[go: up one dir, main page]

 
 

Topic Editors

Department of Industrial Engineering and Mathematical Sciences, Università Politecnica delle Marche, Via Brecce Bianche 12, 60131 Ancona, Italy
Prof. Dr. Archimede Forcellese
Dipartimento di Ingegneria Industriale e Scienze Matematiche (DIISM), Università Politecnica delle Marche, Italy

Advanced Carbon Fiber Reinforced Composite Materials, Volume II

Abstract submission deadline
1 May 2025
Manuscript submission deadline
31 July 2025
Viewed by
8858

Topic Information

Dear Colleagues,

This Topic, entitled “Advanced Carbon Fiber Reinforced Composite Materials, Volume II”, focuses on advanced composite materials such as carbon fiber-reinforced plastics (CFRP), which have gained the attention of different industries, such as aerospace, automotive and motorsports industries, which produce lightweight and high-performance components. Advanced composite materials, primarily governed by the properties of reinforcing fibers such as high strength and high stiffness characteristics, are characterized by their high potential in terms of stiffness/weight ratio, making them very attractive for structural applications in which low weight and high stiffness conditions have to be met. The present Topic aims to collect contributions on the advanced carbon-fiber-reinforced composite materials, as well as to review the state-of-the-art on these materials. The manuscripts of this Issue will focus on the most significant and promising manufacturing technologies, machining and joining processes, modeling, simulation, material characterization and failure mechanisms. A comprehensive overview of the most recent results and findings in the field of advanced composite materials will be provided.

Prof. Dr. Michela Simoncini
Prof. Dr. Archimede Forcellese
Topic Editors

Keywords

  • processing of short, long and continuous fiber composites
  • joining processes
  • machining processes
  • reinforced plastics
  • carbon fiber
  • modeling and simulation
  • material characterization
  • monitoring
  • structural composites
  • functional composites
  • lightweight structures
  • recyclable composites
  • sustainable composites
  • composite fabrication
  • 3D printing

Participating Journals

Journal Name Impact Factor CiteScore Launched Year First Decision (median) APC
Fibers
fibers
4.0 7.0 2013 33.6 Days CHF 2000 Submit
Journal of Composites Science
jcs
3.0 5.0 2017 18.5 Days CHF 1800 Submit
Materials
materials
3.1 5.8 2008 15.5 Days CHF 2600 Submit
Polymers
polymers
4.7 8.0 2009 14.5 Days CHF 2700 Submit

Preprints.org is a multidiscipline platform providing preprint service that is dedicated to sharing your research from the start and empowering your research journey.

MDPI Topics is cooperating with Preprints.org and has built a direct connection between MDPI journals and Preprints.org. Authors are encouraged to enjoy the benefits by posting a preprint at Preprints.org prior to publication:

  1. Immediately share your ideas ahead of publication and establish your research priority;
  2. Protect your idea from being stolen with this time-stamped preprint article;
  3. Enhance the exposure and impact of your research;
  4. Receive feedback from your peers in advance;
  5. Have it indexed in Web of Science (Preprint Citation Index), Google Scholar, Crossref, SHARE, PrePubMed, Scilit and Europe PMC.

Published Papers (7 papers)

Order results
Result details
Journals
Select all
Export citation of selected articles as:
20 pages, 5784 KiB  
Article
Prestressed CFRP Plates and Tendon Strengthening of Steel–Concrete Composite Beams
by Lamies Elgholmy, Hani Salim, Alaa Elsisi, Abdallah Salama, Hesham Shaaban and Ahmed Elbelbisi
J. Compos. Sci. 2024, 8(8), 301; https://doi.org/10.3390/jcs8080301 - 4 Aug 2024
Viewed by 736
Abstract
This study aims to enhance the ultimate capacity and stiffness of steel–concrete composite beams through external strengthening with prestressed carbon fiber-reinforced polymer (CFRP) plates and post-tensioned CFRP tendons. A 3D finite element model was developed using ANSYS and validated using experiments. The impact [...] Read more.
This study aims to enhance the ultimate capacity and stiffness of steel–concrete composite beams through external strengthening with prestressed carbon fiber-reinforced polymer (CFRP) plates and post-tensioned CFRP tendons. A 3D finite element model was developed using ANSYS and validated using experiments. The impact of various parameters on the capacity of the beam was investigated, including the level of post-tensioning in the CFRP tendons, tendon profile, degree of shear connection, and beam load level when adding strengthening CFRP tendons. Results indicate that reinforcing composite beams with bonded CFRP plates using post-tensioning tendons with trapezoidal and parabolic profiles can increase maximum load capacity by 37% and 60%, respectively, while maintaining high stiffness. This study also indicates that the optimal strengthening conditions for the composite beam are when the beam is loaded up to 70% of its capacity and has a composite action degree of 100%. Full article
Show Figures

