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Article

Bonding SiCp/Al Composites via Laser-Induced Exothermic Reactions

by
Yifeng Wang
,
Guangjie Feng
*,
Yan Wei
,
Bingxu Hu
and
Dean Deng
College of Materials Science and Engineering, Chongqing University, No. 174, Shazhengjie, Chongqing 400044, China
*
Author to whom correspondence should be addressed.
Crystals 2021, 11(5), 535; https://doi.org/10.3390/cryst11050535
Submission received: 20 April 2021 / Revised: 6 May 2021 / Accepted: 10 May 2021 / Published: 12 May 2021
(This article belongs to the Special Issue Preparation, Microstructure Evolution and Mechanical Study of the Brazed Joints)
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Abstract

:
In this paper, the SiCp/Al composites were bonded via laser-induced exothermic reactions of a Ni–Al–Zr interlayer. The Ni–Al–Zr interlayer was designed based on its exothermic property and chemical compatibility with the SiCp/Al composites. The influences of the interlayer composition and bonding pressure on the joint microstructure and shear strength were investigated. Results indicated that high exothermic reactions occurred in the Ni–Al–Zr interlayer and realized the reliable bonding with the SiCp/Al composites. The interlayer products were the eutectic structure of NiAl+Ni2AlZr+Ni3Al5Zr2. NiAl3 and Ni2Al3 reaction layers were formed at the bonding interfaces. The interlayer composition and the bonding pressure determined the morphology and distribution of the voids and the reaction layers, thus controlling the joint shear strength. When the SiCp/Al composites were bonded using the interlayer with the Zr content of 15 wt.% under the bonding pressure of 3 MPa, the joint shear strength reached the maximum of 24 MPa.

1. Introduction

Particle-reinforced aluminum matrix composites, such as SiCp/Al composites [1], Si3N4/Al composites [2], SiO2/Al composites [3], Al2O3/Al composites [4], B4C/Al composites [5], and TiC/Al composites [6], process excellent electrical and chemical properties, as well as the comprehensive mechanical performances, and have been important structural materials in aerospace, electronics, and automobile industries. Among them, the SiCp/Al composites are particularly attracting attention and are usually used to manufacture components with complex structures in practical applications [7,8]. However, the poor processibility of the SiCp/Al composites have greatly limited their potential applications. The deformation processing will damage the interfacial bonding between the reinforced SiC particles and the aluminum matrix, thus causing the degeneration of mechanical performances [9]. Due to the SiC particles with high hardness, machining is also not suitable for the SiCp/Al composites [10]. One solution for this issue is that the component with complex structure can be manufactured through bonding modular SiCp/Al composite pieces together. From the above viewpoint, developing a technique for reliable bonding SiCp/Al composites can further broaden their applications and is of great importance.
Since there are great differences in the chemical and physical properties between the reinforcements and matrix, it is extremely difficult to realize the reliable bonding of SiCp/Al composites [11]. It mainly has three difficulties. First, at high temperature, harmful interfacial reactions will occur between the SiC particles and aluminum matrix, forming a large quantity of brittle Al4C3 compounds and resulting in the degeneration of mechanical properties. Long et al. [12] investigated the laser welding of SiCp/Al composites. They found that the high temperature during the laser welding led to the evaporation of the aluminum matrix and the excess interfacial reactions, forming large numbers of pores and brittle Al4C3. Adding appropriate Zr could partly inhibit the generation of large-size brittle phase Al4C3 in the joint. Second, at low temperature, the SiC particles can hardly react with surrounding materials and the bonding at the interface is very weak. Third, the alumina film on the surface of aluminum matrix also blocks the atomic diffusion at the bonding interface. To achieve a sound joint, during the welding, the interfacial reactions between the reinforcements and matrix should be inhibited to prevent the degradation of materials properties. At the same time, the metallurgical reactions between the SiC particles and surrounding materials must be enhanced to form a reliable bonding at the interface. To meet the above requirements, the chemical reactions in the bonding couple must be controlled precisely. Unfortunately, although great efforts have been done on the bonding of SiCp/Al composites, these problems have not been solved fundamentally.
Compared with conventional welding techniques, such as fusion welding [13], brazing [14,15], diffusion bonding [16], etc., the exothermic bonding has some inherent advantages on the bonding of SiCp/Al composites. It utilizes the exothermic reactions in the interlayer as the heat source to enhance the atomic activities and promote the metallurgical reactions at the bonding interface [17]. It can quickly (105–106 K/s) heat the narrow area at the bonding interface to a high temperature (about 2000 K), and the adjacent part of substrates remains a low temperature [18,19]. The transient high temperature could not only significantly increase the chemical activity of SiC particles at the bonding interface and enhance the metallurgical reactions with the filler metals, but also avoid the harmful thermal damage on the substrates. Swiston et al. [20] bonded the bulk metallic glass with the assistance of the exothermic reactions in the reactive multilayer foils. They found that during the bonding, the rapid heating and cooling made crystallization of metallic glasses unlikely. The thermal damage on the metallic glasses was voided successfully. Lin et al. [21] bonded carbon–carbon composites using the Ti/Ni–Al/Ti interlayer. They found that the exothermic reactions in the Ni–Al interlayer enhanced the metallurgical reactions and formed the NiAlx and TiCy(Oz) phases at the bonding interface. In our previous study [22], the Cf/Al composites were bonded to the TiAl alloys using the exothermic bonding technique. A defect-free joint was achieved successfully. Although many efforts have been done on this bonding method, the exothermic bonding of SiCp/Al composites has been seldom reported.
As a fundamental research, this work is to explore the feasibility of bonding SiCp/Al composites via laser-induced exothermic reactions. A Ni–Al–Zr interlayer was designed and used as the bonding interlayer. The exothermic characteristics of the interlayer were analyzed. The typical joint microstructure was characterized. The influences of the bonding parameters on the microstructural evolution and mechanical property of the joint were investigated systematically.

