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J. Manuf. Mater. Process., Volume 8, Issue 5 (October 2024) – 16 articles

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9 pages, 31439 KiB  
Technical Note
A Toolpath Generator Based on Signed Distance Fields and Clustering Algorithms for Optimized Additive Manufacturing
by Alp Karakoç
J. Manuf. Mater. Process. 2024, 8(5), 199; https://doi.org/10.3390/jmmp8050199 (registering DOI) - 15 Sep 2024
Viewed by 61
Abstract
Additive manufacturing (AM) methods have been gaining momentum because they provide vast design and fabrication possibilities, increasing the accessibility of state-of-the-art hardware through recent developments in user-friendly computer-aided drawing/engineering/manufacturing (CAD/CAE/CAM) tools. However, in comparison to the conventional manufacturing methods, AM processes have some [...] Read more.
Additive manufacturing (AM) methods have been gaining momentum because they provide vast design and fabrication possibilities, increasing the accessibility of state-of-the-art hardware through recent developments in user-friendly computer-aided drawing/engineering/manufacturing (CAD/CAE/CAM) tools. However, in comparison to the conventional manufacturing methods, AM processes have some disadvantages, including the machining precision and fabrication process times. The first issue has been mostly resolved through the recent advances in manufacturing hardware, sensors, and controller systems. However, the latter has been widely investigated by researchers with different toolpath planning perspectives. As a contribution to these investigations, the present study proposes a toolpath planning method for AM, which aims to provide highly continuous yet distance-optimized solutions. The approach is based on the utilization of the signed distance field (SDF), clustering, and minimization of toolpath distances among cluster centroids. The method was tested on various geometries with simple closed curves to complex geometries with holes, which provides effective toolpaths, e.g., with relative distance reduction percentages up to 16.5% in comparison to conventional rectilinear infill patterns. Full article
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<p>Workflow: (I) Three-dimensional (3-D) geometry slicing and two-dimensional (2-D) projection, (II) generation of signed distance fields, (III) clustering and distance minimization for optimal toolpaths, (IV) generation of G-Code and additive manufacturing by means of the computed toolpaths.</p>
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<p>Signed distance field calculations for a hollow ellipse.</p>
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<p>Tested samples and generated toolpaths for selected sections by means of the current SDF−based and conventional rectilinear methods. The in−plane resolution was chosen to be 0.2 mm.</p>
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<p>Generated toolpaths and number of clusters for various geometries by means of the current SDF−based and conventional rectilinear methods. The in−plane resolution was chosen to be 0.2 mm. SDF* and NC** refer to signed distance field and NC** refers to neighborhood contraction, respectively.</p>
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<p>Schematic representation of the nozzle movement and material extrusion based on the G-Code commands.</p>
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23 pages, 8179 KiB  
Article
Study on Extraordinarily High-Speed Cutting Mechanics and Its Application to Dry Cutting of Aluminum Alloys with Non-Coated Carbide Tools
by Jun Eto, Takehiro Hayasaka, Eiji Shamoto and Liangji Xu
J. Manuf. Mater. Process. 2024, 8(5), 198; https://doi.org/10.3390/jmmp8050198 - 13 Sep 2024
Viewed by 352
Abstract
The friction/adhesion between the tool and chip is generally large in metal cutting, and it causes many problems such as high cutting energy/rough surface finish. To suppress this, cutting fluid and tool coating are used in practice, but they are high in energy/cost [...] Read more.
The friction/adhesion between the tool and chip is generally large in metal cutting, and it causes many problems such as high cutting energy/rough surface finish. To suppress this, cutting fluid and tool coating are used in practice, but they are high in energy/cost and environmentally unfriendly. Therefore, this paper investigates the extraordinarily high-speed cutting (EHS cutting) mechanics of mainly soft and highly heat-conductive materials and proposes their application to solve the friction/adhesion problem in an environmentally friendly manner. In order to clarify the EHS cutting mechanics, a simple analytical model is constructed and experiments are conducted with measurement of the cutting temperature and forces. As a result, the following points are clarified/found: (1) heat softening at the secondary plastic deformation zone rather than the primary plastic deformation zone, (2) friction coefficient drop to 0.170 in EHS cutting, and (3) gradually increasing trend of cutting temperature in EHS cutting. Finally, EHS cutting is applied to dry cutting of aluminum alloys with a non-coated carbide tool and compared to conventional wet cutting with a DLC-coated carbide tool, and it is shown that a coating/coolant can be omitted in this region to achieve environmentally friendly cutting. Full article
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<p>Schematic of cutting process and cutting temperature distribution [<a href="#B2-jmmp-08-00198" class="html-bibr">2</a>].</p>
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<p>Influence of cutting speed on cutting temperature in dry cutting with Al<sub>2</sub>O<sub>3</sub> ceramic tool [<a href="#B19-jmmp-08-00198" class="html-bibr">19</a>].</p>
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<p>Relation between specific cutting energy <math display="inline"><semantics> <mrow> <mi>k</mi> <mi>s</mi> </mrow> </semantics></math> and specific melt-beginning energy <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>q</mi> </mrow> <mrow> <mi>c</mi> </mrow> </msub> </mrow> </semantics></math>.</p>
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<p>Tensile property of aluminum alloys against temperature [<a href="#B25-jmmp-08-00198" class="html-bibr">25</a>,<a href="#B26-jmmp-08-00198" class="html-bibr">26</a>].</p>
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<p>Schematic illustration of calibration system of thermoelectromotive force.</p>
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<p>Result of TEMF calibration curve between 7050-T7451 alloy and cemented carbide.</p>
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<p>Photographs of experimental setup for milling-like turning experiments.</p>
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<p>Schematic of experimental setup.</p>
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<p>Example of thermoelectromotive force and cutting forces in one spindle revolution at cutting speed <span class="html-italic">V<sub>c</sub></span> = 5184 m/min, feed per revolution <span class="html-italic">f</span> = 0.15 mm/rev, and dry cutting with non-coated carbide tool.</p>
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<p>Effects of cutting speed <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>V</mi> </mrow> <mrow> <mi>c</mi> </mrow> </msub> </mrow> </semantics></math> on temperatures, cutting forces, average friction coefficient, average shear stress at shear plane, and specific cutting energy at feed per revolution <span class="html-italic">f</span> = 0.15 mm/rev, dry environment, and non-coated tool.</p>
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<p>Comparison of ultimate tensile strength against temperature and average friction coefficient <math display="inline"><semantics> <mrow> <mi>μ</mi> </mrow> </semantics></math> against cutting temperature in dry environment and with non-coated tool.</p>
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<p>Effects of feed per revolution <math display="inline"><semantics> <mrow> <mi>f</mi> </mrow> </semantics></math> on cutting temperature and cutting forces at cutting speed <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>V</mi> </mrow> <mrow> <mi>c</mi> </mrow> </msub> </mrow> </semantics></math> = 1465 m/min, dry environment, and non-coated tool.</p>
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<p>Effects of rake angle <math display="inline"><semantics> <mrow> <mi mathvariant="sans-serif">α</mi> </mrow> </semantics></math> and cutting speed <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>V</mi> </mrow> <mrow> <mi>c</mi> </mrow> </msub> </mrow> </semantics></math> on cutting temperature, cutting forces, and average friction coefficient at feed per revolution <math display="inline"><semantics> <mrow> <mi>f</mi> <mo>=</mo> <mn>0.15</mn> </mrow> </semantics></math> mm/rev, dry environment, non-coated tool.</p>
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<p>Photograph of conventional cutting process with external cutting fluid.</p>
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<p>Comparison of cutting forces, average friction coefficient, and cutting ratio between dry cutting with non-coated tool and wet cutting with DLC-coated tool.</p>
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<p>Photographs of (<b>a</b>) machined surfaces, (<b>b</b>) chips, and (<b>c</b>) rake faces after cutting at cutting speed <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>V</mi> </mrow> <mrow> <mi>c</mi> </mrow> </msub> <mo>=</mo> </mrow> </semantics></math> 5184 m/min.</p>
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28 pages, 4771 KiB  
Review
Selective Laser Sintering of Polymers: Process Parameters, Machine Learning Approaches, and Future Directions
by Hossam M. Yehia, Atef Hamada, Tamer A. Sebaey and Walaa Abd-Elaziem
J. Manuf. Mater. Process. 2024, 8(5), 197; https://doi.org/10.3390/jmmp8050197 - 13 Sep 2024
Viewed by 416
Abstract
Selective laser sintering (SLS) is a bed fusion additive manufacturing technology that facilitates rapid, versatile, intricate, and cost-effective prototype production across various applications. It supports a wide array of thermoplastics, such as polyamides, ABS, polycarbonates, and nylons. However, manufacturing plastic components using SLS [...] Read more.
