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Localized microstructural characterization of a dissimilar metal electron beam weld joint from an aerospace component

机译:航空航天零件的异种金属电子束焊接接头的局部微观结构表征

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Hydrogen induced cold cracking (HICC) and hydrogen embrittlement (HE) are influenced by the microstructural evolution, residual plastic strain (i.e. local misorientation), recrystallization of grains and the resultant grain boundary characteristic distribution (GBCD) brought about by welding processes. HICC and HE are known to cause failures in aerospace components and it is vitally important to quantify the microstructural evolution, degree of residual plastic strain and determine the GBCD across dissimilar weld joints in order to assess the susceptibility of the weld joint to these phenomena. In this investigation a full a microstructural characterization study was carried out at various locations within and around a dissimilar weld joint of pulse-plated nickel (PP-Ni) and Inconel 718 (1N718), taken from an aerospace component Areas examined included the base metals, weld fusion zone and heat affected zones on both sides of the weld joint, formed via electron beam welding. Scanning electron microscopy (SEM) in combination with electron backscatter diffraction (EBSD) was employed to measure the residual plastic strain, grain structure, grain size distribution, crystal orientation distribution, grain boundary misorientation distribution and GBCD of the dissimilar metal weld joint. Finally a metallurgical examination was carried out using SEM on the IN718 HAZ in order to investigate the secondary phase precipitation arising from the welding process. The results shows large variety of GBCD, crystallographic orientation distribution, local plastic strain distribution and grain size, shape and structure distribution across dissimilar weld joint And these localized microstructural characterized data sets need to be carefully transferred using data-driven approach in order to develop predictive multiscale material modelling for hydrogen induced cracking and hydrogen embrittlement.
机译:氢致冷裂(HICC)和氢脆(HE)受微观组织演变,残余塑性应变(即局部取向错误),晶粒再结晶以及焊接过程所产生的晶界特征分布(GBCD)的影响。众所周知,HICC和HE会导致航空航天部件失效,因此,量化微观结构演变,残余塑性应变程度并确定不同焊缝之间的GBCD至关重要,以评估焊缝对这些现象的敏感性。在这项调查中,从航空部件中对脉冲镀镍(PP-Ni)和Inconel 718(1N718)的异种焊接接头内和周围的不同位置进行了全面的微结构表征研究,所研究的区域包括贱金属,焊接接头两侧的焊接熔合区和热影响区,是通过电子束焊接形成的。扫描电子显微镜(SEM)结合电子背散射衍射(EBSD)用于测量异种金属焊接接头的残余塑性应变,晶粒结构,晶粒尺寸分布,晶体取向分布,晶界错取向分布和GBCD。最后,使用SEM对IN718 HAZ进行了冶金检查,以研究焊接过程中产生的第二相沉淀。结果表明,GBCD种类繁多,晶体学取向分布,局部塑性应变分布以及不同焊缝之间的晶粒尺寸,形状和结构分布,并且需要使用数据驱动的方法仔细转移这些局部的微观结构特征数据集,以便进行预测。氢致裂纹和氢脆的多尺度材料建模。

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