2. Experimental Procedures

The SiCp/Al composites applied in this study were fabricated using the squeeze casting method. The volume fraction of SiC particles was 50% and the aluminum matrix was the 6063 aluminum alloy. The microstructure of the SiCp/Al composites was given in Figure 1. Prior to the bonding, the SiCp/Al composites were cut into small pieces with the sizes of 12 mm × 6 mm × 2 mm and 5 mm × 5 mm × 4 mm, respectively. Then, all the bonding surfaces were polished by the diamond abrasive discs to 600#, and cleared in acetone for 10 min with the assistance of ultrasonic to remove the impurities.
The raw materials to prepare the powder interlayer were the commercial Ni (99.5%, 28 µm), Al (99.5%, 28µm), and Zr (99.5%, 28 µm) powders purchased from Beijing Xingrongyuan Technology Co., Let. The weighted powders were put in an agate jar and milled with alumina balls for 60 min. Ten (10) mL Hexane was added in the agate jar as the process controlling agent and to prevent the oxidation of the powders. The rotational speed was set as 300 rpm and the mass ratio of the grinding media to the material was 10:1. Then, 0.5 g milled powders were cold-pressured to a cylindrical compact (Φ 10 mm). The bonding process was conducted in the argon atmosphere. The joining schematic diagram is represented in Figure 2. During the bonding, the exothermic interlayer was applied between the SiCp/Al substrates. A laser beam (YAG-W100E, P = 200 W, Han’s Laser Technology Industry Group Co., Ltd, Shenzhen, China) heated the interlayer and ignited the interlayer. Then, the combustion flame propagated to the other side and finished the bonding process.
The exothermic performance of the interlayer, the joint interfacial microstructure, and interlayer products were characterized by the differential scanning calorimetry (DSC, NETZSCH STA449C, Erich NETZSCH GmbH & Co. Holding KG, Selb, Germany), scanning electron microscopy (SEM, FEI Nova400, FEI Company, Hillsboro, OR, USA) equipped with the energy-dispersive spectrometer (EDS, FEI Company, Hillsboro, OR, USA), and X-ray diffraction (XRD, D8 ADVANCE, Bruker Company, Karlsruhe, Germany). The joint shear strength was tested at room temperature using the universal test machine (Instron-1186, Instron Corporation, Canton, OH, USA) with a shear rate of 0.5 mm·min−1. The schematic diagram of the shear test is shown in Figure 3.

