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Search Results (638)

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Keywords = thermal compensation

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18 pages, 8361 KiB  
Article
Multi-Physical Field Coupling Analysis of Electro-Controlled Permanent Magnet Blank Holder Processes Considering Thermal Magnetic Losses
by Zhanshan Wang, Linyuan Meng, Gaochao Yu and Xiaoyu Ji
Metals 2025, 15(1), 39; https://doi.org/10.3390/met15010039 - 3 Jan 2025
Viewed by 170
Abstract
Electro-permanent magnet (EPM) technology is characterized by high integration, strong modularity, and stable magnetic force, making it a current research focus when combined with sheet metal deep drawing processes to develop EPM blank holder deep drawing technology. In this study, we investigated the [...] Read more.
Electro-permanent magnet (EPM) technology is characterized by high integration, strong modularity, and stable magnetic force, making it a current research focus when combined with sheet metal deep drawing processes to develop EPM blank holder deep drawing technology. In this study, we investigated the issue of thermal magnetic quantitative magnetic loss after the prolonged use of the EPMBH process, analyzing the variation in magnetic force with the temperature increase to provide necessary data support for the application of the EPMBH. First, a thermal network model for the four-magnetic pole unit EPM magnetic device was established, and through calculations on this model, the thermal equilibrium temperatures for the permanent magnet (PM)-NdFeB and reversible magnet (RM)-AlNiCo were found to be 72.13 °C and 72.41 °C, respectively. Second, the magnetic performance of PM and RM at different temperature points was measured to analyze the variation in their magnetic characteristics with the temperature increase. Third, a magnetic force model of the EPM magnetic device was established, and finite element analysis was conducted using the measured magnetic characteristics data of RM and PM. The results indicated that an increase in temperature leads to a reduction in magnetic force, with a maximum reduction of 18.57% observed after thermal equilibrium. An experimental testing platform was designed and built to validate the calculation and simulation results. Finally, a sheet metal deep drawing experiment using the EPMBH process was conducted, taking into account thermal magnetic loss factors. The results showed that magnetic force loss due to temperature rise affects the forming quality of the sheet metal. Therefore, in practical applications, it is necessary to establish a real-time temperature monitoring system and develop a temperature-based magnetic force compensation module. Full article
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<p>Principle of the EMPBH: (<b>a</b>) structure of the EPMBH; (<b>b</b>) hysteresis curve of the Al-Ni-Co; (<b>c</b>) schematic of the full-cycle fundamental principle of the proposed EPMH; the red arrows represent the magnetic field direction induced inside the core. The blue dots show the estimated field of the EPMBH in the state with an applied current measured at a certain distance from the core tip.</p>
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<p>Mold for the EPMBH: (<b>a</b>) structure of the EPMBH; (<b>b</b>) EPMBH deep drawing tools and 1. movable beam, 2. connecting rod, 3. upper base, 4. guide pillar, 5. punch, 6. EPM, 7. blank holder, 8. sheet metal, 9. die, 10. suction plate, 11. lower base.</p>
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<p>Mold for FMPUs: (<b>a</b>) 3D diagram; (<b>b</b>) sectional view.</p>
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<p>Node number for FMPUs: (<b>a</b>) the numbering situation of the surface; (<b>b</b>) the numbering situation of the interior.</p>
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<p>Thermal network model of four-pole chuck with compensation.</p>
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<p>Magnetic property detection of magnetic materials with temperature variation: (<b>a</b>) schematic diagram of detection principle; (<b>b</b>) magnetic property curves of NdFeB at different temperatures; (<b>c</b>) magnetic property curves of AlNiCo at different temperatures.</p>
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<p>The analysis results of coupling thermal, magnetic, and stress fields under loading conditions: magnetic induction intensity contour maps of the attracted plate surface at different temperatures ((<b>a</b>) 25 °C, (<b>b</b>) 50 °C, (<b>c</b>) 75 °C); (<b>d</b>) magnetic induction intensity curve recorded by the marking line; (<b>e</b>) magnetic force variation curve graph at different temperatures.</p>
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<p>The analysis results of coupling thermal, magnetic, and stress fields under unloading conditions: distribution of magnetic induction lines at different temperatures ((<b>a</b>) 25 °C, (<b>b</b>) 50 °C, (<b>c</b>) 75 °C); (<b>d</b>) residual magnetic force at different temperatures.</p>
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<p>Temperature–magnetic force test apparatus: (<b>a</b>) the schematic of the device; (<b>b</b>) photo of experimental apparatus; (<b>c</b>) results of experiment.</p>
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<p>Photograph of experimental setup.</p>
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<p>Drawn cups of 08Al sheet with diameter of 60 mm: (<b>a</b>) forming effect with BHF of 55 KN; (<b>b</b>) forming effect with BHF of 45 KN; (<b>c</b>) forming effect with BHF of 42 KN; (<b>d</b>) forming effect with BHF of 34 KN.</p>
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<p>Comparison of energy consumption.</p>
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15 pages, 1187 KiB  
Article
Integrated Assessment of the Quality of Functioning of Local Electric Energy Systems
by Waldemar Wójcik, Petro Lezhniuk, Cezary Kaczmarek, Viacheslav Komar, Iryna Hunko, Nataliia Sobchuk, Laura Yesmakhanova and Zhazira Shermantayeva
Energies 2025, 18(1), 137; https://doi.org/10.3390/en18010137 - 1 Jan 2025
Viewed by 290
Abstract
This research demonstrates the possibility and expediency of forming local electric energy systems (LEESs) based on renewable sources of energy (RSE) as balancing groups in the electric power system (EPS), which can maintain efficiency and provide power supply to consumers in an autonomous [...] Read more.
This research demonstrates the possibility and expediency of forming local electric energy systems (LEESs) based on renewable sources of energy (RSE) as balancing groups in the electric power system (EPS), which can maintain efficiency and provide power supply to consumers in an autonomous mode. The LEES is a part of the EPS of thermal and nuclear power plants and is considered as a separate balancing group. LEESs are designed in such a way that they can operate autonomously in both normal and extreme conditions in the EPS. The sources of electricity in LEESs are small hydroelectric power plants (SHPPs), photovoltaic power plants (PVPPs), and wind power plants (WPPs), whose electricity generation is unstable due to dependence on natural conditions. Therefore, the structure of a LEES with RSE includes an energy storage system with reserves sufficient to compensate for the unstable generation and balancing of the mode. LEESs can differ significantly in terms of key technical and economic indicators (power supply reliability, power losses, and power quality), and therefore, it is necessary to choose the optimal one. It is not advisable to optimize the quality of power supply in a LEES by individual indicators, as improvement of one indicator may lead to deterioration of another. The functional readiness of a LEES should be assessed by the quality of operation, which depends on reliability, power losses, and power quality. To simplify the task of assessing the quality of operation, which is a vector optimization problem, a method for determining the integral indicator as a number that characterizes the LEES and reflects the compromise between the values of reliability, power losses, and power quality has been developed. The integral indicator of the functioning of complex systems is based on a combination of the theory of Markov processes and the criterion method of similarity theory. The value of the integral indicator of the quality of operation of the LEES allows for comparing different variants of power transmission and distribution systems without determining individual components of technical and economic indicators—reliability, power losses, and power quality. The offered integral indicator of the quality of functioning of a LEES with RSE corresponds to the general requirements for such indicators. It reflects the actual operating conditions; allows for assessing the efficiency, quality, and optimality of power supply systems; and can be easily decomposed into partial indicators. Full article
(This article belongs to the Section F: Electrical Engineering)
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<p>Dependence of the intensity of failures on the operating time.</p>
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<p>Graph of changes in system states.</p>
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<p>(<b>a</b>) State graph. (<b>b</b>) Two-circuit power line.</p>
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<p>Graphical interpretation of the assessment of the complex indicator of the quality of functioning of the distribution power grid with distributed generation.</p>
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<p>Curves <math display="inline"><semantics> <mrow> <msub> <mi>U</mi> <mrow> <mo>Δ</mo> <mo>*</mo> </mrow> </msub> <mo>=</mo> <mi>f</mi> <mo stretchy="false">(</mo> <msub> <mi>J</mi> <mrow> <mi>l</mi> <mo>*</mo> </mrow> </msub> <mo stretchy="false">)</mo> </mrow> </semantics></math> for a certain grid.</p>
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<p>Changes in PVPP generation power (1) and load (2) during the year at a given time of day.</p>
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<p>Daily schedules of electric load of the electric grid and generation of PV power plants.</p>
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<p>Graphical representation of a set of statistics on generation (<b>a</b>) and consumption (<b>b</b>).</p>
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<p>Values of the integral indicator of the quality of functioning for various measures considered in this research.</p>
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11 pages, 2106 KiB  
Article
Performance Analysis of Thermal Energy Storage Tanks and Chillers for Optimizing Cooling Efficiency in Smart Greenhouses in Hot and Arid Climates
by Sul-Geon Choi, Doo-Yong Park, Doo-Sung Choi and Yong-Ho Jung
Sustainability 2024, 16(24), 11136; https://doi.org/10.3390/su162411136 - 19 Dec 2024
Viewed by 471
Abstract
This study analyzes the performance of thermal energy storage tanks and chillers in efficiently operating cooling systems for smart greenhouses in hot, arid climates such as the United Arab Emirates (UAE). The performance of chillers is heavily influenced by outdoor air temperatures, with [...] Read more.
