rev/min;
  • transmission capacity Nå = 12 000 kW at maximum speed.

Version III :

  • rotation direction : counter-clockwise;
  • other data according to version II.

Length of the engine (from the inlet up to a flange of power turbine shaft): 6.4 m.

Year of service entry : 1997

Customer : CATIC, PEOPLES REPUBLIC OF CHINA.

If you would like to receive further information concerning our engines, please fill in the form.

Contact

93, Komsomolski prospect, Perm, 614600, Russia.

AVIADVIGATEL

Deputy General Designer -
Chief Designer of Aero Engines 
Alexander N. Semenov
Tel: +7 3422 815568
Fax: +7 3422 815477
E-mail: semenov@avid.ru