3. Results and Discussion

3.1. Design of the Exothermic Interlayer

Unlike the conventional welding methods, the exothermic bonding depends on the exothermic reactions in the interlayer to supply the required heat. At the same time, the reaction products of the interlayer remains in the bonding couple as a part of the joint. Therefore, the bonding quality is determined by the exothermic characteristics of the bonding interlayer and the properties of the interlayer products. To realize the reliable bonding of the SiCp/Al composites, there are two important problems needed to be solved. First, during the bonding process, a reliable metallurgical bonding should be formed between the composites and the filler metals. Second, the harmful interfacial reactions between the reinforcements and matrix should be prevented. Thus, on one hand, it needs a high temperature at the bonding interface to enhance the metallurgical reactions between the SiC particles and the surrounding materials. On the other hand, the high-temperature region should be localized around the bonding interface and should be as smaller as possible. Meanwhile, the high temperature residence time should also be very short to avoid the excess interfacial reactions in the SiCp/Al substrates. In consequence, it requires that the interlayer should have a high exothermicity and a rapid heat releasing characteristic.
There are three kinds of exothermic systems, which were the (i) mixed active metal and nonmetal with a small atomic diameter (Ti–B [23], Ti–C [24], Ti–Al–C [25], Ti–Al–B [26]), (ii) thermites (Al–CuO [27], Al–Fe2O3 [28]), and (iii) mixed metals (Ni–Al [29], Ti–Al [30]), respectively. Among them, the Ni–Al exothermic system has a high exothermic property and a stable combustion characteristic [31]. Thus, the Ni–Al exothermic system was chosen as the fundamental exothermic system. According to the Ni–Al phase diagram in Figure 4a, several exothermic reactions can occur between Ni and Al. Different Ni:Al ratios lead to different exothermic reactions and release different quantity of heat, forming different intermetallic compounds, such as NiAl3, Ni2Al3, NiAl, Ni5Al3, and Ni3Al. To design the exothermic interlayer with the highest exothermicity, the adiabatic temperatures (Tad) of the Ni–Al systems with different Ni:Al ratios were calculated using the following equation.
Δ H 298 + ∫ 298 T a d 298 ∑ n j C P P j d T + ∑ 298 ~ T a d 298 n j L P j = 0
where, Pj and nj respectively refer to the products and their stoichiometric coefficients. CP(Pj) and L(Pj) are the heat capacity and phase transformation enthalpy (if a phase change occurs) of the products, respectively.
The calculation results suggest that the equimolar Ni–Al system has the highest Tad (1912 K). During the exothermic bonding, the combustion stability is also very important. Merzhanov et al. put forward an empirical formula to evaluate the self-sustained reaction [32]. It indicates that when the exothermic reaction has a Tad higher than 1800 K, the exothermic reaction can self-sustained. According to the empirical formula, the equimolar Ni-Al system can self-sustained once being ignited.
During the welding of the SiCp/Al composites, one problem is the weak bonding between the SiC particles and filler metals owing to the high chemical inertness of the SiC reinforcements. To increase the bonding quality, the chemical affinity of the SiC reinforcements and the interlayer products should be promoted. In the brazing of SiC ceramics, the active filler metals (containing Ti or Zr) were usually used. It indicated that the Zr element could react with the SiC ceramics and form the ZrC and Zr2Si reaction layers. By means of the reaction layers between the active elements and the SiC ceramics, a reliable bonding could be ensured. Thus, in this study, the Zr element was added into the Ni–Al system, forming the Ni–Al–Zr interlayer. There are two reasons to the addition of the Zr element. First, the Zr element is the active element and the carbide-forming element. It can easily react with the SiC particles and form a reliable metallurgical bonding. Second, according to the Ni–Al–Zr ternary phase diagram (Figure 4b), the Ni–Al–Zr system can form a eutectic product of NiAl + Ni–Al–Zr. The formation of the eutectic products can lower the solidification temperature and prolong the existence time of the liquid phase. Thus, under the action of the bonding pressure, the interlayer products can be densified much more easily, which can largely decrease the formation of the voids in the joint.
To evaluate the exothermic property of the interlayer, the DSC test was conducted on the Ni–Al and Ni–Al–Zr interlayer (Figure 5). For the Ni–Al interlayer, there were two sharp exothermic peaks, which were located at the heating temperature of 840 K and 916 K, respectively. The main exothermic peak was at the heating temperature of 840 K. After adding a small amount of Zr element, the position of exothermic peaks changed slightly and shifted to 762 K and 904 K, respectively. The height of the exothermic peaks decreased slightly. This is mainly caused by the addition of Zr acting as a diluent and absorbing some reaction heat. Meanwhile, after the addition of Zr in the Ni–Al interlayer, the position of the main exothermic peak decreased by 78 K, which meant that the exothermic reactions in the interlayer could be ignited more easily. The additive Zr is necessary since it can largely enhance the metallurgical bonding and increase the bonding quality. If the Zr content is in an appropriate range, the Ni–Al–Zr interlayer still can maintain a high exothermicity and can provide sufficient heat for the bonding. According to above calculation method and the previous study [17], when the Zr content ranges in 0 wt.% ~36.08 wt.%, the Tad of the Ni–Al–Zr system was still maintained at a high temperature (1912 K) and the high exothermicity of the Ni–Al–Zr interlayer could be ensured.

3.2. Joint Microstructure

Figure 6 shows the microstructure of the SiCp/Al joint bonded using a Ni–Al–Zr interlayer under a pressure of 3 MPa. It could be seen from the overall morphology in Figure 6a that the interlayer reacted completely and formed a good bonding with the substrates. In the center of the joint, the interlayer products were quite dense. Near the bonding interface, there were some pores and some residual Al. This phenomenon was mainly owing to the particularity of the exothermic bonding. During the bonding, the exothermic reactions occurred in the interlayer and released a great amount of heat. At the center of the interlayer, the interlayer products were maintained at a high temperature and were in a solid–liquid state. Under the bonding pressure, they could be easily densified and the pores were largely eliminated. However, in the regions near the bonding interfaces, the SiCp/Al substrates were maintained at the room temperature and absorbed some reaction heat from the interlayer. So, the interlayer products cooled rapidly and could hardly be fully densified, forming the voids in the region near the bonding interface.
To analyze the characteristics of the joint in detail, the morphologies at the bonding interface and the interlayer products were enlarged in Figure 6b,c. It could be seen from Figure 6b that at the bonding interface, the interlayer products bonded well with the SiCp/Al composites. No cracks and voids can be observed at the bonding interface. In the SiCp/Al composites near the bonding interface, some dark gray block phase (point A) and white needle-like phase (point B) were formed. Two continuous reaction layers, which were the dark gray layer (point C) and the gray layer (point D), were formed at the bonding interface. Near the reaction layers, some off-white phases (point E) were also observed. In Figure 6c, the interlayer products presented a eutectic feature. It consisted of large dark block phase (point F), gray reticular phase (point G), and white small block phase (point H). To determine the phase composition of the joint, the EDS analysis was conducted on the above zones and the results were given in Table 1. The dark gray phases (point A and C), gray reaction layer (point D), and off-white phase (point E) consisted of Ni and Al elements. The ratios of Ni:Al were about 1:3, 2:3 and 1:1, respectively. According to the Ni–Al phase diagram and previous studies [17,22], they were supposed to be the NiAl3, Ni2Al3, and NiAl, respectively. The white need-like phase (point B) consisted of Ni, Al, and Zr elements and was confirmed as the (Ni,Zr)Al3 phase. The interlayer products were a mixture of three phases. According to the phase diagram and previous studies [33,34], the dark phase (point F) was confirmed to be the NiAl phase. The gray reticular phase (point G) and white small block phase (point H) were supposed to be the Ni3Al5Zr2 and Ni2AlZr, respectively. The formation of Ni3Al5Zr2 and Ni2AlZr was mainly caused by the Zr atoms replacing the places of Ni or Al atoms in the NiAl space lattice. To further confirm the phase composition of the interlayer products, the XRD test was carried out. The peak refinement was conducted with the assistance of the MDI Jade software. According to the study by Chérif et al. [35] and the peak refinement results in Figure 7, the interlayer products were confirmed as a mixture of NiAl+Ni3Al5Zr2+Ni2AlZr, which proved the above analysis.

