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Article

Preparation and Strengthening Mechanisms of Ultrasonic-Assisted Cr3C2 Particle-Reinforced Al Matrix Composite

1
College of Materials Science and Engineering, Xi’an Shiyou University, Xi’an 710065, China
2
State Key Laboratory for Mechanical Behavior of Materials, Xi’an Jiaotong University, Xi’an 710049, China
*
Authors to whom correspondence should be addressed.
Coatings 2022, 12(4), 459; https://doi.org/10.3390/coatings12040459
Submission received: 11 February 2022 / Revised: 10 March 2022 / Accepted: 22 March 2022 / Published: 28 March 2022

Abstract

:
A novelty Al matrix composite reinforced with Cr3C2 particles was prepared by an ultrasound vibration treatment-assisted casting process. The Cr3C2 content on the microstructure and mechanical properties of Cr3C2p/Al composite were researched systematically. The results indicated that Cr3C2 particles were effectively distributed around the grain boundary and led to a great reduction in crystalline size. The density, porosity, and Vickers hardness of the composites rose simultaneously with the increase of Cr3C2 content. Meanwhile, the tensile strength and yield strength increased by 104.5% and 85.7%, respectively by adding 3.0 wt. % Cr3C2. The fracture morphologies showed that the fracture mechanism was plastic fracture for the pure Al and gradually transformed to brittle fracture as the content of Cr3C2 exceeded 3.0 wt. %. Moreover, the strengthening mechanism of the composite was also discussed.

1. Introduction

Particle-reinforced metal matrix composites (PRMMCs) are widely used for structure applications because of their high specific strength and stiffness compared with conventional alloys, as well as their isotropic properties and relatively straightforward processing compared with continuous fiber-reinforced composites [1]. Particulate ceramic-reinforced Al matrix composite [2,3,4,5] possesses low density, high strength, and outstanding corrosion resistance, which has led to it being considered as a promising material and applied in the fields of electronic engineering, spacecraft, and petroleum engineering. As is generally known, the adhesive strength, wettability, and interfacial reaction of the Al matrix and reinforced particles have a significant effect on the mechanical properties of the composite. A stronger interface would usually allow for effective load transfer from the Al matrix to the reinforced particle, leading to improved strength, stiffness, and resistance to the external environment. Indeed, the pair of their thermal expansion coefficients should be matching between a couple of composites, which can effectively decrease the micro-cracks in the interface and enhance bonding strength during the fabrication process.
Potential reinforcement particles such as Al2O3 [6], TiB2 [7], Si3N4 [8] and TiC [9] were commonly used to improve the microstructure and mechanical properties of Al matrix composite and three preparation methods, namely powder metallurgy [10], in-situ synthesis [11], and stirring casting [12], were available. Guo et al. [13] researched the influence of ceramic particle dimension on the mechanical performance of the SiCp/Al matrix composite. The composite reinforced by 13 μm SiC ceramic particles (high hardness and insulator) possessed the highest hardness, while the highest strength was held by the 5 μm particle of the specimen. The hardness of the specimen accompanied by the strength declined due to the increase in ceramic particle size. Gao et al. [3] prepared the Al–Cu composite reinforced with TiB2 ceramic using the in situ synthesis method and studied the effect of the ultrasonic stirring time on the microstructure, strength, and toughness of the composite. The experimental results indicated that ultrasonic stirring improved the possibility of subsequent reactions and formed more dispersive TiB2. TiB2 ceramic particle agglomeration was reduced and the crystalline size of the material declined with the increase of ultrasonic stirring time. Besides this, the yield strength was also improved by extending the ultrasonic stirring time. The microstructure and mechanical performance of the particulate-reinforced Al matrix composite fabricated by strongly ultrasonic stirring were superior to the one prepared by mechanical stirring. The Cu element’s surface was coated with layer-structural Ti3AlC2 ceramic particles by Wang, which effectively improved the composite interface [14]. Then, the coated Ti3AlC2 was added into the Al matrix composite. The adhesive strength and mechanical properties were enhanced distinctly due to the generation of the Al2Cu transitional phase. Moreover, the tribological properties of the material were also improved, which was attributed to the increase in mechanical performance.
It can be seen that TiB2 and Ti3AlC2 ceramics both exhibited metal-like electrical conductivity through fitting the interface with aluminum. Chromium carbides had three different crystallographic structures: orthorhombic Cr3C2, hexagonal Cr7C3, and cubic Cr23C6. Orthorhombic Cr3C2 possesses the best mechanical properties. Cr3C2 ceramic phase, a highly metallic carbide, was an outstanding potential material with high modulus, high hardness, high melting point, outstanding wear and corrosion resistance. Cr3C2-Ni composites had been fabricated in situ in our previous researche [15,16,17] and the physical performance, tribological properties, and oxidation resistance were studied systematically. The studied results demonstrated that strong interfacial bonding forces and good wettability were present in Cr3C2 and Ni. Cr3C2 can act as the heterogeneous nucleation of Ni. Cr3C2 particles had no interface reaction with aluminum. The coefficient of thermal expansion of Cr3C2 ceramic was similar to metal, like Al and Ni, which can effectually promote the interfacial bonding of ceramic and metallic materials.
Certainly, highly metallic Cr3C2 particles would be possible options to reinforce the Al matrix which may have an impressive combination of mechanical properties and good resistance to corrosion. Based on our previous research, Cr3C2 ceramic particles added into the Al matrix composite by mechanical stirring can effectively eliminate large agglomerations, but this is impossible for 50–100 μm small agglomerations, especially for small particles. Ultrasonic vibration is an outstanding technology to deal with molten-liquid aluminum and magnesium alloys [18,19]. Ultrasonic vibration treatment (UVT) can be used to improve the particulate distribution of composites by dispersing particles to create more effective reinforcements due to Orowan strengthening [20]. Unfortunately, few studies about using UVT to improve the particulate distribution of aluminum matrix composites reinforced with high volumes of Cr3C2 particles were available so far. The smaller Cr3C2 particles are easily agglomerated. In order to improve the situation, we used ultrasonic vibration treatment, which allowed the Cr3C2 particles to be more evenly distributed in the Al matrix.
In this work, a novelty Al matrix composite reinforced with Cr3C2 particles was prepared by an ultrasound vibration treatment-assisted casting process. Micro scale particles (1–5 μm) of Cr3C2 and the influence of its content on microstructure and mechanical properties of Cr2 particle-reinforced Al matrix composite are highlighted in this paper. Besides this, the strengthening mechanism of the composite is also discussed in detail.

