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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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