This study analyzes the performance of thermal energy storage tanks and chillers in efficiently operating cooling systems for smart greenhouses in hot, arid climates such as the United Arab Emirates (UAE). The performance of chillers is heavily influenced by outdoor air temperatures, with the coefficient of performance (COP) of chillers decreasing and energy consumption increasing as daytime temperatures rise. This study found that when the outdoor air temperature reached 46.6 °C, the COP of the chiller dropped to 2.18, representing a 24.6% decrease compared to the COP of 2.89 at 35 °C. Conversely, at night, when the outdoor air temperature dropped to 28.3 °C, the chiller’s performance recovered, with the COP rising to 3.67. To address this, a strategy utilizing thermal energy storage tanks to store chilled water at night for use during the day was proposed, compensating for the decline in chiller performance. The results showed that when the thermal energy storage capacity was set at 40%, energy consumption decreased by up to 15%. However, while increasing the thermal energy storage capacity beyond 50% effectively reduced the peak load on the chiller, further increasing it beyond 60% led to a rise in chiller capacity and energy consumption. Therefore, this study concludes that setting the thermal energy storage capacity to no more than 50% is the most effective strategy to maximize chiller performance and reduce energy consumption. These findings provide crucial guidelines for the design and operation of cooling systems, offering valuable strategies to optimize the operation of smart greenhouses in hot climates. Full article
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<p>Smart greenhouse cooling system.</p>
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<p>Smart greenhouse and simulation modeling image.</p>
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<p>Change in chiller COP with ambient temperature.</p>
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<p>Hourly thermal energy storage tank capacity and chiller operating cooling load.</p>
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<p>Analysis of chiller COP variation with outdoor air temperature.</p>
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<p>Comparison of chiller COP, chiller cooling load, and energy consumption during nighttime thermal energy storage.</p>
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<p>Comparison of chiller energy consumption and capacity based on thermal energy storage tank capacity.</p>
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16 pages, 4072 KiB  
Article
Pyrolysis Modeling and Kinetic Study of Typical Insulation Materials for Building Exterior Envelopes
by Youchao Zhang, Bo Wang, Li Xu and Zhiming Ma
Buildings 2024, 14(12), 3956; https://doi.org/10.3390/buildings14123956 - 12 Dec 2024
Viewed by 429
Abstract
Thermal insulation materials are important for building energy conservation, but the inherent combustibility of these materials increases the fire risk of building facades. To better understand the fire behaviors of these materials, the study of the kinetics of thermal insulation pyrolysis is particularly [...] Read more.
Thermal insulation materials are important for building energy conservation, but the inherent combustibility of these materials increases the fire risk of building facades. To better understand the fire behaviors of these materials, the study of the kinetics of thermal insulation pyrolysis is particularly important because it is the initial step in ignition and combustion during fire. In this paper, the pyrolysis behavior of expanded polystyrene (EPS), a typical non-charring insulation polymer, has been investigated by thermogravimetric analysis at five different heating rates. The model-free kinetic analysis showed that the obtained average values for E and lnA were 151.23 kJ/mol and 21.29 ln/s, respectively. Model-fitting CR and masterplot methods indicated that f(α) = [2(1-α)[-ln(1-α)]]1/2 is considered the pyrolysis reaction mechanism of EPS degradation. Based on these results, the equation of the kinetic compensation effect was further developed as lnA = −3.1955 + 0.1736 Eα. Finally, the reaction model was reconstructed with the result of the expression f(α) = 3.95335α0.24174 (1-α) [-ln(1-α)]1.64712. In addition, PY-GC-MS experiments were conducted to analyze the composition of EPS pyrolysis volatiles. The results showed that the products were mainly compounds of benzene, naphthalene, and biphenyl. The analysis of EPS pyrolysis behavior and evolved gas provides numerical guidance for the future treatment and fire protection of insulation materials. Full article
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<p>The flow diagram of EPS pyrolysis kinetic analysis.</p>
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<p>TG (<b>left</b>) and DTG (<b>right</b>) curves of EPS at different heating rates.</p>
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<p>Eα values at different conversion rates under 4 model-free methods.</p>
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<p>Coats–Redfern method fitting curves of EPS pyrolysis at 5 heating rates (5, 10, 20, 40, and 80 °C/min).</p>
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<p>Theoretical masterplot data for 19 models.</p>
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<p>Theoretical masterplot data for 19 models.</p>
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<p>Coats–Redfern method calculated compensation effect plots for different heating rates.</p>
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<p>Relationship between lnA and conversion rate.</p>
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<p>The experimental kinetics function <span class="html-italic">f</span>(<span class="html-italic">α</span>) reconstructed from isoconventional methods under all heating rates.</p>
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<p>Comparison chart of the calculated value <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>d</mi> <mi>α</mi> <mo>/</mo> <mi>d</mi> <mi>t</mi> </mrow> <mrow> <mi>c</mi> <mi>a</mi> <mi>l</mi> </mrow> </msub> </mrow> </semantics></math> and experimental value <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>d</mi> <mi>α</mi> <mo>/</mo> <mi>d</mi> <mi>t</mi> </mrow> <mrow> <mi>e</mi> <mi>x</mi> <mi>p</mi> </mrow> </msub> </mrow> </semantics></math>.</p>
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<p>Analytical results of EPS by PY-GC-MS at 683 K under helium atmosphere.</p>
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24 pages, 8107 KiB  
Article
Study on High-Temperature Constitutive Model and Plasticity of the Novel Cr-Mo-V Hot-Work Die Steel Forging
by Yasha Yuan, Yichou Lin, Wenyan Wang, Bo Zhang, Ruxing Shi, Yudong Zhang, Jingpei Xie, Chuan Wu and Feng Mao
Materials 2024, 17(24), 6071; https://doi.org/10.3390/ma17246071 - 12 Dec 2024
Viewed by 344
Abstract
In response to the increasingly strict performance requirements of large molds, a novel Cr-Mo-V hot-work die steel has been developed. In order to study the high-temperature hot deformation behavior and plasticity of the novel steel, hot compression tests were conducted on the Gleeble-1500D [...] Read more.