2. Experimental Procedure

2.1. Fabrication of Cr3C2 Particle-Reinforced Al Matrix Composite

In this paper, Cr3C2 particle-reinforced Al matrix composite was fabricated using pure Al ingot (99.99%) and Cr3C2 powder by an ultrasound-assisted casting process at 760 °C for 30 min. The details of the sketch of the UVT system can be found in reference material [3]. The vibration frequency of the UVT system was 20 ± 1 kHz. The purity and crystalline sizes of Cr3C2 powder were 99.9% and 1–5 μm, respectively. The holding time of ultrasonic vibration stirring was 10 min. A certain amount of Cr3C2 particle (1.0 wt. %, 2.0 wt. %, 3.0 wt. % and 4.0 wt. %) was added in the matrix. The molten liquid was poured into the graphite die after removing the contaminants on the surface of the molten liquid. The ingot casting was cut to the standard dimension for microstructure characterization and mechanical properties tests. The sample was ground and polished to remove traces of the linear cutting by using the waterproof abrasive paper from 800# to 7000#. The sample was then slightly etched for 1 min using the Kohler reagent to observe the microstructure of the composite.

2.2. Mechanical Properties Test

The density and porosity were tested by the Archimedean drainage method which had also been reported in reference material [21]. Vickers hardness (HV) tests were conducted using the hardness tester equipped with the diamond cone indenter, and the angle was 120°. The load and loading time were 60 kg and 10 s, respectively. The strength and toughness of the Cr3C2 particle-reinforced Al matrix composite were tested using the tensile testing machine INSTRON 1195 (INSTRON (Shanghai) Test Equipment Trading Co., Ltd., Shanghai, China). The tensile rate was 0.5 mm/min and the average value of three groups of tests was confirmed as the final value.

2.3. Materials Characterization

The detailed phases of the initial powder and the Cr3C2 particle-reinforced Al matrix composite were detected and demarcated by X-Ray Diffraction (XRD). Scanning electron microscopy (SEM) was applied to research the microstructure morphologies of the Cr3C2 particle-reinforced Al matrix composite. The distribution of different elements was detected by Energy Disperse Spectroscopy (EDS). The crystalline grain was dyed and the crystalline grain size was calculated by the software of Image-Pro plus 6.0.