3.3. Influence of the Interlayer Chemical Composition on the Joint Microstructure

With the increase of Zr content in the interlayer, the joint morphology underwent a dramatic change, as shown in Figure 8. These changes were mainly displayed in two aspects. First, with the increase of the Zr content, the density of the joint had a significant improvement. The amount and the size of the voids in the joint decreased obviously. Second, with the increase of the Zr content, the residual white Ni particles gradually increased. When the Zr content was 20 wt.%, there were large numbers of the residual Ni particles around the bonding interfaces and some large voids were also observed at the bonding interfaces.
To analyze the microstructure of the joints in detail, the regions of the interlayer products and the bonding interfaces were enlarged in Figure 9 and Figure 10, respectively. It could be seen that the interlayer products with different Zr contents all presented a eutectic morphology of mixed dark NiAl phase and white Ni–Al–Zr IMC, as shown in Figure 9. When the Zr content was 5 wt.%, the Ni–Al–Zr IMC was less and separated by the dark block NiAl phase. With the increase of the Zr content, its volume fraction increased gradually. The Ni–Al–Zr IMC became continuous gradually and the grain of the NiAl phase decreased obviously. Compared with the NiAl phase, the ternary Ni–Al–Zr compounds had a much higher hardness and brittleness [36]. Thus, with the increase of the Zr content, the high-volume fraction of the Ni–Al–Zr IMC increased the brittleness of the interlayer products. On the other hand, the higher volume fraction of the Ni–Al–Zr IMC also meant the increase of the eutectic liquid in the interlayer products. During the exothermic bonding process, the higher volume fraction of the eutectic liquid promoted the densification process and was conducive to eliminating the voids in the joints. Thus, the amount and the sizes of the voids in the joint gradually decreased.
The interfacial microstructures of the different bonding interfaces with different Zr contents were demonstrated in Figure 10. With the increase of the Zr content, the interfacial microstructures at the bonding interfaces mainly changed in two ways. On one hand, the NiAl3 and Ni2Al3 reaction layers at the interfaces became discontinuous gradually. On the other hand, the amount and the size of the residual Ni particles increased gradually at the bonding interfaces. These changes were mainly due to the different exothermicities of the interlayers with different Zr contents. The analysis in Section 3.1 indicated that the exothermic reactions between the Ni and Al could release a large quantity of heat and provided the required energy for the bonding process. During the bonding, the additive Zr absorbed some reaction heat and acted as the coolant. Thus, with the increase of the Zr content, the exothermicity of the interlayer had a slightly decrease. The decrease of the exothermicity shorted the high-temperature residence time of the bonding interface and reduced the atomic activity at the bonding interface, thus affecting the interfacial reaction. The reaction layers became thinner and continuous gradually. Meanwhile, since the interlayer exothermicity decreased with the increase of the Zr content and the SiCp/Al composites absorbed some heat, the cooling rate at the bonding interface increased significantly. It affected the exothermic reactions in this region. The reactions in this region were incomplete and some residual Ni particles were observed. With the increase of the Zr content, the residual Ni particles became more and more plentiful. Zr element is a carbide-forming element. Qi et al. [37] and Zhou et al. [38] brazed SiC ceramics with filler metals containing Zr element. They suggested the Zr element promoted the metallurgical reactions between the SiC ceramic and the filler metals. In this study, the higher Zr content in the interlayer also enhanced the bonding quality between the SiCp/Al composites and the interlayer. As the Zr content increased, the voids and the unconnected areas gradually disappeared. When the Zr content was 15 wt.%, the SiCp/Al composites had a reliable bonding with the interlayer and no defects were observed at the bonding interface. However, with the further increase of the Zr content, the voids appeared again due to the low exothermicity of the interlayer.

3.4. Influence of the Bonding Pressure on the Joint Microstructure

The microstructures of the SiCp/Al joints bonded at different bonding pressures were shown in Figure 11. Under different bonding pressures, the density of the joints changed significantly. The reaction products were the eutectic structure of NiAl+Ni–Al–Zr IMC, as shown in Figure 6. During the bonding process, the interlayer products were in the solid–liquid state. Under the action of the bonding pressure, the interlayer products were squeezed by the adjacent substrates, and the original pores in the interlayer could be largely eliminated. The higher the bonding pressure was, the denser the interlayer products were. When the bonding pressure was low (1.5 MPa), a large number of the voids were observed in the joint. With the increase of the bonding pressure, the amount and size of the voids decreased significantly. When the bonding pressure reached 3 MPa, large voids disappeared in the joint. There were only some small voids distributed in the region adjacent to the bonding interface. The density and bonding quality of the joint had a dramatic improvement. When the bonding pressure further increased to 4 MPa, the small voids around the bonding interfaces almost disappeared. The joint density was quite high. However, since the interlayer products were a mixture of brittle NiAl and Ni–Al–Zr IMC, under high bonding pressure, a fracture occurred in the interlayer products and propagated to the SiC/Al composites, as shown in Figure 11d.

