SAE ARP6166
Current
The latest, up-to-date edition.
Minisimulator Method
Hardcopy , PDF
English
12-09-2016
1. SCOPE
2. APPLICABLE DOCUMENTS
3. METHOD SUMMARY
4. MINISIMULATOR APPARATUS
5. APPARATUS PREPARATION
6. TEST PROCEDURE
7. QUANTITIZING TEST RESULTS
8. REPORT
9. PRECISION
APPENDIX A - ENGINEERING DRAWINGS OF ESSENTIAL COMPONENTS
OF THE ASSEMBLED TEST HEAD INCLUDING ALL RATED PARTS
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.
DocumentType |
Standard
|
Pages |
35
|
PublisherName |
SAE International
|
Status |
Current
|
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.
MIL-PRF-23699 Revision G:2014 | Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, NATO Code Numbers: O-152, O-154, O-156, and O-167 |
SAE ARP5088B | Test Method for the Determination of Total Acidity in Polyol Ester and Diester Gas Turbine Lubricants by Automatic Potentiometric Titration |
FED-STD-791 Revision D:2007 | TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.