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Search Results (2,418)

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Keywords = topology optimization

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20 pages, 5007 KiB  
Article
Multi-Material Topology Optimization on Separate Tetrahedral Meshes with Explicit Design Resolution by Means of Remeshing
by Robert Renz and Albert Albers
Algorithms 2024, 17(10), 460; https://doi.org/10.3390/a17100460 - 16 Oct 2024
Viewed by 235
Abstract
As a method of lightweight design, multi-material design aims to make targeted use of materials in order to reduce CO2 emissions. In this context, it can be described as one of the product development methods used to meet the challenges of climate [...] Read more.
As a method of lightweight design, multi-material design aims to make targeted use of materials in order to reduce CO2 emissions. In this context, it can be described as one of the product development methods used to meet the challenges of climate change. However, since the design of structures in multi-material design is complex, topology optimization can be used to support the product developer. In this article, a multi-material topology optimization method is developed that combines the Velocity Field Level Set method with the Reconciled Level Set method. Furthermore, the current design is explicitly resolved in each iteration by means of multi-material remeshing. The edge collapse phase in the remeshing process is achieved by applying the producer consumer pattern. The developed method is then validated using known examples from the state of research, and the influence of the parameters of the method on the result is analyzed by means of studies. Full article
(This article belongs to the Section Analysis of Algorithms and Complexity Theory)
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Figure 1

Figure 1
<p>(<b>a</b>) A 2D level set function (blue), which represents a rectangle with two holes. The intersection between the level set function and the plane (green) results in the surface of the rectangle (orange). (<b>b</b>) Representation of the level set function and the corresponding part colored in blue.</p>
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<p>Reconciled level set method: The level set functions <math display="inline"><semantics> <mrow> <msub> <mi>φ</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi mathvariant="bold-italic">x</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> (gray) and <math display="inline"><semantics> <mrow> <msub> <mi>φ</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi mathvariant="bold-italic">x</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> (blue) each represent the boundaries of a material (<math display="inline"><semantics> <mrow> <msub> <mi>φ</mi> <mi>i</mi> </msub> <mrow> <mo>(</mo> <mi mathvariant="bold-italic">x</mi> <mo>)</mo> </mrow> <mo>=</mo> <mn>0</mn> </mrow> </semantics></math>) in the design domain D. <math display="inline"><semantics> <mi mathvariant="sans-serif">Γ</mi> </semantics></math> (orange) is the interface between the two materials.</p>
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<p>Visualization of the MBO operator using two level set functions <math display="inline"><semantics> <mrow> <msub> <mi>φ</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi mathvariant="bold-italic">x</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> (gray) and <math display="inline"><semantics> <mrow> <msub> <mi>φ</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi mathvariant="bold-italic">x</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> (blue) moving towards each other based on [<a href="#B22-algorithms-17-00460" class="html-bibr">22</a>]. (<b>a</b>) <math display="inline"><semantics> <mrow> <msub> <mi>φ</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi mathvariant="bold-italic">x</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msub> <mi>φ</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi mathvariant="bold-italic">x</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> are moving towards each other; there is no overlap. (<b>b</b>) <math display="inline"><semantics> <mrow> <msub> <mi>φ</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi mathvariant="bold-italic">x</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msub> <mi>φ</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi mathvariant="bold-italic">x</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> overlap in the orange area. (<b>c</b>) Correction of <math display="inline"><semantics> <mrow> <msub> <mi>φ</mi> <mn>1</mn> </msub> <mrow> <mo>(</mo> <mi mathvariant="bold-italic">x</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msub> <mi>φ</mi> <mn>2</mn> </msub> <mrow> <mo>(</mo> <mi mathvariant="bold-italic">x</mi> <mo>)</mo> </mrow> </mrow> </semantics></math> by applying the MBO operator; there is no longer any overlap.</p>
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<p>Structure of the optimization loop with the individual components.</p>
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<p>Schematic representation of the velocity extension from the zero level set (blue) to the target vertex based on [<a href="#B33-algorithms-17-00460" class="html-bibr">33</a>]. For this purpose, the pole of the target vertex is determined on the zero level set, and then, the normal velocity of the target vertex (orange) is calculated from the normal velocities of the triangle (green) using linear interpolation.</p>
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<p>Level set mesh (gray) and the dual mesh with corresponding cells (blue) based on [<a href="#B35-algorithms-17-00460" class="html-bibr">35</a>]. The dual mesh is used to develop an accurate upwind approximation of the Hamiltonian. A cellcorner c is shaded black.</p>
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<p>Five unique marching tetrahedra cases based on [<a href="#B36-algorithms-17-00460" class="html-bibr">36</a>]. The resulting discretized interface consisting of triangles is shown in orange.</p>
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<p>(<b>a</b>) Mesh with classification of vertices into volume and boundary vertices based on [<a href="#B38-algorithms-17-00460" class="html-bibr">38</a>]. (<b>b</b>) Invalid edge collapse since the collapse does not preserve the interface position (non-feature preserving). (<b>c</b>) Valid edge collapse since the collapse preserves the interface (feature preserving).</p>
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<p>Examples of cavity operations. (<b>a</b>) Edge collapse: the cavity is initialized with all adjacent elements (triangles or tetrahedra) of vertex A, and vertex B serves as the target vertex for the meshing. (<b>b</b>) Edge swap: the cavity is initialized with all elements adjacent to edge BC, and node A serves as the target node for meshing.</p>
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<p>Pre-processing step for remeshing the blue design area. Determination of the convex hull (orange), offset calculation of the convex hull (gray) with subsequent meshing.</p>
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<p>Design space of a box with chamfered edges, which is supported at four locations in the z-plane and has a load application location on the surface with a force in the negative <span class="html-italic">z</span>-direction in the amount of <span class="html-italic">F</span>.</p>
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<p>Symmetrical design space of the cantilever beam with a fixed support (<math display="inline"><semantics> <mrow> <msub> <mi>u</mi> <mi>x</mi> </msub> <mo>=</mo> <msub> <mi>u</mi> <mi>y</mi> </msub> <mo>=</mo> <msub> <mi>u</mi> <mi>z</mi> </msub> <mo>=</mo> <mn>0</mn> </mrow> </semantics></math>), a floating support (<math display="inline"><semantics> <mrow> <msub> <mi>u</mi> <mi>x</mi> </msub> <mo>=</mo> <msub> <mi>u</mi> <mi>y</mi> </msub> <mo>=</mo> <mn>0</mn> </mrow> </semantics></math>) and a load application point on the front side with a force in the negative <span class="html-italic">z</span>-direction in the amount of <span class="html-italic">F</span>.</p>
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<p>(<b>a</b>) Initial hole structure of the box in the single-material case. (<b>b</b>) Optimization result for the box at iteration 107.</p>
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<p>(<b>a</b>) Objective function for the single-material case of the box. (<b>b</b>) Volume constraint for the single-material case of the box.</p>
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<p>(<b>a</b>) Initial hole structure of the cantilever in the single-material case. (<b>b</b>) Optimization result for the cantilever at iteration 60.</p>
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<p>(<b>a</b>) History of the objective function for the single-material case of the cantilever. (<b>b</b>) History of the volume constraint for the single-material case of the cantilever.</p>
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<p>(<b>a</b>) Initial hole structure of the box in the multi-material case. Material 1 fills the entire design space except for the holes that are filled with material 2 (blue). (<b>b</b>) Optimization result for the box at iteration 293.</p>
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<p>(<b>a</b>) History of the objective function for the multi-material case of the box. (<b>b</b>) History of the volume constraints for the multi-material case of the box (blue material 1, brown material 2).</p>
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<p>(<b>a</b>) Initial hole structure of the cantilever in the multi-material case. Material 1 fills the entire design space except for the holes that are filled with material 2 (blue). (<b>b</b>) Optimization result of the cantilever at iteration 267.</p>
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<p>(<b>a</b>) History of the objective function for the multi-material case of the cantilever. (<b>b</b>) History of the volume constraints for the multi-material case of the cantilever (blue material 1, brown material 2).</p>
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<p>Optimization results of the cantilever for the multi-material case for different average edge lengths of the FE mesh with constant edge length of the LS mesh (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>e</mi> <mi>l</mi> <mi>e</mi> <mi>n</mi> <mi>g</mi> <mi>t</mi> <msub> <mi>h</mi> <mrow> <mi>a</mi> <mi>v</mi> <mi>g</mi> </mrow> </msub> <mo>=</mo> <mn>1.5</mn> </mrow> </semantics></math> (iteration 230). (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>e</mi> <mi>l</mi> <mi>e</mi> <mi>n</mi> <mi>g</mi> <mi>t</mi> <msub> <mi>h</mi> <mrow> <mi>a</mi> <mi>v</mi> <mi>g</mi> </mrow> </msub> <mo>=</mo> <mn>2.0</mn> </mrow> </semantics></math> (iteration 267). (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>e</mi> <mi>l</mi> <mi>e</mi> <mi>n</mi> <mi>g</mi> <mi>t</mi> <msub> <mi>h</mi> <mrow> <mi>a</mi> <mi>v</mi> <mi>g</mi> </mrow> </msub> <mo>=</mo> <mn>2.5</mn> </mrow> </semantics></math> (iteration 163).</p>
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<p>Optimization results of the cantilever for the multi-material case for different values of the Helmholtz filter parameter (<b>a</b>) <math display="inline"><semantics> <mrow> <msub> <mi>r</mi> <mi>f</mi> </msub> <mo>=</mo> <mn>0.75</mn> <mo>∗</mo> <mi>e</mi> <mi>l</mi> <mi>e</mi> <mi>n</mi> <mi>g</mi> <mi>t</mi> <msub> <mi>h</mi> <mrow> <mi>a</mi> <mi>v</mi> <mi>g</mi> </mrow> </msub> </mrow> </semantics></math> (iteration 227). (<b>b</b>) <math display="inline"><semantics> <mrow> <msub> <mi>r</mi> <mi>f</mi> </msub> <mo>=</mo> <mn>1.25</mn> <mo>∗</mo> <mi>e</mi> <mi>l</mi> <mi>e</mi> <mi>n</mi> <mi>g</mi> <mi>t</mi> <msub> <mi>h</mi> <mrow> <mi>a</mi> <mi>v</mi> <mi>g</mi> </mrow> </msub> </mrow> </semantics></math> (iteration 267). (<b>c</b>) <math display="inline"><semantics> <mrow> <msub> <mi>r</mi> <mi>f</mi> </msub> <mo>=</mo> <mn>1.75</mn> <mo>∗</mo> <mi>e</mi> <mi>l</mi> <mi>e</mi> <mi>n</mi> <mi>g</mi> <mi>t</mi> <msub> <mi>h</mi> <mrow> <mi>a</mi> <mi>v</mi> <mi>g</mi> </mrow> </msub> </mrow> </semantics></math> (iteration 205).</p>
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25 pages, 5457 KiB  
Article
Enhancing UAV Swarm Tactics with Edge AI: Adaptive Decision Making in Changing Environments
by Wooyong Jung, Changmin Park, Seunghyeon Lee and Hwangnam Kim
Drones 2024, 8(10), 582; https://doi.org/10.3390/drones8100582 - 15 Oct 2024
Viewed by 276
Abstract
This paper presents a drone system that uses an improved network topology and MultiAgent Reinforcement Learning (MARL) to enhance mission performance in Unmanned Aerial Vehicle (UAV) swarms across various scenarios. We propose a UAV swarm system that allows drones to efficiently perform tasks [...] Read more.