3.5. Joint Shear Strength

The shear strength was used to evaluate the joint mechanical property. With the increase of the Zr content in the interlayer, the joint shear strength first increased and reached the highest value (24 MPa) when the Zr content was 15 wt.%, then it decreased to 15 MPa, as shown in Figure 12. The joint shear strength depended on the joint microstructure [39]. As analyzed in Section 3.3, the Zr content influenced the joint microstructure in three ways, which were (i) the joint density, (ii) the residual Ni particles, and (iii) the reaction layers at the bonding interfaces, respectively. When the Zr content was 5 wt.%, the interlayer products were mainly the NiAl phase. The low-volume fraction of the Ni–Al–Zr IMC led to less eutectic liquid during the bonding process. Thus, the original pores in the interlayer were unable to be eliminated effectively. The large number of the voids in the joint greatly affected the mechanical property of the joint. With the increase of the Zr content, the amount and size of the voids in the joint decreased significantly. When the Zr content was 8 wt.%, the voids were small and mainly distributed around the bonding interfaces. The joint shear strength slightly increased to 16 MPa. When the Zr content reached 15 wt.%, the voids in the joint further decreased. However, the high Zr content slightly reduced the exothermicity of the interlayer. Since the adjacent SiCp/Al substrates absorbed some reaction heat from the interlayer, the reactions in the region near the bonding interfaces were incomplete. Some residual Ni particles were observed around the bonding interfaces. The decrease of the interlayer exothermicity also affected the interfacial reactions at the bonding interfaces. The reaction layers became thinner and uncontinuous gradually. It should be noticed that there was a competitive relationship between the joint density and the reaction layers. With the increase of the Zr content, the joint density gradually increased, which was beneficial to the joint shear strength. Meanwhile, the reaction layers became thinner and uncontinuous gradually, which had unfavorable effects for the bonding quality. The joint mechanical performance was a combined result of these two aspects. When the Zr content was 15 wt.%, these two aspects were in a balance. Thus, the joint shear strength reached the highest value (24 MPa). With the further increase of the Zr content, the joint density did not continue to increase. The high fraction of Ni–Al–Zr IMC greatly increased the brittleness of the interlayer products. The large amount of the residual Ni particles and the thin reaction layers greatly affected the bonding quality. Thus, the joint shear strength decreased to 15 MPa when the Zr content was 20 wt.%.
The influence of the bonding pressure on the joint shear strength was similar to that of Zr content, as shown in Figure 12. The bonding pressure mainly influenced the joint density. When the bonding pressure was 1.5 MPa, the interlayer products only had small extrusion deformation. The original pores in the interlayer were largely kept in the joint. The large amount of the voids decreased the joint’s ability to withstand loads. The joint shear strength was as low as 4 MPa. With the increase of the bonding pressure, the interlayer products suffered a larger extrusion deformation, which effectively reduced the amount and size of the voids. In consequence, the joint shear strength had an obvious increase. When the bonding pressure was 3 MPa, there were only some small voids distributed around the bonding interfaces. The joint shear strength reached the maximum of 24 MPa. When the bonding pressure further increased to 4 MPa, the high pressure led to the fracture of the brittle interlayer products. Continuous cracks were formed in the joint. It significantly affected the joint mechanical performance. The joint shear strength decreased to 21 MPa.

4. Conclusions

(1) The equimolar Ni–Al system was chosen as the fundamental exothermic system due to its high exothermic property. The active Zr element was added to promote the metallurgical reactions between the SiC particles and the interlayer. NiAl3, Ni2Al3 reaction layers were formed at the bonding interfaces and ensured the reliable bonding of the SiCp/Al composites.
(2) The additive Zr transformed the interlayer products from the NiAl to the eutectic organization of NiAl + Ni2AlZr + Ni3Al5Zr. Higher Zr content increased the joint density, but slightly decreased the interlayer exothermicity and led to the thin reaction layers. Higher bonding pressure increased the extrusion deformation of the interlayer products and effectively eliminated the original pores in the interlayer products.
(3) With the increase of the Zr content and the bonding pressure, the joint shear strength first increased and then decreased. When the Zr content was 15 wt.% and the bonding pressure was 3 MPa, the joint shear strength reached the maximum of 24 MPa.

Author Contributions

Conceptualization, G.F. and Y.W. (Yifeng Wang); methodology, G.F.; software, Y.W. (Yan Wei); validation, B.H. and Y.W. (Yan Wei); formal analysis, G.F. and Y.W. (Yan Wei); investigation, G.F. and Y.W. (Yifeng Wang); resources, B.H.; data curation, Y.W. (Yan Wei); writing—original draft preparation, G.F.; writing—review and editing, G.F. and Y.W. (Yan Wei); visualization, D.D.; supervision, Y.W. (Yifeng Wang) and D.D.; project administration, G.F.; funding acquisition, G.F. All authors have read and agreed to the published version of the manuscript.

Funding

This work was funded by the National Natural Science Foundation of China (No. 51905055), the Natural Science Foundation of Chongqing (No. cstc2020jcyj-msxmX0115), and the Fundamental Research Funds for the Central Universities Project (No. 2020CDJ-LHZZ-086).

Institutional Review Board Statement

Not applicable.

Informed Consent Statement

Not applicable.

Data Availability Statement

Not applicable.

Conflicts of Interest

The authors declare no conflict of interest and non-financial interest requiring disclosure in this article.

