Oil Turbonikoyl 600
aviation oil
Description
Oil Turbonikoyl 600 – for gas turbine engines designed for operation in the temperature range from – 54 ° C to + 204 ° C <. /p>
Oil Turbonikoyl 600 (TURBONYCOIL 600) – a lubricating oil having a viscosity of 5 sentistoks at a temperature of 100 ° C, which is a combination of the esters used as a base, and carefully selected unique additive package including anti-oxidation, anti-wear, anti-foam and anti-corrosion additives. This combination provides outstanding lubricating properties of the oil as well as its high thermal stability and resistance to oxidation, which, in turn, during operation prevents such undesirable phenomena as formation of sludge and foam. Turbonycoil 600 designed to operate within the temperature range from – 54 ° C to + 204 ° C.
Applications
Oil Turbonycoil 600 (Turbonikoyl 600) designed for use in gas turbine engines and auxiliary equipment used in airplanes and helicopters in military and civil aircraft, so and in gas turbines of aircraft types used in the industry and on merchant and military fleets.
Technical Specifications
|
Indicator | Norm |
|
Kinematic viscosity, mm2 /c |
|
|
Flash point open cup, ° C | 270 |
|
Pour Point, ° C | -57 |
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Acid number, mg KOH /g | 0.16 |
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Foaming, ml |
|
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Thermal stability and corrosivity 96 h. at 274 ° C viscosity change at 40 ° C,% | -0.3 |
|
Corrosion and oxidation stability 72 hrs. At 175 ° C viscosity change at 40 ° C,% metal weight change, mg /cm2 | +17.0 0.0 |
|
Loss by Evaporation 6.30 hour at 204 ° C,% | 3.4 |