This paper presents a drone system that uses an improved network topology and MultiAgent Reinforcement Learning (MARL) to enhance mission performance in Unmanned Aerial Vehicle (UAV) swarms across various scenarios. We propose a UAV swarm system that allows drones to efficiently perform tasks with limited information sharing and optimal action selection through our Efficient Self UAV Swarm Network (ESUSN) and reinforcement learning (RL). The system reduces communication delay by 53% and energy consumption by 63% compared with traditional MESH networks with five drones and achieves a 64% shorter delay and 78% lower energy consumption with ten drones. Compared with nonreinforcement learning-based systems, mission performance and collision prevention improved significantly, with the proposed system achieving zero collisions in scenarios involving up to ten drones. These results demonstrate that training drone swarms through MARL and optimized information sharing significantly increases mission efficiency and reliability, allowing for the simultaneous operation of multiple drones. Full article
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<p>The concept of the proposed system.</p>
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<p>The overall overview of the proposed system.</p>
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<p>Structure of ESUSN topologies during step.</p>
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<p>Comparison of delay and energy consumption over time with 5 UAVs in the swarm.</p>
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<p>Comparison of delay and energy consumption over time with 10 UAVs in the swarm.</p>
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<p>Comparison of network stability between FANET and ESUSN with 10 UAVs in the swarm.</p>
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<p>Comparison of reward graph.</p>
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<p>Comparison of agent trajectories.</p>
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<p>Comparison of distance between agent and target.</p>
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<p>Expansion of UAV numbers 10 to 15.</p>
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<p>Performance comparison between algorithms as the number of UAVs increases.</p>
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14 pages, 4109 KiB  
Article
The Influence of Temperature on the Spatial Distribution of AuNPs on a Ceramic Substrate for Biosensing Applications
by Yazmín Mariela Hernández-Rodríguez, Esperanza Baños-López, Pablo Damián-Matsumura, Claudia Haydée González de la Rosa and Oscar Eduardo Cigarroa-Mayorga
Chemosensors 2024, 12(10), 212; https://doi.org/10.3390/chemosensors12100212 (registering DOI) - 15 Oct 2024
Viewed by 367
Abstract
In this study, we investigated the spatial distribution and homogeneity of gold nanoparticles (AuNPs) on an alumina (Al2O3; AAO) substrate for potential application as surface-enhanced Raman scattering (SERS) sensors. The AuNPs were synthesized through thermal treatment at 450 °C [...] Read more.
In this study, we investigated the spatial distribution and homogeneity of gold nanoparticles (AuNPs) on an alumina (Al2O3; AAO) substrate for potential application as surface-enhanced Raman scattering (SERS) sensors. The AuNPs were synthesized through thermal treatment at 450 °C at varying times (5, 15, 30, and 60 min), and their distribution was characterized using field-emission scanning electron microscopy (FE-SEM) and scanning transmission electron microscopy (STEM). The FE-SEM and STEM analyses revealed that the size and interparticle distance of the AuNPs were significantly influenced by the duration of thermal treatment, with shorter times promoting smaller and more closely spaced nanoparticles, and longer times resulting in larger and more dispersed particles. Raman spectroscopy, using Rhodamine 6G (R6G) as a probe molecule, was employed to evaluate the SERS enhancement provided by the AuNPs on the AAO substrate. Raman mapping (5 µm × 5 µm) was conducted on five sections of each sample, demonstrating improved homogeneity in the SERS effect across the substrate. The topological features of the AuNPs before and after R6G incubation were analyzed using atomic force microscopy (AFM), confirming the correlation between a decrease in surface roughness and an increase in R6G adsorption. The reproducibility of the SERS effect was quantified using the maximum intensity deviation (D), which was found to be below 20% for all samples, indicating good reproducibility. Among the tested conditions, the sample synthesized for 15 min exhibited the most favorable characteristics, with the smallest average nanoparticle size and interparticle distance, as well as the most consistent SERS enhancement. These findings suggest that AuNPs on AAO substrates, particularly those synthesized under the optimized condition of 15 min at 450 °C, are promising candidates for use in SERS-based sensors for detecting cancer biomarkers. This could be attributed to temperature propagation promoted at the time of synthesis. The results also provide insights into the influence of thermal treatment on the spatial distribution of AuNPs and their subsequent impact on SERS performance. Full article
(This article belongs to the Special Issue Biochemical Sensors Using Nanotechnology)
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Figure 1
<p>A schematic representation of AuNP dispersion on the alumina support after the (<b>a</b>) Al foil, (<b>b</b>) first electropolish, (<b>c</b>) alumina growth, (<b>d</b>) second electropolish, (<b>e</b>) second alumina growth, (<b>f</b>) pore comparison between the first and second anodization, (<b>g</b>) the alumina cleaning process, (<b>h</b>) gold layer deposition, and (<b>i</b>) final result of AuNPs on the AAO substrate.</p>
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<p>FE-SEM image of (<b>a</b>) frontal view and (<b>b</b>) lateral view of AAO substrate.</p>
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<p>Field-emission scanning electron microscopy images from a top view of the AuNPs on the alumina, obtained by exposing the Au layer on the alumina to a temperature of 450 °C for (<b>a</b>) 5 min, (<b>b</b>) 15 min, (<b>c</b>) 30 min, and (<b>d</b>) 60 min.</p>
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<p>AuNPs on the AAO substrate, imaged using scanning transmission electron microscopy at a (<b>a</b>) low magnification and a (<b>b</b>) higher magnification. (<b>c</b>) Display of the average diameters of the AuNPs. (<b>d</b>) The average interparticle distance for each analyzed synthesis condition of AuNPs.</p>
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<p>FE-SEM images of AuNPs on the alumina incubated with R6G, captured using (<b>a</b>) BSE and (<b>b</b>) SE detectors. (<b>c</b>) A schematic representation of the interactions between the substrate (AuNPs on AAO) and R6G. (<b>d</b>) A 3D projection of the Raman mapping, (<b>e</b>) a 2D projection of the Raman mapping, and a (<b>f</b>) Raman spectrum comparison between the highest intensity point and the lowest intensity point in the matrix of mapping.</p>
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<p>The AFM image of AuNPs on an alumina substrate (<b>a</b>) before and (<b>b</b>) after incubation with the R6G solution. Each set of images displays a 3D projection (<b>left</b>) and a 2D projection (<b>right</b>).</p>
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<p>(<b>a</b>) Raman mapping of the sample shown in (<b>b</b>). Each set of images displays a 3D projection (<b>left</b>) and a 2D projection (<b>right</b>).</p>
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<p>Field-emission scanning electron microscopy images from a top view of AuNPs on silicon wafer, obtained by exposing the Au layer on the alumina to a temperature of 450 °C for (<b>a</b>) 5 min, (<b>b</b>) 15 min, (<b>c</b>) 30 min, and (<b>d</b>) 60 min.</p>
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32 pages, 8805 KiB  
Article
The Application of an Improved LESS Dung Beetle Optimization in the Intelligent Topological Reconfiguration of ShipPower Systems
by Yinchao Tan, Sheng Liu, Lanyong Zhang, Jian Song and Yuanjie Ren
J. Mar. Sci. Eng. 2024, 12(10), 1843; https://doi.org/10.3390/jmse12101843 (registering DOI) - 15 Oct 2024
Viewed by 396
Abstract
To address the shortcomings of the Dung Beetle Optimization (DBO) algorithm in ship power-system fault reconfiguration, such as low population diversity and an imbalance between global exploration and local exploitation, the authors of this paper propose an improved Dung Beetle Optimization (LESSDBO) algorithm. [...] Read more.