Figure 1

Figure 1
<p>The FEM mesh for the composite cross-section.</p>
Full article ">Figure 2
<p>Modeling of material: (<b>a</b>) compression stress–strain curve for concrete and (<b>b</b>) model for steel material.</p>
Full article ">Figure 3
<p>Stress–strain behavior of steel and FRP materials.</p>
Full article ">Figure 4
<p>Geometrical properties of the simply supported CB tested by Chen et al.: (<b>a</b>) cross-section and (<b>b</b>) elevation of the beam (dimensions in mm).</p>
Full article ">Figure 5
<p>Mid-span moment–deflection curve comparison: Chen et al. [<a href="#B12-jcs-08-00301" class="html-bibr">12</a>] vs. FEM.</p>
Full article ">Figure 6
<p>The CB’s geometry tested by Emam [<a href="#B28-jcs-08-00301" class="html-bibr">28</a>] (all measurements in mm): (<b>a</b>) cross-section and (<b>b</b>) elevation of the beam.</p>
Full article ">Figure 7
<p>Mid-span moment–deflection curves: a comparison between Emam and FEM [<a href="#B28-jcs-08-00301" class="html-bibr">28</a>].</p>
Full article ">Figure 8
<p>Group (F) model geometries: (<b>a</b>) straight tendon, (<b>b</b>) trapezoidal tendon, and (<b>c</b>) parabola-shaped tendon.</p>
Full article ">Figure 9
<p>Typical loading steps.</p>
Full article ">Figure 10
<p>Midspan moment–deflection curves for group A: (<b>a</b>) the three load steps, and (<b>b</b>) the third load step.</p>
Full article ">Figure 11
<p>Midspan moment–deflection curves for group B: (<b>a</b>) the three load steps, and (<b>b</b>) the third load step.</p>
Full article ">Figure 12
<p>Midspan moment–deflection curves for group C: (<b>a</b>) the three load steps, and (<b>b</b>) the third load step.</p>
Full article ">Figure 13
<p>Midspan moment–deflection curves for group D: (<b>a</b>) the three load steps, and (<b>b</b>) the third load step.</p>
Full article ">Figure 14
<p>(<b>a</b>) Midspan moment–deflection curves for group E (three load steps), (<b>b</b>) the third load step, (<b>c</b>) moment–slippage curves for group E.</p>
Full article ">Figure 15
<p>Midspan moment–deflection curves for group F: (<b>a</b>) the three load steps, and (<b>b</b>) the third load step.</p>
Full article ">Figure 16
<p>Midspan moment–deflection curves for group G: (<b>a</b>) the three load steps, and (<b>b</b>) the third load step.</p>
Full article ">Figure 17
<p>Impact of DOSC: (<b>a</b>) moment–deflection curves at midspan, (<b>b</b>) relationship between moment and slippage, and (<b>c</b>) moment vs. stress in the bottom flange.</p>
Full article ">Figure 18
<p>Midspan Moment–Deflection curves for group I.</p>
Full article ">
16 pages, 5362 KiB  
Article
A Study on the Surface Oxidation Pretreatment and Nickel Plating Mechanism of Carbon Fiber
by Qinghui Wang, Xuesong Li and Dongdong Zhu
Materials 2024, 17(15), 3650; https://doi.org/10.3390/ma17153650 - 24 Jul 2024
Viewed by 658
Abstract
This study explores the effects of various temperatures on the surface modification of carbon fibers, as well as the effect of differing voltages and currents on the morphology, deposition rate, and thickness of the Ni plating layers. Post-treatment characterization of the samples was [...] Read more.
This study explores the effects of various temperatures on the surface modification of carbon fibers, as well as the effect of differing voltages and currents on the morphology, deposition rate, and thickness of the Ni plating layers. Post-treatment characterization of the samples was conducted utilizing scanning electron microscopy (SEM) and X-ray photoelectron spectroscopy (XPS) methods, thus facilitating a discussion on the mechanism of Ni plating. The findings demonstrate that at a temperature of 500 °C, the carbon fiber surface exhibits the highest concentration of functional groups, including hydroxyl (-OH), carboxyl (-COOH), and carbonyl (-C=O), resulting in the most efficacious modification. Specifically, exceeding 500 °C leads to significant carbon fiber mass loss, compromising the reinforcement effect. Under a stable voltage of 7.5 V, the Ni-plated layer on the carbon fibers appear smooth, fine, uniform, and complete. Conversely, at a voltage of 15 V, the instantaneous high voltage induces the continuous growth of Ni2+ ions along a singular deposition point, forming a spherical Ni-plated layer. In addition, a current of 0.6 A yields a comparatively uniform and dense carbon fiber coating. Nickel-plated layers on a carbon fiber surface with different morphologies have certain innovative significance for the structural design of composite reinforcements. Full article
Show Figures