Selective laser sintering (SLS) is a bed fusion additive manufacturing technology that facilitates rapid, versatile, intricate, and cost-effective prototype production across various applications. It supports a wide array of thermoplastics, such as polyamides, ABS, polycarbonates, and nylons. However, manufacturing plastic components using SLS poses significant challenges due to issues like low strength, dimensional inaccuracies, and rough surface finishes. The operational principle of SLS involves utilizing a high-power-density laser to fuse polymer or metallic powder surfaces. This paper presents a comprehensive analysis of the SLS process, emphasizing the impact of different processing variables on material properties and the quality of fabricated parts. Additionally, the study explores the application of machine learning (ML) techniques—supervised, unsupervised, and reinforcement learning—in optimizing processes, detecting defects, and ensuring quality control within SLS. The review addresses key challenges associated with integrating ML in SLS, including data availability, model interpretability, and leveraging domain knowledge. It underscores the potential benefits of coupling ML with in situ monitoring systems and closed-loop control strategies to enable real-time adjustments and defect mitigation during manufacturing. Finally, the review outlines future research directions, advocating for collaborative efforts among researchers, industry professionals, and domain experts to unlock ML’s full potential in SLS. This review provides valuable insights and guidance for researchers in regard to 3D printing, highlighting advanced techniques and charting the course for future investigations. Full article
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<p>Comprehensive overview of 3D printing techniques; the images in this Figure are adapted from Refs. [<a href="#B10-jmmp-08-00197" class="html-bibr">10</a>,<a href="#B11-jmmp-08-00197" class="html-bibr">11</a>,<a href="#B12-jmmp-08-00197" class="html-bibr">12</a>,<a href="#B13-jmmp-08-00197" class="html-bibr">13</a>,<a href="#B14-jmmp-08-00197" class="html-bibr">14</a>,<a href="#B15-jmmp-08-00197" class="html-bibr">15</a>,<a href="#B16-jmmp-08-00197" class="html-bibr">16</a>,<a href="#B17-jmmp-08-00197" class="html-bibr">17</a>,<a href="#B18-jmmp-08-00197" class="html-bibr">18</a>].</p>
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<p>Illustration of SLS procedure [<a href="#B9-jmmp-08-00197" class="html-bibr">9</a>].</p>
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<p>Different applications of SLS 3D Printing using nylon material [<a href="#B31-jmmp-08-00197" class="html-bibr">31</a>].</p>
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<p>Visualization of hatch spacing and its influence on part density and strength [<a href="#B44-jmmp-08-00197" class="html-bibr">44</a>].</p>
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<p>Relationship between glass transition (Tg) and melting (Tm) temperatures and the stiffness/modulus of amorphous and crystalline polymers [<a href="#B60-jmmp-08-00197" class="html-bibr">60</a>].</p>
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<p>Porosity types in SLS parts and their correlation with process parameters [<a href="#B86-jmmp-08-00197" class="html-bibr">86</a>].</p>
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<p>Monitoring techniques used in SLS: (<b>a</b>) fringe projection [<a href="#B99-jmmp-08-00197" class="html-bibr">99</a>], (<b>b</b>) laser profilometer [<a href="#B101-jmmp-08-00197" class="html-bibr">101</a>], (<b>c</b>) thermal infrared camera [<a href="#B102-jmmp-08-00197" class="html-bibr">102</a>], (<b>d</b>) acoustic sensing [<a href="#B105-jmmp-08-00197" class="html-bibr">105</a>], (<b>e</b>) X-ray imaging [<a href="#B106-jmmp-08-00197" class="html-bibr">106</a>].</p>
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<p>Process flow diagram depicting the transfer learning approach using powder bed data [<a href="#B133-jmmp-08-00197" class="html-bibr">133</a>].</p>
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<p>Receiver operating characteristic (ROC) curves and area under the curve (AUC) metrics for the implemented models across three experiments. The linear dashed lines represent the ROC curve for a completely random classifier (diagonal line) and a perfect classifier (top-left corner); (<b>a</b>) depicts the ROC curves of the implemented models; (<b>b</b>) shows a zoomed-in version of the top portion of the plot [<a href="#B133-jmmp-08-00197" class="html-bibr">133</a>].</p>
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11 pages, 4905 KiB  
Article
The Effect of Multiple-Time Applications of Metal Primers Containing 10-MDP on the Repair Strength of Base Metal Alloys to Resin Composite
by Awiruth Klaisiri, Chanakan Paaopanchon and Boonlert Kukiattrakoon
J. Manuf. Mater. Process. 2024, 8(5), 196; https://doi.org/10.3390/jmmp8050196 - 10 Sep 2024
Viewed by 321
Abstract
This experimental study was performed to assess whether applying a metal primer containing 10-MDP multiple times affected the repair shear bonding ability of base metal alloys to resin composites. Ten base metal alloys were randomly assigned to each group in the manner described, [...] Read more.
This experimental study was performed to assess whether applying a metal primer containing 10-MDP multiple times affected the repair shear bonding ability of base metal alloys to resin composites. Ten base metal alloys were randomly assigned to each group in the manner described, following multiple applications of a metal primer (Clearfil Ceramic Primer Plus), namely one to five applications, and no primer application as a negative control. On the specimens’ prepared surfaces, the resin composite was pushed into the mold and then light-activated for 40 s. The bonded samples were kept for 24 h at 37 °C in distilled water in an incubator. The shear bond strength was determined using a universal testing device. A stereomicroscope was used to determine the debonded surface. The one-way ANOVA and Tukey’s test were implemented to statistically analyze. The lowest shear bond strength was found in group 6 (6.14 ± 1.12 MPa), demonstrating a significant difference (p = 0.000) when compared to groups 1 to 5. The shear bond strength of group 3 was highest at 21.49 ± 1.33 MPa; there was no significant difference between group 3 and groups 4 and 5 (20.21 ± 2.08 MPa and 20.98 ± 2.69 MPa, respectively) (p = 0.773, p = 1.000, respectively). All fractured specimens in groups 1, 2, and 6 were identified as adhesive failure. Groups 3 and 4 exhibited the highest percentage of mixed failures. To achieve the repair shear bonding ability of base metal alloys to resin composites, the sandblasted base metal alloys should be coated with three applications of a metal primer before applying the adhesive agent. Full article
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<p>Base metal alloy rod specimens.</p>
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<p>Bonded specimens.</p>
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<p>The schematic of the SBS test.</p>
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<p>The adhesive failure mode of group 1 (Ad, adhesive failure).</p>
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<p>The adhesive failure mode of group 2 (Ad, adhesive failure).</p>
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<p>Failure mode of group 3: (<b>A</b>) adhesive failure mode; (<b>B</b>) mixed failure mode (Ad, adhesive failure; Co, cohesive failure in the resin composite).</p>
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<p>Failure mode of group 4: (<b>A</b>) adhesive failure mode; (<b>B</b>) mixed failure mode (Ad, adhesive failure; Co, cohesive failure in the resin composite).</p>
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<p>Failure mode of group 5: (<b>A</b>) adhesive failure mode; (<b>B</b>) mixed failure mode (Ad, adhesive failure; Co, cohesive failure in the resin composite).</p>
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<p>The adhesive failure mode of group 6 (Ad, adhesive failure).</p>
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14 pages, 4713 KiB  
Article
Effect of Drilling Parameters on Surface Roughness and Delamination of Ramie–Bamboo-Reinforced Natural Hybrid Composites
by Krishna Kumar P, Gaddam Lokeshwar, Chamakura Uday Kiran Reddy, Arun Jyotis, Surendra Shetty, Subash Acharya and Nagaraja Shetty
J. Manuf. Mater. Process. 2024, 8(5), 195; https://doi.org/10.3390/jmmp8050195 - 5 Sep 2024
Viewed by 492
Abstract
Plastics reinforced with glass fiber have a significant likelihood of being replaced by natural fiber hybrid composites (NFHCs). Making holes helps in part assembly, which is a crucial activity in the machining of composite constructions. As a result, choosing the right drill bit [...] Read more.
