AI-336-1/-2-10 INDUSTRIAL GAS-TURBINE DRIVE

It is used as a drive for gas pumping units GTK-10I, GTK-10-2, GTK-10-4 with rated capacity of 10 MW. The engine features three-shaft design and comprises a two-spool gas generator and a free turbine.

The engine design provides for modular assembly principle, use of a highly effective system of cooling of hot parts and use of material with high-strength characteristics.

• high economic efficiency;

• stability of parameters;

• reliability and trouble-free operation;

• long service life;

• controllability;

• reparability without removal from pumping unit;

• low maintenance cost;

• low maintenance cost;

• low emission of contaminating substances;

• acceptable level of acoustic characteristics.

• Rated power (sea level. ISA), RW ................................................... 10000

• Turbine rotor rated rotational speed, min^-1

  • Al-336-1-10........................................................... 4800-counter-clockwise

  • AI-336-2-10................................................................. 6500-clockwise

• Fuel type..................................................................... gaseous (natural or oil gas)

• Fuel consumption (at C.V. = 11950 kcal/kg), kg/h .................................2085

• Effective efficiency, % ..........................................................................34,5

• Emission of contaminating substances:

  • content of nitrogen oxides, mg/m³, max ....................................... 50

  • content of carbon oxides, mg/m³, max ......................................... 80

• Free turbine exhaust gas temperature , К .............................................. 709

• Overall dimensions, mm ......................................................... 5840 х 2120 х 2275

• Mass, kg, max................................................................................... 5200

• Total service life, h, not less than .................................................... 100000

According to the customer's request, the engine can be modified to operate on liquid fuel — kerosene PT, TC-1 or similar fuel of foreign manufacture.

The engines can be successfully operated in different climatic areas at ambient temperature from -45°C to +45°C at altitudes up to 2000 m above sea level.

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