In response to the increasingly strict performance requirements of large molds, a novel Cr-Mo-V hot-work die steel has been developed. In order to study the high-temperature hot deformation behavior and plasticity of the novel steel, hot compression tests were conducted on the Gleeble-1500D thermal simulation testing machine at a deformation temperature of 950~1200 °C and a strain rate of 0.001~5 s−1. Based on the Arrhenius constitutive model, a novel Cr-Mo-V steel high-temperature constitutive model considering strain was established. The reliability and applicability of this modified model, which includes strain compensation, were assessed using the phase relationship coefficient (R) and the average absolute relative error (AARE). The values of R and AARE for comparing predicted outcomes with experimental data were 0.98902 and 3.21%, respectively, indicating that the model demonstrated high precision and reliability. Based on the Prasad criterion, a 3D hot processing map of the novel Cr-Mo-V steel was established, and the instability zone of the material was determined through the hot processing map: the deformation temperature (950~1050 °C) and strain rate (0.001~0.01 s−1) were prone to adiabatic shear and crystal mixing. The suitable processing range was determined based on the hot processing map: The first suitable processing area was the strain range of 0.05~0.35, the temperature range was 1100~1175 °C, and the strain rate was 0.001~0.009 s−1. The second suitable processing area was a strain of 0.45~0.65, a temperature of 1100~1200 °C, and a strain rate of 0.0024~0.33 s−1. Finally, the forging process of hundred-ton die steel forging was developed by combining 3D hot processing maps with finite element simulation, and the forging trial production of 183 t forging was carried out. The good forging quality indicated that the established hot processing map had a good guiding effect on the production of 100-ton test steel forging. Full article
(This article belongs to the Special Issue Research on Performance Improvement of Advanced Alloys)
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<p>The initial microstructure of novel Cr-Mo-V steel.</p>
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<p>Test process scheme of the test steel.</p>
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<p>True stress–strain and temperature–stress curves for the test steel under different temperatures and strain rates. (<b>a</b>) 950 °C; (<b>b</b>) 1000 °C; (<b>c</b>) 1050 °C; (<b>d</b>) 1100 °C; (<b>e</b>) 1150 °C; (<b>f</b>) 1200 °C; (<b>g</b>) Curve of temperature-stress.</p>
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<p>Microstructure under different deformation conditions: (<b>a</b>) 950 °C and 0.1 s<sup>−1</sup>, (<b>b</b>) 1050 °C and 0.1 s<sup>−1</sup>, (<b>c</b>) 1150 °C and 0.1 s<sup>−1</sup>, (<b>d</b>) 1200 °C and 0.1 s<sup>−1</sup>, (<b>e</b>) 1100 °C and 5 s<sup>−1</sup>, (<b>f</b>) 1100 °C and 0.1 s<sup>−1</sup>, (<b>g</b>) 1100 °C and 0.01 s<sup>−1</sup>, and (<b>h</b>) 1100 °C and 0.001 s<sup>−1</sup>.</p>
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<p>Microstructure under different deformation conditions: (<b>a</b>) 950 °C and 0.1 s<sup>−1</sup>, (<b>b</b>) 1050 °C and 0.1 s<sup>−1</sup>, (<b>c</b>) 1150 °C and 0.1 s<sup>−1</sup>, (<b>d</b>) 1200 °C and 0.1 s<sup>−1</sup>, (<b>e</b>) 1100 °C and 5 s<sup>−1</sup>, (<b>f</b>) 1100 °C and 0.1 s<sup>−1</sup>, (<b>g</b>) 1100 °C and 0.01 s<sup>−1</sup>, and (<b>h</b>) 1100 °C and 0.001 s<sup>−1</sup>.</p>
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<p>Fitting curves for test steel under different temperatures and strain rates: (<b>a</b>) ln<math display="inline"><semantics> <mrow> <mover> <mi mathvariant="normal">ε</mi> <mo>·</mo> </mover> </mrow> </semantics></math>–lnσp, (<b>b</b>) ln<math display="inline"><semantics> <mrow> <mover> <mi mathvariant="normal">ε</mi> <mo>·</mo> </mover> </mrow> </semantics></math>–σp; (<b>c</b>) ln(sinh(ασ))–ln<math display="inline"><semantics> <mrow> <mover> <mi mathvariant="normal">ε</mi> <mo>·</mo> </mover> </mrow> </semantics></math>, and (<b>d</b>) ln(sinh(ασ))–1000/T.</p>
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<p>Fitting curve of lnZ–ln(sinh(ασ)).</p>
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<p>Relationship between material parameters and true strain and the polynomial fitting curve of eight degrees: (<b>a</b>) α, (<b>b</b>) n, (<b>c</b>) Q, and (<b>d</b>) lnA.</p>
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<p>Theoretical and experimental values under different deformation conditions. (<b>a</b>) 950 °C; (<b>b</b>) 1000 °C; (<b>c</b>) 1050 °C; (<b>d</b>) 1100 °C; (<b>e</b>) 1150 °C; (<b>f</b>) 1200 °C.</p>
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<p>The correlation curve of theoretical and experimental values.</p>
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<p>Hot processing maps at different strains: (<b>a</b>) 0.05, (<b>b</b>) 0.2, (<b>c</b>) 0.35, (<b>d</b>) 0.5, (<b>e</b>) 0.65, and (<b>f</b>) 0.8.</p>
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<p>The 3D power dissipation map (<b>a</b>) and 3D instability map (<b>b</b>).</p>
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<p>Microstructures of the safe zone and unstable zone of the novel Cr-Mo-V steel: (<b>a</b>) 1100 °C-0.1 s<sup>−1</sup> and (<b>b</b>) 1000 °C-1 s<sup>−1</sup>.</p>
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<p>The size diagram of 183 t module forging.</p>
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<p>The FEM of billet and dies of the 183 t ingot forging process.</p>
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<p>Simulation results of upsetting of the novel Cr-Mo-V die steel of 183 t.</p>
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<p>Simulation results of the novel Cr-Mo-V die steel of 183 t.</p>
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<p>The 183 t forging of a novel Cr-Mo-V die steel: (<b>a</b>) upsetting, (<b>b</b>) forged product, (<b>c</b>) finished forging, and (<b>d</b>) ultrasonic testing.</p>
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<p>SEM images at the surface and 1/2 height of the 183 t forging. (<b>a</b>) surface; (<b>b</b>) 1/2 height.</p>
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11 pages, 2574 KiB  
Article
Photo-Excited Carrier Dynamics in Ammonothermal Mn-Compensated GaN Semiconductor
by Patrik Ščajev, Paweł Prystawko, Robert Kucharski and Irmantas Kašalynas
Materials 2024, 17(23), 5995; https://doi.org/10.3390/ma17235995 - 7 Dec 2024
Viewed by 581
Abstract
We investigated the carrier dynamics of ammonothermal Mn-compensated gallium nitride (GaN:Mn) semiconductors by using sub-bandgap and above-bandgap photo-excitation in a photoluminescence analysis and pump–probe measurements. The contactless probing methods elucidated their versatility for the complex analysis of defects in GaN:Mn crystals. The impurities [...] Read more.
We investigated the carrier dynamics of ammonothermal Mn-compensated gallium nitride (GaN:Mn) semiconductors by using sub-bandgap and above-bandgap photo-excitation in a photoluminescence analysis and pump–probe measurements. The contactless probing methods elucidated their versatility for the complex analysis of defects in GaN:Mn crystals. The impurities of Mn were found to show photoconductivity and absorption bands starting at the 700 nm wavelength threshold and a broad peak located at 800 nm. Here, we determined the impact of Mn-induced states and Mg acceptors on the relaxation rates of charge carriers in GaN:Mn based on a photoluminescence analysis and pump–probe measurements. The electrons in the conduction band tails were found to be responsible for both the photoconductivity and yellow luminescence decays. The slower red luminescence and pump–probe decays were dominated by Mg acceptors. After photo-excitation, the electrons and holes were quickly thermalized to the conduction band tails and Mg acceptors, respectively. The yellow photoluminescence decays exhibited a 1 ns decay time at low laser excitations, whereas, at the highest ones, it increased up to 7 ns due to the saturation of the nonradiative defects, resembling the photoconductivity lifetime dependence. The fast photo-carrier decay time observed in ammonothermal GaN:Mn is of critical importance in high-frequency and high-voltage device applications. Full article
(This article belongs to the Special Issue Optical Properties of Crystalline Semiconductors and Nanomaterials)
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<p>(<b>a</b>) The PL spectra of SI Am-GaN:Mn with conductive epitaxial GaN epilayer. For comparison purposes, the absorption and photoconductivity spectra adapted from Ref. [<a href="#B8-materials-17-05995" class="html-bibr">8</a>] are also shown. Near-band emission (NBE) PL was excited by 330 nm, while defect PL was excited by 400 nm wavelength at 300 K. Note: 1—fast band tail-to-hole transitions; 2—band tail-to-Mg<sup>0</sup> transitions; 3—internal Mn-IB-to-VB transitions; 4—Mn-IB-to-CB transition; 5—VB-to-free Mn-IB-state transition; 8—Mn-IB-to-band tail transition; 6—Urbach tail (95 meV); 7—high purity GaN band-edge absorption. (<b>b</b>) Tentative optical transitions via impurity states of Mn and Mg atoms. Note: Mg—acceptor; YL—yellow luminescence; RL—red luminescence. (<b>c</b>) Scheme of the electron transitions in the SI-n junction.</p>
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<p>Fast BB (NBE1), e<sup>−</sup>Mg<sup>0</sup>(NBE2), YL, and RL TRPL decay at 300 K.</p>