To address the shortcomings of the Dung Beetle Optimization (DBO) algorithm in ship power-system fault reconfiguration, such as low population diversity and an imbalance between global exploration and local exploitation, the authors of this paper propose an improved Dung Beetle Optimization (LESSDBO) algorithm. The improvements include optimizing the initial population using Latin hypercube sampling and an elite population strategy, optimizing parameters with an improved sigmoid activation function, introducing the sine–cosine algorithm (SCA) for position update optimization, and performing multi-population mutation operations based on individual quality. The LESSDBO algorithm was applied to simulate the fault reconfiguration of a ship power system, and it was compared with the traditional DBO, Genetic Algorithm (GA), and Modified Particle Swarm Optimization (MSCPSO) methods. The simulation results showed that LESSDBO outperformed the other algorithms in terms of convergence accuracy, convergence speed, and global search capability. Specifically, in the reconfiguration under Fault 1, LESSDBO achieved optimal convergence in seven iterations, reducing convergence iterations by more than 30% compared with the other algorithms. In the reconfiguration under Fault 2, LESSDBO achieved optimal convergence in eight iterations, reducing convergence iterations by more than 23% compared with the other algorithms. Additionally, in the reconfiguration under Fault Condition 1, LESSDBO achieved a minimum of four switch actions, which is 33% fewer than the other algorithms, on average. In the reconfiguration under Fault Condition 2, LESSDBO achieved a minimum of eight switch actions, which is a 5.9% reduction compared with the other algorithms. Furthermore, LESSDBO obtained the optimal reconfiguration solution in all 50 trials for both Faults 1 and 2, demonstrating a 100% optimal convergence probability and significantly enhancing the reliability and stability of the algorithm. The proposed method effectively overcomes the limitations of the traditional DBO in fault reconfiguration, providing an efficient and stable solution for the intelligent topology reconfiguration of ship power systems. Full article
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<p>Image of MV Dali incident.</p>
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<p>Rolling dung beetles.</p>
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<p>Dancing dung beetles.</p>
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<p>Spawning boundary diagram.</p>
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<p>Egg-laying dung beetles.</p>
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<p>Foraging dung beetles.</p>
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<p>Standard initialization population.</p>
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<p>Latin hypercube sampling used to initialize the population.</p>
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<p>Latin hypercube sampling and elite population strategy.</p>
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<p>Comparison of control factor R.</p>
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<p>A typical ring-type power system of a large vessel.</p>
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<p>Symbolic diagram of the ship’s power system.</p>
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<p>Power grid diagram.</p>
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<p>Flowchart of program design.</p>
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<p>DBO optimal individual.</p>
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<p>MSCPSO optimal individual.</p>
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<p>GA optimal individual.</p>
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<p>LESSDBO optimal individual.</p>
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<p>Comparison of iterations and switch actions for different algorithms.</p>
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<p>Comparison of fitness values over iterations for different algorithms.</p>
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<p>Optimal load supply scheme for DBO under Fault Condition 2.</p>
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<p>Optimal load supply scheme for MSCPSO under Fault Condition 2.</p>
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<p>Optimal load supply scheme for GA under Fault Condition 2.</p>
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<p>Optimal load supply scheme for LESSDBO under Fault Condition 2.</p>
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<p>Comparison chart of the relationship between iteration counts and optimal switch actions for the four algorithms under Fault Condition 2.</p>
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<p>Comparison chart of iteration counts and optimal fitness values for the four algorithms under Fault Condition 2.</p>
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15 pages, 3144 KiB  
Communication
Optimizing Ammonia Detection with a Polyaniline−Magnesia Nano Composite
by Sharanabasava V. Ganachari, Fatheali A. Shilar, Veerabhadragouda B. Patil, T. M. Yunus Khan, C. Ahamed Saleel and Mohammed Azam Ali
Polymers 2024, 16(20), 2892; https://doi.org/10.3390/polym16202892 - 14 Oct 2024
Viewed by 315
Abstract
Polyaniline−magnesia (PANI/MgO) composites with a fibrous nanostructure were synthesized via in situ oxidative polymerization, enabling uniform MgO integration into the polyaniline matrix. These composites were characterized using FTIR spectroscopy to analyze intermolecular bonding, XRD to assess crystallographic structure and phase purity, and SEM [...] Read more.
Polyaniline−magnesia (PANI/MgO) composites with a fibrous nanostructure were synthesized via in situ oxidative polymerization, enabling uniform MgO integration into the polyaniline matrix. These composites were characterized using FTIR spectroscopy to analyze intermolecular bonding, XRD to assess crystallographic structure and phase purity, and SEM to examine surface morphology and topological features. The resulting PANI/MgO nanofibers were utilized to develop ammonia (NH3) gas-sensing probes with evaluations conducted at room temperature. The study addresses the critical challenge of achieving high sensitivity and selectivity in ammonia detection at low concentrations, which is a problem that persists in many existing sensor technologies. The nanofibers demonstrated high selectivity and optimal sensitivity for ammonia detection, which was attributed to the synergistic effects between the polyaniline and MgO that enhance gas adsorption. Furthermore, the study revealed that the MgO content critically influences both the morphology and the sensing performance, with higher MgO concentrations improving sensor response. This work underscores the potential of PANI/MgO composites as efficient and selective ammonia sensors, highlighting the importance of MgO content in optimizing material properties for gas-sensing applications. Full article
(This article belongs to the Collection Progress in Polymer Composites and Nanocomposites)
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<p>Synthesis of the PANI–magnesium oxide composite. The formation of Mg(II)-doped PANI is illustrated, with Mg acting as the interlink between two polymeric chains during polymerization. However, in a broader context, the resulting structure is referred to as a MgO/PANI composite, Reproduced with permission from ref. [<a href="#B21-polymers-16-02892" class="html-bibr">21</a>], Patil, V.B et al., Polymers. Adv. Technol, Wiley Publisher, 2021.</p>
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<p>FTIR curve of sample PANI/MgO nanocomposites.</p>
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<p>(<b>a</b>) SEM image and surface studies of PANI/MgO (0.1%), (<b>b</b>) PANI/MgO (0.2%), (<b>c</b>) PANI/MgO (0.3%) composites; (<b>d</b>) pure MgO nanoparticles; and (<b>e</b>) EDS of the MgO nanoparticles.</p>
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<p>XRD curves for the PANI/MgO nanocomposites.</p>
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<p>Sensor probe preparation: (<b>a</b>) Copper clad board (CCB), (<b>b</b>) sensor probe pattern printed on CCB, (<b>c</b>) sensor probe pattern etched using ferric chloride (FeCl₃), (<b>d</b>) sensor probe coated with PANI nanocomposite, (<b>e</b>) sensor dried at room temperature, (<b>f</b>) final prepared sensor probe.</p>
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<p>Results of sensing of ammonia vapors employing PANI/MgO composite with different concentrations of MgO (in %).</p>
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<p>(<b>a</b>) DC conductivity of PANI/MgO Composites (<b>b</b>) sensor setup.</p>
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26 pages, 16455 KiB  
Article
Optimal Energy Storage Allocation for Combined Wind-PV-EVs-ES System Based on Improved Triangulation Topology Aggregation Optimizer
by Chuanxi Fan, Haizheng Wang, Jinhua Zhang, Peng Cheng and Yuhua Bian
Electronics 2024, 13(20), 4041; https://doi.org/10.3390/electronics13204041 - 14 Oct 2024
Viewed by 337
Abstract
To determine the ES allocation based on a specific number of EVs connected to a combined WPESS, this paper develops an ESS allocation model that considers the impact of EV charging behavior on LSD, ES allocation cost, new energy utilization rate, and self-power [...] Read more.
To determine the ES allocation based on a specific number of EVs connected to a combined WPESS, this paper develops an ESS allocation model that considers the impact of EV charging behavior on LSD, ES allocation cost, new energy utilization rate, and self-power rate. First, several scenarios are generated using Monte Carlo sampling (MCS), and a typical day is selected through Backward Reduction (BR). Next, the Monte Carlo method is employed to generate conventional EV charging curves and optimize EV charging behavior by considering LSD and user charging costs. Subsequently, an ES capacity allocation model is developed, considering system costs, new energy utilization rate, and self-power rate. Finally, an improved triangulation topology aggregation optimizer (TTAO) is proposed, incorporating the logistic map, Golden Sine Algorithm (Gold-SA) strategy, and lens inverse imaging learning strategy. These enhancements improve the algorithm’s ability to identify global optimal solutions and facilitate its escape from local optima, significantly enhancing the optimization effectiveness of TTAO. The analysis of the calculation example indicates that after optimizing the charging behavior of EVs, the average daily cost is reduced by 204.94, the self-power rate increases by 2.25%, and the utilization rate of new energy sources rises by 2.50%, all while maintaining the same ES capacity. Full article
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<p>New energy system structure diagram.</p>
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<p>Flowchart of the scenario analysis model.</p>
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<p>Flowchart of the EV charging model.</p>
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<p>Flowchart of ES allocation and operation optimization.</p>
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<p>Flowchart of Wind-PV-EVs-ES system.</p>
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<p>Wind scenarios after reduction.</p>
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<p>PV scenarios after reduction.</p>
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<p>Load scenarios after reduction.</p>
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<p>Typical Wind-PV-Load scene.</p>
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<p>EV disorderly and orderly charging power.</p>
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<p>Load curves.</p>
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<p>Average daily investment comparison.</p>
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<p>Self-powered rate comparison.</p>
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<p>New energy utilization rate comparison.</p>
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<p>Pareto solution set comparison.</p>
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<p>Box plots of the optimal compromise solutions for each objective.</p>
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<p>Pareto solution set obtained by MOITTAO.</p>
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<p>Power balance diagram of Scenario 2.</p>
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<p>Power balance diagram of Scenario 3.</p>
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<p>SOC of Scenario 2.</p>
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<p>SOC of Scenario 3.</p>
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48 pages, 25488 KiB  
Review
High Mechanical Performance of Lattice Structures Fabricated by Additive Manufacturing
by Yuhua Li, Deyu Jiang, Rong Zhao, Xin Wang, Liqiang Wang and Lai-Chang Zhang
Metals 2024, 14(10), 1165; https://doi.org/10.3390/met14101165 - 12 Oct 2024
Viewed by 404
Abstract
Lattice structures show advantages in mechanical properties and energy absorption efficiency owing to their lightweight, high strength and adjustable geometry. This article reviews lattice structure classification, design and applications, especially those based on additive manufacturing (AM) technology. This article first introduces the basic [...] Read more.