Figure 1

Figure 1
<p>Morphology of carbon fibers under different temperature treatments: (<b>a</b>) 300 °C; (<b>b</b>) 400 °C; (<b>c</b>) 500 °C; (<b>d</b>) 600 °C.</p>
Full article ">Figure 2
<p>XPS of carbon fibers at different oxidation temperatures.</p>
Full article ">Figure 3
<p>Peak spectrum of C1s before and after oxidation treatment of carbon fibers at (<b>a</b>) 300 °C; (<b>b</b>) 400 °C; (<b>c</b>) 500 °C; (<b>d</b>) 600 °C.</p>
Full article ">Figure 4
<p>Peak spectrum of O1s before and after oxidation treatment of carbon fibers at (<b>a</b>) 300 °C; (<b>b</b>) 400 °C; (<b>c</b>) 500 °C; (<b>d</b>) 600 °C.</p>
Full article ">Figure 5
<p>Infrared absorption spectra of carbon fibers before and after oxidation treatment.</p>
Full article ">Figure 6
<p>Raman spectrum of carbon fiber after oxidation treatment.</p>
Full article ">Figure 7
<p>Chemical reactions during combustion process of carbon fibers.</p>
Full article ">Figure 8
<p>Morphology of Ni electroplating on carbon fiber surfaces at different voltages: (<b>a</b>) 5 V; (<b>b</b>) 7.5 V; (<b>c</b>) 10 V; (<b>d</b>) 12.5 V; (<b>e</b>) 15 V.</p>
Full article ">Figure 9
<p>Morphology of Ni electroplating on carbon fiber surfaces at different current intensities: (<b>a</b>) 0.2 A; (<b>b</b>) 0.4 A; (<b>c</b>) 0.6 A; (<b>d</b>) 0.8 A; (<b>e</b>) 1.0 A.</p>
Full article ">Figure 10
<p>Deposition rate and coating thickness of carbon fibers at different current intensities: (<b>a</b>) deposition rate; (<b>b</b>) coating thickness.</p>
Full article ">Figure 11
<p>XPS spectra of Ni electrodeposition on carbon fiber surfaces: (<b>a</b>) full spectrum of Ni electrodeposition; (<b>b</b>) C1s spectrum; (<b>c</b>) O1s spectrum; (<b>d</b>) Ni2p spectrum.</p>
Full article ">Figure 12
<p>Schematic of Ni deposition with different morphologies on carbon fiber surfaces. (<b>a</b>) low deposition voltage (<b>b</b>) High deposition voltage.</p>
Full article ">
16 pages, 683 KiB  
Article
Exploring Damage Patterns in CFRP Reinforcements: Insights from Simulation and Experimentation
by Youssef Bounjoum, Oumayma Hamlaoui, Mohamed Karim Hajji, Khalil Essaadaoui, Jalal Chafiq and Mohmmed Ait El Fqih
Polymers 2024, 16(14), 2057; https://doi.org/10.3390/polym16142057 - 18 Jul 2024
Viewed by 611
Abstract
Carbon Fiber Reinforced Polymers (CFRP) have become increasingly significant in real-world applications due to their superior strength-to-weight ratio, corrosion resistance, and high stiffness. These properties make CFRP an ideal material for reinforcing concrete structures, particularly in scenarios where weight reduction is crucial, such [...] Read more.
Carbon Fiber Reinforced Polymers (CFRP) have become increasingly significant in real-world applications due to their superior strength-to-weight ratio, corrosion resistance, and high stiffness. These properties make CFRP an ideal material for reinforcing concrete structures, particularly in scenarios where weight reduction is crucial, such as in bridges and high-rise buildings. The transformative potential of CFRP lies in its ability to enhance the durability and load-bearing capacity of concrete structures while minimizing maintenance costs and extending the lifespan of the infrastructure. This research explores the impact of reinforcing structural elements with advanced composite materials on the strength and durability of concrete and reinforced concrete structures. By integrating Carbon Fiber Reinforced Polymer (CFRP) reinforcements, we subjected both rectangular and T-section concrete beams to comprehensive three-point bending tests, revealing a substantial increase in flexural strength by 45% and crack resistance due to CFRP reinforcement. The study revealed that CFRP reinforcement increased the flexural strength of concrete beams by 45% and improved crack resistance significantly. Additionally, the load-bearing capacity of the beams was enhanced by 40% compared to unreinforced specimens. These improvements were validated through finite element simulations, which showed a close alignment with the experimental data. Furthermore, an innovative simulation study was conducted using a finely tuned finite element numerical model within the Abaqus calculation code. This model accurately replicated the laboratory specimens in terms of shape, dimensions, and loading conditions. The simulation results not only validated the experimental observations but also provided deeper insights into the stress distribution and failure mechanisms of the reinforced beams. Novel aspects of this study include the identification of specific failure patterns unique to CFRP-reinforced beams and the introduction of an enhanced interaction model that more accurately reflects the composite behavior under load. In CFRP-reinforced beams, specific failure patterns were identified, including flexural cracks in the tension zone and debonding of the CFRP sheets. These patterns indicate the points of maximum stress concentration and potential weaknesses in the reinforcement strategy. The study revealed that while CFRP significantly improves the overall strength and stiffness, careful attention must be given to the bonding process and the quality of the adhesive used to ensure optimal performance. These findings contribute significantly to the understanding of material interactions and structural performance, offering new pathways for the design and optimization of composite-reinforced concrete structures. This research underscores the transformative potential of composite materials in elevating the structural integrity and longevity of concrete infrastructures. Full article
Show Figures