Plastics reinforced with glass fiber have a significant likelihood of being replaced by natural fiber hybrid composites (NFHCs). Making holes helps in part assembly, which is a crucial activity in the machining of composite constructions. As a result, choosing the right drill bit and cutting parameters is crucial to creating a precise and high-quality hole in composite materials. The present study employs the Taguchi approach to examine the delamination behavior and hole quality of ramie–bamboo composite laminates consisting of epoxy and nano-fillers (SiC, Al2O3) with feed, spindle speed, and three distinct drill bit types. Surface roughness and delamination are significantly influenced by feed and spindle speed, as indicated by the results of the analysis of variance. It was found that the spindle speed had a major impact on the delamination factor and surface roughness, while the feed and drill bit type had a minor influence. The surface roughness (76.5%) and delamination factor (66.7%) are significantly affected by the spindle speed. Full article
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<p>Drilling experimental setup.</p>
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<p>Different types of drill bits: (<b>a</b>) twist drill, (<b>b</b>) step drill, and (<b>c</b>) core drill.</p>
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<p>Optical microscope for capturing images to measure delamination.</p>
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<p>Surface roughness measuring instrument.</p>
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<p>Main effects plot for mean surface roughness.</p>
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<p>Main effects plot for S/N ratios for surface roughness.</p>
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<p>Surface roughness vs. feed at various speeds: (<b>a</b>) interaction plot of TS1, (<b>b</b>) interaction plot of TS2, (<b>c</b>) interaction plot of TS3, (<b>d</b>) interaction plot of TS4, and (<b>e</b>) interaction plot of TS5.</p>
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<p>(<b>a</b>) Original image. (<b>b</b>) Image after decreasing brightness.</p>
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<p>Main effects plot for S/N ratios for delamination factor.</p>
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<p>Main effects plot for means for delamination factor.</p>
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<p>Delamination vs. feed at various speeds: (<b>a</b>) interaction plot of TS1, (<b>b</b>) interaction plot of TS2, (<b>c</b>) interaction plot of TS3, (<b>d</b>) interaction plot of TS4, and (<b>e</b>) interaction plot of TS5.</p>
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19 pages, 4551 KiB  
Article
Development of a Method and a Smart System for Tool Critical Life Real-Time Monitoring
by Shih-Ming Wang, Wan-Shing Tsou, Jian-Wei Huang, Shao-En Chen and Chia-Che Wu
J. Manuf. Mater. Process. 2024, 8(5), 194; https://doi.org/10.3390/jmmp8050194 - 5 Sep 2024
Viewed by 373
Abstract
Tool wear management and real-time machining quality monitoring are pivotal components of realizing smart manufacturing objectives, as they directly influence machining precision and productivity. Traditionally, measuring and analyzing cutting force fluctuations in the time domain has been employed to diagnose tool wear effects. [...] Read more.
Tool wear management and real-time machining quality monitoring are pivotal components of realizing smart manufacturing objectives, as they directly influence machining precision and productivity. Traditionally, measuring and analyzing cutting force fluctuations in the time domain has been employed to diagnose tool wear effects. This study introduces a novel, indirect approach that leverages spindle-load current variations as a proxy for cutting force analysis. Compared to conventional methods relying on machining vibration or direct cutting force measurement, this technique provides a safer, simpler, and more cost-effective means of data aquisition, with reduced computational demands. Consequently, it is ideally suited for real-time monitoring and long-term analyses such as tool-life prediction and surface-roughness evolution induced by tool wear. An intelligent tool wear monitoring system was developed based on spindle-load current data. The system employs extensive cutting experiments to identify and analyze the correlation between tool wear and spindle-load current signal patterns. By establishing a tool wear near-end-of-life threshold, the system enables intelligent monitoring using C#. Experimental validation under both roughing and finishing conditions demonstrated the system’s exceptional diagnostic accuracy and reliability. The results demonstrate that the current ratio threshold value has good universality in different materials, indicating that monitoring the machining current ratio to estimate the degree of tool wear is a feasible research direction, and that the average error between the experimental surface-roughness measurement value and the predicted value was 10%. Full article
(This article belongs to the Special Issue Smart Manufacturing in the Era of Industry 4.0)
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<p>Schematic diagram of end-mill wear [<a href="#B13-jmmp-08-00194" class="html-bibr">13</a>]. (<b>a</b>) Three types of wear; (<b>b</b>) tool tip fractures.</p>
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<p>Current characteristic diagram during stable and rapid-wear stages.</p>
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<p>Spindle current variation over time.</p>
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<p>The schematic diagram of the quartile method.</p>
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<p>Schematic diagram of experimental setup.</p>
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<p>AOI imaging system.</p>
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<p>Image of surface roughness gauge.</p>
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<p>Schematic diagram of the process of tool critical life diagnosis rule.</p>
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<p>The relationship between the spindle-load current ratio and the surface-roughness ratio of the T01 tool experiment.</p>
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<p>Schematic diagram of the process of machining surface-roughness prediction rule.</p>
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<p>Picture of the tool-life estimation HCI system. (<b>a</b>) Monitoring interface; (<b>b</b>) Setting interface.</p>
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<p>Rocker arm component. (<b>a</b>) Photo of machined workpieces; (<b>b</b>) Simulated cutting path.</p>
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<p>The average load current in time-domain.</p>
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<p>Photos of end-mill blades. (<b>a</b>) Unworn state; (<b>b</b>) Worn state (partially chipped).</p>
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<p>Schematic diagram of measuring points on the workpiece surface.</p>
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12 pages, 4342 KiB  
Article
Investigating the Impact of 3D Printing Parameters on Hexagonal Structured PLA+ Samples and Analyzing the Incorporation of Sawdust and Soybean Oil as Post-Print Fillers
by Yeswanth Teja Ramisetty, Jens Schuster and Yousuf Pasha Shaik
J. Manuf. Mater. Process. 2024, 8(5), 193; https://doi.org/10.3390/jmmp8050193 - 3 Sep 2024
Viewed by 671
Abstract
Today, around the world, there is huge demand for natural materials that are biodegradable and possess suitable properties. Natural fibers reveal distinct aspects like the combination of good mechanical and thermal properties that allow these types of materials to be used for different [...] Read more.
Today, around the world, there is huge demand for natural materials that are biodegradable and possess suitable properties. Natural fibers reveal distinct aspects like the combination of good mechanical and thermal properties that allow these types of materials to be used for different applications. However, fibers alone cannot meet the required expectations; design modifications and a wide variety of combinations must be synthesized and evaluated. It is of great importance to research and develop materials that are bio-degradable and widely available. The combination of PLA+, a bio-based polymer, with natural fillers like sawdust and soybean oil offers a novel way to create sustainable composites. It reduces the reliance on petrochemical-based plastics while enhancing the material’s properties using renewable resources. This study explores the creation of continuous hexagonal-shaped 3D-printed PLA+ samples and the application of post-print fillers, specifically sawdust and soybean oil. PLA+ is recognized for its eco-friendliness and low carbon footprint, and incorporating a hexagonal pattern into the 3D-printed PLA+ enhances its structural strength while maintaining its density. The addition of fillers is crucial for reducing shrinkage and improving binding capabilities, addressing some of PLA+’s inherent challenges and enhancing its load-bearing capacity and performance at elevated temperatures. Additionally, this study examines the impact of varying filler percentages and pattern orientations on the mechanical properties of the samples, which were printed with an infill design. Full article
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<p>The Creality Ender 5S1 3D printer with its axis and components.</p>
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<p>(<b>a</b>) Intersection of the sample in slicing software; (<b>b</b>) final sample in slicing software.</p>
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<p>(<b>a</b>) Sample with 0° orientation with reference axis R. (<b>b</b>) Sample with 45° orientation with reference axis R.</p>
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<p>(<b>a</b>) View of 3D-printed samples with sawdust. (<b>b</b>) Final view of the samples after printing.</p>
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<p>(<b>a</b>) Samples for the flexural test with sawdust. (<b>b</b>) Samples without sawdust.</p>
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18 pages, 10991 KiB  
Article
The Influence of Shot Peening Media on Surface Properties and Fatigue Behaviour of Aluminium Alloy 6082 T6
by Erik Calvo-García, Jesús del Val, Antonio Riveiro, Sara Valverde-Pérez, David Álvarez, Manuel Román, César Magdalena, Aida Badaoui, Pablo Pou-Álvarez and Rafael Comesaña
J. Manuf. Mater. Process. 2024, 8(5), 192; https://doi.org/10.3390/jmmp8050192 - 3 Sep 2024
Viewed by 451
Abstract
Shot peening is generally used to improve the fatigue performance of mechanical components. However, identifying the geometrical and mechanical characteristics of the shots that improve fatigue strength is still a challenging task, as there are many variables involved in the shot peening process. [...] Read more.
