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SAE ARP8462

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Evaluation of Fouling Propensity of Aviation Lubricants, Using the Mixed-Phase Flow Technique (High-Temperature Deposition Test)

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The high-temperature deposition test (HTDT) method is designed to evaluate the deposition and degradation characteristics of turbine lubricants when stressed under mixed-phase flow conditions found in certain parts of aviation gas turbine engines. This method is applicable to lubricants that form deposits in the range of 0.1 to 100 mg during the course of a test.

SDO SAE: SAE International
Document Number ARP8462
Publication Date Oct. 5, 2023
Language en - English
Page Count 29
Revision Level
Supercedes
Committee
Publish Date Document Id Type View
Oct. 5, 2023 ARP8462 Revision