Figure 1

Figure 1
<p>Detailed Flowchart of the Concrete Specimen Preparation Process.</p>
Full article ">Figure 2
<p>Geometric details of RC section T beams modelled.</p>
Full article ">Figure 3
<p>Bending test setup configuration.</p>
Full article ">Figure 4
<p>RC T section Beam reinforcement layout.</p>
Full article ">Figure 5
<p>Details of RC section tee beam (experimental test): (<b>a</b>) Elevation (<b>b</b>) Cross-section [<a href="#B1-polymers-16-02057" class="html-bibr">1</a>].</p>
Full article ">Figure 6
<p>Validation of results between the experimental model and the model developed by EF.</p>
Full article ">Figure 7
<p>Perfect connection (Embedded region) of rebars in the digital model.</p>
Full article ">Figure 8
<p>Load curves according to the deflection of the T-beams (T0-Ref and T-PRFC).</p>
Full article ">Figure 9
<p>Curves Tensile damage as a function of the magnitude of plastic deformations of T-beams (T0-Ref and T-PRFC).</p>
Full article ">
14 pages, 3886 KiB  
Article
The Study of Functional Glass Fiber Veils for Composites Protection: Flame Resistance and Mechanical Performance
by Chenkai Zhu, Zhiwei Qiao, Hongwei Wang and Changyong Huang
J. Compos. Sci. 2024, 8(7), 268; https://doi.org/10.3390/jcs8070268 - 11 Jul 2024
Viewed by 727
Abstract
The flame-retardant performance of carbon fiber-reinforced composites is crucial for ensuring structural stability. Traditional additive flame-retardant methods often struggle to balance structural integrity with fire resistance. Herein, Ni(OH)2 and 9,10-dihydro-9-oxa-10-phosphaphenanthrene-10-oxide (DOPO) were used as flame-retardant agents and mixed with glass fibers to [...] Read more.
The flame-retardant performance of carbon fiber-reinforced composites is crucial for ensuring structural stability. Traditional additive flame-retardant methods often struggle to balance structural integrity with fire resistance. Herein, Ni(OH)2 and 9,10-dihydro-9-oxa-10-phosphaphenanthrene-10-oxide (DOPO) were used as flame-retardant agents and mixed with glass fibers to construct the flame-retardant functional fiber veil which was used as the skin layer on the composite surface for fire protection. The structure performance and flame retardancy of composites were characterized via Fourier transform infrared spectroscopy (FTIR), scanning electron microscope (SEM), and a cone calorimeter test. The results confirmed that a flame-retardant glass fiber mat could effectively improve the flame-retardant and smoke-suppressive properties of the composite material. Due to the synergistic flame-retardant mechanism of Ni(OH)2 and DOPO, the C-N3-D2 composite with the highest LOI value of 32.3% has shown significant reduction in peak heat release rate (PHRR) and total smoke production (TSP) by 31.3% and 19.5%, respectively. In addition, due to flame-retardant agents only being employed in the skin layer of the composite, the core layer of a carbon fiber-reinforced structure could be protected without structure disruption. This approach maintained consistent interlayer shear strength, highlighting the effectiveness of using a flame-retardant fiber veil as a protective skin layer. This strategy could offer a viable solution for safeguarding high-performance composite materials from fire hazards without compromising their structural integrity. Full article
Show Figures