References

  1. Chen, R.F.; Zhao, Y.H.; Shen, Z.X.; Dai, L.G.; Zhang, X.L.; Zhu, R. Study on the Joint Strength of SiCp/ Al Metal Matrix Composite by Magnetron Sputtering Method. Mater. Sci. Forum 2009, 628–629, 569–574. [Google Scholar] [CrossRef]
  2. Venkatachalam, A.; Anurag, P.V.S.; Sadanand, T.D.; Nachimuthu, R. Optimization of the milling parameters for an Al/Si3N4 functionally graded composite using grey relational analysis. Mater. Test 2018, 60, 215–221. [Google Scholar] [CrossRef]
  3. Zhang, W.; Xiao, D.; Ding, D. A first-principles investigation of interfacial properties and electronic structure of SiO2/Al interface. Comput. Mater. Sci. 2021, 188. [Google Scholar] [CrossRef]
  4. Wang, X.; Chen, Z.; Ma, T.; Zhu, D.; Dong, D.; Yang, X.; Liu, L.; Wang, G. Evolution of primary and eutectic Si phase and mechanical properties of Al2O3/Al-20Si composites under high pressure. Crystals 2021, 11, 364. [Google Scholar] [CrossRef]
  5. Guo, H.; Zhang, Z.; Zhang, Y.; Cui, Y.; Sun, L.; Chen, D. Improving the mechanical properties of B4C/Al composites by solid-state interfacial reaction. J. Alloy. Compd. 2020, 829. [Google Scholar] [CrossRef]
  6. Duygulu, O. High-resolution transmission electron microscopy investigation of in situ TiC/Al composites. Met. Mater. 2018, 56, 265–275. [Google Scholar] [CrossRef] [Green Version]
  7. Qiao, Q.; Su, Y.; Cao, H.; Zhang, D.; Ouyang, Q. Effect of post-weld heat treatment on double-sided friction stir welded joint of 120 mm ultra-thick SiCp/Al composite plates. Mater. Charact. 2020, 169, 110668. [Google Scholar] [CrossRef]
  8. Adebisi, A.A.; Maleque, M.A.; Ali, M.Y.; Bello, K.A. Effect of variable particle size reinforcement on mechanical and wear properties of 6061Al-SiCp composite. Compos. Interface 2016, 23, 533–547. [Google Scholar] [CrossRef]
  9. Xiang, D.; Zhang, Z.; Wu, B.; Feng, H.; Shi, Z.; Zhao, B. Effect of Ultrasonic Vibration Tensile on the Mechanical Properties of High-Volume Fraction SiCp/Al Composite. Int. J. Precis. Eng. Man. 2020, 21, 2051–2066. [Google Scholar] [CrossRef]
  10. Huang, S.T.; Zhou, L.; Chen, J.; Xu, L.F. Drilling of SiCp/Al Metal Matrix Composites with Polycrystalline Diamond (PCD) Tools. Mater. Manuf. Process. 2012, 27, 1090–1094. [Google Scholar] [CrossRef]
  11. Kwok, Y. Effects of pulse-impact on the welding of SiCP/Al-6061 aluminium matrix composites. Mater. Sci. Technol. 2017, 33, 2298–2304. [Google Scholar] [CrossRef]
  12. Long, J.; Zhang, L.J.; Zhang, L.L.; Wang, X.; Zhang, G.F.; Zhang, J.X.; Na, S.J. Effects of minor Zr addition on the microstructure and mechanical properties of laser welded joint of Al/SiCp metal-matrix composite. J. Manuf. Process. 2020, 49, 373–384. [Google Scholar] [CrossRef]
  13. Xi-He, W.; Ji-Tai, N.; Shao-Kang, G.; Le-Jun, W.; Dong-Feng, C. Investigation on TIG welding of SiCp-reinforced aluminum-matrix composite using mixed shielding gas and Al-Si filler. Mater. Sci. Eng. A 2009, 499, 106–110. [Google Scholar] [CrossRef]
  14. Wang, P.; Gao, Z.; Niu, J. Micro-nano filler metal foil on vacuum brazing of SiCp/Al composites. Appl. Phys. A 2016, 122. [Google Scholar] [CrossRef]
  15. Chen, H.; Nai, X.; Zhao, S.; Lu, D.; Shen, Z.; Li, W.; Cao, J. Improvement for interfacial microstructure and mechanical properties of Ti3SiC2/Cu joint brazed by Ag-Cu-Ti filler with copper mesh. Crystals 2021, 11, 401. [Google Scholar] [CrossRef]
  16. Gao, Z.; Yang, H.; Feng, J.; Ji, F.; Niu, J.; Brnic, J. Flux-Free Diffusion Joining of SiCp/6063 Al Matrix Composites Using Liquid Gallium with Nano-Copper Particles in Atmosphere Environment. Nanomaterials 2020, 10, 437. [Google Scholar] [CrossRef] [Green Version]
  17. Feng, G.; Li, Z.; Zhou, Z.; Wang, Y. Joining of Cf/Al composites and TiAl intermetallics by laser-induced self-propagating high-temperature synthesis using the Ni-Al-Zr interlayer. Mater. Des. 2016, 110, 130–137. [Google Scholar] [CrossRef]
  18. Trenkle, J.C.; Koerner, L.J.; Tate, M.W.; Gruner, S.M.; Weihs, T.P.; Hufnagel, T.C. Phase transformations during rapid heating of Al/Ni multilayer foils. Appl. Phys. Lett. 2008, 93. [Google Scholar] [CrossRef] [Green Version]
  19. Pascal, C.; Marin-Ayral, R.M.; Tedenac, J.C. Joining of nickel monoaluminide to a superalloy substrate by high pressure self-propagating high-temperature synthesis. J. Alloy. Compd. 2002, 337, 221–225. [Google Scholar] [CrossRef]
