Temperature Dependence of the Deformation Behavior of High-Entropy Alloys Co20Cr20Fe20Mn20Ni20, Co19Cr20Fe20Mn20Ni20С1, and Co17Cr20Fe20Mn20Ni20С3. Mechanical Properties and Temperature Dependence of Yield Stress

• Published in: Physical mesomechanics 2024-04, Vol.27 (2), p.113-123
• Main Authors: Astafurova, E. G., Reunova, K. A., Astafurov, S. V., Astapov, D. O.
• Format: Article
• Language: English
• Subjects: Alloys; Carbon; Chromium carbide; Classical Mechanics; Crystal lattices; Crystal structure; Deformation; Dependence; Dispersion hardening alloys; Doping; Elongation; Embrittlement; Grain boundaries; Grain refinement; High entropy alloys; Low temperature; Materials Science; Mechanical properties; Physics; Physics and Astronomy; Plastic flow; Solid solutions; Solid State Physics; Solution strengthening; Temperature; Temperature dependence; Thermal stress; Thermomechanical treatment; Yield strength; Yield stress
• ISSN: 1029-9599; 1990-5424
• DOI: 10.1134/S1029959924020012

This paper discusses the temperature dependence of the mechanical properties of multicomponent alloys Co 20 Cr 20 Fe 20 Mn 20 Ni 20 (Cantor alloy), Co 19 Cr 20 Fe 20 Mn 20 Ni 20 С 1 , and Co 17 Cr 20 Fe 20 Mn 20 Ni 20 С 3 under uniaxial static tension in the temperature range from 77 to 473 K. It is shown that all the alloys acquire an fcc crystal structure after thermomechanical treatment, but the alloy with 3 at % carbon exhibits large incoherent chromium carbides unlike single-phase Co 20 Cr 20 Fe 20 Mn 20 Ni 20 and Co 19 Cr 20 Fe 20 Mn 20 Ni 20 С 1 alloys. Doping with carbon causes solid solution strengthening of the austenitic phase as well as dispersion hardening and moreover promotes grain refinement in the Cantor alloy. Solid solution strengthening contributes to an increase in the athermal and thermal stress components of σ 0.2 , leading to higher yield stress values and stronger temperature dependences σ 0.2 ( T ) in Co 19 Cr 20 Fe 20 Mn 20 Ni 20 С 1 and Co 17 Cr 20 Fe 20 Mn 20 Ni 20 С 3 alloys than in the Cantor alloy. The results of X-ray diffraction and microscopic analysis indicate that, despite the difference in the total concentrations of interstitial atoms in Co 19 Cr 20 Fe 20 Mn 20 Ni 20 С 1 and Co 17 Cr 20 Fe 20 Mn 20 Ni 20 С 3 alloys, the concentrations of carbon dissolved in the crystal lattice of the austenitic phase are close. However, the higher strength properties of Co 17 Cr 20 Fe 20 Mn 20 Ni 20 С 3 compared to Co 19 Cr 20 Fe 20 Mn 20 Ni 20 С 1 are determined primarily by grain boundary strengthening and, to a lesser extent, by dispersion hardening. Both factors such as lowering the deformation temperature and doping with carbon contribute to an increase in the deforming stresses of the Cantor alloy. It is shown that carbon doping affects the staged plastic flow of the Cantor alloy: the tensile curves of Co 19 Cr 20 Fe 20 Mn 20 Ni 20 С 1 carbon alloy exhibit a well-defined stage of microplastic deformation, and the flow curves of Co 17 Cr 20 Fe 20 Mn 20 Ni 20 С 3 alloy have a parabolic shape at the initial stages of plastic flow, which is typical of the deformation of alloys with large incoherent particles. The elongation to failure of Co 20 Cr 20 Fe 20 Mn 20 Ni 20 and Co 19 Cr 20 Fe 20 Mn 20 Ni 20 С 1 alloys increases linearly with decreasing deformation temperature, i.e. the mechanical properties of single-phase alloys are improved in the region of low test temperatures. For Co 17 Cr 20 Fe 20 Mn 20 Ni 20 С 3 alloy, an increase i