Gas turbine engine NK-38

Price on demand

Supplier: Kazan Motor Production Association, JSC

Description

Purpose: Used to drive the compressor in the composition of the gas pumping agehachou. Description: Engine is developed on the basis of the modern aircraft engine NK-93. Effective efficiency (ISO conditions) at least 38%. Installs on GPA-16 "Volga". In case of replacement of NK-16ST NK-38СТ comes spetskomplekt to be converted. Fuel gas consumption, and life cycle cost of the engine NK-38СТ for 100,000 hours of an assigned resource below in comparison with similar indicators of other engine suppliers. Enterprise released 11 engines.

Characteristics

Overhaul life, h.: 30000
Warranty resource, h.: 5000
Applied oil: Petrim
Gas temperature at the outlet of a free turbine, ° С: 447
Assigned resource, h.: 100000
Power, MW, not less: 16
Effective efficiency,%, not less: 38
Range of change of the frequency of rotation of the drive shaft of a free turbine, rpm.: 3700-5500
Content in exhaust gases, mg / nm3 - nitrogen oxides: 50
Exhaust gas content, mg / nm3 carbon monoxide: 150
Maximum sound pressure level, dB: 133
Engine weight with frame, kg: 6650
Fuel gas consumption, nm3 / h: 4 647
Engine start (at the request of the Customer): electric, pneumatic