Gas turbine engine NK-16-18STDV is designed for use as a blower drive of gas pumping unit GPA-C-16 and GPA-16 "Volga". It is developed on the basis of the aircraft engine NK-8-2U ser.2.
The NK-16-18STDV engine has an electronic-hydraulic control system. As an actuator dosing fuel gas supply to the combustion chamber is used dosing unit DVB with a control unit.
The engines are manufactured both from new parts and assemblies and using parts and assemblies of the NK-8 family of aircraft engines that have outlived their service life in flight operation. In this case, parts and assemblies of the basic aircraft engines must be repaired according to the repair documentation in force for them.
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