J. Mater. Sci. Technol. ›› 2020, Vol. 54: 14-19.DOI: 10.1016/j.jmst.2020.02.070
• Research Article • Previous Articles Next Articles
Jia Lia, Haotian Chena, Hui Fenga, Qihong Fanga,*(), Yong Liub, Feng Liub,*(), Hong Wub, Peter K Liawc,*()
Received:
2019-10-10
Revised:
2020-02-06
Accepted:
2020-02-26
Published:
2020-10-01
Online:
2020-10-21
Contact:
Qihong Fang,Feng Liu,Peter K Liaw
Jia Li, Haotian Chen, Hui Feng, Qihong Fang, Yong Liu, Feng Liu, Hong Wu, Peter K Liaw. Microstructure evolution and deformation mechanism of amorphous/crystalline high-entropy-alloy composites[J]. J. Mater. Sci. Technol., 2020, 54: 14-19.
Fig. 1. (a) The amorphous/crystalline HEA FeCoCrNi composite prepared by high-pressure torsion from the experiment [8] and (b, c) the tension model of the amorphous/crystalline HEA structures ( Fe, Co, Cr, and Ni). The atoms are colored by the atom types (b). The atoms are represented by different colors based on the structure types (c).
Fig. 2. Stress vs. strain in the amorphous, crystal, and amorphous/crystal HEA at different thicknesses of the amorphous HEA layer (a) and yielding strength and strain at different thicknesses of the amorphous HEA layers (b).
Fig. 3. The structural evolution at the strain of 20% and different materials: the crystalline HEA (a), the amorphous HEA layer with 3?nm (b), the amorphous HEA layer with 6?nm (c), the amorphous HEA layer with 9?nm (d), the amorphous HEA layer with 12?nm (e), and the amorphous HEA (f) at a strain of 20%. Dotted lines represent interfaces.
Fig. 4. The deformation twins at the strain of 20 % and different amorphous HEA layers: (a, b) 3?nm; (c, d) 6?nm. This region is marked by the blue circles in Fig. 3. TB represents the deformation twin boundary.
Fig. 5. The interface morphology in the strain of 20% and different amorphous HEA layers: (a, e) amorphous HEA layer with 3?nm; (b, f) amorphous HEA layer with 6?nm; (c, g) amorphous HEA layer with 9?nm; (d, h) amorphous HEA layer with 12?nm. (a-d) represent the surface morphology of the interface, and (e-h) represent the atom displacement from the interface.
Fig. 6. The shear strain distribution at the strain of 20% and different materials: the crystalline HEA (a), amorphous HEA layer with 3?nm (b), amorphous HEA layer with 6?nm (c), amorphous HEA layer with 9?nm (d), amorphous HEA layer with 12?nm (e), and amorphous HEA (f). Dotted lines represent interfaces.
Fig. 7. The stress distribution at the strain of 20% and different materials: the crystalline HEA (a), amorphous HEA layer with 3?nm (b), amorphous HEA layer with 6?nm (c), amorphous HEA layer with 9?nm (d), amorphous HEA layer with 12?nm (e), and amorphous HEA (f). Dotted line represents the interface.
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