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首页> 外文期刊>Corrosion Reviews >Transgranular corrosion fatigue crack growth in age-hardened Al-Zn-Mg(-Cu) alloys
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Transgranular corrosion fatigue crack growth in age-hardened Al-Zn-Mg(-Cu) alloys

机译:时效硬化Al-Zn-Mg(-Cu)合金的经晶腐蚀疲劳裂纹扩展

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摘要

The mechanisms of transgranular corrosion fatigue in age-hardened Al-Zn-Mg (-Cu) alloys are reviewed, with an emphasis on accounting for fractographic observations. The effects of cycle frequency, solution composition, temperature, and electrode potential on crack-growth rates (and striation spacing and appearance) at intermediate to high Delta K are discussed in particular. It is concluded that corrosion fatigue, resulting in cleavage-like {100} <110> cracking with extensive slip on {111} planes intersecting crack fronts, can best be explained by an adsorption-induced dislocation emission mechanism (involving weakening of interatomic bonds at crack tips by adsorbed hydrogen). Solute hydrogen ahead of cracks appears to play little, if any, role in facilitating cleavage-like cracking, and the mechanisms based on decohesion are at odds with the locally high strains around cracks and the formation of nanovoids ahead of cracks.
机译:本文对时效硬化的Al-Zn-Mg(-Cu)合金的经晶腐蚀疲劳机理进行了综述,重点是解释了分形观察。特别讨论了中高Delta K时循环频率,溶液成分,温度和电极电势对裂纹扩展速率(以及条纹间距和外观)的影响。可以得出结论,腐蚀疲劳会导致{111}面与裂纹前沿相交的类似滑移的{100} <110>断裂,并产生开裂,这可以用吸附诱导的位错释放机理来解释(涉及原子间键的弱化)。吸附氢引起的裂纹尖端)。裂纹前的溶质氢似乎对促进类似裂解的作用几乎没有作用,并且基于解聚的机理与裂纹周围的局部高应变以及裂纹前形成的纳米空隙不一致。

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