Abstract
The effect of the degree of severe plastic deformation (SPD) on the thermal stability of a nanocrystalline CoCrFeNi multi-principal element alloy was studied. The SPD method of high-pressure torsion (HPT) was utilized to achieve the nanocrystalline microstructure. The structural stability was investigated near the centers and edges of the HPT-processed disks deformed for ½, 1, 5 and 10 turns. For almost all studied samples, two exothermic peaks in the temperature ranges of 600–750 and 750–950 K were observed by differential scanning calorimetry (DSC) between room temperature and 1000 K. The saturation released heat value for the first DSC peak was about 4 J/g that was achieved at the shear strain of ∼200. For the second exothermic peak, the released heat saturated at the shear strain of about 20 with the value of about 6–7 J/g. It was revealed that the first DSC peak is related to the annihilation of dislocations for low degree of deformation. At the same time, for edge parts of the disks processed by one or higher numbers of turns the vacancy annihilation has also a major contribution to the first exothermic peak. The annihilated vacancy concentration estimated from the released heat was between (0.6–0.9) × 10−3. The second DSC peak was related to the disappearance of grain boundaries due to recrystallization and annihilation of the remaining dislocations. The HPT-processed CoCrFeNi MPEA samples exhibited very high hardness values between 4000 and 5100 MPa, depending on the number of turns and the location along the disk radius. The hardness decreased only during the second exothermic peak when recrystallization occurred.
Original language | English |
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Article number | 107445 |
Journal | Intermetallics |
Volume | 142 |
DOIs | |
State | Published - Mar 2022 |
Externally published | Yes |
Funding
This work was supported in part by the Ministry of Human Capacities of Hungary within the ELTE University Excellence program ( 1783-3/2018/FEKUTSRAT ); in part by the grant no. VEKOP-2.3.3-15-2016-00002 of the European Structural and Investment Funds; and in part by the National Science Foundation of the United States under Grant No. DMR-1810343 . We acknowledge DESY (Hamburg, Germany), a member of the Helmholtz Association HGF, for the provision of experimental facilities. The preparation of the TEM lamellae by Levente Illés and Andrea Fenyvesi-Jakab is also acknowledged. The authors are grateful to Dr. Zoltán Dankházi and Mr. Gábor Varga for their help in taking the EBSD images. This work was supported in part by the Ministry of Human Capacities of Hungary within the ELTE University Excellence program (1783-3/2018/FEKUTSRAT); in part by the grant no. VEKOP-2.3.3-15-2016-00002 of the European Structural and Investment Funds; and in part by the National Science Foundation of the United States under Grant No. DMR-1810343. We acknowledge DESY (Hamburg, Germany), a member of the Helmholtz Association HGF, for the provision of experimental facilities. The preparation of the TEM lamellae by Levente Ill?s and Andrea Fenyvesi-Jakab is also acknowledged. The authors are grateful to Dr. Zolt?n Dankh?zi and Mr. G?bor Varga for their help in taking the EBSD images.
Keywords
- CoCrFeNi multi-principal element alloy
- Dislocations
- Hardness
- High-pressure torsion
- Released heat
- Thermal stability