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<p>Slow YL (<b>a</b>) and RL (<b>b</b>) decays at 300 K. Straight lines show exponential fits. Excitation intensities are the same as in <a href="#materials-17-05995-f004" class="html-fig">Figure 4</a>.</p>
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<p>YL excitation-dependent decay (<b>a</b>), and time-dependent PL spectra at 80 K (<b>b</b>), YL, and RL band intensity vs. excitation (<b>c</b>).</p>
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<p>YL decays at high excitation at different temperatures (<b>a</b>). Initial YL lifetime vs. T at high and low excitations (<b>b</b>); Straight lines in (<b>a</b>) show exponential fits, while in (<b>b</b>) provides activation fit for BTs, function τ = 1/(a + b × exp(−E<sub>a</sub>/kT)) was applied for fitting; a = 3.6 × 10<sup>7</sup> s<sup>−1</sup>, b = 4 × 10<sup>9</sup> s<sup>−1</sup>.</p>
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<p>PP decays vs. pump intensity at 527 nm and 1550 nm probes at 300 K (<b>a</b>); PP signal excitation dependence linearity (<b>b</b>).</p>
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<p>Temperature-dependent PP decays (<b>a</b>) and their initial decay time thermal activation (<b>b</b>). Straight lines in (<b>a</b>) show exponential fits, while in (<b>b</b>) function τ = 1/(a + b × exp(–E<sub>a</sub>/kT)) was applied for fitting; a = 7.5 × 10<sup>6</sup> s<sup>−1</sup>, b = 7 × 10<sup>8</sup> s<sup>−1</sup>, with Ea = 69 meV and 77 meV for the fast and the slow parts, respectively. Initial (red points) and slow (green points) decay parts provide almost the same activation energy.</p>
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<p>Photoconductive signal decays at different laser excitation pulse energies (corresponding to the carrier densities shown in <a href="#materials-17-05995-f009" class="html-fig">Figure 9</a>) at 16 V bias voltage at 300 K. The second decay peak at the 10 ns time mark corresponds to the decay excited by a parasitic (by a magnitude weaker) laser pulse arriving after the main pulse; solid lines are exponential fits providing PC lifetime in <a href="#materials-17-05995-f009" class="html-fig">Figure 9</a>.</p>
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<p>Decay time vs. excited carrier density by time-resolved pump–probe (PP), photoluminescence (PL), and photoconductivity (PC) [<a href="#B8-materials-17-05995" class="html-bibr">8</a>]. For RL and YL, different time windows are indicated where lifetime was determined in <a href="#materials-17-05995-f003" class="html-fig">Figure 3</a>.</p>
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34 pages, 7043 KiB  
Review
Biofuels and Their Blends—A Review of the Effect of Low Carbon Fuels on Engine Performance
by Qian Xiong, Yulong Duan, Dezhi Liang, Tie Li, Hongliang Luo and Run Chen
Sustainability 2024, 16(23), 10300; https://doi.org/10.3390/su162310300 - 25 Nov 2024
Viewed by 826
Abstract
Energy is an important aspect concerning global economic development and environmental conservation. Economic growth has been accompanied by extensive use of fossil fuels, resulting in significant emissions of greenhouse gases and other pollutants. Therefore, researchers have turned their attention to low/zero carbon fuels. [...] Read more.
Energy is an important aspect concerning global economic development and environmental conservation. Economic growth has been accompanied by extensive use of fossil fuels, resulting in significant emissions of greenhouse gases and other pollutants. Therefore, researchers have turned their attention to low/zero carbon fuels. Among these, biofuels have attracted wide attention due to their relatively low cost, clean combustion products and renewability. This article reviews the combustion, performance and emission characteristics of internal combustion (IC) engines fueled with biofuels categorized into three generations by their raw material sources. According to most research findings, biofuels generally exhibit poorer combustion performance in IC engines compared to fossil fuels due to their high viscosity and low lower heating value. However, these biofuels, characterized by a high oxygen content, facilitate more complete combustion and reduce emissions of CO, UHC and smoke, albeit increasing NOx emission and fuel consumption. Both thermal efficiency and brake power also tend to decrease, but various optimization strategies such as advanced combustion modes or injection control methods can partially compensate for these drawbacks. In conclusion, biofuels should be a promising low-carbon fuel for IC engines in the future. Full article
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<p>The Initial Strategy on Reduction of Greenhouse Gas (GHG) Emission from Ships introduced by the IMO.</p>
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<p>Costs and volumes for the total capacities of diesel fuel and alternative fuels for a bulk vessel.</p>
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<p>CP of microalgae biofuel with different proportions of CNG as additions [<a href="#B30-sustainability-16-10300" class="html-bibr">30</a>].</p>
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<p>HRR of traditional diesel fuel and sunflower biofuel at different EGR rates [<a href="#B32-sustainability-16-10300" class="html-bibr">32</a>].</p>
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<p>HRR of B20I, B20B and traditional diesel fuel [<a href="#B34-sustainability-16-10300" class="html-bibr">34</a>].</p>
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<p>The relationship between ID and temperature of different biofuels and traditional diesel fuel [<a href="#B36-sustainability-16-10300" class="html-bibr">36</a>].</p>
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<p>The relationship between ID and engine load of different biofuels and traditional diesel fuel [<a href="#B37-sustainability-16-10300" class="html-bibr">37</a>].</p>
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<p>The relationship between BTE and engine speed of mustard biofuel blends with different proportions [<a href="#B42-sustainability-16-10300" class="html-bibr">42</a>].</p>
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<p>The relationship between BTE and engine load of different biofuel blends with different proportions and traditional diesel fuel [<a href="#B47-sustainability-16-10300" class="html-bibr">47</a>].</p>
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<p>The relationship between BSFC and engine speed of cottonseed biofuel–ethanol blends with different proportions at 100% load [<a href="#B57-sustainability-16-10300" class="html-bibr">57</a>].</p>
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<p>The relationship between BSFC and engine load of algae oil biofuel mixtures with different proportions and traditional diesel fuel [<a href="#B63-sustainability-16-10300" class="html-bibr">63</a>].</p>
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<p>The relationship between BP, EGR rates and preheating temperatures of sunflower biofuel and traditional diesel fuel at 100% load [<a href="#B32-sustainability-16-10300" class="html-bibr">32</a>].</p>
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<p>The relationship between BP and engine speed of microalgae biofuel mixtures with different proportions and traditional diesel fuel [<a href="#B68-sustainability-16-10300" class="html-bibr">68</a>].</p>
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<p>The relationship between NO<sub>x</sub> emission and engine speed of soybean oil biofuel mixtures with different proportions and traditional diesel fuel [<a href="#B75-sustainability-16-10300" class="html-bibr">75</a>].</p>
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<p>The relationship between NO<sub>x</sub> emission and engine load of Chlorella protothecoides biofuel mixtures with different proportions and traditional diesel fuel [<a href="#B28-sustainability-16-10300" class="html-bibr">28</a>].</p>
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<p>Mode-wise percentage distribution of CO emissions for different fuels [<a href="#B95-sustainability-16-10300" class="html-bibr">95</a>].</p>
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<p>The relationship between CO emission and engine load of CSO mixtures with different proportions and traditional diesel fuel [<a href="#B99-sustainability-16-10300" class="html-bibr">99</a>].</p>
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<p>The relationship between CO<sub>2</sub> emission and engine load of Cymbopogon flexuosus biofuel mixtures with different proportions and traditional diesel fuel [<a href="#B102-sustainability-16-10300" class="html-bibr">102</a>].</p>
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<p>The relationship between CO<sub>2</sub> emission and engine load of SMB mixtures with different proportions [<a href="#B107-sustainability-16-10300" class="html-bibr">107</a>].</p>
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15 pages, 8416 KiB  
Article
Interference Measurements Across Vacuum and Atmospheric Environments for Characterization of Space-Borne Telescope
by Yi-Kai Huang and Cheng-Huan Chen
Photonics 2024, 11(12), 1105; https://doi.org/10.3390/photonics11121105 - 22 Nov 2024
Viewed by 541
Abstract
A space-borne telescope is used for Earth observation at about 500 km above sea level in the thermosphere where the air density is very low and the temperature increases significantly during daytime. If the telescopes are aligned and characterized on the ground with [...] Read more.