  20. Swiston, A.J.; Hufnagel, T.C.; Weihs, T.P. Joining bulk metallic glass using reactive multilayer foils. Scripta Mater. 2003, 48, 1575–1580. [Google Scholar] [CrossRef]
  21. Lin, Y.C.; Nepapushev, A.A.; Mcginn, P.J.; Rogachev, A.S.; Mukasyan, A.S. Combustion joinining of carbon/carbon composites by a reactive mixture of titanium and mechanically activated nickel/aluminum powders. Ceram. Int. 2013, 39, 7499–7505. [Google Scholar] [CrossRef]
  22. Feng, G.; Li, Z.; Jacob, R.J.; Yang, Y.; Wang, Y.; Zhou, Z.; Sekulic, D.P.; Zachariah, M.R. Laser-induced exothermic bonding of carbon fiber/Al composites and TiAl alloys. Mater. Des. 2017, 126, 197–206. [Google Scholar] [CrossRef]
  23. Royal, T.E.; Namjoshi, S.; Thadhani, N.N. Mechanistic processes influencing shock chemistry in powder mixtures of the Ti-Si, Ti-Al, and Ti-B systems. Met. Mater. Trans. A 1996, 27, 1761–1771. [Google Scholar] [CrossRef]
  24. Manukyan, K.V.; Lin, Y.; Rouvimov, S.; McGinn, P.J.; Mukasyan, A.S. Microstructure-reactivity relationship of Ti plus C reactive nanomaterials. J. Appl. Phys. 2013, 113. [Google Scholar] [CrossRef]
  25. Ligachev, A.E.; Potemkin, G.V.; Lepakova, O.K.; Zhidkov, M.V.; Teresov, A.D.; Golobokov, N.N.; Maksimov, Y.M.; Kolobov, Y.R.; Koval, N.N. Ignition of a Ti-Al-C System by an Electron Beam. Combust. Explo Shock+ 2018, 54, 158–164. [Google Scholar] [CrossRef] [Green Version]
  26. Epshteyn, A.; Weismiller, M.R.; Huba, Z.J.; Maling, E.L.; Chaimowitz, A.S. Optimization of a High-Energy Ti-Al-B Nanopowder Fuel. Energy Fuels 2017, 31, 1811–1819. [Google Scholar] [CrossRef]
  27. Umbrajkar, S.M.; Schoenitz, M.; Dreizin, E.L. Exothermic reactions in Al-CuO nanocomposites. Thermochim. Acta 2006, 451, 34–43. [Google Scholar] [CrossRef]
  28. Song, J.; Guo, T.; Yao, M.; Chen, J.; Ding, W.; Bei, F.; Mao, Y.; Yu, Z.; Huang, J.; Zhang, X.; et al. A comparative study of thermal kinetics and combustion performance of Al/CuO, Al/Fe2O3 and Al/MnO2 nanothermites. Vacuum 2020, 176. [Google Scholar] [CrossRef]
  29. Shteinberg, A.S.; Lin, Y.; Son, S.F.; Mukasyan, A.S. Kinetics of High Temperature Reaction in Ni-Al System: Influence of Mechanical Activation. J. Phys. Chem. A 2010, 114, 6111–6116. [Google Scholar] [CrossRef] [PubMed]
  30. Cao, J.; Feng, J.C.; Li, Z.R. Joining of TiAl intermetallic by self-propagating high-temperature synthesis. J. Mater. Sci. 2006, 41, 4720–4724. [Google Scholar] [CrossRef]
  31. Morris, C.J.; Mary, B.; Zakar, E.; Barron, S.; Fritz, G.; Knio, O.; Weihs, T.P.; Hodgin, R.; Wilkins, P.; May, C. Rapid initiation of reactions in Al/Ni multilayers with nanoscale layering. J. Phys. Chem Solids 2010, 71, 84–89. [Google Scholar] [CrossRef]
  32. Naiborodenko, Y.S.; Lavrenchuk, G.V.; Filatov, V.M. Self-propagating high-temperature synthesis of aluminides I. Thermodynamic analysis. Powder Metall. Met. Ceram. 1982, 21, 909–912. [Google Scholar] [CrossRef]
  33. Feng, G.; Li, Z.; Zhou, Z.; Yang, Y.; Sekulic, D.P.; Zachariah, M.R. Microstructure and mechanical properties of C-f/Al-TiAl laser-assisted brazed joint. J. Mater. Process. Technol. 2018, 255, 195–203. [Google Scholar] [CrossRef]
  34. Feng, G.; Li, Z.; Feng, S.; Zhang, W. Microstructure evolution and formation mechanism of laser-ignited SHS joining between Cf/Al composites and TiAl alloys with Ni–Al–Ti interlayer. Rare Metals 2017, 36, 746–752. [Google Scholar] [CrossRef]
  35. Chérif, A.; Bachaga, T.; Saurina, J.; Suñol, J.J.; Khitouni, M.; Makhlouf, T. Morphology and structure effect of Ti additive on the solid-state reaction between Ni and Al powders during mechanical alloying. Int. J. Adv. Manuf. Technol. 2016, 86, 2937–2943. [Google Scholar] [CrossRef]
  36. Li, Z.; Feng, G.; Wang, S.; Feng, S. High-efficiency Joining of Cf/Al Composites and TiAl Alloys under the Heat Effect of Laser-ignited Self-propagating High-temperature Synthesis. J. Mater. Sci. Technol. 2016, 32, 1111–1116. [Google Scholar] [CrossRef]
  37. Qi, Q.; Zhang, J.; Hu, H.; Lu, C. Benefits of Zr additive element in the Ti-24Ni eutectic filler in vacuum brazing of SiC ceramics. Vacuum 2019, 162, 110–113. [Google Scholar] [CrossRef]
  38. Zhou, B.; Wang, J.; Feng, K.; Cai, Y.; Chen, S. Effect of Brazing Parameters on the Microstructure and Properties of SiC Ceramic Joint with Zr-Cu Filler Metal. Crystals 2020, 10, 93. [Google Scholar] [CrossRef] [Green Version]
