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Technical Specifications and Features of RIPP 4050 Aviation Lubricating Oil

2024-12-27 16:28:18

I. Product Specifications & Standards

  1. Compliance Standards

    • Complies with GJB-1263-1991 (Synthetic Lubricants for Aviation Turbine Engines) 136, equivalent to the U.S. MIL-L-23699C standard 1310.

    • Validated through national tests, including kinematic viscosity, pour point, and acid value 136.

  2. Key Technical Parameters

    ParameterSpecificationTest ResultTest Method
    Kinematic Viscosity (100°C)4.9-5.5 mm²/s5.02GB/T 265
    Pour Point≤-54°C-60°CGB/T 3536
    Flash Point (Open Cup)≥246°C252°CGB/T 3536
    Evaporation Loss (71°C)≤10%4.53%GB/T 7325

II. Performance Characteristics

  1. Superior Temperature Resistance

    • Operating Range: -40°C to 200°C, with short-term tolerance up to 220°C .

    • Excellent low-temperature fluidity (pour point: -60°C) for extreme environments .

  2. Oxidation Stability & Corrosion Resistance

    • High thermal-oxidative stability; color darkening under prolonged high temperatures does not affect performance .

    • Low acid value (0.22 mg KOH/g) minimizes metal corrosion .


III. Applications

  • Engine Compatibility:

    • Turbojet, turbofan, and turboshaft engines .

  • Typical Use Cases:

    • Military/civil aircraft, helicopter transmission systems .


IV. Usage Guidelines

  1. Storage & Handling

    • Store in cool, dry conditions; avoid contamination by moisture or dust .

    • Do not mix with other lubricants to prevent performance degradation .

  2. Packaging

    • Standard: 3.5 kg/4L per pail; bulk options (e.g., 17L drums) available from select suppliers .


V. Competitive Advantages

  • Market Position: Cost-effective alternative to imports like MobilJet Oil II, with comparable high-temperature stability and low-temperature fluidity .

  • Technical Edge: Fills the gap in China’s high-end aviation lubricant market, meeting both military and civil aviation demands .


Summary: RIPP 4050 is a high-performance synthetic aviation lubricant designed for extreme-temperature turbine engines. Its technical specifications align with global standards, making it a critical choice for domestic aerospace applications.


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