Additive manufacturing (AM) technology, which could turn 3D models into physical entities, has been extensively investigated in recent years, in which the complex structural parts are fabricated by AM processes via layer-by-layer accumulation of material [1–3]. There are two categories of additive manufacturing technologies, which are fusion-based AM and solid phase AM [4]. The principle of fusion-based AM is using high-energy heat sources under protective gas or vacuum conditions to heat metal materials (including powder, wire, etc.), so that they can be rapidly melted, solidified and stacked layer by layer to form the desired components [5, 6]. Depending on the form of heat source, fusion-based AM technology mainly includes laser AM, electron beam AM and arc AM [7–9]. However, the defects which are internal porosity, local metallurgical defects and thermal cracking of light metal alloys such as aluminum alloys and magnesium alloys occur in the processes of fusion-based AM inevitably. solid phase AM does not generally cause the above-mentioned problems caused by fusion-based AM, because the material does not melt and solidification during the process [10]. The main solid phase AM technologies currently available include ultrasonic additive manufacturing (UAM), cold spray additive manufacturing (CSAM), and friction-based additive manufacturing (FAM) [11–13].
In 2012, Additive Friction Stir Deposition (AFSD) was developed by MELD manufacturing company based on the principle of friction stir welding (FSW). As shown in Fig. 1a hollow and rotating tool head to feed pre-processed metal powder or wire to deposit on the substrate is applied in AFSD. The feed material is softened by the frictional heat of the rotating tool, but the temperature does not reach its melting point. Therefore, the process has advantages that fusion-based AM does not have, such as avoidance of porosity, thermal cracking and ablation of alloying elements [14, 15]. The material undergoes severe plastic deformation and thus generates dynamic recrystallization (DRX) under the action of the tool head, and the rotating tool has a strong stirring effect on the deposited material, promoting the formation of fragmentation and redistribution of the metal particles [16, 17]. In friction stir welding (FSW) and friction stir spot welding (FSSW), the heat mainly generates from the frictional interaction between the tool shoulder and plastic deformation of the workpiece materials [18–21]. However, the heat generation in AFSD derives from the frictional interaction between the deposited material and the tool shoulder or the substrate. The peak temperature is estimated to be between 0.6 and 0.9 Tm, where Tm is the melting point of the substrate material. Although no melting occurs in the as-deposited material, temperatures are high enough to cause dissolution of strengthening phases in the filler feedstock [22, 23]. Tool rotational speed, tool traversing velocity and feedstock feed rate are the more important parameters in the AFSD process, as they determine the temperatures and material flow patterns, which are critical to the quality of the additive layer [24, 25].
Garcia et al. investigated the heat generation mechanism during AFSD of Cu and Al-Mg-Si alloys. In the deposition zone of Cu, the tool head and the deposited material are in a complete slipping state, so the main heat generation of the Cu deposition layers comes from interfacial friction. For Al-Mg-Si, the interfacial friction is partial slipping, so the heat generation mechanism of Al-Mg-Si deposited layers mainly originated from interfacial friction and volumetric energy dissipation. In AFSD, unlike Cu where the peak temperature TPeak is bounded at 49%-79% of the melting point TM, the peak temperature TPeak of Al-Mg-Si lies in the range of 76%-92% of the melting point TM. This is due to the fact that the yield strength of Cu decreases more rapidly with increasing of temperature than that of aluminum alloys [26, 27]. For the comparison of Cu and Al-Mg-Si, Griffiths et al. also conducted a detailed investigation, which indicated that a large amount of material rotation was observed in the deposition zone of Al-Mg-Si, which was not present in Cu, and therefore the strain of Al-Mg-Si was higher. Meanwhile, the larger transition zone boundaries were observed in Al-Mg-Si produced more deformation than Cu because the surface area and friction coefficient between Al-Al was higher than that between Cu-Cu [28]. Rivera et al. studied the microstructure of AA2219 deposition using EBSD and found that the average grain size of the deposited material was 2.5 µm, which is much smaller than that of the base material (30 µm), and they also observed that the grain size remained essentially uniform in the deposition direction [29]. Priedeman et al. investigated microstructural evolution in AFSD of Cu with a hardness of 63 HV for the deposition, 62% of the hardness of the base material, which can be attributed to the disappearance of high density dislocations caused by the recrystallization of Cu during the AFSD process. Whereas the reason for the decrease in hardness is in agreement