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SAE ARP6166

Current

Current

The latest, up-to-date edition.

Minisimulator Method

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

12-09-2016

€146.44
Excluding VAT

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

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