3. Results and Discussion

3.1. Microstructure of Cr3C2p/Al Composite

The SEM figure and EDS result of the initial Cr3C2 powder can be seen the Figure 1a,b. The crystalline grain sizes of the Cr3C2 powder were 1–5 μm and the distribution of the powder is homogeneous. The EDS results indicate high purity of the Cr3C2 powder. Figure 1c shows the particle size distribution of the initial Cr3C2 powder. The percentages of the Cr3C2 powder with 0–1 μm, 1–2 μm, 2–3 μm, 3–4 μm, and 4–5 μm are 26%, 38%, 24%, 7%, and 5%, respectively. The average particle size of the initial Cr3C2 powder was 1.83 μm after calculation.
Figure 2a shows the XRD results of Cr3C2 particle-reinforced Al matrix composite. The enlarged drawing for the 4.0 wt. % Cr3C2p/Al sample is shown in Figure 2b. Compared with the pure Al sample, the diffraction peaks of Cr3C2 can be detected for the Cr3C2p/Al samples. Moreover, the diffraction peaks of Al shift to the left side, which can be attributed to the mutual diffusion of Cr and Al elements. The diffusion of Cr in Al will lead to an increase in the lattice constant and interplanar crystal spacing (d) of Al atoms. According to the Bragg law (2d·sinθ = n·λ), the diffraction angle (θ) will decrease and the diffraction peaks of Al will shift to the left side.
The SEM morphologies and dyed results of Cr3C2 particle-reinforced Al matrix composite are shown in Figure 3a–j. The average crystalline size of the pure Al sample is about 105 μm. The distribution of the microstructure becomes homogeneous with the increase of Cr3C2 content. Besides, the average crystalline size of the composite declines at the first stage and then increases slightly with the increase of Cr3C2 content. Some etch pits of Cr3C2 ceramic particles can be seen in the microstructure because of the slightly corrosion of Kohler reagent, as shown in Figure 3d,e. The grain shapes of the big Cr3C2 ceramic particles are granular, which well corresponds with the initial Cr3C2 powder in Figure 1. According to the computed results by using the software of Image-Pro plus 6.0, the average crystalline sizes of the 2.0 wt. % and 4.0 wt. % Cr3C2 particle-reinforced Al matrix composite samples are about 21 μm and 51 μm, respectively. Therefore, their average crystalline sizes decrease by 80% and 51.4%, respectively. The declined average crystalline grain size can improve simultaneously the strength and toughness of the Cr3C2 particle-reinforced Al matrix composite via grain refinement.
The element distributions of the 1.0 wt. % Cr3C2p/Al composite sample are also shown in Figure 4. The grain boundaries are clear and homogeneous. It can be observed that the Al element as the matrix can be detected distinctly (Figure 4b). As shown in Figure 4c,d, Cr and C elements congregate among the grain boundaries, indicating that Cr3C2 ceramic particles serve as the heterogeneous nucleus regions for the Al matrix during the process of solidification. The average crystalline grain size can be refined.

3.2. Mechanical Properties of Cr3C2p/Al Composite

Figure 5a–c represents the effects of Cr3C2 content on the density, porosity, and Vickers hardness of Cr3C2 particle-reinforced Al matrix composite, respectively. The densities of Cr3C2 and Al are 6.68 and 2.7 g/cm3, respectively. As we know, the hardness of Cr3C2 is higher than that of Al matrix. Logically, the density and hardness of the Cr3C2p/Al composite will rise simultaneously with the increase in Cr3C2 content. In contrast, the increase in porosity can be attributed to the increase in the grain boundaries. Figure 5d–f shows the SEM morphologies of the indenter for the pure Al, 2.0 wt. %, and 4.0 wt. % Cr3C2p/Al composite samples. The outlines of the indenter are clear and the micro-cracks were not detected after the hardness tests, indicating excellent toughness of the Cr3C2p/Al composite. The areas of the indenter decrease obviously with the increase in Cr3C2 content, which can also indicate the higher hardness of the Cr3C2 particle-reinforced Al matrix composite compared to pure Al. From Figure 5f, it can be seen that the Cr3C2 ceramic particles are removed because of the corrosion action of the Kohler reagent. Moreover, the micro-cracks are also not detected at the grain boundaries of Cr3C2 and Al, which can be attributed to the bonding strength interface.
Figure 6a shows the stress–strain curves of the Cr3C2 particle-reinforced Al matrix composite with different Cr3C2 amounts added. Obviously, the stress rises, while the strain declines with the addition of Cr3C2 ceramic particles. Pure Al possesses the best toughness, and the toughness declines rapidly as the Cr3C2 content exceeds 3.0 wt. %. The 3.0 wt. % Cr3C2p/Al composite sample behaves with the best tensile strength and yield strength. As shown in Figure 6b,c, the tensile strengths of pure Al, 1.0 wt. %, 2.0 wt. %, 3.0 wt. %, and 4.0 wt. % Cr3C2p/Al composite samples are 44 MPa, 62 MPa, 73 MPa, 90 MPa, and 79 MPa, respectively. Their yield strengths are 26.3 MPa, 33.1 MPa, 37.4 MPa, 48.8 MPa, and 45.7 MPa, respectively. Compared with the pure Al sample, the tensile strengths of 1.0 wt. %, 2.0 wt. %, 3.0 wt. %, and 4.0 wt. % Cr3C2p/Al composite samples increase by 40.9%, 65.9%, 104.5%, and 79.5%, respectively. Therefore, it can be concluded that the strength is enhanced distinctly due to the addition of the Cr3C2 ceramic particles.