Shot peening is generally used to improve the fatigue performance of mechanical components. However, identifying the geometrical and mechanical characteristics of the shots that improve fatigue strength is still a challenging task, as there are many variables involved in the shot peening process. The present work addresses the effect of different shot media on the fatigue behaviour of an aluminium alloy 6082 T6. Four different shot types were used: silica microspheres, alumina shots, aluminium cut wire and zinc cut wire. Axial fatigue tests were carried out to obtain the Wöhler curves corresponding to each shot peening treatment. The surface properties of the shot-peened specimens, such as grain size, hardness, residual stress and roughness were measured to determine their effect on the fatigue results. The fatigue results revealed that silica and zinc shots increased significantly the fatigue life of the alloy, whereas alumina and aluminium shots reduced its fatigue strength. Almen intensities have shown to correlate well with grain refinement and strain hardening. However, better fatigue results were obtained with the shots that generated higher surface compressive residual stresses. It is believed that small and smooth shots are preferable to sharp and irregular ones, regardless of the Almen intensity or surface hardness attained with the latter. Full article
(This article belongs to the Special Issue Deformation and Mechanical Behavior of Metals and Alloys)
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Graphical abstract

Graphical abstract
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<p>Grain structure of the non-treated aluminium alloy 6082 T6.</p>
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<p>Particles used in the shot peening process: (<b>a</b>) silica microspheres, (<b>b</b>) alumina, (<b>c</b>) aluminium cut wire and (<b>d</b>) zinc cut wire.</p>
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<p>Dimensions and requirements of the fatigue test specimens.</p>
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<p>Grain structures at the surface of the aluminium alloy 6082 T6 after shot peening treatments with (<b>a</b>) silica microspheres, (<b>b</b>) alumina, (<b>c</b>) aluminium cut wire and (<b>d</b>) zinc cut wire.</p>
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<p>Nanohardness measurements as a function of depth for different shot peening treatments.</p>
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<p>Effect of Almen intensity on (<b>a</b>) grain refinement and (<b>b</b>) surface nanohardness increase.</p>
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<p>Surface residual stresses for different shot peening treatments.</p>
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<p>Surface topography of aluminium alloy 6082 T6 specimens (<b>a</b>) with no surface treatment and shot-peened with (<b>b</b>) silica microspheres, (<b>c</b>) alumina particles, (<b>d</b>) aluminium cut wire and (<b>e</b>) zinc cut wire.</p>
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<p>Wöhler diagrams of the 6082 T6 alloy subjected to different shot peening treatments.</p>
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<p>Fracture surface (front and lateral) of a non-treated specimen of 6082 aluminium alloy tested to a maximum stress of 305 MPa.</p>
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<p>Fracture surfaces (front and lateral) of the 6082 aluminium alloy shot-peened with (<b>a</b>) silica microspheres, (<b>b</b>) alumina particles, (<b>c</b>) aluminium cut wire and (<b>d</b>) zinc cut wire, all tested to a maximum stress of 305 MPa.</p>
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<p>Fatigue crack (<b>a</b>) initiation and (<b>b</b>) propagation of a non-treated specimen of 6082 aluminium alloy tested to a maximum stress of 305 MPa.</p>
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<p>Fatigue crack initiation sites of 6082 aluminium alloy specimens shot-peened with (<b>a</b>) silica microspheres, (<b>b</b>) alumina particles, (<b>c</b>) aluminium cut wire and (<b>d</b>) zinc cut wire, all tested to a maximum stress of 305 MPa.</p>
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28 pages, 18753 KiB  
Article
Photopolymerization of Stainless Steel 420 Metal Suspension: Printing System and Process Development of Additive Manufacturing Technology toward High-Volume Production
by Hoa Xuan Nguyen, Bibek Poudel, Zhiyuan Qu, Patrick Kwon and Haseung Chung
J. Manuf. Mater. Process. 2024, 8(5), 191; https://doi.org/10.3390/jmmp8050191 - 1 Sep 2024
Viewed by 386
Abstract
As the metal additive manufacturing (AM) field evolves with an increasing demand for highly complex and customizable products, there is a critical need to close the gap in productivity between metal AM and traditional manufacturing (TM) processes such as continuous casting, machining, etc., [...] Read more.
As the metal additive manufacturing (AM) field evolves with an increasing demand for highly complex and customizable products, there is a critical need to close the gap in productivity between metal AM and traditional manufacturing (TM) processes such as continuous casting, machining, etc., designed for mass production. This paper presents the development of the scalable and expeditious additive manufacturing (SEAM) process, which hybridizes binder jet printing and stereolithography principles, and capitalizes on their advantages to improve productivity. The proposed SEAM process was applied to stainless steel 420 (SS420) and the processing conditions (green part printing, debinding, and sintering) were optimized. Finally, an SS420 turbine fabricated using these conditions successfully reached a relative density of 99.7%. The SEAM process is not only suitable for a high-volume production environment but is also capable of fabricating components with excellent accuracy and resolution. Once fully developed, the process is well-suited to bridge the productivity gap between metal AM and TM processes, making it an attractive candidate for further development and future commercialization as a feasible solution to high-volume production AM. Full article
(This article belongs to the Special Issue Recent Advances in Multi-Material Metal Additive Manufacturing)
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<p>Binder jet printing schematic diagram [<a href="#B6-jmmp-08-00191" class="html-bibr">6</a>]. (<b>a</b>) Spreading 1st layer (<b>b</b>) Printing 1st layer (<b>c</b>) Spreading a new layer (<b>d</b>) Curing binder in the oven (<b>e</b>) Removing looase powder (<b>f</b>) Infiltrating molten material.</p>
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<p>Schematic diagram of stereolithography process [<a href="#B9-jmmp-08-00191" class="html-bibr">9</a>].</p>
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<p>SEAM process basic workflow.</p>
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<p>Sedimentation behavior of SS420 suspension over time. In the graduated cylinder: grey region—SS420 powder; transparent green region—photopolymer resin. Reading unit is mL.</p>
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<p>Physical mask experimental setup, showing the UV irradiation from the LED light source through the dug-out hole on the mask.</p>
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<p>Disk fabricated using physical mask setup. A total of 10 layers were fabricated with an irradiation time of 30 s for each layer.</p>
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<p><b>Left</b>: original LCD-based bottom-up Anycubic SLA 3D printer; <b>right</b>: modified SLA system setup, showing the top-down projection through an LCD mask; the original LED chip has been replaced with a higher power unit.</p>
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<p>Modified DLP projector experimental setup showing a circular pattern projected onto the printing platform. The color wheel has been replaced with the bandpass filter in this image.</p>
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<p>Transmissible wavelength range of the FSQ-KG5 heat-absorbing bandpass filter (light blue line). Data are from [<a href="#B29-jmmp-08-00191" class="html-bibr">29</a>].</p>
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<p>Disk and tensile bar fabricated by the modified DLP projector. The color wheel in the projector has been replaced by a bandpass filter.</p>
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<p><b>Left</b>: pattern projected by the modified DLP projector. <b>Right</b>: corresponding fabricated parts from the projected patterns. The bottom two parts failed to fabricate due to the low light uniformity of the projector.</p>
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<p>Schematic diagram of the green part fabrication working principles of the SEAM process.</p>
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<p>First-generation SEAM system prototype showing its main components.</p>
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<p>Schematic diagram of (<b>a</b>) sedimentation of metal powder in the suspension, (<b>b</b>) printing challenges due to the gradual separation of metal and photopolymer resin in the print bed, and (<b>c</b>) the proposed two-step curing strategy.</p>
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<p>Single layer geometry after different soft-curing times of 1, 2, and 3 s. Visible resolution loss is observed with 3 s of soft-curing time.</p>
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<p>SS420 green sample set fabricated from a single build using a two-size powder mixture suspension by the SEAM process.</p>
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<p>SS420 green turbine fabricated by the SEAM process.</p>
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<p>Liquidus lines for various elements at different concentrations in iron [<a href="#B41-jmmp-08-00191" class="html-bibr">41</a>].</p>
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<p>Pareto charts and main effect plots of sintering temperature and additive wt.% addition on final part relative density for boron as sintering additive.</p>
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<p>Pareto charts and main effect plots of sintering temperature and additive wt.% addition on final part relative density for boron as sintering additive.</p>
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<p>Pareto charts and main effect plots of sintering temperature and additive wt.% addition on final part relative density for boron carbide as sintering additive.</p>
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<p>Pareto charts and main effect plots of sintering temperature and additive wt.% addition on final part relative density for boron nitride as sintering additive.</p>
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<p>SEAM-sintered SS420 coupons corresponding to the designed optimization matrix. Samples in column D exhibited “barreling” deformation.</p>
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<p>SS420 turbine fabricated by the SEAM process.</p>
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<p>EDS mappings of a sample from the sintered turbine.</p>
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24 pages, 15472 KiB  
Article
Determination of Chip Compression Ratio for the Orthogonal Cutting Process
by Michael Storchak
J. Manuf. Mater. Process. 2024, 8(5), 190; https://doi.org/10.3390/jmmp8050190 - 1 Sep 2024
Viewed by 257
Abstract
The chip compression ratio is the most important characteristic of various machining processes with chip generation. This characteristic enables the determination of kinetic and other energy loads on the tool and the machined material. This provides an overall evaluation of the machining process [...] Read more.