Lattice structures show advantages in mechanical properties and energy absorption efficiency owing to their lightweight, high strength and adjustable geometry. This article reviews lattice structure classification, design and applications, especially those based on additive manufacturing (AM) technology. This article first introduces the basic concepts and classification of lattice structures, including the classification based on topological shapes, such as strut, surface, shell, hollow-strut, and so on, and the classification based on the deformation mechanism. Then, the design methods of lattice structure are analyzed in detail, including the design based on basic unit, mathematical algorithm and gradient structure. Next, the effects of different lattice elements, relative density, material system, load direction and fabrication methods on the mechanical performance of AM-produced lattice structures are discussed. Finally, the advantages of lattice structures in energy absorption performance are summarized, aiming at providing theoretical guidance for further optimizing and expanding the engineering application potential of lattices. Full article
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<p>Lattice structure classification based on structure and surface. Reproduced from Ref. [<a href="#B26-metals-14-01165" class="html-bibr">26</a>] under terms of the CC-BY license.</p>
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<p>An array of surface-based lattice structures: (<b>a</b>) basic cubic, (<b>b</b>) geometrically balanced BCC, (<b>c</b>) FCC, (<b>d</b>) hexagonally patterned honeycomb, (<b>e</b>) triangularly configured honeycomb, (<b>f</b>) complex re-entrant honeycomb, (<b>g</b>) uniquely shaped Schwartz, (<b>h</b>) curvature-defined gyroid, (<b>i</b>) gem-like diamond, (<b>j</b>) bisected split-p, and (<b>k</b>) characteristic Lidinoid. The red, blue, and green lines represent the three vertical dimensions. Reproduced from Ref. [<a href="#B102-metals-14-01165" class="html-bibr">102</a>] under terms of the CC-BY license.</p>
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<p>Origami structure types. The arrows in the rotating rigid structure indicate that the structure changes when the force is applied. The arrows in the spring-arm structure indicate changes in the original structure by replacing it with a spring structure. Reproduced with permission from Ref. [<a href="#B53-metals-14-01165" class="html-bibr">53</a>]. Copyright 2022 Elsevier. Reproduced from Ref. [<a href="#B127-metals-14-01165" class="html-bibr">127</a>] under terms of the CC-BY license.</p>
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<p>Design of lattice structures based on Maxwell’s criterion. (<b>A</b>) flexural structures; (<b>B</b>,<b>C</b>) tensile structures; (<b>D</b>) BCC lattice structures; (<b>E</b>) Octet-truss lattice structures; (<b>F</b>) FBCCXYZ lattice structures. Reproduced from Ref. [<a href="#B46-metals-14-01165" class="html-bibr">46</a>] under terms of the CC-BY license.</p>
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<p>Deformation mechanisms of stretch-dominated (or tension-dominated) and bending-dominated lattice structures. Reproduced from Ref. [<a href="#B46-metals-14-01165" class="html-bibr">46</a>] under terms of the CC-BY license.</p>
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<p>The relationship between properties and relative density of lattice structures. (<b>a</b>) The specific stiffness E, and (<b>b</b>) the specific strength of lattice structures as functions of their relative density. Reproduced from Ref. [<a href="#B46-metals-14-01165" class="html-bibr">46</a>] under terms of the CC-BY license.</p>
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<p>TPMS unit cells: (<b>a</b>) Primitive Schwartz, (<b>b</b>) Schoen Gyroid, (<b>c</b>) Schwarz Diamond, (<b>d</b>) Schoen-I-WP (IWP), (<b>e</b>) Fischer—Koch S (FKS), and (<b>f</b>) Schoen-F-RD (FRD). Reproduced from Ref. [<a href="#B151-metals-14-01165" class="html-bibr">151</a>] under terms of the CC-BY license.</p>
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<p>Gradient lattice structure design. Reproduced with permission from Ref. [<a href="#B40-metals-14-01165" class="html-bibr">40</a>]. Copyright 2021 Elsevier.</p>
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<p>The effect of replacing solid struts by hollow or layered struts. (<b>a</b>,<b>b</b>) Schematic diagram; (<b>c</b>,<b>d</b>) l/d; (<b>e</b>,<b>f</b>) predicted deformation under tensile + shear (η tensile + shear, %); and (<b>g</b>,<b>h</b>) representative compressive stress–strain plots for each design strategy (experiment). Reproduced from Ref. [<a href="#B157-metals-14-01165" class="html-bibr">157</a>] under terms of the CC-BY license.</p>
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<p>Stress–strain curves for different Ti2448 lattice structures at different strain levels: (<b>a</b>) 1–6% strain; (<b>b</b>) 1% strain; and (<b>c</b>) 2% strain. (<b>d</b>) Stress distribution at 1% strain. Reproduced with permission from Ref. [<a href="#B159-metals-14-01165" class="html-bibr">159</a>]. Copyright 2018 Elsevier.</p>
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<p>Mechanical properties of lattice structure with different porosity levels. (<b>a</b>) Superelastic properties of Ti2448 lattice structures of different porosity levels, and (<b>b</b>) stress distribution under 3% compressive strain in rhombohedral dodecahedron structures of different porosity levels. Reproduced with permission from Ref. [<a href="#B161-metals-14-01165" class="html-bibr">161</a>]. Copyright 2016 Elsevier.</p>
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<p>Applicability of the Gibson–Ashby model (red curve) to lattice structures manufactured by AM. (<b>a</b>,<b>d</b>) Bending-dominated TC4 lattice structures. (<b>b</b>,<b>e</b>) Tension-dominated TC4 lattice structures. (<b>c</b>,<b>f</b>) Other lattice structures subjected to bending. The blue curves are the corresponding prediction of the new theoretical model. * Represents the properties of the lattice structure. Reproduced from Ref. [<a href="#B157-metals-14-01165" class="html-bibr">157</a>] under terms of the CC-BY license.</p>
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<p>Comparison of lattice structure properties of different alloys. (<b>a</b>) S-N and (<b>b</b>) normalized S-N of Ti2448 and TC4 lattice structures with different porosity, and (<b>c</b>) the relationship between elastic modulus and fatigue strength of porous Ti2448 and TC4 samples. Reproduced with permission from Ref. [<a href="#B161-metals-14-01165" class="html-bibr">161</a>]. Copyright 2016, Elsevier.</p>
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<p>Loading directions dependent on the mechanical properties of lattice structures. Reproduced with permission from Ref. [<a href="#B168-metals-14-01165" class="html-bibr">168</a>]. Copyright 2022 Elsevier.</p>
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<p>Mechanical response of lattice structures to diverse loading scenarios: (<b>a</b>) compression, (<b>b</b>) tension, (<b>c</b>) three-point bending, (<b>d</b>) localized compression, (<b>e</b>) torsional stress, (<b>f</b>) shear forces, (<b>g</b>) localized torsion, (<b>h</b>) a combination of shear and compression, and (<b>i</b>) combined compression and torsion. Reproduced with permission from Ref. [<a href="#B9-metals-14-01165" class="html-bibr">9</a>]. Copyright 2022 Elsevier.</p>
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<p>Performance of gradient lattice structure. (<b>a</b>) Lattice structures with different gradients and (<b>b</b>) their corresponding stress–strain curves under compression. The numbers 1–7 marked in the figure represent the collapsed layers of the corresponding lattice structures. (<b>c</b>,<b>d</b>) are partially enlarged images. Reprinted with permission from Ref. [<a href="#B199-metals-14-01165" class="html-bibr">199</a>]. Copyright 2020 Elsevier.</p>
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<p>Deformation of lattice structure in different gradient directions: (<b>a</b>) gradient lattice structure in two directions; (<b>b</b>) experimental and simulated deformation process. Reproduced from Ref. [<a href="#B200-metals-14-01165" class="html-bibr">200</a>] under terms of the CC-BY license.</p>
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<p>Comparison of specific energy absorption of various lattice structures (the PA 11 FG lattice structures from this study are shown in red). Reproduced from Ref. [<a href="#B203-metals-14-01165" class="html-bibr">203</a>] under terms of the CC-BY license.</p>
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24 pages, 6036 KiB  
Article
Design and Optimization of a Custom-Made Six-Bar Exoskeleton for Pulp Pinch Grasp Rehabilitation in Stroke Patients
by Javier Andrés-Esperanza, José L. Iserte-Vilar and Víctor Roda-Casanova
Biomimetics 2024, 9(10), 616; https://doi.org/10.3390/biomimetics9100616 - 11 Oct 2024
Viewed by 796
Abstract
Stroke often causes neuromotor disabilities, impacting index finger function in daily activities. Due to the role of repetitive, even passive, finger movements in neuromuscular re-education and spasticity control, this study aims to design a rehabilitation exoskeleton based on the pulp pinch movement. The [...] Read more.
