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Frontiers of Mechanical Engineering

ISSN 2095-0233

ISSN 2095-0241(Online)

CN 11-5984/TH

Postal Subscription Code 80-975

2018 Impact Factor: 0.989

Front. Mech. Eng.    2023, Vol. 18 Issue (1) : 11    https://doi.org/10.1007/s11465-022-0727-x
RESEARCH ARTICLE
Rapid in situ alloying of CoCrFeMnNi high-entropy alloy from elemental feedstock toward high-throughput synthesis via laser powder bed fusion
Bowen WANG1,2,3, Bingheng LU1,2,3(), Lijuan ZHANG2,3(), Jianxun ZHANG3,4, Bobo LI1,2,3, Qianyu JI1,2,3, Peng LUO2,5, Qian LIU1,2,3
1. School of Mechanical Engineering, Xi’an Jiaotong University, Xi’an 710049, China
2. State Key Laboratory of Manufacturing Systems Engineering, Xi’an Jiaotong University, Xi’an 710049, China
3. National Innovation Institute of Additive Manufacturing, Xi’an 710300, China
4. State Key Laboratory for Mechanical Behavior of Materials, Xi’an Jiaotong University, Xi’an 710049, China
5. Institute of Materials, China Academy of Engineering Physics, Mianyang 621908, China
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Abstract

High-entropy alloys (HEAs) are considered alternatives to traditional structural materials because of their superior mechanical, physical, and chemical properties. However, alloy composition combinations are too numerous to explore. Finding a rapid synthesis method to accelerate the development of HEA bulks is imperative. Existing in situ synthesis methods based on additive manufacturing are insufficient for efficiently controlling the uniformity and accuracy of components. In this work, laser powder bed fusion (L-PBF) is adopted for the in situ synthesis of equiatomic CoCrFeMnNi HEA from elemental powder mixtures. High composition accuracy is achieved in parallel with ensuring internal density. The L-PBF-based process parameters are optimized; and two different methods, namely, a multi-melting process and homogenization heat treatment, are adopted to address the problem of incompletely melted Cr particles in the single-melted samples. X-ray diffraction indicates that HEA microstructure can be obtained from elemental powders via L-PBF. In the triple-melted samples, a strong crystallographic texture can be observed through electron backscatter diffraction, with a maximum polar density of 9.92 and a high ultimate tensile strength (UTS) of (735.3 ± 14.1) MPa. The homogenization heat-treated samples appear more like coarse equiaxed grains, with a UTS of (650.8 ± 16.1) MPa and an elongation of (40.2% ± 1.3%). Cellular substructures are also observed in the triple-melted samples, but not in the homogenization heat-treated samples. The differences in mechanical properties primarily originate from the changes in strengthening mechanism. The even and flat fractographic morphologies of the homogenization heat-treated samples represent a more uniform internal microstructure that is different from the complex morphologies of the triple-melted samples. Relative to the multi-melted samples, the homogenization heat-treated samples exhibit better processability, with a smaller composition deviation, i.e., ≤ 0.32 at.%. The two methods presented in this study are expected to have considerable potential for developing HEAs with high composition accuracy and composition flexibility.