with the literature on FSW of Cu [30, 31]. Phillips investigated role of rotation speed and traversing velocity on the deposition quality of AA6061. Parts fabricated using low feed rates and high traversing speeds produced obvious nibbles and voids due to insufficient material flow. Conversely, when it was fabricated using high feed rates and low traversing speeds, the deposition efficiency was reduced andcharacterized by large amounts of material being pushed out from under the tool face as the form of flash. They also determined the 𝛽″ precipitates by transmission electron microscopy (TEM) and atom probe tomography (APT) analysis, and thus analyzed the causes of the degradation of the mechanical properties of the deposited AA6061, found that the 𝛽″ reinforced precipitate was dissolved and then reprecipitated as Mg-Si solute clusters in the deposited material [32]. Perry et al. found that both AA2024 and AA6061 underwent continuous DRX characterized by dynamic recovery, subgrain formation, and strain-induced high angle boundary (HAB) formation. The difference is that recrystallization is almost complete in AA2024; whereas in AA6061, deformation only causes a portion of the low angle boundaries (LABs) to become high angle boundaries (HABs), resulting in partial recrystallization [33]. Hartley et al. investigated the feasibility of AFSD for solid-state cladding on automotive Al-Mg-Si thin sheet metal (1.4 mm thick). It was found that for thin substrates for automotive use, geometry of the tool determines the cladding quality, and that flat tools are more beneficial to develop good cladding quality. Although the protruding tool facilitates material flow and interfacial bonding, this can easily penetrate the substrate and a thicker deposition layer must be taken to avoid scratching the substrate, which in turn can lead to insufficient deformation of the deposited material to affect the cladding quality [34].
Beck et al. investigated the effect of heat treatment on AFSDed AA6061. ultimate tensile strength of as-deposited (AD) material was reduced by 47% due to dissolution of β. Solutionized/quenched (SQ) showed a 10% reduction in ductility and 58% increase in ultimate tensile strength compared to that of the AD material. Solutionized/quenched/artificially aged (SQA) resulted in regeneration of strength, hardness and β deposition of T6. However, no adverse effect of abnormal grain growth (AGG) on strength and ductility was observed in artificially aged AFSD specimens, thus demonstrating that β precipitation caused by post deposition heat treatment (PDHT) plays a more critical role in determining the strengthening mechanism of AFSDed AA6061 [35]. Griffiths et al. explored the use of AFSD to repair bulk damage in AA7075. It was found that the deposited material was well mixed with the sidewalls of the repaired upper hole or slot. This is a gradual transition from the elongated grains of the AA7075 plate to the fine equiaxed grains of the deposited AA7075 with no visible interface. The lower part of the repaired quality is generally worse than that of the upper part, sometimes showing straight, sharp interfaces separating the elongated grains from the fine, equiaxed grains [36]. Yang simulated the temperature field and stress state of AFSDed Al6061-T6, and the results showed that the heated affected zone presented a bowl-shaped appearance, and the highest temperature reached approximately 78.7% of the melting point at the contact surface between the filled bar and the substrate. As the filler bar moves down, the deposited material on the substrate is extruded to form a deposited layer [37]. Ahmed et al. found that the optimum condition for AFSDed AA2011-T6 of was 1200 rpm and 3–9 mm/min, while the optimum condition for AFSDed AA2011-O was 200 rpm and 1–3 mm/min. In addition, they investigated the effect of alloy temper conditions on the behavior of AFSDed AA2011-T6, and the results indicated that the use of the T6 temper alloy resulted in a lower hardness of additive manufacturing parts (AMPs) than the that in base material, reaching 61% and 51% of the hardness of the base material at 3 and 9 mm/min, respectively. However, the hardness of AMPs fabricated using O temper alloy was higher than that in the starting material and increased by approximately 163% over the hardness of the initial material [38]. AFSD was also applied to fabricate aluminum matrix composites, where fine equiaxed grains were observed, and the deposited material was completely dense with the substrate, no pores can be observed [39–41].
In this work, the first single-layer deposition of AA5B70 was fabricated using the AFSD method. The quality of the first layer deposited is of utmost importance, which determines the reliability of the subsequent deposited layers, since the subsequent deposition process still causes complex thermo-mechanical coupling effects on the first layer of the build. Therefore, the focus was given to the microstructure and mechanical properties of the first layer of this alloy deposited by the AFSD, and thus on whether usable building blocks could be obtained under this experimental parameter.