The chip compression ratio is the most important characteristic of various machining processes with chip generation. This characteristic enables the determination of kinetic and other energy loads on the tool and the machined material. This provides an overall evaluation of the machining process and the possibility of its subsequent optimization. This paper presents the results of determining this cutting characteristic by experimental method, analytical calculation, and numerical modeling. For the analytical calculation of the chip compression ratio, an analytical cutting model developed based on the variational principle of the minimum potential energy was used. A finite element model of orthogonal cutting was used for the numerical simulation of the above process characteristic. Experimentally, the chip compression ratio was determined by the ratio of the chip thickness to the cutting depth (undeformed cutting thickness). The chip thickness was determined by direct measurement using chip slices obtained during the cutting process. The Johnson–Cook constitutive equation was used as the machined material model and the Coulomb model was used as the friction model. The generalized parameters’ determination of the constitutive equation was performed through a DOE (Design of Experiment) sensitivity analysis. The variation range of these parameters was chosen based on the analysis of the effect of individual parameters of the constitutive equation on the chip compression ratio value. The largest deviations between the experimental and analytically calculated values of the chip compression ratio did not exceed 21%. At the same time, the largest deviations of simulated values of the indicated cutting characteristic and its experimental values did not exceed 20%. When comparing the experimental values of the chip compression ratio with the corresponding calculated and simulated values, the deviations were within 22%. Full article
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<p>Methodological scheme for determining the chip compression ratio.</p>
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<p>Experimental setup for the realization of the orthogonal cutting process.</p>
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<p>Metallographic slice to determine chip thickness and chip structure: (<b>a</b>) metallographic slice; (<b>b</b>) chip microstructure.</p>
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<p>Relationship between measured cutting force component and depth of cut.</p>
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<p>Initial geometry, boundary conditions, and mesh of the FE cutting model.</p>
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<p>Dependence of measured cutting force components on cutting speed at different tool rake angles: (<b>a</b>) variation of cutting force <span class="html-italic">F<sub>X</sub></span>; (<b>b</b>) variation of thrust force <span class="html-italic">F<sub>Z</sub></span>.</p>
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<p>Effect of cutting speed on chip compression ratio and true final shear of machined material at different tool rake angles: (<b>a</b>) chip compression ratio; (<b>b</b>) true final shear.</p>
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<p>Results of analytical determination of chip compression ratio: (<b>a</b>) cutting speed effect on analytically determined chip compression ratio values at different tool rake angles; (<b>b</b>) deviation between measured and analytically calculated chip compression ratio values.</p>
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<p>Results of the first iteration for the DOE sensitivity analysis: (<b>a</b>) at a tool rake angle of −10°; (<b>b</b>) at a tool rake angle of 10°.</p>
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<p>Effect analysis of hardening term parameters on chip compression ratio: (<b>a</b>) effect of parameter A at tool rake angle of 0°; (<b>b</b>) effect of parameter A at all studied tool rake angles simultaneously; (<b>c</b>) effect of parameter B at tool rake angle of 0°; (<b>d</b>) effect of parameter B at all studied tool rake angles simultaneously; (<b>e</b>) effect of parameter n at tool rake angle of 0°; (<b>f</b>) effect of parameter n at all studied tool rake angles simultaneously.</p>
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<p>Effect analysis of strain rate term parameter on chip compression ratio: (<b>a</b>) effect of parameter C at a tool rake angle of 0°; (<b>b</b>) effect of parameter C at all studied tool rake angles simultaneously.</p>
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<p>Effect analysis of thermic term parameter on chip compression ratio: (<b>a</b>) effect of parameter m at a tool rake angle of 0°; (<b>b</b>) effect of parameter m at all studied tool rake angles simultaneously.</p>
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<p>Results of the secondary iteration of the simulated chip compression ratio at different tool rake angles: (<b>a</b>) tool rake angle is −10°; (<b>b</b>) tool rake angle is 0°; (<b>c</b>) tool rake angle is 10°.</p>
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<p>Results comparing simulated and measured chip compression ratio values for different cutting speeds and tool rake angles: (<b>a)</b> tool rake angle <span class="html-italic">γ</span> = −10°; (<b>b</b>) tool rake angle <span class="html-italic">γ</span> = 0°; (<b>c</b>) tool rake angle <span class="html-italic">γ</span> = 10°.</p>
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<p>Contrasting experimental, calculated, and simulated values of shear angle for different cutting speeds and rake angles: (<b>a</b>) tool rake angle is −10°; (<b>b</b>) tool rake angle is 0°; (<b>c</b>) tool rake angle is =10°.</p>
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18 pages, 15654 KiB  
Article
Optimization of Material Utilization by Developing a Reliable Design Criterion for Tool Construction in Cross-Wedge Rolling
by Patrick Kramer, Abdulkerim Karaman and Michael Marré
J. Manuf. Mater. Process. 2024, 8(5), 189; https://doi.org/10.3390/jmmp8050189 - 27 Aug 2024
Viewed by 383
Abstract
The massive forming industry in Germany produces around 1.4 million parts every year, which are mainly used in safety-relevant areas such as the automotive industry. The production of these parts requires a considerable amount of energy, much of which remains unused and causes [...] Read more.
