SAE ARP6166 PDF
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Minisimulator Method
Description
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.
History
| ARP6166 | 2016-09-12 | Latest | Reaffirmed |
| ISSUING COMMITTEE | E-34 Propulsion Lubricants Committee |
|---|---|
| DATE | 2016-09-12 |
| DOI | |
| ISCURRENT | Current |
| PAGE | 35 |
| PUBLISHER | SAE International |
| REVISED | REAFFIRMED |
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