
Gas turbine engine NK-16-18ST ser.2
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Key Highlights
- Made in Russia - engineered for durability
- Suitable for challenging environments
- Lower cost of ownership than European alternatives
- Bulk orders available with volume discounts
- Documentation and customs clearance assistance provided
Description
Gas turbine engine NK-16-18ST is designed for use as a blower drive for gas pumping unit GPA-C-16 and GPA-16 "Volga". It is developed on the basis of aircraft engine NK-8-2U ser.2. The engine NK-16-18-ST ser.2 has a hydromechanical control system. The engine is manufactured both from new parts and assemblies and with the use of parts and assemblies of aircraft engines of the NK-8 family that have outlived their service life in flight operation. In this case, parts and assemblies of basic aircraft engines must be repaired according to the repair documentation in force for them. In the resources of the engine parts and assemblies as part of the basic aircraft parts are not taken into account but are fixed
Specifications
Rated power at the drive shaft of the ST as part of the GCU under station conditions at the compressor inlet air temperature of
18000 kW
Effective efficiency at the drive shaft of ST as part of GCU under station conditions at 18000 kW capacity
29.4 %
ST shaft speed at power 18000kW, temperature 15°C, full pressure loss in the inlet 100 mm waterst,
5350
Fuel gas consumption at calorific value of gas 8100 kcal/m³ (33906 kJ/m³), at power of 18000kW
1.236
The motor is operable at ambient air temperature
-60...45 °C
The motor is operable at relative humidity of air, up to
100 %
Weight of the motor as part of the delivery with frame
7.8 kg
GG engine weight with frame
4 kg
Weight of ST motor with frame
3.8 kg
Engine weight without frame
6 kg
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Delivery Time
Sea freight: 30-60 days (depending on destination)
Air freight: 14-21 days (for urgent orders)
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