3.3. Fracture Morphology

The fracture morphologies of the Cr3C2 particle-reinforced Al matrix composite samples are shown in Figure 7a–j. Figure 7a shows the fracture morphologies of the pure Al sample. There is no impurity element for the pure Al sample and it can be seen that the fracture is smooth. From Figure 7a–e, it can be observed that the area of the fracture morphology rises distinctly with an increase of the Cr3C2 content, which is in good agreement with the result of the section shrinkage rate. Cr3C2 ceramic particles and large dimples can be seen in Figure 7g,h, indicating that the 1.0 wt. % and 2.0 wt. % Cr3C2p/Al composite samples exhibit excellent ductility. However, the sizes of the dimples decrease as the Cr3C2 content exceeds 3.0 wt. %. Moreover, the micro-cracks and cleavage steps exist on the fracture morphologies for the 3.0 wt. % and 4.0 wt. % Cr3C2p/Al composite samples, as labeled in Figure 7i,j. The generation and extension of the micro-cracks will result in fracture mechanism changes from ductile fracture to brittle fracture.
Figure 8 represents the effects of the Cr3C2 content on the elongation and section shrinkage rate of the Cr3C2 particle-reinforced Al matrix composite. The tensile strength and yield strength increase distinctly as mentioned above, while the elongation and section shrinkage rate decline with the addition of Cr3C2 ceramic particles. The 2.0 wt. % Cr3C2p/Al composite sample exhibits the best elongation and the 1.0 wt. % Cr3C2p/Al composite sample shows the best section shrinkage rate by adding Cr3C2 ceramic particles. From Figure 8a,b, it can be observed that the elongation and section shrinkage rate decline obviously when the addition of Cr3C2 ceramic particle exceeding 3.0 wt. %. The declining ductility will transform the fracture mechanism from ductile fracture to brittle fracture.

3.4. Strengthening Mechanism

There are four accessible strengthening mechanisms [22,23,24,25,26] for the enhancement of the yield strength of the Cr3C2 particle-reinforced Al matrix composite: grain refinement strengthening (σg), load-bearing strengthening (σLoad), CTE mismatch strengthening (σCTE), and Orowan strengthening (σOrowan). Orowan strengthening is mainly because of the dislocation movement, which can go through or around the second phase particles. However, the limit of Orowan strengthening [27] is the crystalline grain sizes of the second phase particles, which should be less than 1 μm. In this study, the crystalline grain sizes of Cr3C2 ceramic particles are 1–5 μm. Therefore, Orowan strengthening is not appropriate for this study. The final predicted result of yield strength (σp) can be calculated by the following equation:
σp = σm + σg + σLoad + σCTE
where σm is the yield strength of the Al matrix. In this study, σm is 26.3 MPa. As we know, grain refinement strengthening (σg) can be calculated by the Hall–Petch equation [28] as following:
σg = k(dc−1/2 − dm−1/2)
where k is the strengthening factor, dc is the average crystalline grain size of the Cr3C2 particle-reinforced Al matrix composite, and dm is the average crystalline grain size of the Al matrix. According to the reference [29], the strengthening factor of Al is 68 MPa μm1/2. In this study, the average crystalline grain sizes of pure Al, 1.0 wt. %, 2.0 wt. %, 3.0 wt. %, and 4.0 wt. % Cr3C2p/Al composite samples are 105 μm, 23 μm, 21 μm, 34 μm, and 51 μm, respectively.
During the experimental process, the load has an important factor on the yield strength of the Cr3C2 particle-reinforced Al matrix composite. The load-bearing strengthening (σLoad) can be calculated by the following equation [30]:
σLoad = 1/2Vpσm
where Vp is volume fraction of Cr3C2 ceramic particles. In this study, the volume fractions of 1.0 wt. %, 2.0 wt. %, 3.0 wt. %, and 4.0 wt. % Cr3C2p/Al composite samples are 0.41%, 0.82%, 1.23%, and 1.66%, respectively.
The difference of the coefficient of thermal expansion (CTE) between Cr3C2 ceramic particles and the pure Al matrix will easily generate dislocations during the solidification process, which also has a significant effect on the yield strength of the Cr3C2 particle-reinforced Al matrix composite. In this study, the coefficient of thermal expansion of Cr3C2 ceramic particle and pure Al are 10.3 × 10−6 K−1 and 23.6 × 10−6 K−1, respectively. The CTE mismatch strengthening (σCTE) can be calculated by the following equations [31]:
σCTE = βGmb(ρCTE)1/2
ρCTE = 12ΔαΔTVp/(bdp(1 − Vp))
where β is the constant value of 1.25, and Gm is the shear modulus of pure Al; it can be calculated by Gm = Em/(2(1 + v)), in which Em and v are the Young modulus and Poisson’s ratio of pure Al, respectively. Δα is the difference value of the coefficient of thermal expansion of the pure Al and Cr3C2 ceramic particles, ΔT is the difference value of the casting temperature and room temperature, Vp is the volume fraction of Cr3C2 ceramic particle, b is the Burgers vector with the value of 0.286 nm, and dp is the average crystalline grain size of the Cr3C2 particles. The detailed parameter values of them for the enhancement of the yield strength of Cr3C2 particle-reinforced Al matrix composite are shown in Table 1.
The final predicted result and experimental result of the yield strength of Cr3C2p/Al composite are shown in Table 2. From this table, it can be seen that the predicted result of the yield strength is in good accordance with the experimental result for the Cr3C2p/Al composite samples. Moreover, it can be concluded that the main strengthening mechanisms for the improvement of the yield strength are grain refinement strengthening (σg) and CTE mismatch strengthening (σCTE).