A space-borne telescope is used for Earth observation at about 500 km above sea level in the thermosphere where the air density is very low and the temperature increases significantly during daytime. If the telescopes are aligned and characterized on the ground with standard temperature and pressure (STP) conditions, different from that of the thermosphere, their performance could drift during their mission. Therefore, they are usually placed in a thermal vacuum chamber during ground testing in order to verify the system can perform well and withstand the harsh environment such as a high vacuum level and large temperature variations before being launched. Nevertheless, it remains a challenge to build up an in situ optical measurement system for a large aperture telescope in a thermal vacuum chamber due to the finite internal space of the chamber, limited aperture size of the vacuum view port and thermal dissipation problem of the measuring instruments. In this paper, a novel architecture of an interferometer whose light path travels across a vacuum chamber and an atmospheric environment has been proposed to resolve all of these technical issues. The major feature of the architecture is the diverger lens being located within the vacuum chamber, leaving the rest of the interferometer outside. The variation of the interference fringe due to the relocation of the diverger lens has been investigated with optical simulations and the solutions for compensation have also been proposed. Together with a specific alignment procedure for the proposed architecture, the interferogram has been successfully acquired from a prototype testbed. Full article
(This article belongs to the Special Issue Optical Systems for Astronomy)
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<p>Opto-mechanical design of the space-borne catadioptric telescope.</p>
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<p>Double pass interferometry setup across thermal vacuum chamber and STP environment.</p>
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<p>Feasibility test of separating the diverger lens from the interferometer. (<b>a</b>) Feasibility test for bias measurement, which includes the interferometer, vacuum view port, diverger lens and auto collimation flat mirror with cat’s eye architecture. (<b>b</b>) WFE result of bias measurement.</p>
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<p>Separation distance D versus the interferogram and WFE map.</p>
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<p>Double pass simulation model with the parametric separation distance D in ASAP.</p>
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<p>Fringe distribution of interferogram versus the separation distance D.</p>
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<p>Simulation model of object beam from telescope.</p>
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<p>Simulation result of object beam from telescope.</p>
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<p>Geometrical schematic of defocus versus propagated beam size.</p>
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<p>Diffraction effect of spider mechanism versus the separation distance.</p>
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<p>Simulation model for interferometric system with relay optics.</p>
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<p>Simulated fringe distribution of separation distance variation with the addition of a relay lens.</p>
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<p>Comparison of simulated fringe distribution. (<b>a</b>) Fringe of 150 cm separation distance case without relay optics. (<b>b</b>) Fringe of 150 cm separation distance case with relay optics. (<b>c</b>) Fringe of 7 cm separation distance case.</p>
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<p>Mechanical structure modification of the chamber door. (<b>a</b>) Original vacuum view port. (<b>b</b>) New vacuum view port.</p>
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<p>Improved measurement setup. (<b>a</b>) Measurement setup in thermal vacuum chamber. (<b>b</b>) Interferometer in STP environment.</p>
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<p>Improved measurement setup. (<b>a</b>) Measurement setup in thermal vacuum chamber. (<b>b</b>) Interferometer in STP environment.</p>
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<p>Alignment process of telescope and interferometer. (<b>a</b>) Alignment scheme of telescope and interferometer. (<b>b</b>) Interferogram with tilt and decenter. (<b>c</b>) Interferogram without tilt and decenter.</p>
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<p>Alignment process of telescope and interferometer. (<b>a</b>) Alignment scheme of telescope and interferometer. (<b>b</b>) Interferogram with tilt and decenter. (<b>c</b>) Interferogram without tilt and decenter.</p>
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<p>Alignment process of telescope and diverger lens. (<b>a</b>) Alignment of telescope and diverger lens with cat’s eye position. (<b>b</b>) Interferogram with defocus. (<b>c</b>) Interferogram without defocus.</p>
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<p>Interferogram and WFE map of the telescope under thermal vacuum circumstances.</p>
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<p>Focus term variation with time under high vacuum level circumstances.</p>
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<p>Focus term variation with temperature under thermal cycling conditions.</p>
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13 pages, 5641 KiB  
Article
Thermal Softening Measurements of Refractory High-Entropy Alloys
by Ottó K. Temesi, Albert Karacs, Nguyen Q. Chinh and Lajos K. Varga
Materials 2024, 17(23), 5718; https://doi.org/10.3390/ma17235718 - 22 Nov 2024
Viewed by 397
Abstract
Home-built equipment will be presented able to measure the thermal expansion (with a flat indenter) and indentation depth (with a pointed indenter) up to 1100 °C. In dilatometer mode, the allotropic phase transformations can be studied. For hardness, a Rockwell-type measurement is adopted. [...] Read more.
Home-built equipment will be presented able to measure the thermal expansion (with a flat indenter) and indentation depth (with a pointed indenter) up to 1100 °C. In dilatometer mode, the allotropic phase transformations can be studied. For hardness, a Rockwell-type measurement is adopted. First, we apply a small load and measure the displacement consisting of a dominant positive thermal expansion and a small negative indentation depth contribution. Then, we repeat the thermal cycle with such a high load that the compensation appears at around 250–300 °C. With increasing temperature, the indentation depth starts to dominate and we can notice a contraction. The indentation depth as a function of temperature, ID(T), will be obtained by subtracting the high load curve from the low load curve. A new rational fraction expression will be tested to describe the thermal softening of pure metals and refractory HEAs. Still, we are working on improving the equipment to extend the working temperature up to 1200 °C. Full article
(This article belongs to the Special Issue Future Trends in High-Entropy Alloys (2nd Edition))
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<p>Schematic drawing of the softening measurement. 1. The tube furnace that can be shifted; 2. the stressing load; 3. the fix point for indentation measurement; 4. the thermocouple; 5. the indenter; 6. the guide, moving united gliding on ball bearings; 7. the inductive displacement sensor; 8. rods and tubes made from quartz; 9. the sample; 10. (a) the sample temperature (ΔT), (b) the displacement of the indenter (Δl); 11. the Argon gas inlet; 12. the brittle rail structure.</p>
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<p>Operational form of the equipment. (<b>a</b>) Overall view of the equipment; (<b>b</b>) white—hot sample and indenter at around 1000 °C without Ar protection (furnace is shifted); (<b>c</b>) the W indenter tip preserving its form after several applications (1 div = 75 µm); (<b>d</b>) indent views after indentation with the 2.5 kg load.</p>
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<p>Linear thermal expansion of Titanium and phase transition at T<sub>tr</sub> = 888 °C.</p>
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<p>The linear expansion coefficient scales with the reciprocal of the melting temperature.</p>
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<p>(<b>a</b>) Titanium under 0.5 kg and 1.5 kg loads. The red hardness point (<span class="html-italic">T<sub>m</sub></span>/2) was found to be around the phase transition temperature. (<b>b</b>) The determination of Rockwell-type hardness (RH) is calculated as RH = 300 − ID using Equation (9).</p>
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<p>Softening measurement with a high heating rate (30 K/min) on pure iron. (<b>a</b>) Temperature dependence of displacement for different loads. (<b>b</b>) Rockwell-type hardness as a function of temperature.</p>
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<p>Rapid evaluation protocol for softening measurement on Fe. (<b>a</b>) Construction of a thermal expansion line (TEL) based on the initial part of the measured displacement curve (D). (<b>b</b>) Representing the indentation depth obtained as ID = TEL − D and the corresponding Rockwell-type hardness RH = 300 − ID.</p>
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<p>Thermal softening measurement of TiZrHfNb refractory HEA. (<b>a</b>) presents the original displacement measurement (D), the thermal expansion line (TEL) determined from the extrapolation of the initial part of the D versus T curve, and the indentation depth (ID) obtained by subtraction ID = TEL − D. (<b>b</b>) Rockwell-type hardness is determined by the subtraction RH = 200 − ID and the softening <span class="html-italic">Ts</span> temperature is determined only visually from the intersection of two tangent lines.</p>
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<p>Thermal softening measurement of TiZrHf refractory HEA. (<b>a</b>) The parameter ID is calculated following the protocol described above. (<b>b</b>) The hardness calculated from 150-ID shows beyond doubt the phase transformation around 800–900 °C, where the second softening starts. The first softening happens at a surprisingly low temperature, <span class="html-italic">Ts</span>1 = 450 °C.</p>
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<p>Thermal softening measurements of our refractory HEA samples (see data in <a href="#materials-17-05718-t001" class="html-table">Table 1</a>). (<b>a</b>) Measured displacement data. (<b>b</b>) Calculated RH data.</p>
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<p>The thermal softening temperature for pure metals is equal to half of the melting point.The fitted (blue) line almost coincides with the first angle bisector (black line).</p>
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15 pages, 14093 KiB  
Article
Integrating Multiple Hierarchical Parameters to Achieve the Self-Compensation of Scale Factor in a Micro-Electromechanical System Gyroscope
by Rui Zhou, Rang Cui, Daren An, Chong Shen, Yu Bai and Huiliang Cao
Micromachines 2024, 15(11), 1385; https://doi.org/10.3390/mi15111385 - 16 Nov 2024
Viewed by 1501
Abstract
The scale factor of thermal sensitivity serves as a crucial performance metric for micro-electromechanical system (MEMS) gyroscopes, and is commonly employed to assess the temperature stability of inertial sensors. To improve the temperature stability of the scale factor of MEMS gyroscopes, a self-compensation [...] Read more.