Keywords laser powder bed fusion (L-PBF)      in situ alloying      high-entropy alloys      heat treatment      rapid synthesis     
Corresponding Author(s): Bingheng LU,Lijuan ZHANG   
Just Accepted Date: 30 August 2022   Issue Date: 10 January 2023
 Cite this article:   
Bowen WANG,Bingheng LU,Lijuan ZHANG, et al. Rapid in situ alloying of CoCrFeMnNi high-entropy alloy from elemental feedstock toward high-throughput synthesis via laser powder bed fusion[J]. Front. Mech. Eng., 2023, 18(1): 11.
 URL:  
https://academic.hep.com.cn/fme/EN/10.1007/s11465-022-0727-x
https://academic.hep.com.cn/fme/EN/Y2023/V18/I1/11
Fig.1  Secondary electron micrographs of the different morphologies of the used powders.
Powder elementD10/μmD50/μmD90/μmAverage diameter/μm
Co20.61 ± 0.4838.71 ± 0.0859.16 ± 0.0639.44
Cr25.31 ± 0.2741.84 ± 0.2162.76 ± 0.0943.13
Fe24.25 ± 0.0239.96 ± 0.0459.32 ± 0.0241.13
Mn4.20 ± 0.0324.48 ± 0.0265.44 ± 0.4630.27
Ni25.08 ± 0.3039.90 ± 0.0158.98 ± 0.1041.17
Blended powder14.28 ± 0.1838.21 ± 0.1461.67 ± 0.5338.61
Tab.1  Particle size distributions of the Co, Cr, Fe, Mn, and Ni elemental powders and the blended powder
Fig.2  (a) Morphologies of the prepared elemental powder mixtures, (b) energy-dispersive X-ray spectroscopy mapping, and (c) forming strategy.
SamplesBlended powder/at.%Triple-melted sample/at.%Homogenization heat-treated sample/at.%
Co20.00 ± 0.1521.18 ± 0.2619.80 ± 0.18
Cr20.13 ± 0.2521.18 ± 0.3520.32 ± 0.36
Fe20.02 ± 0.2521.16 ± 0.2820.22 ± 0.31
Mn20.03 ± 0.1816.40 ± 0.2419.93 ± 0.25
Ni19.82 ± 0.1820.39 ± 0.1919.72 ± 0.21
Tab.2  Inductively coupled plasma analysis results of the raw materials used in this study and the chemical composition of the in situ-synthesized CoCrFeMnNi HEA samples via different L-PBF sequences
No.Laser power/WScanning speed/(mm?s?1)Hatch distance/μmLayer thickness/μmVED/(J?mm?3)
1280970904080
2280870904089
32807709040101
42806709040116
52805709040136
62804709040165
Tab.3  Process parameters used in this study
Fig.3  Longitudinal section optical micrographs of as-built single-melted samples at VEDs of (a) 80 J/mm3, (b) 89 J/mm3, (c) 101 J/mm3, (d) 116 J/mm3, (e) 136 J/mm3, and (f) 165 J/mm3.
Fig.4  Longitudinal section optical micrographs of in situ-alloyed CoCrFeMnNi HEA with different numbers of melting steps: (a) single melting, (b) double melting, (c) triple melting, and (d) quadruple melting.
Fig.5  Scanning electron microscopy and energy-dispersive X-ray spectroscopy mapping of the in situ-synthesized CoCrFeMnNi high-entropy alloy from elemental powders through different processes: (a) single-melted samples (laser power: 280 W, scanning speed: 670 mm/s, hatch space: 90 μm, layer thickness: 40 μm, and VED: 116 J/mm3), (b) triple-melted samples, and (c) single-melted + homogenization heat-treated samples.
Fig.6  XRD patterns of the initial elemental powder mixture, single-melted samples, triple-melted samples, and homogenization heat-treated samples, with peak (111) enlarged.
Fig.7  3D crystallographic orientation demonstration and the corresponding pole figures and inverse pole figures of the (a) single-melted samples, (b) triple-melted samples, and (c) homogenization heat-treated samples (applied to single-melted samples).
Fig.8  Engineering tensile stress–strain curves of the triple-melted samples and homogenization heat-treated samples.
Samplesσ0/MPaσGB/MPaσdis/MPaσy/MPaEstimated YS/MPaDeviation/%
Triple-melted samples14791.6347.3585.9610.24.0
Homogenized samples14782.495.6325.0293.810.6
Tab.4  All strengthening components and estimated YS
Fig.9  Transmission electron microscopy bright field images of (a) triple-melted samples with cellular substructures and (b) homogenization heat-treated samples (applied to single-melted samples) without cellular substructures.
Samplesσy/MPaUTS/MPaεf/%Reference
Triple-melting samples610.2 ± 15.8735.3 ± 14.114.4 ± 0.9Present work
Homogenized samples293.8 ± 8.1650.8 ± 16.140.2 ± 1.3Present work
L-PBF samples from pre-alloyed powders582.9 ± 10.8679.8 ± 12.923.8 ± 1.4[16]
L-PBF samples from pre-alloyed powders519.0601.035.0[26]
LMD samples from pre-alloyed powders346.0566.026.0[50]
Electron beam welding samples320.0617.027.0[51]
Gas W arc welding samples297.0530.015.0[51]
Tab.5  Tensile properties of triple-melted samples, homogenization heat-treated samples, and samples produced using other processes
Fig.10  (a) Tensile fracture surface of the triple-melted samples and (b) homogenization heat-treated samples.
Abbreviations
AMAdditive manufacturing
EBSDElectron backscatter diffraction
EDSEnergy-dispersive X-ray spectroscopy
FCCFace-centered cubic
HEAHigh-entropy alloy
ICPInductively coupled plasma
IPFInverse pole figure
L-PBFLaser powder bed fusion
LMDLaser metal deposition
PFPole figure
SEMScanning electron microscopy
TEMTransmission electron microscopy
UTSUltimate tensile strength
VEDVolumetric energy density
XRDX-ray diffraction
YSYield strength
Variables
aA constant
bBurgers vector
dAverage grain size
GShear modulus
hHatch spacing
kStrengthening coefficient
MTaylor factor
PLaser power
tLayer thickness
vScanning speed
ρDislocation density
σ0Friction stress
σdisStrengthened dislocation
σGBGrain boundary strengthening
σyYield strength
εfElongation to failure
  
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