SAE ARP1795A

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Stress Corrosion of Titanium Alloys Effect of Cleaning Agents on Aircraft Engine Materials

Published by Publication Date Number of Pages
SAE 1990

SAE ARP1795A – 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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