The scale factor of thermal sensitivity serves as a crucial performance metric for micro-electromechanical system (MEMS) gyroscopes, and is commonly employed to assess the temperature stability of inertial sensors. To improve the temperature stability of the scale factor of MEMS gyroscopes, a self-compensation method is proposed. This is achieved by integrating the primary and secondary relevant parameters of the scale factor using the partial least squares regression (PLSR) algorithm. In this paper, a scale factor prediction model is presented. The model indicates that the resonant frequency and demodulation phase angle are the primary correlation terms of the scale factor, while the drive control voltage and quadrature feedback voltage are the secondary correlation terms of the scale factor. By employing a weighted fusion of correlated terms through PLSR, the scale factor for temperature sensitivity is markedly enhanced by leveraging the predicted results to compensate for the output. The results indicate that the maximum error of the predicted scale factor is 0.124% within the temperature range of −40 °C to 60 °C, and the temperature sensitivity of the scale factor decreases from 6180 ppm/°C to 9.39 ppm/°C. Full article
(This article belongs to the Special Issue MEMS Sensors and Actuators: Design, Fabrication and Applications)
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<p>SVRG structure chip diagram.</p>
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<p>(<b>a</b>) Vibrational form of drive mode. (<b>b</b>) Vibrational form of sense mode. SVRG’s primary and secondary modal vibration forms.</p>
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<p>Electrode distribution of SVRG.</p>
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<p>Mechanical model of SVRG.</p>
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<p>Block diagram of gyroscope’s sense mode of operation.</p>
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<p>Heatmap of correlation analysis for each parameter.</p>
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<p>Scale factor prediction results.</p>
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<p>(<b>a</b>) Gyro chip package size. (<b>b</b>) Gyro physical structure. (<b>c</b>) Hardware circuit of gyro self-compensation system. Gyro self-compensation system composition.</p>
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<p>Block diagram of self-compensating system.</p>
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<p>Test experiment environment setup.</p>
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<p>Test results of each parameter across a wide temperature range.</p>
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<p>Comparison of scale factor temperature sensitivity results before and after SVRG compensation.</p>
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<p>Gyroscope zero-bias stability test results before and after compensation.</p>
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11 pages, 4564 KiB  
Article
Managing Residual Heat Effects in Femtosecond Laser Material Processing by Pulse-on-Demand Operation
by Jaka Petelin, Matevž Marš, Jaka Mur and Rok Petkovšek
J. Manuf. Mater. Process. 2024, 8(6), 254; https://doi.org/10.3390/jmmp8060254 - 12 Nov 2024
Viewed by 905
Abstract
Femtosecond laser processing combines highly accurate structuring with low residual heating of materials, low thermal damage, and nonlinear absorption processes, making it suitable for the machining of transparent brittle materials. However, with high average powers and laser pulse repetition rates, residual heating becomes [...] Read more.
Femtosecond laser processing combines highly accurate structuring with low residual heating of materials, low thermal damage, and nonlinear absorption processes, making it suitable for the machining of transparent brittle materials. However, with high average powers and laser pulse repetition rates, residual heating becomes relevant. Here, we present a study of the femtosecond laser pulse-on-demand operation regime, combined with regular scanners, aiming to improve throughput and quality of processing regardless of the scanner’s capabilities. We developed two methods to define the needed pulse-on-demand trigger sequences that compensate for the initial accelerating scanner movements. The effects of pulse-on-demand operation were studied in detail using direct process monitoring with a fast thermal camera and indirect process monitoring with optical and topographical surface imaging of final structures, both showing clear advantages of pulse-on-demand operation in precision, thermal effects, and structure shape control. The ability to compensate for irregular scanner movement is the basis for simplified, cheaper, and faster femtosecond laser processing of brittle and heat-susceptible materials. Full article
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<p>(<b>a</b>) Experimental setup schematic. (<b>b</b>) An example PoD sequence of pulses.</p>
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<p>(<b>a</b>) Chosen frames from a high-speed camera sequence and respective recognized crater positions. (<b>b</b>) Graph of reconstructed crater positions and the final PoD sequence for 4 m/s target scanner speeds and laser frequency 100 kHz. (<b>c</b>) Graph showing PoD sequence position deviation from target position. (<b>d</b>) Microscope picture of PoD sequence presented in (<b>b</b>). Both scalebars in (<b>a</b>,<b>d</b>) represent 200 µm.</p>
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<p>Crater distributions using (<b>a</b>) 20 kHz, (<b>b</b>) 30 kHz, and (<b>c</b>) 50 kHz repetition rates at 4 m/s target scanning speed. (<b>d</b>) PoD sequence craters at 100 kHz laser repetition rate and 4 m/s target scanner speed, as calculated from microscope-based method and applied for processing. (<b>e</b>) Graph of reconstructed positions from (<b>a</b>–<b>c</b>) and the fit for calculating PoD sequence. All scalebars in (<b>a</b>–<b>d</b>) represent 200 µm.</p>
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<p>Fast IR camera showing temperature evolution on steel with (<b>a</b>) regular processing and (<b>b</b>) PoD processing. (<b>c</b>) Comparison graph for the hotspot temperature (moving position) using regular fixed frequency processing (blue) vs. PoD (orange). All scalebars (line below timestamp) in (<b>a</b>,<b>b</b>) represent 200 µm.</p>
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<p>Fast IR camera showing temperature evolution on glass with (<b>a</b>) regular processing and (<b>b</b>) PoD processing. (<b>c</b>) Comparison graph for the hotspot temperature (moving position) using regular fixed frequency processing (blue) vs. PoD (orange). All scalebars (line below timestamp) in (<b>a</b>,<b>b</b>) represent 200 µm.</p>
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<p>Wide channels in glass processed using (<b>a</b>) regular processing and (<b>b</b>) PoD processing, both showing horizontal and vertical cross-section topography measurements.</p>
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<p>Wide channels in stainless steel processed using (<b>a</b>) regular processing and (<b>b</b>) PoD processing, both showing horizontal and vertical cross-section topography measurements.</p>
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29 pages, 61165 KiB  
Article
LiDAR-360 RGB Camera-360 Thermal Camera Targetless Calibration for Dynamic Situations
by Khanh Bao Tran, Alexander Carballo and Kazuya Takeda
Sensors 2024, 24(22), 7199; https://doi.org/10.3390/s24227199 - 10 Nov 2024
Viewed by 1024
Abstract
Integrating multiple types of sensors into autonomous systems, such as cars and robots, has become a widely adopted approach in modern technology. Among these sensors, RGB cameras, thermal cameras, and LiDAR are particularly valued for their ability to provide comprehensive environmental data. However, [...] Read more.