4. Conclusions

In this paper, a novel Al matrix composite reinforced with Cr3C2 particles was prepared by an ultrasound-assisted casting process at 760 °C for 30 min. The effects of Cr3C2 content on the microstructure and mechanical properties of Cr3C2p/Al composite were researched systematically for the first time. The conclusions could be obtained as following:
  • Compared with the pure Al sample, the average crystalline sizes of 1.0 wt. % Cr3C2p/Al composite decreased by 80%. The decreased average crystalline grain size can simultaneously improve the strength and toughness of the Cr3C2p/Al composite via grain refinement strengthening.
  • The fracture morphologies showed that the fracture mechanism was plastic fracture for the pure Al, 1.0 wt. %, and 2.0 wt. % Cr3C2p/Al composite samples, which gradually transformed to brittle fracture as the content of Cr3C2 exceeded 3.0 wt. %.
  • After calculation, the predicted result of the yield strength was in good accordance with the experimental result for the Cr3C2p/Al composite samples. The main strengthening mechanisms for the improvement of the yield strength were grain refinement strengthening (σg) and CTE mismatch strengthening (σCTE).

Author Contributions

Conceptualization, W.Z. and L.S.; methodology, W.Z.; software, X.L.; validation, Y.X. and Y.W.; formal analysis, Y.L.; investigation, H.D.; resources, W.Z.; data curation, Y.X.; writing—original draft preparation, W.Z.; writing—review and editing, W.Z.; visualization, L.S.; supervision, X.L.; project administration, Y.L.; funding acquisition, W.Z. All authors have read and agreed to the published version of the manuscript.

Funding

This research was funded by [W. Zhai] grant number [20192110, HKDNM2019018, 2020JQ-777 and 20JK0837], [L. Sun] grant number [20202212, HKDNM201811 and 2019JQ-821] and [Y. Xue] grant number [YCS21111016].

Institutional Review Board Statement

The study was approved by the Institutional Review Board of Xi’an Shiyou University.

Informed Consent Statement

Not applicable.

Data Availability Statement

Not applicable.

Acknowledgments

This work was supported by the Open Fund of State Key Laboratory for Mechanical Behavior of Materials (20192110 and 20202212), the Open Fund of National Joint Engineering Research Center for Abrasion Control and Molding of Metal Materials (HKDNM201811 and HKDNM2019018), the Natural Science Basic Research Plan in Shaanxi Province of China (2019JQ-821 and 2020JQ-777), the Scientific Research Program Funded by Shaanxi Provincial Education Department (20JK0837) and the Graduate Student Innovation and Practical Ability Training Program of Xi’an Shiyou University (YCS21111016).

Conflicts of Interest

The authors declare no conflict of interest.

