首页> 外文会议>Annual Conference of the Australasian Corrosion Association >THE USE OF X-RAY TOMOGRAPHY IN THE STUDY OF INTERGRANULAR CORROSION ON AIRCRAFT ALUMINIUM ALLOYS
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THE USE OF X-RAY TOMOGRAPHY IN THE STUDY OF INTERGRANULAR CORROSION ON AIRCRAFT ALUMINIUM ALLOYS

机译:X射线层析成像在飞机铝合金中晶间腐蚀研究中的使用

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High-strength aluminium alloys have a microstructure that is highly susceptible to localised corrosion such as intergranular and pitting corrosion. The susceptible microstructure results from the thermo-mechanical processing given to these alloys to develop optimal mechanical properties. Intergranular and pitting corrosion are known to develop on many of the aluminium alloys used on Australian Defence Force (ADF) aircraft. However, there is little information available in the literature covering the conditions that cause atmospheric intergranular corrosion (IGC) and the resulting kinetics. Furthermore, the occurrence and extent of pitting corrosion is generally easily measured, whereas IGC is more difficult to identify and quantify. Historically, experimental investigation of IGC has required destructive, time consuming analysis with results that do not fully describe the extent of attack. Due to increases in computing power, computed X-ray tomography can now be used routinely in the laboratory for the study of metal defects such as corrosion damage. To support the ADF, Defence Science and Technology Organisation (DSTO) has undertaken an experimental program to understand the causality and propagation of IGC of 2024-T351 and 7050-T7451. This study has involved exposure of aluminium alloy specimens contaminated with salts to simulated atmospheric conditions. X-ray micro-computed tomography has been employed to measure the extent of IGC damage and provide visualisation of the networks of intergranular attack in 3-dimensions (3-D). The results showed that the depth and volume of intergranular corrosion increased with time in a 97% relative humidity environment, and also showed the depth and volume of intergranular corrosion increased with increasing relative humidity.
机译:高强度铝合金具有高度易受局部腐蚀的微观结构,例如晶间和点蚀腐蚀。敏感的微观结构由给予这些合金的热机械加工产生最佳的机械性能。已知在澳大利亚国防军(ADF)飞机上使用的许多铝合金中发育晶间和点蚀腐蚀。然而,文献中有很少的信息,涵盖导致大气晶间腐蚀(IGC)和所得动力学的条件。此外,通常可以容易地测量蚀腐蚀的发生和程度,而IGC更难以识别和量化。从历史上看,IGC的实验调查需要破坏性,耗时的分析,结果没有完全描述攻击程度的结果。由于计算能力的增加,所计算的X射线断层扫描现在可以在实验室中常规使用,以研究金属缺陷,例如腐蚀损坏。为了支持ADF,国防科学和技术组织(DSTO)承担了理解IGC为2024-T351和7050-T7451的因果关系和传播的实验计划。本研究涉及含有盐污染的铝合金标本的暴露于模拟大气条件。 X射线微计算断层扫描已被用于测量IGC损伤的程度,并提供3维(3-D)中的晶间攻击网络的可视化。结果表明,在97%相对湿度环境中随着时间的推移,晶间腐蚀的深度和体积增加,并且还随着相对湿度的增加而增加的晶间腐蚀的深度和体积增加。

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