Integrating multiple types of sensors into autonomous systems, such as cars and robots, has become a widely adopted approach in modern technology. Among these sensors, RGB cameras, thermal cameras, and LiDAR are particularly valued for their ability to provide comprehensive environmental data. However, despite their advantages, current research primarily focuses on the one or combination of two sensors at a time. The full potential of utilizing all three sensors is often neglected. One key challenge is the ego-motion compensation of data in dynamic situations, which results from the rotational nature of the LiDAR sensor, and the blind spots of standard cameras due to their limited field of view. To resolve this problem, this paper proposes a novel method for the simultaneous registration of LiDAR, panoramic RGB cameras, and panoramic thermal cameras in dynamic environments without the need for calibration targets. Initially, essential features from RGB images, thermal data, and LiDAR point clouds are extracted through a novel method, designed to capture significant raw data characteristics. These extracted features then serve as a foundation for ego-motion compensation, optimizing the initial dataset. Subsequently, the raw features can be further refined to enhance calibration accuracy, achieving more precise alignment results. The results of the paper demonstrate the effectiveness of this approach in enhancing multiple sensor calibration compared to other ways. In the case of a high speed of around 9 m/s, some situations can improve the accuracy about 30 percent higher for LiDAR and Camera calibration. The proposed method has the potential to significantly improve the reliability and accuracy of autonomous systems in real-world scenarios, particularly under challenging environmental conditions. Full article
(This article belongs to the Section Radar Sensors)
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<p>Visualization of the system including RGB cameras, thermal cameras, and LiDAR. 360 RGB camera and 360 thermal camera are made from independent cameras to remove blind spots. Images and point clouds are compensated to decrease negative impacts of motion. Then, point clouds and images are used for sensor calibration based on extracted features.</p>
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<p>Visualization of the target detected by two types of cameras. The (<b>left image</b>) is the target detected by the RGB camera and the (<b>right image</b>) is the target detected by the thermal camera.</p>
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<p>Our system includes sensors: LiDAR Velodyne Alpha Prime, LadyBug-5 camera, 6 FLIR ADK cameras, LiDAR Ouster-128, LiDAR Ouster-64 and LiDAR Hesai Pandar.</p>
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<p>Visualization of stitching 360 thermal images and 360 RGB images.</p>
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<p>Pipeline of the registration process. The approach is divided into two parts, one part focuses on detecting key points from RGB images and thermal images, while the other part detects key points from images converted from LiDAR point clouds. For images generated from LiDAR point clouds, a velocity estimation step is required to perform distortion correction, ensuring the accurate positioning of the scanned points. After getting results from distortion correction, external parameters of LiDAR, 360 RGB camera and 360 thermal camera can be calibrated.</p>
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<p>Visualization of features extracted from RGB images.</p>
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<p>Pipeline of our approach. The first step is enhancing images by Retinex Decomposition. The second step is to extract key features from <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>+</mo> <mn>1</mn> </mrow> </semantics></math> consecutive images. The third step is using MobileNetV3 to remove noise features on moving objects.</p>
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<p>The (<b>above image</b>) shows results before being enhanced by Retinex Decomposition. The (<b>below image</b>) shows results after being enhanced by Retinex Decomposition.</p>
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<p>The (<b>above image</b>) including the red rectangles shows reliable features extracted from <math display="inline"><semantics> <mrow> <mi>n</mi> <mo>+</mo> <mn>1</mn> </mrow> </semantics></math> consecutive RGB images. The (<b>below image</b>) including the green rectangles shows reliable features after filtering by MobileNetV3.</p>
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<p>Visualization of features extracted from thermal images.</p>
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<p>Visualization of image projection. (<b>a</b>) shows the 3D point cloud data from the LiDAR. (<b>b</b>) presents the 2D image data with the intensity channel. (<b>c</b>) presents the 2D image data with the range channel. The height of the image is 128, corresponding to the number of channels in the LiDAR.</p>
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<p>Visualization of key points extracted from LiDAR images. (<b>a</b>) simulates key points across two frames, while (<b>b</b>) simulates selecting key points with similarity across the two frames.</p>
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<p>Pipeline of our approach. Key features of projected images are extracted by Superpoint enhanced by LSTM. These features are matched to find pair points in two consecutive frames.</p>
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<p>Pipeline of the ego-motion compensation process. First, the point clouds are converted into two-dimensional images using Spherical Projection. Key features are then identified within these range images, and corresponding point pairs are matched. By matching key feature pairs, the distance between frames can be determined, allowing for velocity estimation. Finally, velocity and timestamp will be used to resolve ego-motion compensation and point cloud accumulation.</p>
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<p>Visualization of distortion correction. The motion of the vehicle is presented by the circles, and the LiDAR is also sotating while the vehicle is in motion. (<b>a</b>) shows the actual shape of the obstacle. (<b>b</b>) depicts the shape of the obstacle scanned by LiDAR. (<b>c</b>) illustrates the shape of the obstacle after distortion correction.</p>
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<p>Visualization of the differences in distortion correction on 3D point clouds within a frame with a speed of 54 km/h and a frequency of 10 Hz. The red part shows the original points of the point clouds, while the green part shows the corrected points. The left image shows points on the <math display="inline"><semantics> <mrow> <mi>x</mi> <mi>y</mi> </mrow> </semantics></math>-plane. The right image shows points on the <math display="inline"><semantics> <mrow> <mi>y</mi> <mi>z</mi> </mrow> </semantics></math>-plane.</p>
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<p>Visualization of distortion correction of cameras. The blue rectangle is the actual shape, and the red rectangle is the shape distorted by ego-motion.</p>
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<p>Visualization of 360 RGB–LiDAR images calibration. The (<b>above image</b>) including the red rectangles indicate the calibration results before applying correction. The (<b>below image</b>) including the green rectangles indicates the calibration results after applying correction.</p>
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<p>Visualization of 360 RGB–thermal images calibration. The (<b>above image</b>) includes red rectangles that indicate the calibration results before applying correction. The (<b>below image</b>) includes green rectangles that indicate the calibration results after applying correction.</p>
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<p>Visualization of point clouds extracted from Ouster OS1-128 and Velodyne Alpha prime.</p>
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<p>Visualization of image projection. (<b>a</b>) presents the 2D image data with the intensity channel from Ouster OS1-128. (<b>b</b>) presents the 2D image data with the range channel from Ouster OS1-128. (<b>c</b>) presents the 2D image data with the intensity channel from Velodyne Alpha prime. (<b>d</b>) presents the 2D image data with the range channel from Velodyne Alpha prime.</p>
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<p>Visualization of velocity comparison between estimated velocity and ground truth over a continuous duration of 720 s. The intervals between approximately 100 to 200 s and 400 to 500 s corresponded to periods when the vehicle was turning. Conversely, the intervals from 0 to approximately 100 s, 200 to 400 s, and 500 to 600 s represented phases when the vehicle was moving straight. The vehicle decelerated and came to a halt between 600 and 720 s. The maximum observed velocity difference was 0.36 m/s, while the average velocity difference over the 720 s period was 0.03 m/s, as in <a href="#sensors-24-07199-t001" class="html-table">Table 1</a>.</p>
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<p>Comparison with CNN, RIFT, RI-MFM by MAE.</p>
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<p>Comparison with CNN, RIFT, RI-MFM by Accuracy.</p>
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<p>Comparison with CNN, RIFT, RI-MFM by RMSE.</p>
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<p>Red points represent the results of calibration without distortion correction, while blue points represent the results with distortion correction in static situations. The dashed line is the results from the target based method.</p>
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<p>Red points and blue points represent the results of calibration without and with distortion correction in dynamic situations. The dashed lines present the results using the actual data.</p>
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<p>Comparison of error in rotation and translation of three methods.</p>
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23 pages, 10593 KiB  
Article
Mechanical, Durability, and Microstructure Characterization of Pervious Concrete Incorporating Polypropylene Fibers and Fly Ash/Silica Fume
by Hassan Bilal, Xiaojian Gao, Liborio Cavaleri, Alamgir Khan and Miao Ren
J. Compos. Sci. 2024, 8(11), 456; https://doi.org/10.3390/jcs8110456 - 3 Nov 2024
Viewed by 1398
Abstract
Pervious concrete, because of its high porosity, is a suitable material for reducing the effects of water precipitations and is primarily utilized in road pavements. In this study, the effects of binder-to-aggregate (B/A) ratios, as well as mineral admixtures with and without polypropylene [...] Read more.
