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    Mobil Turbo 319A-2詳細(xì)說明 (瀏覽2465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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