Stroke often causes neuromotor disabilities, impacting index finger function in daily activities. Due to the role of repetitive, even passive, finger movements in neuromuscular re-education and spasticity control, this study aims to design a rehabilitation exoskeleton based on the pulp pinch movement. The exoskeleton uses an underactuated RML topology with a single degree of mobility, customized from 3D scans of the patient’s hand. It consists of eight links, incorporating two consecutive four-bar mechanisms and the third inversion of a crank–slider. A two-stage genetic optimization was applied, first to the location of the intermediate joint between the two four-bar mechanisms and later to the remaining dimensions. A targeted genetic optimization process monitored two quality metrics: average mechanical advantage from extension to flexion, and its variability. By analyzing the relationship between these metrics and key parameters at different synthesis stages, the population evaluated is reduced by up to 96.2%, compared to previous studies for the same problem. This custom-fit exoskeleton uses a small linear actuator to deliver a stable 12.45 N force to the fingertip with near-constant mechanical advantage during flexion. It enables repetitive pulp pinch movements in a flaccid finger, improving rehabilitation consistency and facilitating home-based therapy. Full article
(This article belongs to the Special Issue Bionic Technology—Robotic Exoskeletons and Prostheses: 2nd Edition)
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Graphical abstract

Graphical abstract
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<p>Schematics of various RHEx topologies for transmitting motion to the patient’s fingers: (<b>a</b>) matched axes; (<b>b</b>) redundant linkage; (<b>c</b>) remote center of motion; (<b>d</b>) base-to-distal; and (<b>e</b>) compliant [<a href="#B12-biomimetics-09-00616" class="html-bibr">12</a>,<a href="#B14-biomimetics-09-00616" class="html-bibr">14</a>].</p>
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<p>Overlapped 3D-scanned hand in two different postures: extended index (pink) and pulp pinch grasp (green).</p>
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<p>TBM and RML mechanisms compared: (<b>a</b>) TBM consisting of two four-bar mechanisms and a crank–slider in the first inversion; (<b>b</b>) change of the crank–slider to its third inversion; (<b>c</b>) resulting RML mechanism having selected link 4 as the coupler of the crank–slider.</p>
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<p>(<b>Left</b>) nomenclature of the segments that form the concatenated four-bar mechanisms; (<b>Right</b>) region where to locate point <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>C</mi> </mrow> <mrow> <mn>14</mn> <mi>p</mi> </mrow> </msub> </mrow> </semantics></math>, delimited by the maximum and minimum values of <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>φ</mi> </mrow> <mrow> <mn>1</mn> <mi>p</mi> </mrow> </msub> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>L</mi> </mrow> <mrow> <mn>1</mn> <mi>p</mi> </mrow> </msub> </mrow> </semantics></math>.</p>
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<p>(<b>a</b>) Location of <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>B</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msup> </mrow> </semantics></math> and determination of the lengths <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>L</mi> </mrow> <mrow> <mn>2</mn> <mi>p</mi> </mrow> </msub> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>L</mi> </mrow> <mrow> <mn>2</mn> <mi>d</mi> </mrow> </msub> </mrow> </semantics></math> and of <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>B</mi> </mrow> <mrow> <mi>f</mi> <mi>i</mi> <mi>n</mi> </mrow> </msup> </mrow> </semantics></math>. (<b>b</b>) Selection of the design parameters: <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>L</mi> </mrow> <mrow> <mn>3</mn> <mi>p</mi> </mrow> </msub> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <msub> <mrow> <msub> <mrow> <mi>φ</mi> </mrow> <mrow> <mn>2</mn> <mi>p</mi> </mrow> </msub> <mo>,</mo> <msub> <mrow> <mi>φ</mi> </mrow> <mrow> <mn>1</mn> <mi>p</mi> </mrow> </msub> <mo>,</mo> <mi>L</mi> </mrow> <mrow> <mn>3</mn> <mi>d</mi> </mrow> </msub> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>φ</mi> </mrow> <mrow> <mn>2</mn> <mi>d</mi> </mrow> </msub> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>φ</mi> </mrow> <mrow> <mn>1</mn> <mi>d</mi> </mrow> </msub> </mrow> </semantics></math>. (<b>c</b>) Determination of <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>C</mi> </mrow> <mrow> <mn>14</mn> <mi>p</mi> </mrow> </msub> </mrow> </semantics></math> and therefore of <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>L</mi> </mrow> <mrow> <mn>1</mn> <mi>p</mi> </mrow> </msub> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>L</mi> </mrow> <mrow> <mn>4</mn> <mi>p</mi> </mrow> </msub> </mrow> </semantics></math>. (<b>d</b>) Superimposition of <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>L</mi> </mrow> <mrow> <mn>2</mn> <mi>p</mi> </mrow> </msub> </mrow> </semantics></math> bars in both postures to obtain <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>C</mi> </mrow> <mrow> <mn>14</mn> <mi>d</mi> </mrow> </msub> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>L</mi> </mrow> <mrow> <mn>1</mn> <mi>d</mi> </mrow> </msub> </mrow> </semantics></math>, and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>L</mi> </mrow> <mrow> <mn>4</mn> <mi>d</mi> </mrow> </msub> </mrow> </semantics></math> in an analogous procedure.</p>
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<p>Two generations were studied, for a total of 2211 mechanisms.</p>
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<p>(<b>a</b>) The figure illustrates how some initial re-locations of <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>B</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msup> </mrow> </semantics></math> around the initial hypothesis (<math display="inline"><semantics> <mrow> <msubsup> <mrow> <mi>B</mi> </mrow> <mrow> <mi>c</mi> <mi>e</mi> <mi>n</mi> <mi>t</mi> <mi>e</mi> <mi>r</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msubsup> </mrow> </semantics></math>) lead to configurations where <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>B</mi> </mrow> <mrow> <mi>f</mi> <mi>i</mi> <mi>n</mi> </mrow> </msup> </mrow> </semantics></math> ends up above (accepted solutions, in green) or below (rejected solutions, in red) the line <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>S</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msup> <mi>O</mi> </mrow> </semantics></math>. In grey in the background, two additional mechanisms generated under the <math display="inline"><semantics> <mrow> <msubsup> <mrow> <mi>B</mi> </mrow> <mrow> <mn>90</mn> <mo>°</mo> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msubsup> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msubsup> <mrow> <mi>B</mi> </mrow> <mrow> <mn>135</mn> <mo>°</mo> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msubsup> </mrow> </semantics></math> hypotheses are exemplified. (<b>b</b>) Four proposals generated after dimensional synthesis for the same <math display="inline"><semantics> <mrow> <msubsup> <mrow> <mi>B</mi> </mrow> <mrow> <mi>c</mi> <mi>e</mi> <mi>n</mi> <mi>t</mi> <mi>e</mi> <mi>r</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msubsup> </mrow> </semantics></math>, with random values for the parameters of <a href="#biomimetics-09-00616-t002" class="html-table">Table 2</a>.</p>
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<p>In black, the sequence of motion of the RHEx from extension (<math display="inline"><semantics> <mrow> <msup> <mrow> <mi>S</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msup> <msup> <mrow> <mi>T</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msup> <mo stretchy="false">)</mo> </mrow> </semantics></math> to flexion (<math display="inline"><semantics> <mrow> <msup> <mrow> <mi>S</mi> </mrow> <mrow> <mi>f</mi> <mi>i</mi> <mi>n</mi> </mrow> </msup> <msup> <mrow> <mi>T</mi> </mrow> <mrow> <mi>f</mi> <mi>i</mi> <mi>n</mi> </mrow> </msup> </mrow> </semantics></math>) is shown. The grey background represents the wide spectrum of possible linkages studied, achieved by generating and simulating four mechanisms with varied dimensions for each of the six possible <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>B</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msup> </mrow> </semantics></math> locations detailed in <a href="#biomimetics-09-00616-f007" class="html-fig">Figure 7</a>a.</p>
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<p>Preselection for the <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>B</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msup> </mrow> </semantics></math> locations, as explained in <a href="#sec2dot3dot2-biomimetics-09-00616" class="html-sec">Section 2.3.2</a>-(1), was conducted based on <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>δ</mi> </mrow> <mrow> <mi>M</mi> <mi>A</mi> </mrow> </msub> </mrow> </semantics></math> as it exhibits a higher coefficient of variation (<math display="inline"><semantics> <mrow> <mi>C</mi> <mi>V</mi> </mrow> </semantics></math>) compared to <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>M</mi> <mi>A</mi> </mrow> <mrow> <mi>a</mi> <mi>v</mi> <mi>g</mi> </mrow> </msub> </mrow> </semantics></math> across the 24 proposed cases. The colored region highlights the quartile of the population with the lowest <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>δ</mi> </mrow> <mrow> <mi>M</mi> <mi>A</mi> </mrow> </msub> </mrow> </semantics></math>, narrowing down this preselection to six possible RHEx proposals.</p>
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<p>Selection for the optimal <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>B</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msup> </mrow> </semantics></math> locations, as explained in <a href="#sec2dot3dot2-biomimetics-09-00616" class="html-sec">Section 2.3.2</a>-(1), was conducted based on <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>M</mi> <mi>A</mi> </mrow> <mrow> <mi>a</mi> <mi>v</mi> <mi>g</mi> </mrow> </msub> </mrow> </semantics></math> over the previous pre-selection of 6 cases. The colored region highlights the half of the pre-selected cases with the best <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>M</mi> <mi>A</mi> </mrow> <mrow> <mi>a</mi> <mi>v</mi> <mi>g</mi> </mrow> </msub> </mrow> </semantics></math>, that is, the three cases selected for further optimization.</p>
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<p>(<b>a</b>–<b>c</b>) In black, the representation of the three mechanisms selected from <a href="#biomimetics-09-00616-t003" class="html-table">Table 3</a> (after optimization for the location of joint <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>B</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msup> </mrow> </semantics></math>, following <a href="#sec2dot3dot2-biomimetics-09-00616" class="html-sec">Section 2.3.2</a>-(1)). The corresponding sets of mechanisms resulting from parameter variations are shown in grey in the background. (<b>d</b>) In black, the selected best mechanism after the optimization of the design parameters (following <a href="#sec2dot3dot2-biomimetics-09-00616" class="html-sec">Section 2.3.2</a>-(2)), overlapping with the preliminary design (in red).</p>
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<p>Dispersion of the different <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>δ</mi> </mrow> <mrow> <mi>M</mi> <mi>A</mi> </mrow> </msub> </mrow> </semantics></math> of the <math display="inline"><semantics> <mrow> <msup> <mrow> <mn>3</mn> <mo>·</mo> <mn>3</mn> </mrow> <mrow> <mn>6</mn> </mrow> </msup> <mo>=</mo> <mn>2187</mn> </mrow> </semantics></math> mechanisms resulting from an incremental, null, or decremental variation of the six parameters of <a href="#biomimetics-09-00616-t002" class="html-table">Table 2</a> in those three selected cases which resulted from the optimization of the location of the joint <math display="inline"><semantics> <mrow> <msup> <mrow> <mi>B</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> <mi>i</mi> </mrow> </msup> </mrow> </semantics></math> (resumed in <a href="#biomimetics-09-00616-t003" class="html-table">Table 3</a>). The colored region highlights the quartile of the population with the lowest <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>δ</mi> </mrow> <mrow> <mi>M</mi> <mi>A</mi> </mrow> </msub> </mrow> </semantics></math>, resulting in 547 proposals of RHEx.</p>
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<p>Final design and testing of the RHEx.</p>
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14 pages, 5999 KiB  
Article
Effect of Initial Surface Morphology and Laser Parameters on the Laser Polishing of Stainless Steel Manufactured by Laser Powder Bed Fusion
by Jiangwei Liu, Kangkang Zhao, Xiebin Wang and Hu Li
Materials 2024, 17(20), 4968; https://doi.org/10.3390/ma17204968 - 11 Oct 2024
Viewed by 379
Abstract
The topological characteristics of the down-skin surfaces for as-built components by laser powder bed fusion (LPBF) are particularly representative, while the study on the improvement of the surface quality of these surfaces remains largely unexplored. Herein, the laser polishing of LPBF-built components with [...] Read more.