Figure 1

Figure 1
<p>Manufacturing process of flame-retardant GF veil and composites.</p>
Full article ">Figure 2
<p>The (<b>a</b>) epoxy resin contact angle and (<b>b</b>) FTIR analysis for retardant GF veils.</p>
Full article ">Figure 3
<p>The (<b>a</b>) thermogravimetric analysis and (<b>b</b>) limited oxygen index of composites with flame retardant GF veils.</p>
Full article ">Figure 4
<p>The cone calorimetry test of (<b>a</b>) heat release rate (HRR), (<b>b</b>) total heat release (THR) and (<b>c</b>) total smoke production (TSP) for flame-retardant composites.</p>
Full article ">Figure 5
<p>Morphology of composites after cone calorimetry test and SEM morphology of surface coke layer after combustion.</p>
Full article ">Figure 6
<p>The flame-retardant mechanism of composites in this study.</p>
Full article ">Figure 7
<p>The mechanical properties analysis of (<b>a</b>) flexural properties, (<b>b</b>) interlaminar shear strength and impact strength for flame retardant composites.</p>
Full article ">Figure 8
<p>Scanning electron microscope image of fracture surface for composites.</p>
Full article ">
26 pages, 5031 KiB  
Review
Mechanical Recycling of Carbon Fiber-Reinforced Polymer in a Circular Economy
by Salem M. Aldosari, Bandar M. AlOtaibi, Khalid S. Alblalaihid, Saad A. Aldoihi, Khaled A. AlOgab, Sami S. Alsaleh, Dham O. Alshamary, Thaar H. Alanazi, Sami D. Aldrees and Basheer A. Alshammari
Polymers 2024, 16(10), 1363; https://doi.org/10.3390/polym16101363 - 10 May 2024
Cited by 5 | Viewed by 2166
Abstract
This review thoroughly investigates the mechanical recycling of carbon fiber-reinforced polymer composites (CFRPCs), a critical area for sustainable material management. With CFRPC widely used in high-performance areas like aerospace, transportation, and energy, developing effective recycling methods is essential for tackling environmental and economic [...] Read more.
This review thoroughly investigates the mechanical recycling of carbon fiber-reinforced polymer composites (CFRPCs), a critical area for sustainable material management. With CFRPC widely used in high-performance areas like aerospace, transportation, and energy, developing effective recycling methods is essential for tackling environmental and economic issues. Mechanical recycling stands out for its low energy consumption and minimal environmental impact. This paper reviews current mechanical recycling techniques, highlighting their benefits in terms of energy efficiency and material recovery, but also points out their challenges, such as the degradation of mechanical properties due to fiber damage and difficulties in achieving strong interfacial adhesion in recycled composites. A novel part of this review is the use of finite element analysis (FEA) to predict the behavior of recycled CFRPCs, showing the potential of recycled fibers to preserve structural integrity and performance. This review also emphasizes the need for more research to develop standardized mechanical recycling protocols for CFRPCs that enhance material properties, optimize recycling processes, and assess environmental impacts thoroughly. By combining experimental and numerical studies, this review identifies knowledge gaps and suggests future research directions. It aims to advance the development of sustainable, efficient, and economically viable CFRPC recycling methods. The insights from this review could significantly benefit the circular economy by reducing waste and enabling the reuse of valuable carbon fibers in new composite materials. Full article
Show Figures

