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Description
The oil IPM-10 – a synthetic hydrocarbon with a complex of high-performance additives. Workable in the temperature range from -50 to +200 ° C.
Applications
Applied heat-turbine engines military and civil aircraft (civil aviation Yak-42 and Tu-204, Tu-214, etc.) With the oil temperature at the outlet from the engine to 200 ° C, as well as in aviation cooling turbines as uniform oil grades and other aggregates, particularly in units with a gas compressor driven by the aircraft engine. It can be used for non-durable preservation. Aviation oil IPM-10 zatarivatsya in cans from tinplate 15 kg. can be used along with oil VNII NP 50-1-4F, VNII NP 50-1-4U, Turbonikoyl 210A, Mobil Turbo 319A-2
Technical Specifications
Indicator | Norm GOST (TU) |
---|---|
Appearance | Transparent yellow liquid |
Kinematic viscosity, mm 2 /a: | |
at 100 ° C, at least | 3,0 |
at -30 ° C, no more than | – |
at -40 ° C, no more than | 2000 |
at -54 ° C, no more than | – |
Temperature, ° C: | |
flash in the open crucible, not lower | 190 |
pour point, not higher than | -50 |
Acid number, mg KOH /g, not more than | 0,05 |
Content: | |
water-soluble acids, bases, solids, water | The lack |
thermooxidative stability, h (temperature, ° C) | 50 (200) (air dm 3 3 /h) |
Performance after oxidation: | |
Kinematic viscosity, mm 2 /s, not more than: | |
at 100 ° C | 4,5 |
at -40 ° C | 5000 |
Change viscosity at 100 ° C, not more than | – |
Acid number, mg KOH /g, not more than | 8,0 |
Mass fraction of residue, insoluble in iso-octane,%, no more than | 0,35 |
Corrosion on plates, g /m 2 : | |
Steel ShKh15 | The lack |
copper M1 and M2 | ± 0,2 |
Aluminum Alloy AK4 | The lack |
Coking ability,%, not more than | – |
Density at 20 ° C, kg /m 3 | ? 820 |
Tribological characteristics on CHSHMT at (20 ± 5) ° C: | |
the critical load, N, not less than | 710 |
wear rate under axial load 196 N, not more than | 0,35 |
Additional information
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appointment | |
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