References

  1. Gupta, S.; Hammann, T.; Johnson, R.; Riyad, M.F. Synthesis and Characterization of Novel Al-Matrix Composites Reinforced with Ti3SiC2 Particulates. J. Mater. Eng. Perform. 2014, 24, 1011–1017. [Google Scholar] [CrossRef]
  2. Durai, T.; Das, K.; Das, S. Synthesis and characterization of Al matrix composites reinforced by in situ alumina particulates. Mater. Sci. Eng. A 2007, 445-446, 100–105. [Google Scholar] [CrossRef]
  3. Gao, Q.; Wu, S.; Lü, S.; Xiong, X.; Du, R.; An, P. Improvement of particles distribution of in-situ 5 vol% TiB2 particulates reinforced Al-4.5Cu alloy matrix composites with ultrasonic vibration treatment. J. Alloy. Compd. 2017, 692, 1–9. [Google Scholar] [CrossRef]
  4. Yu, Z.; Wu, G.; Sun, D.; Chen, J.; Jiang, L. Rare-earth oxide coating for sub-micro particulates reinforced aluminum matrix com-posites. Mater. Sci. Eng. A 2003, 357, 61–66. [Google Scholar] [CrossRef]
  5. Elsabbagh, M.; Soliman, M.; Taha, M.; Palkowski, H. Hot rolling behaviour of stir-cast Al 6061 and Al 6082 alloys—SiC fine particulates reinforced composites. J. Mater. Process. Technol. 2012, 212, 497–508. [Google Scholar] [CrossRef]
  6. Li, Y.; Langdon, T.G. Creep behavior of an Al-6061 metal matrix composite reinforced with alumina particulates. Acta Mater. 1997, 45, 4797–4806. [Google Scholar] [CrossRef]
  7. Zhang, Y.; Ma, N.; Wang, H.; Le, Y.; Li, X. Damping capacity of in situ TiB2 particulates reinforced aluminium composites with Ti addition. Mater. Des. 2007, 28, 628–632. [Google Scholar] [CrossRef]
  8. Chen, W.; Shi, H.; Xin, H.; He, N.R.; Yang, W.; Gao, H. Friction and wear properties of Si3N4-hBN ceramic composites using different synthetic lubricants. Ceram. Int. 2018, 44, 16799–16808. [Google Scholar] [CrossRef]
  9. Kaftelen, H.; Ünlü, N.; Goller, G.; Öveçoğlu, M.L.; Henein, H. Comparative processing-structure–property studies of Al–Cu matrix composites reinforced with TiC particulates. Compos. A Appl. Sci. Manuf. 2011, 42, 812–824. [Google Scholar] [CrossRef]
  10. Fathy, A.; El-Kady, O.; Mohammed, M.M. Effect of iron addition on microstructure, mechanical and magnetic properties of Al-matrix composite produced by powder metallurgy route. Trans. Nonferrous Met. Soc. China 2015, 25, 46–53. [Google Scholar] [CrossRef]
  11. Li, S.; Su, Y.; Ouyang, Q.; Zhang, D. In-situ carbon nanotube-covered silicon carbide particle reinforced aluminum matrix composites fabricated by powder metallurgy. Mater. Lett. 2016, 167, 118–121. [Google Scholar] [CrossRef]
  12. Wang, H.; Li, G.; Zhao, Y.; Chen, G. In situ fabrication and microstructure of Al2O3 particles reinforced aluminum matrix com-posites. Mater. Sci. Eng. A 2010, 527, 2881–2885. [Google Scholar] [CrossRef]
  13. Guo, X.; Guo, Q.; Nie, J.; Liu, Z.; Li, Z.; Fan, G.; Xiong, D.-B.; Su, Y.; Fan, J.; Zhang, D. Particle size effect on the interfacial properties of SiC particle-reinforced Al-Cu-Mg composites. Mater. Sci. Eng. A 2018, 711, 643–649. [Google Scholar] [CrossRef]
  14. Wang, S.; Zhu, S.; Cheng, J.; Qiao, Z.; Yang, J.; Liu, W. Microstructural, mechanical and tribological properties of Al matrix composites reinforced with Cu coated Ti3AlC2. J. Alloy. Compd. 2017, 690, 612–620. [Google Scholar] [CrossRef]
  15. Zhai, W.; Gao, Y.; Huang, Z.; He, L. Cr3C2-20% Ni cermets prepared by high energy milling and reactive sintering, and their mechanical properties. Adv. Appl. Ceram. 2016, 115, 327–332. [Google Scholar] [CrossRef]
  16. Zhai, W.; Gao, Y.; Sun, L.; Wang, Y.; Niwa, K.; Hasegawa, M. High pressure in-situ synthesis and physical properties of Cr3C2-Ni cermets. Ceram. Int. 2017, 43, 17202–17205. [Google Scholar] [CrossRef]
  17. Zhai, W.; Gao, Y.; Sun, L.; He, L.; Wang, Y. Improvement of high temperature oxidation behavior of Cr3C2-20wt.% Ni cermets by adding 1wt.% Mo. J. Alloy. Compd. 2018, 731, 271–278. [Google Scholar] [CrossRef]
  18. Lü, S.; Wu, S.; Lin, C.; Hu, Z.; An, P. Preparation and rheocasting of semisolid slurry of 5083 Al alloy with indirect ultrasonic vibration process. Mater. Sci. Eng. A 2011, 528, 8635–8640. [Google Scholar] [CrossRef]