The topological characteristics of the down-skin surfaces for as-built components by laser powder bed fusion (LPBF) are particularly representative, while the study on the improvement of the surface quality of these surfaces remains largely unexplored. Herein, the laser polishing of LPBF-built components with different inclination angles was systematically investigated with an emphasis on the down-skin surfaces. Our result shows that the topography of the top surface is independent of the inclination angle, and the surface topography of the down-skin surface is dominated by additional angle-dependent surface characteristics. It also indicates that the surface roughness can be reduced sharply when increasing the laser power from 40 W to 60 W, and the reduction slows down when further increasing the laser power while decreasing the scanning speed leads to a progressive improvement of the surface morphology. Moreover, a second-order regression model was established to evaluate the influence of the initial surface morphology and polishing parameters on the polished surface roughness and to achieve surface roughness optimization. Therefore, our established methodology can be readily applied to surface morphology manipulation and process optimization for laser polishing of widely used metals and alloys fabricated by the additive manufacturing process. Full article
(This article belongs to the Special Issue Nonconventional Technology in Materials Processing-3rd Edition)
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<p>(<b>a</b>) Flowchart of the steps of the experimental process. Schematic view of (<b>b</b>) the inclination angles varying from 50° to 90° and (<b>c</b>) the surfaces on a LPBF-built specimen.</p>
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<p>Three-dimensional and two-dimensional surface topographies of the LPBF-built specimen with an inclination angle of 50°: (<b>a</b>) the side surface and (<b>b</b>) the top surface.</p>
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<p>Three-dimensional surface height map of (<b>a</b>) the side surface and (<b>b</b>) the top surface of the as-built specimen with an inclination angle of 90°.</p>
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<p>Profile curves on the side surface of LPBF-built specimens with the inclination angle of (<b>a</b>) 50° and (<b>b</b>) 90°. L2 indicates the profile curve along the vertical direction and L5 is the profile curve along the horizontal direction.</p>
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<p>Morphological characteristics of LPBF-built specimens as a function of the inclination angle: (<b>a</b>) areal roughness <span class="html-italic">S<sub>a</sub></span> and profile roughness <span class="html-italic">R<sub>a</sub></span>; (<b>b</b>) areal kurtosis <span class="html-italic">S<sub>ku</sub></span> and areal skewness <span class="html-italic">S<sub>sk</sub></span>; (<b>c</b>) maximum height of peaks <span class="html-italic">S<sub>p</sub></span> and of valleys <span class="html-italic">S<sub>v</sub></span>; and (<b>d</b>) cross-sectional area on the 2D profile for peaks <span class="html-italic">A<sub>p</sub></span> and for valleys <span class="html-italic">A<sub>v</sub></span>.</p>
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<p>SEM image of the side surface before (<b>up</b>) and after (<b>down</b>) laser polishing for the specimen with an inclination angle of 50° (P3).</p>
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<p>D morphology and 2D profile curve of the polished surface of the specimen with 50° inclination angle: (<b>a</b>) 40 W and 300 mm/s (P1), (<b>b</b>) 120 W and 300 mm/s (P5).</p>
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<p>Profile morphology on the polished surface of specimens under various scanning speeds: (<b>a</b>) 500 mm/s, (<b>b</b>) 400 mm/s, (<b>c</b>) 300 mm/s, (<b>d</b>) 200 mm/s, and (<b>e</b>) 100 mm/s. L2 indicates the profile along the polishing direction, and L5 displays the profile vertically to the polishing direction.</p>
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<p>Surface roughness <span class="html-italic">S<sub>a</sub></span> and its decrease after laser polishing: (<b>a</b>–<b>c</b>) under different laser powers, and (<b>b</b>–<b>d</b>) under different scanning speeds.</p>
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<p>(<b>a</b>) Distribution of normal probability with residuals; (<b>b</b>) comparison of the actual and predicted values; (<b>c</b>) three-dimensional response surface model with the influence of the initial surface roughness and the laser power on the polished surface roughness.</p>
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26 pages, 4218 KiB  
Article
Optimal Scheduling of Integrated Energy System Considering Virtual Heat Storage and Electric Vehicles
by Yinjun Liu, Yongqing Zhu, Shunjiang Yu, Zhibang Wang, Zhen Li, Changming Chen, Li Yang and Zhenzhi Lin
World Electr. Veh. J. 2024, 15(10), 461; https://doi.org/10.3390/wevj15100461 - 11 Oct 2024
Viewed by 455
Abstract
Integrated energy systems (IESs) are complex multisource supply systems with integrated source, grid, load, and storage systems, which can provide various flexible resources. Nowadays, there exists the phenomenon of a current power system lacking flexibility. Thus, more research focuses on enhancing the flexibility [...] Read more.
Integrated energy systems (IESs) are complex multisource supply systems with integrated source, grid, load, and storage systems, which can provide various flexible resources. Nowadays, there exists the phenomenon of a current power system lacking flexibility. Thus, more research focuses on enhancing the flexibility of power systems by considering the participation of IESs in distribution network optimization scheduling. Therefore, the optimal scheduling of IESs considering virtual heat storage and electric vehicles (EVs) is proposed in this paper. Firstly, the basic structure of IESs and mathematical models for the operation of the relevant equipment are presented. Then, an optimal scheduling strategy of an IES considering virtual heat storage and electric vehicles is proposed. Finally, an IES with an IEEE 33-node distribution network, 20-node Belgian natural gas network, and 44-node heating network topologies is selected to validate the proposed strategy. The proposed models of integrated demand response (IDR), EV orderly charging participation, virtual heat storage, and actual multitype energy storage devices play the role of peak shaving and valley filling, which also helps to reduce the scheduling cost from CNY 11,253.0 to CNY 11,184.4. The simulation results also demonstrate that the proposed model can effectively improve the operational economy of IESs, and the scheduling strategy can promote the consumption of renewable energy, with the wind curtailment rate decreasing from 63.62% to 12.50% and the solar curtailment rate decreasing from 56.92% to 21.34%. Full article
(This article belongs to the Special Issue Power and Energy Systems for E-mobility)
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<p>Schematic diagram of integrated energy system structure.</p>
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<p>Vertical section of a supply pipeline <span class="html-italic">p</span> in heating networks.</p>
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<p>Distribution network structure diagram.</p>
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<p>Renewable resource output, electricity price, and load curve: (<b>a</b>) EV charged in an orderly manner; (<b>b</b>) EV charged in a disorderly manner.</p>
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<p>Electric power optimization scheduling result.</p>
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<p>Thermal power optimization scheduling result.</p>
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<p>Gas power optimization scheduling result.</p>
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<p>Participation of IDR of multitype energy in IES.</p>
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<p>Participation of EVs in electricity demand response.</p>
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<p>Electric power scheduling of charge and discharge.</p>
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<p>Thermal power scheduling of charge and discharge.</p>
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<p>Electric power optimization scheduling result of M-ENEVD.</p>
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<p>Comparisons of wind and solar curtailment rate before and after IES participation in distribution network scheduling.</p>
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27 pages, 14786 KiB  
Article
New Model for Defining and Implementing Performance Tests
by Marek Bolanowski, Michał Ćmil and Adrian Starzec
Future Internet 2024, 16(10), 366; https://doi.org/10.3390/fi16100366 - 10 Oct 2024
Viewed by 385
Abstract
The article proposes a new model for defining and implementing performance tests used in the process of designing and operating IT systems. By defining the objectives, types, topological patterns, and methods of implementation, a coherent description of the test preparation and execution is [...] Read more.
