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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.
Key Technical Parameters
Parameter | Specification | Test Result | Test Method |
---|---|---|---|
Kinematic Viscosity (100°C) | 4.9-5.5 mm²/s | 5.02 | GB/T 265 |
Pour Point | ≤-54°C | -60°C | GB/T 3536 |
Flash Point (Open Cup) | ≥246°C | 252°C | GB/T 3536 |
Evaporation Loss (71°C) | ≤10% | 4.53% | GB/T 7325 |
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 .
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 .
Engine Compatibility:
Turbojet, turbofan, and turboshaft engines .
Typical Use Cases:
Military/civil aircraft, helicopter transmission systems .
Storage & Handling
Store in cool, dry conditions; avoid contamination by moisture or dust .
Do not mix with other lubricants to prevent performance degradation .
Packaging
Standard: 3.5 kg/4L per pail; bulk options (e.g., 17L drums) available from select suppliers .
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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