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OIL SYNTHETIC TURBINE ENGINES VNIINP-50-1-4U

Technical Specifications 38.401-58-12-91 with the changes to 1.2

VNII NP-50-1-4U - high quality synthetic dee-ether oil. It contains more effective composition of additive than VNII NP-50-1-4F contains. This which allows to increase thermo-oxidative stability of the oil to 200°C with overheating up to 225°C while maintaining the excellent low temperature (possibility of application up to -60°C) and other characteristics. Oil VNII NP-50-1-4U is combined with the oil VNII NP-50-1-4F in all respects, does not require replacement of rubbers and construction materials and can be applied on existing promising technique.

VNII NP-50-1-4U is mostly used in military equipment.

VNII NP-50-1-4U can be also used in aircraft turbojet engines: civil aviation - the Il-96-300, Tu-204, Yak-42, An-74, An-124 Ruslan; military aviation - MiG – 23, MiG-27, MiG-29, An-72, Mi-26.

Indicator name

Norm

Kinematic viscosity, mm2/s (St):
at 100°C, not less

3,2

at minus 40°C, not more

2700

at minus 50°C not more than

8500

The flash point determined in open crucible °C, not below

204

Pour point, °C, not above

-60

Thermal-oxidative stability at 200°C for 50 hours and air flow rate (10±0,5) dm3/h:

 

a) mass fraction of precipitate insoluble in isooctane, %, not more

0,15

b) acid number after oxidation, mg KOH/g oil not more than

4,5

C) kinematic viscosity after oxidation:

 

at minus 40°C, mm2/s (St), not more

-

at 100°C, mm2/s (St), not more

3,7

d) weight corrosion index after oxidation, mg/cm2, on LP:

 

alloy wrought aluminium brand AK4 (GOST 4784-74), max.

±0,1

of copper grade M1 or M2(GOST 859-78), max.

±0,4

steel SH-15 (GOST 801-78)

±0,1