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L12-strengthened high-entropy alloys for advanced structural applications

Published online by Cambridge University Press:  22 June 2018

Tao Yang
Affiliation:
Center for Advanced Structural Materials, College of Science and Engineering, City University of Hong Kong, Hong Kong, China
Yilu Zhao
Affiliation:
Center for Advanced Structural Materials, College of Science and Engineering, City University of Hong Kong, Hong Kong, China
Weihong Liu*
Affiliation:
Center for Advanced Structural Materials, College of Science and Engineering, City University of Hong Kong, Hong Kong, China
Jijung Kai
Affiliation:
Center for Advanced Structural Materials, College of Science and Engineering, City University of Hong Kong, Hong Kong, China
Chaintsuan Liu*
Affiliation:
Center for Advanced Structural Materials, College of Science and Engineering, City University of Hong Kong, Hong Kong, China
*
a)Address all correspondence to this author. e-mail: chainliu@cityu.edu.hk

Abstract

Advanced alloys with both high strength and ductility are highly desirable for a wide range of engineering applications. Conventional alloy design strategies based on the single-principle element are approaching their limits in further optimization of their performances. Precipitation-hardened high-entropy alloys (HEAs), especially those strengthened by coherent L12-nanoparticles, have received considerable interest in recent years, enabling a new space for the development of advanced structural materials with superior mechanical properties. In this review, we highlight recent important advances of the newly developed L12-strengthened HEAs, including the aspects of computation-aided alloy design, unique properties, atomic-level characterization, phase evolution, and stability. In particular, we focus our attention on elucidating fundamental scientific issues involving the alloying effects, precipitation behaviors, mechanical performances, and the corresponding deformation mechanisms, all of which provide a comprehensive metallurgical understanding and guidance for the design of this new class of HEAs. Finally, future research directions and prospects are also critically assessed.

Information

Type
Invited Review
Copyright
Copyright © Materials Research Society 2018 
Figure 0

FIG. 1. Phase diagram calculations of the (a) (CoCrNi)97−xTi3Alx alloy (at.%) and (b) AlxCo1.5CrFeNi1.5Tiy alloy (in mole ratio) using Thermo-Calc software.28,52 The equilibrium phase mole fraction of the (c) L12 phase and (d) Heusler phase as a function of temperature calculated using the thermal-calc method for the (FeCoNiCr)100−x−yAlxTiy system (at.%).30 Some experimental data points are marked in (c) and (d).

Figure 1

FIG. 2. (a–d) TEM images and electron diffraction patterns from the as-cast Al0.5CrFeCoNiCu HEA (in mole ratio). STEM-EDX maps of the Cu-rich dendritic region are shown at the bottom of the figure, revealing the nanoscale spinodal decomposed structures with L12 nanoparticles.53

Figure 2

FIG. 3. APT results and DFT calculations of the L12-strengthened Fe–Co–Ni–Al–Ti-based HEA.57 (a) Atom maps showing the nanoscale element distribution. (b) Proximity histogram constructed across the interface between the matrix and precipitates. (c) First-principles calculations of the L12 nanoparticles with different sublattice occupancies.

Figure 3

TABLE I. Tensile properties of representative single-fcc and L12-strengthened HEAs at room temperature.

Figure 4

FIG. 4. (a) Mechanical properties of the L12-strengthened (CoCrNi)94Al3Ti3 alloy (at.%) compared to that of single-phase CoCrNi base alloy.28 (b) Ultimate tensile strength at room temperature versus tensile elongation of the present alloy in comparison with commercial superalloys.

Figure 5

FIG. 5. (a) Tensile properties of the L12-strengthened Fe–Co–Ni–Al–Ti-based HEA at ambient and cryogenic temperature.57 The inset shows the typical microstructure before deformation. (b) TEM images showing the deformation microstructures of high-density nanospacing SFs at cryogenic temperature.

Figure 6

FIG. 6. (a) Staircase-like true stress–strain curves of the (NiCoFeCr)94Ti2Al4 HEA (at.%) at six different temperatures from 750 to 900 °C using a strain-rate-jump method.61 (b) Steady-state flow stress as a function of strain rate at different temperatures. The tensile data of FeCoNiCrMn at 800 °C are also included for a direct comparison.

Figure 7

FIG. 7. TEM observations of the (NiCoFeCr)94Ti2Al4 HEA (at.%) deformed at 750 °C, showing apparent dislocation shearing through numerous γ′ particles in the matrix. (a) dark field image showing high-density sphere γ′ particles, (b) corresponding SAED pattern showing L12 superlattice, (c) magnified image showing single particle with clear anti-phase boundary and (d) bright field image showing apparent dislocation shearing through numerous γ′ particles in the matrix.61

Figure 8

FIG. 8. High-temperature properties of Ni47.9Al10.2Co16.9Cr7.4Fe8.9Ti5.8Mo0.9Nb1.2W0.4C0.4 (at.%) high-entropy superalloy (HESA).38 (a) Creep performance at 982, 850, and 750 ºC/159 MPa. (b) γ′ rafting parallel to the stress axis under 982 ºC/159 MPa creep. The dislocation morphology of the as-crept HESA also shown as inset. (c) Deconvolution of the {200} reflection peak of the L12-strengthened HESA at 982 °C. (d) Unrafted γ′ microstructure after 800 h creep tests at 750 °C.

Figure 9

FIG. 9. Phase identification (a–c) and elemental distribution (d–i) of the Al0.3CuFeCrNi2 HEA (in mole ratio) aged at 700 °C.35

Figure 10

FIG. 10. Coarsening rates for the (NiCoFeCr)94Ti2Al4 HEA (at.%) with respect to aging temperature compared to a number of Ni-based alloys.41