The massive forming industry in Germany produces around 1.4 million parts every year, which are mainly used in safety-relevant areas such as the automotive industry. The production of these parts requires a considerable amount of energy, much of which remains unused and causes high CO2 emissions. An efficient approach to reduce these emissions and improve material utilization is cross-wedge rolling, which enables efficient material utilization but is limited by the so-called Mannesmann effect, which leads to unwanted material defects. This paper describes the development and validation of a safe design criterion for cross-wedge rolling tools in order to avoid material damage caused by the Mannesmann effect and thus increase resource efficiency in forging. Based on simulation-supported investigations and experimental tests, process maps are created for various materials. The validation is carried out both in an experimental test facility with real tools and in an industrial production facility, which leads to a significant reduction in excess material and CO2 emissions. The results show that the full resource potential of cross-wedge rolling can be exploited by optimizing process parameters and tool geometries. Full article
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<p>Ratio of energy required for production and heating for 1 kg of forged part.</p>
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<p>Definition and examples of the bite ratio <span class="html-italic">s<sub>B</sub></span>/<span class="html-italic">h</span> (the colors represent a quantitative visualization of stress levels, with each color corresponding to a specific range of stress values).</p>
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<p>Description of the length of the reduced diameter using the example of a symmetrical tool.</p>
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<p>Cause-effect diagram to identify the relevant process parameters.</p>
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<p>Construction of the CWR test facility by integration into a hydraulic press.</p>
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<p>Results of the tests on 46MnVS5 with a diameter reduction of 55%.</p>
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<p>Statistical analysis of the influence of the investigated parameters.</p>
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<p>Structure of characteristic field map.</p>
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<p>Overview of the test specimen of the penetration tests with AlMgSi1.</p>
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<p>Dependence of mean crack width on variable <span class="html-italic">n</span> for 46MnVS5 material at different tool speeds.</p>
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<p>Characteristic diagrams of the steel materials for wedge geometry type A.</p>
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<p>Characteristic map (lines) of the material 46MnVS5 with the results of the real tools (points) for the cross-sectional areas A and M of the cross-wedge rolled part.</p>
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<p>Definitions of tool geometries and their influence on internal crack formation.</p>
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<p>Tool and test specimen for investigating the influence of the burr line.</p>
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<p>Influences of the different tool areas on the crack width.</p>
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16 pages, 9712 KiB  
Article
Study of Structure Formation in Multilayer Composite Material AA1070-AlMg6-AA1070-Titanium (VT1-0)-08Cr18Ni10Ti Steel after Explosive Welding and Heat Treatment
by Andrey Malakhov, Nemat Niyozbekov, Igor Denisov, Ivan Saikov, Denis Shakhray and Evgenii Volchenko
J. Manuf. Mater. Process. 2024, 8(5), 188; https://doi.org/10.3390/jmmp8050188 - 26 Aug 2024
Viewed by 465
Abstract
Multilayer composite materials, consisting of layers of aluminum alloy and steel, are used in the manufacturing of large engineering structures, including in the shipbuilding and railcar industries. Due to the different properties of aluminum alloys and steels, it is difficult to achieve high-strength [...] Read more.
Multilayer composite materials, consisting of layers of aluminum alloy and steel, are used in the manufacturing of large engineering structures, including in the shipbuilding and railcar industries. Due to the different properties of aluminum alloys and steels, it is difficult to achieve high-strength joints by conventional welding. Therefore, these joints are produced by explosive welding. In the present work, the structure of a multilayer material, AA1070-AlMg6-AA1070 (aluminum alloys)-VT1-0-08Cr18Ni10Ti (steel), was investigated after explosive welding and heat treatments were performed under different conditions. The microstructure of the AlMg6 layer at the AlMg6-AA1070 interface consists of shaped anisotropic grains extending along the weld interface. The AA1070 layer is enriched with magnesium due to its diffusive influx from AlMg6. In the AlMg6 and VT1-0 layers, adiabatic shear bands are found that start at the weld interface and propagate deep into the material. The optimal temperature for the heat treatment is 450–500 °C, as internal stresses are reduced at this temperature and the grain structure of the AlMg6 layer is not coarse. Tear strength testing revealed that the tear strength of the composite material after explosive welding was 130 ± 10 MPa, which exceeded the strength of the AA1070 alloy. Full article
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<p>Microstructure of the initial AlMg6 and EDS results: Spectrum 1 and 2 are scanning areas.</p>
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<p>Element distribution maps in AlMg6: (<b>a</b>) Al; (<b>b</b>) Mg; (<b>c</b>) Mn; (<b>d</b>) Fe.</p>
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<p>Schematic diagram of the experimental assembly (<b>a</b>) EW process (<b>b</b>): 1—sand; 2—detonator; 3—copper supports, 4—sand; 5—anvil; 6—base plate; 7—interlayer; 8—flyer plate; 9—explosive; 10—detonation products; h<sub>1</sub>—upper stand-off distance; h<sub>2</sub>—lower stand-off distance.</p>
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<p>Scheme of specimens and sections cutting: 1—specimens for tear strength testing; 2—metallographic sections; arrow D shows the detonation direction.</p>
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<p>Heat treatment modes.</p>
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<p>Scheme of tear strength testing: (<b>a</b>) tear specimen; (<b>b</b>) tear testing diagram: 1—mold, 2—base layer, 3—interlayer, 4—flyer layer, 5—male die, <span class="html-italic">P</span> is the applied load.</p>
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<p>Schematic illustration of the multilayer composite after ultrasonic testing (<b>a</b>) and the microstructure of the weld interface (<b>b</b>).</p>
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<p>Optical microstructure of the specimens after explosive welding and heat treatment: (<b>a</b>), (<b>e</b>), (<b>g</b>) after EW; (<b>b</b>) after HT at 450 °C; (<b>c</b>) at 500 °C; (<b>d</b>), (<b>f</b>), (<b>h</b>) at 550 °C.</p>
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<p>Optical microstructure of the specimens after explosive welding and heat treatment: (<b>a</b>), (<b>e</b>), (<b>g</b>) after EW; (<b>b</b>) after HT at 450 °C; (<b>c</b>) at 500 °C; (<b>d</b>), (<b>f</b>), (<b>h</b>) at 550 °C.</p>
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<p>Microstructure of the AA1070-VT1-0 weld interface: (<b>a</b>) after EW; (<b>b</b>) 550 °C.</p>
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<p>Microstructure of the VT1-0-08Cr18Ni10Ti weld interface: (<b>a</b>) after EW; (<b>b</b>) 450 °C; (<b>c</b>) 500 °C; (<b>d</b>) 550 °C.</p>
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<p>SEM image of the 08Cr18Ni10Ti–AlMg6 weld interface: (<b>a</b>) after EW; (<b>b</b>) after HT (550 °C).</p>
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<p>Microhardness distribution in the AlMg6-AA1070-VT1-0-08Cr18Ni10Ti.</p>
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<p>The tear strength value distribution along the bimetal plate.</p>
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17 pages, 5805 KiB  
Article
Application of Pattern Search and Genetic Algorithms to Optimize HDPE Pipe Joint Profiles and Strength in the Butt Fusion Welding Process
by Mahdi Saleh Mathkoor, Raad Jamal Jassim and Raheem Al-Sabur
J. Manuf. Mater. Process. 2024, 8(5), 187; https://doi.org/10.3390/jmmp8050187 - 25 Aug 2024
Viewed by 545
Abstract
The rapid spread of the use of high-density polyethylene (HDPE) pipes is due to the wide variety of methods for connecting them. This study keeps pace with the developments of butt fusion welding of HDPE pipes by exploring the relationship between the performance [...] Read more.
