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.


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    Title :

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


    Publication date :

    1990-10-01



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English