SAE ARP1795 Revision A

SAE ARP1795 – Revision A – Stress Corrosion of Titanium Alloys, Effect of Cleaning Agents on Aircraft Engine Materials

This document establishes a test procedure for determining the propensity of aircraft turbine engine cleaning and maintenance materials for causing stress-corrosion cracking of titanium alloy parts. The evaluation is conducted on representative titanium alloys by determining the effect of contact with cleaning and maintenance materials on tendency of pre-stressed titanium alloys to crack when subsequently heated to elevated temperatures.

Product Details

Published:

10/01/1990

File Size:

1 file , 440 KB

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