The article proposes a new model for defining and implementing performance tests used in the process of designing and operating IT systems. By defining the objectives, types, topological patterns, and methods of implementation, a coherent description of the test preparation and execution is achieved, facilitating the interpretation of results and enabling straightforward replication of test scenarios. The model was used to develop and implement performance tests in a laboratory environment and in a production system. The proposed division of the testing process into layers correlated with the test preparation steps allows to separate quasi-independent areas, which can be handled by isolated teams of engineers. Such an approach allows to accelerate the process of implementation of performance tests and may affect the optimization of the cost of their implementation. Full article
(This article belongs to the Special Issue Internet of Things Technology and Service Computing)
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<p>Dependency matrix of objectives and test types.</p>
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<p>Dependency matrix of objectives and test types for file server.</p>
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<p>Topological pattern of performance test execution.</p>
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<p>Examples of elements of sets <span class="html-italic">G</span>, <span class="html-italic">N</span>, <span class="html-italic">C</span>.</p>
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<p>Steps in the test definition process.</p>
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<p>Template of the test topology for scenario 1.</p>
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<p>Graph of the dependence of the number of connections per second on time on the test web server.</p>
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<p>Report on http client-server communication for test <span class="html-italic">t</span><sub>0</sub> in Scenario 1.</p>
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<p>Throughput vs. time graph on test web server for test <span class="html-italic">t</span><sub>1</sub> in Scenario 1.</p>
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<p>Report on http client-server communication for test <span class="html-italic">t</span><sub>1</sub> in Scenario 1.</p>
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<p>Template of the test topology for scenario 2.</p>
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<p>Graph of the dependence of the CPS on time on e-learning platform.</p>
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<p>Graph of the number of concurrent connections versus time on e-learning platform.</p>
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<p>Report on http client-server communication for test <span class="html-italic">t</span><sub>0</sub> in Scenario 2 (maximum possible CPS).</p>
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<p>Graph of the dependence of the resource load on the Moodle virtual machine on time for test <span class="html-italic">t</span><sub>0</sub> in Scenario 2 (maximum possible CPS).</p>
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<p>Dependence graph of resource load of the virtual machine with the database on time for test <span class="html-italic">t</span><sub>0</sub> in Scenario 2 (maximum possible CPS).</p>
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<p>Graph of the dependence of the CPS on time.</p>
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<p>Graph of the number of concurrent connections versus time for test <span class="html-italic">t</span><sub>0</sub> in Scenario 2.</p>
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<p>Report on http client-server communication for test <span class="html-italic">t</span><sub>0</sub> in Scenario 2 (CPS limited to 400).</p>
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<p>Graph of the dependence of the resource load on the Moodle virtual machine on time for test <span class="html-italic">t</span><sub>0</sub> in Scenario 2 (CPS limited to 400).</p>
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<p>Dependence graph of resource load of the virtual machine with the database on time for test <span class="html-italic">t</span><sub>0</sub> in Scenario 2 (CPS limited to 400).</p>
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<p>Graph of the number of concurrent connections versus time for test <span class="html-italic">t</span><sub>2</sub> in Scenario 2.</p>
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<p>Graph of the dependence of the resource load on the Moodle virtual machine on time for test <span class="html-italic">t</span><sub>2</sub> in Scenario 2.</p>
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<p>Dependence graph of resource load of the virtual machine with the database on time for test <span class="html-italic">t</span><sub>2</sub> in Scenario 2.</p>
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<p>Throughput vs. time graph on test web server for test <span class="html-italic">t</span><sub>1</sub> in Scenario 2.</p>
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<p>Report on http client-server communication for test <span class="html-italic">t</span><sub>1</sub> in Scenario 2.</p>
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<p>Graph of the dependence of the resource load on the Moodle virtual machine on time for test <span class="html-italic">t</span><sub>1</sub> in Scenario 2.</p>
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<p>Dependence graph of resource load of the virtual machine with the database on time for test <span class="html-italic">t</span><sub>1</sub> in Scenario 2.</p>
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24 pages, 16233 KiB  
Article
The Development of a Fillet Design Tool Based on Light-Weight Marine Diesel Engine Crankshafts
by Guangku Chen, Guixin Wang, Shuaining Liu, Jialiang Zhu, Xiaoxiao Niu and Yinyan Wang
J. Mar. Sci. Eng. 2024, 12(10), 1806; https://doi.org/10.3390/jmse12101806 - 10 Oct 2024
Viewed by 354
Abstract
As modern diesel engine design progresses toward higher burst pressure and power density, strict performance indices impose greater demands on the structural strength and reliability of crankshafts. We integrated finite element analysis and strength testing methods to achieve a lightweight crankshaft design. A [...] Read more.
As modern diesel engine design progresses toward higher burst pressure and power density, strict performance indices impose greater demands on the structural strength and reliability of crankshafts. We integrated finite element analysis and strength testing methods to achieve a lightweight crankshaft design. A comparison of the simulated results with the test data revealed that the crankshaft safety factor surpassed the permissible safety factor by 3.5 times, demonstrating significant safety redundancy in the design. We employed topology optimization techniques to create various crankshaft optimization models, yielding near-optimal solutions. Consequently, we identified the crankshaft with the best overall performance following comparative evaluations. We examined the influence of the fillet structure on the safety factor to mitigate stress concentration issues. Through multibody dynamic fatigue analysis, optimizing the crankshaft fillet resulted in a 6~7% increase in the safety factor. The minimum safety factor for the designed crankshaft was 1.6 times higher than the material permissible safety factor, which was 1.15. Utilizing the developed transient dynamics model of the lightweight crankshaft and a backpropagation genetic algorithm, we created a crankshaft fillet design tool to streamline the design process, which holds significant importance for the marine engine sector. Full article
(This article belongs to the Section Ocean Engineering)
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<p>Research pathway.</p>
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<p>The crankshaft mode.</p>
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<p>Cylinder pressure test schematic.</p>
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<p>The crankshaft stress cloud diagram.</p>
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<p>The Goodman fatigue curve.</p>
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<p>The upper fixture of the strength test.</p>
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<p>The paste position.</p>
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<p>The crankshaft strength test bench.</p>
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<p>Universal testing machine load loading sequence.</p>
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<p>The model validation results.</p>
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<p>The guidance model.</p>
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<p>The stress results of all optimization models.</p>
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<p>The comparison chart of relevant parameters.</p>
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<p>The independent influence of a factor.</p>
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<p>The effect of fillet radius on the safety factor.</p>
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<p>The comprehensive stress results of all optimization models.</p>
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<p>The initial three orders of natural frequencies.</p>
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<p>The dynamic analysis result.</p>
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<p>The comparative results before and after optimization.</p>
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<p>The prediction model.</p>
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<p>The curve of training result.</p>
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<p>The principle of fillet design tool.</p>
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16 pages, 2211 KiB  
Article
A Two-Player Game for Multi-Scale Topology Optimization of Static and Dynamic Compliances of Triply Periodic Minimal Surface-Based Lattice Structures
by Niclas Strömberg
Dynamics 2024, 4(4), 757-772; https://doi.org/10.3390/dynamics4040038 - 10 Oct 2024
Viewed by 368
Abstract
In this study, a novel non-cooperative two-player game for minimizing static (Player 1) and dynamic (Player 2) compliances is introduced, implemented, and demonstrated using a multi-scale topology optimization framework for triply periodic minimal surface (TPMS)-based lattice structures. Player 1 determines the optimal macro-layout [...] Read more.