The rapid spread of the use of high-density polyethylene (HDPE) pipes is due to the wide variety of methods for connecting them. This study keeps pace with the developments of butt fusion welding of HDPE pipes by exploring the relationship between the performance of the weld joints by studying ultimate tensile strength and exploring the joint welding profiles by studying the shape of the joint at the outer surface of the pipe (height and width of the joint cap) and the shape of the joint at the internal surface (height and width of the joint root). Welding pressure, heater temperature, stocking time, and cooling time were the parameters for the welding process. Regression was analyzed using ANOVA, and an ANN was used to analyze the experimental results and predict the outputs. Two optimization techniques (pattern search and genetic algorithm) were applied to obtain the ideal operating conditions and compare their performance. The results showed that pattern search and genetic algorithms can determine the optimal output results and corresponding welding parameters. In comparison between the two methods, pattern search has a limited relative advantage. The optimal values for the obtained outputs revolved around a tensile strength of 35 MPa (3.45 and 4.5 mm for the cap and root heights, and 8 and 6.98 mm for the cap and root widths, respectively). When comparing the effects of welding parameters on the results, welding pressure had the best effect on tensile strength, and plate surface temperature had the most significant effect on the welding profile geometries. Full article
(This article belongs to the Special Issue Advances in Welding Technology)
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<p>Phases developing during butt fusion welding according to pressure with time variation.</p>
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<p>Sequential stages in the butt fusion welding process.</p>
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<p>Joint profile for HDPE in the butt fusion welding process.</p>
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<p>Main parts of the butt fusion welding machine.</p>
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<p>HDPE specimens tensile test: (<b>a</b>) universal tensile machine, (<b>b</b>) specimen preparation according to ASTM D638, (<b>c</b>) specimen fixation, and (<b>d</b>) specimen during failure.</p>
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<p>Regression analysis plotting of welding parameters used to train the algorithm: (<b>a</b>) training; (<b>b</b>) testing.</p>
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<p>Influence of welding pressure on joint welding profile at T = 160 °C, ST = 2 min, and CT = 10 min.</p>
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<p>Influence of welding pressure on joint tensile strength at T = 160 °C, ST = 2 min, and CT = 10 min.</p>
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<p>Influence of heating plate temperature on joint welding profile at P = 0.6 bar, ST = 2 min, and CT = 10 min.</p>
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<p>Influence of heating plate temperature on joint tensile strength at P = 0.6 bar, ST = 2 min, and CT = 10 min.</p>
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<p>Genetic algorithm fitness values and current best individuals from the genetic algorithm results for (<b>a</b>) cap height, (<b>b</b>) root height, (<b>c</b>) cap width, (<b>d</b>) root width, and (<b>e</b>) tensile strength.</p>
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<p>Pattern search fitness values and current best individuals from the genetic algorithm results for (<b>a</b>) cap height, (<b>b</b>) root height, (<b>c</b>) cap width, (<b>d</b>) root width, and (<b>e</b>) tensile strength.</p>
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22 pages, 8360 KiB  
Review
Review Regarding the Influence of Cryogenic Milling on Materials Used in the Aerospace Industry
by Bogdan Nita, Raluca Ioana Tampu, Catalin Tampu, Bogdan Alexandru Chirita, Eugen Herghelegiu and Carol Schnakovszky
J. Manuf. Mater. Process. 2024, 8(5), 186; https://doi.org/10.3390/jmmp8050186 - 24 Aug 2024
Viewed by 428
Abstract
In the aerospace industry, an important number of machined parts are submitted for high-performance requirements regarding surface integrity. Key components are made of materials selected for their unique properties and they are obtained by milling processes. In most situations, the milling process uses [...] Read more.
In the aerospace industry, an important number of machined parts are submitted for high-performance requirements regarding surface integrity. Key components are made of materials selected for their unique properties and they are obtained by milling processes. In most situations, the milling process uses cooling methods because, in their absence, the material surface could be affected by the generated heat (temperatures could reach up to 850 °C), the residual stress, the cutting forces, and other factors that can lead to bad integrity. Cryogenic cooling has emerged as a pivotal technology in the manufacturing of aeronautical materials, offering enhanced properties and efficiency in the production process. By utilizing extremely low temperatures, typically involving liquid nitrogen or carbon dioxide, cryogenic cooling can significantly enhance the material’s properties and machining processes. Cryogenic gases are tasteless, odorless, colorless, and nontoxic, and they evaporate without affecting the workers’ health or producing residues. Thus, cryogenic cooling is also considered an environmentally friendly method. This paper presents the advantages of cryogenic cooling compared with the classic cooling systems used industrially. Improvements in terms of surface finishing, tool life, and cutting force are highlighted. Full article
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<p>Main materials and temperatures in jet engines [<a href="#B61-jmmp-08-00186" class="html-bibr">61</a>,<a href="#B62-jmmp-08-00186" class="html-bibr">62</a>].</p>
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<p>Main parts that use steel alloys on Airbus and Boeing.</p>
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<p>Classification of main cooling/lubricating fluids.</p>
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<p>Internal injection cooling method [<a href="#B108-jmmp-08-00186" class="html-bibr">108</a>].</p>
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<p>Schematic diagram of cryogenic spray cooling method [<a href="#B103-jmmp-08-00186" class="html-bibr">103</a>].</p>
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<p>CO<sub>2</sub> adaptor mounted on the MQL nozzle [<a href="#B109-jmmp-08-00186" class="html-bibr">109</a>].</p>
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<p>Coanda effect nozzle [<a href="#B110-jmmp-08-00186" class="html-bibr">110</a>].</p>
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<p>Average surface roughness in dry and cryogenic milling of AISI 4340 at (<b>a</b>) Vc: 180 m/min, fz: 0.1 mm/tooth, ap: 0.3 mm; (<b>b</b>) Vc: 220 m/min, fz: 0.15 mm/tooth, ap: 0.3 mm [<a href="#B122-jmmp-08-00186" class="html-bibr">122</a>].</p>
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<p>Surface roughness developed with machining time under different environments at Vc = 264 m/min [<a href="#B107-jmmp-08-00186" class="html-bibr">107</a>].</p>
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<p>Surface roughness: dry vs. wet vs. cryo [<a href="#B39-jmmp-08-00186" class="html-bibr">39</a>].</p>
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<p>Surface roughness: dry vs. MQL vs. cryo vs. cryo + MQL: (<b>a</b>) f = 0.1 mm/rev; (<b>b</b>) f = 0.2 mm/rev [<a href="#B84-jmmp-08-00186" class="html-bibr">84</a>].</p>
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<p>Surface roughness: dry vs. cryo for all 8 parameters [<a href="#B66-jmmp-08-00186" class="html-bibr">66</a>].</p>
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<p>Tool flank wear for a. f = 0.1 mm/rev and b. f = 0.2 mm/rev: (<b>a</b>) f = 0.1 mm/rev; (<b>b</b>) f = 0.2 mm/rev [<a href="#B84-jmmp-08-00186" class="html-bibr">84</a>].</p>
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<p>Average flank wear for all 6 cooling methods [<a href="#B24-jmmp-08-00186" class="html-bibr">24</a>].</p>
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<p>Approximate time until the PVD coating wears off [<a href="#B116-jmmp-08-00186" class="html-bibr">116</a>].</p>
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<p>Average flank wear for all 3 parameters [<a href="#B13-jmmp-08-00186" class="html-bibr">13</a>].</p>
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<p>Cutting force for all cooling/lubrications methods [<a href="#B24-jmmp-08-00186" class="html-bibr">24</a>].</p>
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<p>Cutting force for all cooling/lubrication methods [<a href="#B21-jmmp-08-00186" class="html-bibr">21</a>].</p>
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<p>Cutting forces under cryo conditions (Case 1–4) and under dry conditions (Case 5–8) [<a href="#B10-jmmp-08-00186" class="html-bibr">10</a>].</p>
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18 pages, 6328 KiB  
Article
Enhancement of Additively Manufactured Bagasse Fiber-Reinforced Composite Material Properties Utilizing a Novel Fiber Extraction Process Used for 3D SLA Printing
by Md. Shahnewaz Bhuiyan, Ahmed Fardin, M. Azizur Rahman, Arafath Mohiv, Rashedul Islam, Md. Kharshiduzzaman, Md. Ershad Khan and Mohammad Rejaul Haque
J. Manuf. Mater. Process. 2024, 8(5), 185; https://doi.org/10.3390/jmmp8050185 - 23 Aug 2024
Viewed by 967
Abstract
The growing interest in sustainable and biodegradable materials has prompted significant attention towards natural fiber-reinforced composites (FRC) due to their lower environmental impacts. In a similar sustainable vein, this study fabricated composite materials utilizing bagasse fibers with the 3D SLA (Stereolithography) printing method. [...] Read more.
