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Mobil Turbo 319A-2

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价格：￥电议

型号：原产地：中国大陆发布时间：2021/3/19 9:18:46更新时间：2024/8/6 11:51:48

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详细内容

Mobil Turbo 319A-2 is a fully synthetic lubricant developed to meet the performance requirements of Russian gas turbine aircraft engines which operate on mineral-oil-based lubricants. Formulated from a synthetic hydrocarbon combination of polyalphaolefin (PAO) ａnd hindered ester based stock, Mobil Turbo 319A-2 is fortified with a unique chemical additive system. The resulting product has far superior thermal ａnd oxidation stability than mineral-oil-based lubricants. The ability of Mobil Turbo 319A-2 to resist deterioration ａnd deposit formation allows the potential for extended oil drain intervals ａnd less frequent maintenance.

The closely controlled viscosity of Mobil Turbo 319A-2 at -51º C, along with a -60ºC pour point, ensure good low-temperature fluidity, permitting engine starting ａnd lubrication at low temperatures. Mobil Turbo 319A-2 exhibits excellent bulk oil stability at temperatures up to 200º C (392º F). The evaporation rate of Mobil Turbo 319A-2 at high temperatures is significantly lower than mineral-oil-based products, ａnd helps minimize oil consumption. The lubricant has excellent resistance to foaming.

Mobil Turbo 319A-2 is compatible with existing seal materials, including F Rubber (Viton A), H Rubber (Buna N), ａnd silicone, as well as 11 metals used in gas turbine construction.

Features ａnd Benefits

Mobil Turbo 319A-2 offers the following advantages ａnd benefits:

· Low evaporation loss ａnd oil consumption

· Reduced sludge ａnd carbon deposits

· Improved bulk oil oxidation stability ａnd extended oil drain intervals

· Compatible with existing seal materials

· Reduced engine maintenance, including potential for extended drain intervals

Applications

Mobil Turbo 319A-2 is recommended for aircraft gas turbine engines that normally operate on mineral-oil-based lubricants, as well as engines approved to operate on oils meeting the specifications listed below.

Mobil Turbo 319A-2 is approved against the following specification of the Russian Central Institute of Aeronatutical Motors (CIAM):

· IMP-10

· MS, 8P, MS-8RK

· 36/1 Ku-A

· VNII NP 50-1-4f ａnd -4u

· B3V ａnd LZ-240

· Mobil Turbo 319A-2 also meets U.S. Military Specification MIL-L-6081C, as well as the essential performance requirements of U.S. MIL-L-7808K, Grade 3.

Typical Characteristics

Mobil Turbo 319A-2
Physical properties are listed in the table below. Values shown are typical ａnd may vary slightly.
Viscosity
cSt at 40º C	16.2
cSt at 100º C	3.70
cSt at -40º C	2917
cSt at -51º C	12545
Flash point, º C (ºF)	234 (453.2)
Pour point, º C (ºF)	-60 (-76)
Specific Gravity	0.852
TAN	0.03
Evaporation Loss, %	0.999
5 hr at 175 ºC (347ºF)	2.4
Foam, ml
Sequence 1, 24ºC (75ºF)	30
Foam Stability, after 1 min settling, ml	0
Rubber Swell, %
NBR-H, 168 hr at 70ºC (158ºF)	11.9
FKM, 72 hr at 175ºC (347ºF)	3.0