In this study, a novel non-cooperative two-player game for minimizing static (Player 1) and dynamic (Player 2) compliances is introduced, implemented, and demonstrated using a multi-scale topology optimization framework for triply periodic minimal surface (TPMS)-based lattice structures. Player 1 determines the optimal macro-layout by minimizing the static compliance based on a micro-layout provided by Player 2. Conversely, player 2 identifies the optimal micro-layout (grading of the TPMS-based lattice structure) by minimizing the dynamic compliance given a macro-layout from Player 1. The multi-scale topology optimization formulations are derived using two density variables in each finite element. The first variable is the standard density, which dictates whether the finite element is void or contains the graded lattice structure and is governed by the rational approximation of material properties (RAMP) model. The second density variable represents the local relative density of the TPMS-based lattice structure, determining the effective orthotropic elastic properties of the finite element. The multi-scale game is implemented for three-dimensional problems, and solved using a Gauss–Seidel algorithm with sequential linear programming. It is numerically demonstrated for several benchmarks that the proposed multi-scale game generates equilibrium designs with strong performance for both static and harmonic load cases, effectively avoiding resonance at harmonic load frequencies. Validation is achieved through modal analyses of finite element models of the optimal designs. Full article
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<p>An optimal design of graded TPMS-based lattice structure of a pin-jointed beam for a static load case using the multi-scale topology optimization approach suggested in [<a href="#B7-dynamics-04-00038" class="html-bibr">7</a>]. The optimal design has a critical resonance frequency at 1604 Hz.</p>
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<p>The Sigmoid-like function in (<a href="#FD6-dynamics-04-00038" class="html-disp-formula">6</a>) plotted for <math display="inline"><semantics> <mrow> <msub> <mi>λ</mi> <mi>m</mi> </msub> <mo>=</mo> <mn>50</mn> </mrow> </semantics></math> and <math display="inline"><semantics> <msub> <mover accent="true"> <mi>ρ</mi> <mo stretchy="false">^</mo> </mover> <mi>m</mi> </msub> </semantics></math> = 0.2.</p>
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<p><b>Left</b>: The convergence of Harker’s benchmark in (<a href="#FD24-dynamics-04-00038" class="html-disp-formula">24</a>) using the Gauss–Seidel algorithm. <b>Right</b>: The convergence of the compliances for the pin-jointed beam benchmark with <math display="inline"><semantics> <mrow> <mo>Ω</mo> <mo>=</mo> <mn>1604</mn> </mrow> </semantics></math> Hz.</p>
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<p>The pin-jointed beam. The optimal grading on the macro-layout for the Static and the dynamic design, respectively, is depicted as well as the corresponding stl-file for the dynamic design. The modal analyses for both designs are also presented. <span class="html-italic">L</span> = 50 mm.</p>
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<p>Representative volume element (RVE) of the shell-based Schwarz-D structure plotted for the lower and upper bounds of 0.2 and 0.6, respectively, and the corresponding material interpolation laws <math display="inline"><semantics> <msub> <mi>f</mi> <mrow> <mi>i</mi> <mi>j</mi> </mrow> </msub> </semantics></math> in (<a href="#FD26-dynamics-04-00038" class="html-disp-formula">26</a>) (see also <a href="#dynamics-04-00038-t001" class="html-table">Table 1</a>). The RVEs are meshed using 5–10 million linear tetrahedral elements, not depicted here for clarity, when the numerical homogenization is performed. More details can be found in [<a href="#B8-dynamics-04-00038" class="html-bibr">8</a>].</p>
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<p>The clamped beam. Macro-layouts showing grading for the static case (<math display="inline"><semantics> <mrow> <mo>Ω</mo> <mo>=</mo> <mn>0</mn> </mrow> </semantics></math>) and the harmonic case (<math display="inline"><semantics> <mrow> <mo>Ω</mo> <mo>=</mo> <mn>2383</mn> </mrow> </semantics></math> Hz) are depicted as well as modal analyses of the designs. <span class="html-italic">L</span> = 50 mm.</p>
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<p>The L-shaped benchmark. Two critical modes are identified for the static design. The game is generating two optimal dynamic designs for the corresponding harmonic excitations. <span class="html-italic">L</span> = 40 mm.</p>
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<p>Modal analyses of the L-shaped designs. The dynamic design effectively avoids resonance at 372 Hz and 1206 Hz. The dashed window in the upper plot is increased to the right by decreasing the damping factor.</p>
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<p>A 3D L-shaped benchmark. The dynamic design avoids resonance at the frequency 986 Hz unlike the static design. Here, the colors represent the amplitudes of the corresponding mode. <span class="html-italic">L</span> = 75 mm.</p>
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<p>The amplification function <math display="inline"><semantics> <mrow> <mi>χ</mi> <mo>(</mo> <mi>ω</mi> <mo>)</mo> </mrow> </semantics></math> and the phase angle <math display="inline"><semantics> <mrow> <mo>Φ</mo> <mo>(</mo> <mi>ω</mi> <mo>)</mo> </mrow> </semantics></math> for <math display="inline"><semantics> <mrow> <mi>γ</mi> <mo>=</mo> <mn>0.02</mn> </mrow> </semantics></math>.</p>
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18 pages, 918 KiB  
Article
Self-Organizing and Routing Approach for Condition Monitoring of Railway Tunnels Based on Linear Wireless Sensor Network
by Haibo Yang, Huidong Guo, Junying Jia, Zhengfeng Jia and Aiyang Ren
Sensors 2024, 24(20), 6502; https://doi.org/10.3390/s24206502 - 10 Oct 2024
Viewed by 310
Abstract
Real-time status monitoring is crucial in ensuring the safety of railway tunnel traffic. The primary monitoring method currently involves deploying sensors to form a Wireless Sensor Network (WSN). Due to the linear characteristics of railway tunnels, the resulting sensor networks usually have a [...] Read more.
Real-time status monitoring is crucial in ensuring the safety of railway tunnel traffic. The primary monitoring method currently involves deploying sensors to form a Wireless Sensor Network (WSN). Due to the linear characteristics of railway tunnels, the resulting sensor networks usually have a linear topology known as a thick Linear Wireless Sensor Network (LWSN). In practice, sensors are deployed randomly within the area, and to balance the energy consumption among nodes and extend the network’s lifespan, this paper proposes a self-organizing network and routing method based on thick LWSNs. This method can discover the topology, form the network from randomly deployed sensor nodes, establish adjacency relationships, and automatically form clusters using a timing mechanism. In the routing, considering the cluster heads’ load, residual energy, and the distance to the sink node, the optimal next-hop cluster head is selected to minimize energy disparity among nodes. Simulation experiments demonstrate that this method has significant advantages in balancing network energy and extending network lifespan for LWSNs. Full article
(This article belongs to the Special Issue Energy Efficient Design in Wireless Ad Hoc and Sensor Networks)
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<p>Long rectangular monitoring area.</p>
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<p>The workflow of thick LWSN.</p>
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<p>Monitoring area in Cartesian coordinate system.</p>
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<p>The unique location of node <math display="inline"><semantics> <msub> <mi>N</mi> <mi>i</mi> </msub> </semantics></math>.</p>
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<p>The maximum distance <span class="html-italic">L</span> between anchor nodes.</p>
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<p>Coordinates of node <math display="inline"><semantics> <msub> <mi>N</mi> <mi>i</mi> </msub> </semantics></math>.</p>
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<p>The connectivity of node <math display="inline"><semantics> <msub> <mi>N</mi> <mn>0</mn> </msub> </semantics></math>.</p>
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<p>The connectivity of node <math display="inline"><semantics> <msub> <mi>N</mi> <mi>i</mi> </msub> </semantics></math>.</p>
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<p>Clustering through the timing mechanism.</p>
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<p>The clusters of network.</p>
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<p>Number of surviving nodes.</p>
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<p>Number of cluster heads.</p>
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<p>Total system energy.</p>
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9 pages, 4380 KiB  
Proceeding Paper
Fluidic Properties of Diamond and SplitP Structures with Varying Porosity Levels in Tissue Engineering Applications: A Computational Fluid Dynamics Analysis
by Muhammad Noman Shahid, Muhammad Mahabat Khan, Muhammad Usman Shahid and Shummaila Rasheed
Eng. Proc. 2024, 75(1), 39; https://doi.org/10.3390/engproc2024075039 - 9 Oct 2024
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Abstract
This study investigates the fluidic properties of the Diamond and SplitP structures with varying porosity levels (55%, 65%, and 75%) for tissue engineering applications using computational analysis. The scaffolds were designed using nTopology software and optimized to achieve the desired porosity and mechanical [...] Read more.
This study investigates the fluidic properties of the Diamond and SplitP structures with varying porosity levels (55%, 65%, and 75%) for tissue engineering applications using computational analysis. The scaffolds were designed using nTopology software and optimized to achieve the desired porosity and mechanical properties. The power law model was utilized to analyze blood as a non-Newtonian fluid. The study aims to optimize the scaffolds by observing fluidic characteristics such as permeability, pressure drop, and wall shear stress (WSS) to make them the optimal choice for bone tissue engineering applications. The results demonstrate that increasing porosity leads to higher permeability and lower pressure drop and WSS across the scaffolds. The findings suggest that the optimized Diamond and SplitP scaffolds with appropriate porosity levels can provide a suitable environment for cell adhesion, migration, proliferation, and differentiation, making them promising candidates for bone tissue engineering applications. Full article
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Figure 1

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<p>CAD models at 55% porosity: (<b>a</b>) SplitP scaffold; (<b>b</b>) Diamond scaffold.</p>
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<p>Boundary conditions on scaffolds.</p>
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<p>Comparison of permeability results for the Gyroid structure [<a href="#B14-engproc-75-00039" class="html-bibr">14</a>].</p>
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<p>Velocity contour for the Diamond structure at (<b>a</b>–<b>c</b>) 55% porosity, (<b>d</b>–<b>f</b>) 65% porosity, and (<b>g</b>–<b>i</b>) 75% porosity.</p>
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<p>Velocity contour for the SplitP structure at (<b>a</b>–<b>c</b>) 55% porosity, (<b>d</b>–<b>f</b>) 65% porosity, and (<b>g</b>–<b>i</b>) 75% porosity.</p>
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<p>Pressure contour for the Diamond structure at (<b>a</b>–<b>c</b>) 55% porosity, (<b>d</b>–<b>f</b>) 65% porosity, and (<b>g</b>–<b>i</b>) 75% porosity.</p>
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<p>Pressure contour for the SplitP structure at (<b>a</b>–<b>c</b>) 55% porosity, (<b>d</b>–<b>f</b>) 65% porosity, and (<b>g</b>–<b>i</b>) 75% porosity.</p>
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<p>(<b>a</b>) Porosity vs. permeability; (<b>b</b>) porosity vs. pressure drop; (<b>c</b>) porosity vs. WSS.</p>
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