Figure 1

Figure 1
<p>Worldwide demand for CF and estimation of its wastes, adapted from [<a href="#B19-polymers-16-01363" class="html-bibr">19</a>].</p>
Full article ">Figure 2
<p>Circular economy model for polymeric composite materials, adapted from [<a href="#B25-polymers-16-01363" class="html-bibr">25</a>].</p>
Full article ">Figure 3
<p>CFRPC waste and dry CF scrap management routes, adapted from [<a href="#B28-polymers-16-01363" class="html-bibr">28</a>].</p>
Full article ">Figure 4
<p>Classification of the three major recycling methods, adapted from [<a href="#B37-polymers-16-01363" class="html-bibr">37</a>].</p>
Full article ">Figure 5
<p>A comparison between the main recycling techniques for CFRPCs, adapted from [<a href="#B30-polymers-16-01363" class="html-bibr">30</a>].</p>
Full article ">Figure 6
<p>Illustration of multiple shaft machine: (<b>a</b>) front and top views, (<b>b</b>) inside view, (<b>c</b>) CFRPCs before shredding, and (<b>d</b>) CFRPCs after shredding, adapted from [<a href="#B45-polymers-16-01363" class="html-bibr">45</a>].</p>
Full article ">Figure 7
<p>The stages of the recycling processes, modified from [<a href="#B47-polymers-16-01363" class="html-bibr">47</a>].</p>
Full article ">Figure 8
<p>Tensile strength of CFRPCs reinforced with virgin and recycled CFs, adapted from [<a href="#B20-polymers-16-01363" class="html-bibr">20</a>].</p>
Full article ">Figure 9
<p>Scheme of CFRPC structures: (<b>a</b>) unidirectional CF orientation, (<b>b</b>) bidirectional CF orientation (woven), and (<b>c</b>) multi-CF orientation laminate, quasi-isotropic laying-up sequence [0°/45°/90°/−45°]. Modified from [<a href="#B59-polymers-16-01363" class="html-bibr">59</a>].</p>
Full article ">Figure 10
<p>SEM images of the recycled CF: (<b>a</b>,<b>b</b>) poor interfacial adhesion of recycled CF-reinforced epoxy matrix; (<b>c</b>,<b>d</b>) poor interfacial adhesion between the polypropylene matrix and recycled CF, adapted from [<a href="#B37-polymers-16-01363" class="html-bibr">37</a>]; red arrows shows segregation the separation between the epoxy matrix and recycled CF.</p>
Full article ">Figure 11
<p>Global CFRPC demand in kilotons by year, adapted from [<a href="#B13-polymers-16-01363" class="html-bibr">13</a>].</p>
Full article ">
13 pages, 5111 KiB  
Article
Ag-MWCNT Composites for Improving the Electrical and Thermal Properties of Electronic Paste
by Yunkai Wang, Danlei Jing, Zikai Xiong, Yongqing Hu, Wei Li, Haotian Wu and Chuan Zuo
Polymers 2024, 16(8), 1173; https://doi.org/10.3390/polym16081173 - 22 Apr 2024
Viewed by 1312
Abstract
With the development of microelectronics products with high density and high power, it is urgent to improve the electrical and thermal conductivity of electronic paste to achieve the new requirements of packaging materials. In this work, a new synthesis method of Ag-MWCNTs was [...] Read more.
With the development of microelectronics products with high density and high power, it is urgent to improve the electrical and thermal conductivity of electronic paste to achieve the new requirements of packaging materials. In this work, a new synthesis method of Ag-MWCNTs was designed: Firstly, carboxylated MWCNTs and stannous chloride were used as raw materials to prepare high-loading-rate Sn-MWCNT composite material to ensure the high loading rate of metal on the MWCNT surface. Then, Ag-MWCNT composite material was prepared by the chemical displacement method to solve the problem of the low loading rate of silver nanoparticles on the MWCNT surface. On the basis of this innovation, we analyzed and compared the electrical, thermal, and mechanical properties of Ag-MWCNT composite electronic paste. Compared with the electronic paste without adding Ag-MWCNTs, the resistivity was reduced by 77%, the thermal conductivity was increased by 66%, and the shear strength was increased by 15%. Therefore, the addition of Ag-MWCNTs effectively improves the electrical, thermal, and mechanical properties of the paste, making it a promising and competitive choice for new packaging materials in the future. Full article
Show Figures

