疲劳FeCrAl合金位错组织的几个方面

S.C. Tjong, L.T. Wu, N.J. Ho
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引用次数: 17

摘要

Fe25Cr4Al和Fe25Cr2Al (wt.%)合金在不同的总应变幅下在空气中循环变形。根据应变减小的顺序,观察到四种不同的组织:在总应变约1%及以上时,两种合金中均有普通的位错胞结构;中间应变下的“迷宫”或“迷宫”结构,同样适用于两种合金;然而,在最低应变率下,在2%铝合金中发现了典型的环状斑块结构,而在4%合金中发现了迷宫(迷宫)结构的前体。这种前体结构似乎与Mori等人观察到的相同。因此,两种合金之间的区别似乎在于绕过了4%合金中的环片结构,而是直接构建了偶极或多极壁。因此,在2%合金中观察到的软化是由于环形斑块的形成。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Some aspects of the dislocation microstructures in fatigued FeCrAl alloys

Fe25Cr4Al and Fe25Cr2Al (wt.%) alloys were cyclically deformed in air at various total strain amplitudes. Four different structures were observed, in order of decreasing strain: ordinary dislocation cell structures in both alloys at about 1% total strain and above; and “maze” or “labyrinth” structures at intermediate strains, again for both alloys; however, at the lowest strain rates, a typical loop patch structure was found in the 2% aluminium alloy but a precursor to the maze (labyrinth) structure was found in the 4% alloy. That precursor structure seems to be the same as that observed by Mori et al. It would thus appear that the difference between the two alloys lies in the bypassing of the loop-patch structure in the 4% alloy, with, instead, direct construction of dipolar or multipolar walls. Thus the softening observed in the 2% alloy is due to the formation of the loop patches.

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