  19. Hu, Z.; Li, X.; Yan, H.; Wu, X.Q.; Qun, H.; Lin, J.W. Effects of ultrasonic vibration on microstructure evolution and elevat-ed-temperature mechanical properties of hot-extruded Mg-6Al-0.8Zn-2.0Sm wrought magnesium alloys. J. Alloys. Compd. 2016, 685, 58e64. [Google Scholar] [CrossRef]
  20. Zhang, Z.; Chen, D.L. Consideration of Orowan strengthening effect in particulate-reinforced metal matrix nanocomposites: A model for predicting their yield strength. Scr. Mater. 2006, 54, 1321–1326. [Google Scholar] [CrossRef]
  21. Wang, L.; Wang, Q.; Lu, K. Density of liquid GaSb measured by an improved Archimedean method. J. Cryst. Growth 2006, 293, 14–17. [Google Scholar] [CrossRef]
  22. Sajjadi, S.; Ezatpour, H.; Parizi, M.T. Comparison of microstructure and mechanical properties of A356 aluminum alloy/Al2O3 composites fabricated by stir and compo-casting processes. Mater. Des. 2012, 34, 106–111. [Google Scholar] [CrossRef]
  23. Xue, N.; Liu, W.; Zhu, L. Muthuramalingam. Effect of scandium in Al-Sc and Al-Sc-Zr alloys under precipitation strengthening mechanism at 350 °C Aging. Met. Mater. Int. 2021, 27, 5145–5153. [Google Scholar]
  24. Cao, F.; Chen, C.; Wang, Z.; Muthuramalingam, T.; Anbuchezhiyan, G. Effects of silicon carbide and tungsten carbide in aluminium metal matrix composites. Silicon 2019, 11, 2625–2632. [Google Scholar]
  25. Liu, S.; Wang, Y.; Muthuramalingam, T.; Anbuchezhiyan, G. Effect of B4C and MOS2 reinforcement on micro structure and wear properties of aluminum hybrid composite for automotive applications. Compos. B Eng. 2019, 176, 107329. [Google Scholar] [CrossRef]
  26. Manoj, M.; Jinu, G.R.; Muthuramalingam, T. Multi Response Optimization of AWJM Process Parameters on Machining TiB2 Particles Reinforced Al7075 Composite Using Taguchi-DEAR Methodology. Silicon 2018, 10, 2287–2293. [Google Scholar] [CrossRef]
  27. Miller, W.; Humphreys, F. Strengthening mechanisms in particulate metal matrix composites. Scr. Met. Mater. 1991, 25, 33–38. [Google Scholar] [CrossRef]
  28. Sigworth, G.K. Communication on mechanism of grain refinement in aluminum. Scr. Mater. 1995, 34, 919–922. [Google Scholar] [CrossRef]
  29. Kumar, N.; Gautam, R.K.; Mohan, S. In-situ development of ZrB2 particles and their effect on microstructure and mechanical properties of AA5052 metal-matrix composites. Mater. Des. 2015, 80, 129–136. [Google Scholar] [CrossRef]
  30. Kim, C.; Sohn, I.; Nezafati, M.; Ferguson, J.; Schultz, B.; Bajestani-Gohari, Z.; Rohatgi, P.; Cho, K. Prediction models for the yield strength of particle-reinforced unimodal pure magnesium (Mg) metal matrix nanocomposites (MMNCs). J. Mater. Sci. 2013, 48, 4191–4204. [Google Scholar] [CrossRef]
  31. Alizadeh, M. Strengthening mechanisms in particulate Al/B4C composites produced by repeated rolling bonding process. J. Alloy. Compd. 2011, 509, 2243–2247. [Google Scholar] [CrossRef]
Figure 1. SEM figure, EDS result and particle size distribution of the initial Cr3C2 powder: (a) SEM figure, (b) EDS result, and (c) particle size distribution.
Figure 1. SEM figure, EDS result and particle size distribution of the initial Cr3C2 powder: (a) SEM figure, (b) EDS result, and (c) particle size distribution.
Coatings 12 00459 g001
Figure 2. The XRD results of Cr3C2 particle-reinforced Al matrix composite: (a) XRD results and (b) the enlarged drawing for the 4.0 wt. % Cr3C2p/Al sample.
Figure 2. The XRD results of Cr3C2 particle-reinforced Al matrix composite: (a) XRD results and (b) the enlarged drawing for the 4.0 wt. % Cr3C2p/Al sample.
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Figure 3. SEM morphologies and dyed results of Cr3C2 particle-reinforced Al matrix composite: (a,f) pure Al, (b,g) 1.0 wt. % Cr3C2p/Al composite, (c,h) 2.0 wt. % Cr3C2p/Al composite, (d,i) 3.0 wt. % Cr3C2p/Al composite, and (e,j) 4.0 wt. % Cr3C2p/Al composite.
Figure 3. SEM morphologies and dyed results of Cr3C2 particle-reinforced Al matrix composite: (a,f) pure Al, (b,g) 1.0 wt. % Cr3C2p/Al composite, (c,h) 2.0 wt. % Cr3C2p/Al composite, (d,i) 3.0 wt. % Cr3C2p/Al composite, and (e,j) 4.0 wt. % Cr3C2p/Al composite.
