Advanced auxiliary two-shaft gas-turbine engine with equivalent power of 238 kW. It is used for installation in auxiliary power units of fixed and rotor-wing aircraft of civil and state aviation.
Purporse:
generation of compressed air for starting propulsion gas-turbine engines;
electrical power supply with 200/115 VAC, 400 Hz, power up to 40 kVA;
generation of compressed air for aircraft conditioning system;
generation of compressed air for aircraft anti-icing system.
Main advantages of the engine:
high reliability;
high resource and service life;
low specific fuel consumption;
ease of maintenance and repair;
high technical characteristics;
low prices and operating costs.