The growing interest in sustainable and biodegradable materials has prompted significant attention towards natural fiber-reinforced composites (FRC) due to their lower environmental impacts. In a similar sustainable vein, this study fabricated composite materials utilizing bagasse fibers with the 3D SLA (Stereolithography) printing method. To start with, a novel fiber extraction process was adopted for extracting fiber from the bagasse stem in three distinct methods (Process-1, Process-2, and Process-3). The fiber extraction process includes washing, sun-drying, manual collection of rind fibers, immersion of rind fibers in NaOH at specific concentrations for specific durations, combing, and drying. In Process-1, the rind fibers were immersed in 5% NaOH for 15 h, while in Process-2 and Process-3, the rind fibers were immersed in 1% NaOH, but the soaking time varied: 25 h for Process-2 and 18 h for Process-3.for 25 h, and in Process-3, the rind fibers were immersed in 1% NaOH for 18 h. The resulting bagasse fibers underwent comprehensive property assessment with a focus on functional group analysis, diameter measurement, and tensile strength assessment. Subsequently, these fibers were used to fabricate composite materials via the 3D SLA printing technique after being treated in a NaOH solution. The Fourier Transform Infrared (FTIR) Spectroscopy results clearly showed that a fraction of hemicellulose and lignin was removed by NaOH, resulting in improved tensile strength of the bagasse fibers. Three-dimensional-printed composites reinforced with bagasse fibers extracted through the P1 method showed the highest improvement in tensile strength (approximately 70%) compared to specimens made from pure resin. The lack of pores in the composite and the observable fiber fracture phenomena clearly indicate that 3D printing technology effectively enhances the quality of the interface between the fiber and the matrix interfacial bonding, consequently resulting in improved tensile properties of the composites. The 3D-printed composites reinforced with bagasse fiber showcased impressive tensile properties and provided solutions to the limitations of traditional composite manufacturing methods. This sets the stage for developing innovative composite materials that combine natural fibers with cutting-edge fabrication techniques, offering a promising path to tackle present and future economic and ecological challenges. Full article
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Graphical abstract

Graphical abstract
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<p>Steps of sugarcane bagasse fiber generation: (<b>a</b>) Cleaned chopped stems prepared for juice production, (<b>b</b>) sugarcane bagasse fibrous residue after juice extraction, (<b>c</b>) sugarcane rind fibers, and (<b>d</b>) sugarcane bagasse fiber obtained using chemical retting process.</p>
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<p>Flow chart highlighting the steps employed in the preparation of bagasse fiber.</p>
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<p>(<b>a</b>) Geometry and the dimension of the tensile test specimen (unit: mm). (<b>b</b>) Bagasse fiber-reinforced 3D-printed composite specimen.</p>
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<p>FTIR spectra of fibers.</p>
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<p>Histogram illustrating the variation in diameter of bagasse fibers extracted through (<b>a</b>) Process-1; (<b>b</b>) Process-2; and (<b>c</b>) Process-3.</p>
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<p>Representative load-versus-displacement curve for fiber.</p>
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<p>(<b>a</b>) Two-parameter Weibull plot of the tensile breaking load of bagasse fibers obtained from different processing methods. (<b>b</b>) Failure probability of bagasse fibers obtained from different processing methods.</p>
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<p>Load-versus-displacement curve for bagasse fiber-reinforced composite.</p>
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<p>(<b>a</b>) SEM images showing the fiber–matrix interface of 3D-printed bagasse-reinforced composite; (<b>b</b>) magnified view of the part outlined by red rectangle in (<b>a</b>).</p>
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<p>SEM images of the fracture surface of 3D-printed bagasse fiber-reinforced composite under tension showing (<b>a</b>) fracture of resin material; (<b>b</b>) magnified image of river-like line shown in (<b>a</b>) outlined by red rectangle; (<b>c</b>) fiber breakage; and (<b>d</b>) fibrillation of fiber.</p>
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<p>Comparison of ultimate tensile strength of 3D-printed bagasse-reinforced composites with literature data. Figure drawn based on data from Refs. [<a href="#B29-jmmp-08-00185" class="html-bibr">29</a>,<a href="#B45-jmmp-08-00185" class="html-bibr">45</a>,<a href="#B46-jmmp-08-00185" class="html-bibr">46</a>,<a href="#B47-jmmp-08-00185" class="html-bibr">47</a>,<a href="#B48-jmmp-08-00185" class="html-bibr">48</a>].</p>
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18 pages, 12668 KiB  
Article
The Mechanical Properties of a Transient Liquid Phase Diffusion Bonded SSM-ADC12 Aluminum Alloy with a ZnAl4Cu3 Zinc Alloy Interlayer
by Chaiyoot Meengam, Yongyuth Dunyakul and Dech Maunkhaw
J. Manuf. Mater. Process. 2024, 8(5), 184; https://doi.org/10.3390/jmmp8050184 - 23 Aug 2024
Viewed by 480
Abstract
In this study, the mechanical properties of SSM-ADC12 aluminum alloy specimens with a ZnAl4Cu3 zinc alloy interlayer were observed after Transient Liquid Phase Diffusion Bonding (TLPDB), a welding process conducted in a semi-solid state. The purpose of the experiment was to study how [...] Read more.
In this study, the mechanical properties of SSM-ADC12 aluminum alloy specimens with a ZnAl4Cu3 zinc alloy interlayer were observed after Transient Liquid Phase Diffusion Bonding (TLPDB), a welding process conducted in a semi-solid state. The purpose of the experiment was to study how the following parameters—bonding temperature (400, 430, 460, 490, and 520 °C), bonding time (60, 90, and 120 min), and thickness of the ZnAl4Cu3 zinc alloy (0.5, 1.0, and 2.0 mm)—affect the mechanical properties and the types of defects that formed. The results show that the bonding strength varied significantly with different parameters following the TLPDB process. A maximum bonding strength of 32.21 MPa was achieved at a bonding temperature of 490 °C, with 20 min of bonding and a ZnAl4Cu3 zinc alloy layer that was 2.0 mm thick. Conversely, changing the welding parameters influenced the bonding strength. A minimum bonding strength of 2.73 MPa was achieved at a bonding temperature of 400 °C, with a bonding time of 90 min and a ZnAl4Cu3 zinc alloy interlayer that was 2.0 mm thick. The Vickers microhardness results showed that the bonded zone had a lower hardness value compared to the base materials (BMs) of the SSM-ADC12 aluminum alloy (86.60 HV) and the ZnAl4Cu3 zinc alloy (129.37 HV). The maximum hardness was 83.27 HV, which resulted from a bonding temperature of 520 °C, a bonding time of 90 min, and a ZnAl4Cu3 zinc alloy that was 2.0 mm thick. However, in the near interface, the hardness value increased because of the formation of MgZn2 intermetallic compounds (IMCs). The fatigue results showed that the stress amplitude was 31.21 MPa in the BMs of the SSM-ADC12 aluminum alloy and 20.92 MPa in the material that results from this TLPDB process (TLPDB Material) when the limit of cyclic loading exceeded 106 cycles. Microstructural examination revealed that transformation from a β-eutectic Si IMC recrystallization structure to η(Zn–Al–Cu) and β(Al2Mg3Zn3) IMCs occurred. A size reduction to a width of 6–11 µm and a length of 16–44 µm was observed via SEM. Finally, voids or porosity and bucking defects were found in this experiment. Full article
(This article belongs to the Special Issue Advances in Dissimilar Metal Joining and Welding)
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Figure 1
<p>Photograph of the base microstructure of the SSM-ADC12 aluminum alloy formed using GISS casting.</p>
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<p>Equipment used for the TLPDB of SSM-ADC12 aluminum alloy using the ZnAl4Cu3 zinc alloy interlayer material.</p>
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<p>A schematic view of the temperature of TLPDB of the SSM-ADC12 aluminum alloy.</p>
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<p>Micrographs showing the characteristics of the samples and cross sections after TLPDB of the SSM-ADC12 aluminum alloy using a ZnAl4Cu3 zinc alloy with a 2.0 mm interlayer at 490 °C for (<b>a</b>) 60 min, (<b>b</b>) 90 min, and (<b>c</b>) 120 min.</p>
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<p>Bond strengths for the TLPDB of the SSM-ADC12 aluminum alloy using a ZnAl4Cu3 zinc alloy as the interlayer with different bonding times of (<b>a</b>) 60 min, (<b>b</b>) 90 min, and (<b>c</b>) 120 min.</p>
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<p>The fatigue S–N curves for the BMs and TLPDB material of the SSM-ADC12 aluminum alloy using a ZnAl4Cu3 zinc alloy as an interlayer.</p>
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<p>Micrographs of the microstructure in the bonded zone (<b>a</b>–<b>g</b>) and BM around diffused area after TLPDB.</p>
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<p>SEM micrographs (taken in EDX mode) of different characteristics of the eutectic Si IMCs show the following: (<b>a</b>) entire bond, (<b>b</b>) BMs, (<b>c</b>) bonding zone, (<b>d</b>) near-bonding zone, and (<b>e</b>) center interlayer.</p>
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<p>EDX mapping analysis of the composition (wt%) in the bonded zone.</p>
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<p>The Vickers microhardness values of the SSM-ADC12 aluminum alloy after TLPDB with a ZnAl4Cu3 zinc alloy interlayer that was 2.0 mm thick: (<b>a</b>) 60 min bonding time, (<b>b</b>) 90 min bonding time, and (<b>c</b>) 120 min bonding time.</p>
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