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Figure 4. The element distributions of the 1.0 wt. % Cr3C2p/Al composite sample: (a) microstructure, (b) Al element, (c) Cr element, and (d) C element.
Figure 4. The element distributions of the 1.0 wt. % Cr3C2p/Al composite sample: (a) microstructure, (b) Al element, (c) Cr element, and (d) C element.
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Figure 5. The mechanical properties and the indenter morphologies of the Cr3C2 particle-reinforced Al matrix composite: (a) density, (b) porosity, (c) Vickers hardness, (d) pure Al, (e) 2.0 wt. % Cr3C2p/Al composite, and (f) 4.0 wt. % Cr3C2p/Al composite.
Figure 5. The mechanical properties and the indenter morphologies of the Cr3C2 particle-reinforced Al matrix composite: (a) density, (b) porosity, (c) Vickers hardness, (d) pure Al, (e) 2.0 wt. % Cr3C2p/Al composite, and (f) 4.0 wt. % Cr3C2p/Al composite.
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Figure 6. The stress-strain curves, tensile strength, and yield strength of the Cr3C2 particle-reinforced Al matrix composite with different Cr3C2 amounts added: (a) stress–strain curves, (b) tensile strength and (c) yield strength.
Figure 6. The stress-strain curves, tensile strength, and yield strength of the Cr3C2 particle-reinforced Al matrix composite with different Cr3C2 amounts added: (a) stress–strain curves, (b) tensile strength and (c) yield strength.
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Figure 7. The fracture morphologies of the Cr3C2 particle-reinforced Al matrix composite: (a,f) pure Al, (b,g) 1.0 wt. % Cr3C2p/Al composite, (c,h) 2.0 wt. % Cr3C2p/Al composite, (d,i) 3.0 wt. % Cr3C2p/Al composite, and (e,j) 4.0 wt. % Cr3C2p/Al composite.
Figure 7. The fracture morphologies of the Cr3C2 particle-reinforced Al matrix composite: (a,f) pure Al, (b,g) 1.0 wt. % Cr3C2p/Al composite, (c,h) 2.0 wt. % Cr3C2p/Al composite, (d,i) 3.0 wt. % Cr3C2p/Al composite, and (e,j) 4.0 wt. % Cr3C2p/Al composite.
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Figure 8. The elongation and section shrinkage rate of the Cr3C2 particle-reinforced Al matrix composite: (a) elongation and (b) section shrinkage rate.
Figure 8. The elongation and section shrinkage rate of the Cr3C2 particle-reinforced Al matrix composite: (a) elongation and (b) section shrinkage rate.
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Table 1. The detailed parameter values for the CTE mismatch strengthening of the Cr3C2p/Al composite.
Table 1. The detailed parameter values for the CTE mismatch strengthening of the Cr3C2p/Al composite.
Sampledp/nmVpβGm/GPaEm/GPavb/nmΔα/10−6 K−1ΔT/K
1.0 wt. % Cr3C2p/Al32000.41%1.2526.3700.330.28613.3735
2.0 wt. % Cr3C2p/Al0.82%
3.0 wt. % Cr3C2p/Al1.23%
4.0 wt. % Cr3C2p/Al1.66%
Table 2. The final predicted result and experimental result of the yield strength.
Table 2. The final predicted result and experimental result of the yield strength.
Sampleσm/MPaσg/MPaσLoad/MPaσCTE/MPaσp/MPaMeasured YS/MPa
1.0 wt. % Cr3C2p/Al26.37.50.0546.840.633.1
2.0 wt. % Cr3C2p/Al26.38.20.1089.744.337.4
3.0 wt. % Cr3C2p/Al26.35.00.16211.943.448.8
4.0 wt. % Cr3C2p/Al26.32.90.21813.843.245.7
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MDPI and ACS Style

Xue, Y.; Zhai, W.; Li, X.; Sun, L.; Wang, Y.; Liu, Y.; Dong, H. Preparation and Strengthening Mechanisms of Ultrasonic-Assisted Cr3C2 Particle-Reinforced Al Matrix Composite. Coatings 2022, 12, 459. https://doi.org/10.3390/coatings12040459

AMA Style

Xue Y, Zhai W, Li X, Sun L, Wang Y, Liu Y, Dong H. Preparation and Strengthening Mechanisms of Ultrasonic-Assisted Cr3C2 Particle-Reinforced Al Matrix Composite. Coatings. 2022; 12(4):459. https://doi.org/10.3390/coatings12040459

Chicago/Turabian Style

Xue, Yisong, Wenyan Zhai, Xiao Li, Liang Sun, Yiran Wang, Yanming Liu, and Hui Dong. 2022. "Preparation and Strengthening Mechanisms of Ultrasonic-Assisted Cr3C2 Particle-Reinforced Al Matrix Composite" Coatings 12, no. 4: 459. https://doi.org/10.3390/coatings12040459

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