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This test method is designed to simulate the synergistic combinations of oil flow, temperature cycling, hot spots, and tribology that would typically be found in a gas turbine engine. The method is intended to quantitatively characterize changes in four basic oil properties that are brought about by exposure to the afore mentioned simulated turbine engine environment: the tendency of aviation lubricants to form coke deposits, viscosity changes, total acid number changes (TAN), and oil consumption.
| Author | SAE |
|---|---|
| Editor | SAE |
| Document type | Standard |
| Format | File |
| Confirmation date | 2016-09-12 |
| ICS | 49.050 : Aerospace engines and propulsion systems 75.100 : Lubricants, industrial oils and related products |
| Number of pages | 35 |
| Set | AEROPAKS10U-10 |
| Year | 2016 |
| Country | USA |
| Keyword | SAE 6166;SAE ARP6166;SAE ARP6166;SAE ARP 6166 |