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Mobil Turbo 319A-2详细说明 (浏览1893次)
Mobil Turbo 319A-2
Mobil Turbo 319A-2
Synthetic Aircraft-Type Gas Turbine Lubricant
Description
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
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