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INFLUENCE OF GRAIN SIZE AND PERCIPITATIONS ON THE FATIGUE LIVES AND DEFORMATION MECHANISMS IN THE VHCF-REGIME

机译:晶粒尺寸和腐败对伏烃制度疲劳寿命及变形机制的影响

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Research in the field of very high cycle fatigue (VHCF) strongly increased during the last decade. It is meanwhile established that when investigating the deformation mechanisms in the VHCF-regime it has to be separated between inclusion free type I materials and materials with inclusions (type II). Despite all the attempts made so far, a basic understanding on the dominating deformation mechanisms in the VHCF-regime is still missing. Hence, in this study the deformation mechanisms of the aluminium alloy AA6082 ( type II material) were investigated. The material was investigated in the as-received condition and after different heat treatments. The heat treatment changes the deformation mechanism from internal crack initiation to initiation from the surface. In the as-received condition a non-defect crack initiation site was detected. By thorough investigations using EBSD, FIB-techniques and nanoindentation it is shown that featureless crack initiation is rather unlikely to be triggered by the supergrain-mechanism, as it was suggested in literature.
机译:在过去十年中,在非常高的循环疲劳(VHCF)领域的研究强烈增加。同时确定,当研究VHCF制度中的变形机制时,必须在包裹式I型材料和材料之间分离出夹杂物(II型)。尽管迄今为止所做的所有尝试,但仍然缺失了对VHCF制度的主导变形机制的基本理解。因此,在该研究中,研究了铝合金AA6082(II型材料)的变形机制。在接受的条件下和不同的热处理后研究了该材料。热处理改变了从内部裂纹开始的变形机制与表面引发。在接收的条件下,检测到非缺陷裂纹引发位点。通过使用EBSD的彻底调查,FIB技术和纳米凸缘表明,由于在文献中提出了表达,因此不可于衷地触发无特征裂纹启动。

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