  39. Simoes, S.; Sofia Ramos, A.; Viana, F.; Teresa Vieira, M.; Vieira, M.F. TiAl diffusion bonding using Ni/Ti multilayers. Weld. World 2017, 61, 1267–1273. [Google Scholar] [CrossRef]
Crystals 11 00535 g001 550
Figure 1. Microstructure of the SiCp/Al composites.
Figure 1. Microstructure of the SiCp/Al composites.
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Figure 2. Schematic diagram of the bonding process.
Figure 2. Schematic diagram of the bonding process.
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Figure 3. Schematic diagram of the shear test.
Figure 3. Schematic diagram of the shear test.
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Figure 4. (a) Ni–Al phase diagram; (b) Ni–Al–Zr ternary phase diagram.
Figure 4. (a) Ni–Al phase diagram; (b) Ni–Al–Zr ternary phase diagram.
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Figure 5. DSC curves of the interlayers.
Figure 5. DSC curves of the interlayers.
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Figure 6. Typical microstructure of the SiCp/Al joint bonded with a Ni–Al–Zr interlayer (Zr 15 wt.%, 3 MPa). (a) The overall joint; (b) the bonding interface; (c) the interlayer products.
Figure 6. Typical microstructure of the SiCp/Al joint bonded with a Ni–Al–Zr interlayer (Zr 15 wt.%, 3 MPa). (a) The overall joint; (b) the bonding interface; (c) the interlayer products.
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Figure 7. XRD results of the interlayer products.
Figure 7. XRD results of the interlayer products.
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Figure 8. Microstructures of the joints bonded with different interlayers. (a) Zr 5 wt.%; (b) 8 wt.%; (c) 15 wt.%; (d) 20 wt.%.
Figure 8. Microstructures of the joints bonded with different interlayers. (a) Zr 5 wt.%; (b) 8 wt.%; (c) 15 wt.%; (d) 20 wt.%.
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Figure 9. Microstructures of the different interlayer products. (a) Zr 5 wt.%; (b) 8 wt.%; (c) 15 wt.%; (d) 20 wt.%.
Figure 9. Microstructures of the different interlayer products. (a) Zr 5 wt.%; (b) 8 wt.%; (c) 15 wt.%; (d) 20 wt.%.
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Figure 10. Interfacial bonding characteristics of the joints bonded with different interlayers. (a) Zr 5 wt.%; (b) 8 wt.%; (c) 15 wt.%; (d) 20 wt.%.
Figure 10. Interfacial bonding characteristics of the joints bonded with different interlayers. (a) Zr 5 wt.%; (b) 8 wt.%; (c) 15 wt.%; (d) 20 wt.%.
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Figure 11. Microstructures of the joints bonded under different pressures. (a) 1.5 MPa; (b) 2 MPa; (c) 3 MPa; (d) 4 MPa.
Figure 11. Microstructures of the joints bonded under different pressures. (a) 1.5 MPa; (b) 2 MPa; (c) 3 MPa; (d) 4 MPa.
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Figure 12. Influence of the (a) interlayer composition and (b) bonding pressure on the joint shear strength.
Figure 12. Influence of the (a) interlayer composition and (b) bonding pressure on the joint shear strength.
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Table
Table 1. EDS results on zones in Figure 6 (at.%).
Table 1. EDS results on zones in Figure 6 (at.%).
ZoneNiAlZrPossible Phase
A26.6373.37—NiAl3
B6.0384.959.02(Ni,Zr)Al3
C28.0771.670.26NiAl3
D42.7357.080.19Ni2Al3
E60.3339.67—NiAl
F50.4547.512.04NiAl
G37.9342.1719.9Ni3Al5Zr2
H53.0325.3921.59Ni2AlZr
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Wang, Y.; Feng, G.; Wei, Y.; Hu, B.; Deng, D. Bonding SiCp/Al Composites via Laser-Induced Exothermic Reactions. Crystals 2021, 11, 535. https://doi.org/10.3390/cryst11050535

AMA Style

Wang Y, Feng G, Wei Y, Hu B, Deng D. Bonding SiCp/Al Composites via Laser-Induced Exothermic Reactions. Crystals. 2021; 11(5):535. https://doi.org/10.3390/cryst11050535

Chicago/Turabian Style

Wang, Yifeng, Guangjie Feng, Yan Wei, Bingxu Hu, and Dean Deng. 2021. "Bonding SiCp/Al Composites via Laser-Induced Exothermic Reactions" Crystals 11, no. 5: 535. https://doi.org/10.3390/cryst11050535

APA Style

Wang, Y., Feng, G., Wei, Y., Hu, B., & Deng, D. (2021). Bonding SiCp/Al Composites via Laser-Induced Exothermic Reactions. Crystals, 11(5), 535. https://doi.org/10.3390/cryst11050535

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