Pervious concrete, because of its high porosity, is a suitable material for reducing the effects of water precipitations and is primarily utilized in road pavements. In this study, the effects of binder-to-aggregate (B/A) ratios, as well as mineral admixtures with and without polypropylene fibers (PPFs) (0.2% by volume), including fly ash (FA) or silica fume (SF) (10% by substitution of cement), on the mechanical properties and durability of pervious concrete were experimentally observed. The experimental campaign included the following tests: permeability, porosity, compressive strength, splitting tensile strength, and flexural strength tests. The durability performance was evaluated by observing freeze–thaw cycles and abrasion resistance after 28 d curing. X-ray diffraction (XRD), Fourier transform infrared spectroscopy (FTIR), thermal analysis (TGA-DTA), and scanning electron microscopy (SEM) combined with energy dispersive spectroscopy (EDS) were employed to investigate the phase composition and microstructure. The results revealed that, for an assigned B/A ratio identified as optimal, the incorporation of mineral admixtures and fibers mutually compensated for their respective negative effects, resulting in the effective enhancement of both mechanical/microstructural characteristics and durability properties. In general, pervious concrete developed with fly ash or silica fume achieved higher compressive strength (>35 MPA) and permeability of 4 mm/s, whereas the binary combination of fly ash or silica fume with 0.2% PPFs yielded a flexural strength greater than 6 MPA and a permeability of 6 mm/s. Silica fume-based pervious concrete exhibited excellent performance in terms of freeze–thaw (F-T) cycling and abrasion resistance, followed by fiber-reinforced pervious concrete, except fly ash-based pervious concrete. Microstructural analysis showed that the inclusion of fly ash or silica fume reduced the harmful capillary pores and refined the pore enlargement caused by PPFs in the cement interface matrix through micro-filling and a pozzolanic reaction, leading to improved mechanical and durability characteristics of pervious concrete. Full article
(This article belongs to the Special Issue Polymer Composites and Fibers, 3rd Edition)
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<p>Raw materials (<b>a</b>), mixture consistency (<b>b</b>), compaction of fresh pervious concrete (<b>c</b>), specimens (<b>d</b>), and sand grading curve (<b>e</b>).</p>
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<p>Permeability test: (<b>a</b>) test set up; (<b>b</b>) NELD-PC370 tester; (<b>c</b>) specimens laterally wrapped.</p>
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<p>Specimens prior to (<b>a</b>) and during (<b>b</b>) freeze–thaw testing under saturated conditions.</p>
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<p>The effect of the binder/aggregate ratio (B/A) (<b>a</b>) on the compressive strength and (<b>b</b>) on the porosity and permeability coefficient.</p>
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<p>The skeleton pore structure of pervious concrete based on image analysis (white represents pores).</p>
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<p>The compressive behaviour of the different mixes: (<b>a</b>) strenght vs. curing days; (<b>b</b>) failure modes.</p>
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<p>The compressive behaviour of the different mixes: (<b>a</b>) strenght vs. curing days; (<b>b</b>) failure modes.</p>
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<p>Splitting tensile and flexural strength. Legend: PC1-FA (mix with fly ash), PC3-SF (mix with silica fume), PC2-FAP (mix with fly ash and polypropylene fibers), PC4-SFP (mix with silica fume and polypropylene fibers), PP5-PP-Rf (reference mix with only polypropylene fibers).</p>
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<p>Permeability (<b>a</b>) and Cantabro mass loss (<b>b</b>) after 28 d of curing.</p>
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<p>Freeze-thaw durability performance based on mass loss criteria.</p>
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<p>TGA-DTA profiles of control and binder cement pastes after 28 days.</p>
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<p>XRD spectrum (<b>a</b>) and FTIR spectra (<b>b</b>) of control and binder cement paste at 28 days of standard curing.</p>
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<p>The porosity (<b>a</b>) and pore size distribution (<b>b</b>) of control and blended cement pastes at 28 days of standard curing.</p>
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<p>SEM and EDS micrographs of porous concrete after 28 days of standard curing: PC1-FA and PC2-FAP.</p>
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<p>SEM and EDS micrographs of porous concrete after 28 days of standard curing: PC3-SF and PC4-SFP.</p>
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<p>SEM and EDS micrographs of porous concrete after 28 days of standard curing: PC3-SF and PC4-SFP.</p>
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<p>SEM and EDS micrographs of porous concrete after 28 days of standard curing: PC5-PP-Rf, PC2-FAP, and PC4SFP.</p>
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26 pages, 1397 KiB  
Article
Inertial Measurement Unit Self-Calibration by Quantization-Aware and Memory-Parsimonious Neural Networks
by Matteo Cardoni, Danilo Pietro Pau, Kiarash Rezaei and Camilla Mura
Electronics 2024, 13(21), 4278; https://doi.org/10.3390/electronics13214278 - 31 Oct 2024
Viewed by 2271
Abstract
This paper introduces a methodology to compensate inertial Micro-Electro-Mechanical System (IMU-MEMS) time-varying calibration loss, induced by stress and aging. The approach relies on a periodic assessment of the sensor through specific stimuli, producing outputs which are compared with the response of a high-precision [...] Read more.
This paper introduces a methodology to compensate inertial Micro-Electro-Mechanical System (IMU-MEMS) time-varying calibration loss, induced by stress and aging. The approach relies on a periodic assessment of the sensor through specific stimuli, producing outputs which are compared with the response of a high-precision sensor, used as ground truth. At any re-calibration iteration, differences with respect to the ground truth are approximated by quantization-aware trained tiny neural networks, allowing calibration-loss compensations. Due to the unavailability of aging IMU-MEMS datasets, a synthetic dataset has been produced, taking into account aging effects with both linear and nonlinear calibration loss. Also, field-collected data in conditions of thermal stress have been used. A model relying on Dense and 1D Convolution layers was devised and compensated for an average of 1.97 g and a variance of 1.07 g2, with only 903 represented with 16 bit parameters. The proposed model can be executed on an intelligent signal processing inertial sensor in 126.4 ms. This work represents a step forward toward in-sensor machine learning computing through integrating the computing capabilities into the sensor package that hosts the accelerometer and gyroscope sensing elements. Full article
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<p>Design schema of silicon comb-like structure, used for accelerometers and gyroscopes.</p>
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<p>Compensation block incorporating the tiny neural network. The subtraction block indicates the element-wise subtraction of the compensation error to the uncompensated output.</p>
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<p>Golden Reference and MEMS response data collection procedure. Element-wise subtraction of each couple of responses (from the MEMS and from the GR) is used to compute the compensation error for each response.</p>
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<p>Tiny neural network inference procedure, with MEMS uncompensated responses as input and compensation error as output.</p>
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<p>Re-calibration system architecture featuring periodic network updates. The compensation block is the one from <a href="#electronics-13-04278-f002" class="html-fig">Figure 2</a>. The subtraction operator indicates the element-wise subtraction of each response in output from the compensation block to the Golden Reference responses.</p>
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<p>Architectural diagram of the Neural Network training implemented inside a Microcontroller or a Microprocessor.</p>
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<p>Simulated MEMS model illustration.</p>
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<p>Example MEMS and GR model responses to impulse, square and sine training functions. The MEMS model for these measurements is the resulting model after 3 days of simulated time.</p>
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<p>One of the LSM6DSV IMU device under test acceleration readings on the X, Y, and Z axes, along with the measured temperature during a thermal cycle. Acceleration measurement error is visibly temperature dependent.</p>
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<p>The calibration and re-calibration process. Stimuli could be applied at the beginning of each period (of 1 day of duration) to perform calibration and/or re-calibration.</p>
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<p>MCP of the models as the number of re-calibration iterations changes, from <a href="#sec8dot2dot1-electronics-13-04278" class="html-sec">Section 8.2.1</a>. The error bars represent the maximum and minimum compensation percentage.</p>
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<p>MCP, separately for each model, as the number of re-calibration iterations changes, from <a href="#sec8dot2dot1-electronics-13-04278" class="html-sec">Section 8.2.1</a>. The error bars represent the maximum and minimum compensation percentages.</p>
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<p>An example of the MEMS, GR, and calibrated responses to the test sequence of 4 days and 5 s of <span class="html-italic">X</span>-axis data utilizing Quantized Conv1D-Dense as the (re-)calibration model.</p>
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27 pages, 2839 KiB  
Article
Cooperation and Profit Allocation Mechanism of Traditional and New Energy Complementary Power Generation: A Framework for Renewable Portfolio Standards
by Bo Shang
Sustainability 2024, 16(20), 8965; https://doi.org/10.3390/su16208965 - 16 Oct 2024
Viewed by 838
Abstract
To boost the sustainable development of energy and the environment, a new power system with clean energy sources has been proposed by the Chinese government and traditional coal-fired power units are being transformed into regulation service providers for this new energy power system. [...] Read more.
To boost the sustainable development of energy and the environment, a new power system with clean energy sources has been proposed by the Chinese government and traditional coal-fired power units are being transformed into regulation service providers for this new energy power system. Then, in this study, complementary power generation cooperation between traditional coal-fired power and new energy power producers is analyzed and discussed, and the energy quota agents, power sellers, are also included. Based on the cooperation game idea, different decision-making models of the tripartite power entities are elaborately constructed. Then, according to the price linkage mechanism between new energy and traditional thermal power, the profit of all power subjects is calculated and the profit allocation process is also analyzed. The conclusions show that the similarity of the two wholesale power price coefficients verifies the symmetry of the cooperative status of power producers. For BPC and SPC quota patterns, for example, BPC is bundled with new energy power and green certificates, whereas SPC is separate. Under the SPC pattern, there is a critical value for effective cooperation between the two power producers in the price range of traditional thermal power or new energy, which can achieve a win–win situation of increasing economic benefits and the consumption scale. Under the BPC pattern, the dynamic benefit compensation mechanism, which is the corrected Shapley value based on the RPS quota ratio, can solve the compressed profit of traditional coal-fired power producers. In contrast, the overall effect of profit allocation using the nucleolar method is not ideal. This study aims to give full play to the elastic induction effect of RPS to promote the sustainable transformation of traditional thermal power energy, especially combining the market mechanism to encourage traditional coal-fired power units to improve green technology to advance the construction of the green power market in China. Full article
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<p>The interest flow nexus between power producers and sellers based on RPS.</p>
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<p>New energy power generation under different decision-making cases.</p>
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<p>Thermal power generation under different decision-making cases.</p>
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<p>Thermal power price under different decision-making cases.</p>
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<p>Power retail price under different decision-making cases.</p>
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<p>Green certificates price under different decision-making cases.</p>
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<p>Initial profit of power entities under different decision-making cases.</p>
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<p>Initial profit of power entities under different decision-making cases.</p>
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