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Standard Test Method for Stress-Corrosion of Titanium Alloys by Aircraft Engine Cleaning Materials

contributor authorASTM - ASTM International
date accessioned2017-09-04T17:29:36Z
date available2017-09-04T17:29:36Z
date copyright41214
date issued2012
identifier otherCSNYAFAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/152631
description abstractThis test method 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 prestressed titanium alloys to crack when subsequently heated to elevated temperatures.
Test conditions are based upon manufacturer's maximum recommended operating solution concentration.
The values stated in inch-pound units are to be regarded as standard. The values given in parentheses are mathematical conversions to SI units that are provided for information only and are not considered standard.
This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use. For specific precautionary statements, see 5.3 and 5.6.
languageEnglish
titleASTM F945num
titleStandard Test Method for Stress-Corrosion of Titanium Alloys by Aircraft Engine Cleaning Materialsen
typestandard
page5
statusActive
treeASTM - ASTM International:;2012
contenttypefulltext


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