Figure 1

Figure 1
<p>Sn-MWCNTs prepared from different MWCNTs: (<b>a</b>) Sn-MWCNTs prepared from unfunctionalized MWCNTs; (<b>b</b>) Sn-MWCNTs prepared from hydroxylated MWCNTs; (<b>c</b>) Sn-MWCNTs prepared from carboxylated MWCNTs.</p>
Full article ">Figure 2
<p>Sn-MWCNTs prepared with different dispersants. (<b>a</b>) The application of dispersants was not employed. (<b>b</b>) The dispersant used is SDBS. (<b>c</b>) The dispersant used is SDS.</p>
Full article ">Figure 3
<p>The influence of stannous chloride dosage on the morphology of Ag-MWCNTs. (<b>a</b>) The addition amount of stannous chloride is 0.2 g. (<b>b</b>) The addition amount of stannous chloride is 0.5 g. (<b>c</b>) The addition amount of stannous chloride is 1.0 g. (<b>d</b>) The addition amount of stannous chloride is 1.5 g.</p>
Full article ">Figure 4
<p>Metal content on the surface of carbon nanotubes.</p>
Full article ">Figure 5
<p>The XRD curves of (<b>a</b>) carboxylated MWCNTs, (<b>b</b>) Sn-MWCNTs, and (<b>c</b>) Ag-MWCNTs.</p>
Full article ">Figure 6
<p>TG curves of (<b>a</b>) carboxylated MWCNT, (<b>b</b>) Sn-MWCNT, and Ag-MWCNT composites.</p>
Full article ">Figure 7
<p>DSC curve of Ag-MWCNTs.</p>
Full article ">Figure 8
<p>Results of thermogravimetric analysis for the modified pastes obtained.</p>
Full article ">Figure 9
<p>Resistivity of three kinds of pastes.</p>
Full article ">Figure 10
<p>Effects of paste resistance through the addition of Ag-MWCNTs.</p>
Full article ">Figure 11
<p>Thermal conductivity of three kinds of paste.</p>
Full article ">Figure 12
<p>Shear strength of two types of pastes.</p>
Full article ">
19 pages, 25086 KiB  
Article
Biomechanical Fatigue Behavior of a Dental Implant Due to Chewing Forces: A Finite Element Analysis
by Miguel Martinez-Mondragon, Guillermo Urriolagoitia-Sosa, Beatriz Romero-Ángeles, Miguel Angel García-Laguna, Aldo Saul Laguna-Canales, Juan Carlos Pérez-Partida, Jonatan Mireles-Hernández, Francisco Carrasco-Hernández and Guillermo Manuel Urriolagoitia-Calderón
Materials 2024, 17(7), 1669; https://doi.org/10.3390/ma17071669 - 5 Apr 2024
Cited by 2 | Viewed by 1757
Abstract
The use of titanium as a biomaterial for the treatment of dental implants has been successful and has become the most viable and common option. However, in the last three decades, new alternatives have emerged, such as polymers that could replace metallic materials. [...] Read more.
The use of titanium as a biomaterial for the treatment of dental implants has been successful and has become the most viable and common option. However, in the last three decades, new alternatives have emerged, such as polymers that could replace metallic materials. The aim of this research work is to demonstrate the structural effects caused by the fatigue phenomenon and the comparison with polymeric materials that may be biomechanically viable by reducing the stress shielding effect at the bone–implant interface. A numerical simulation was performed using the finite element method. Variables such as Young’s modulus, Poisson’s coefficient, density, yield strength, ultimate strength, and the S-N curve were included. Prior to the simulation, a representative digital model of both a dental implant and the bone was developed. A maximum load of 550 N was applied, and the analysis was considered linear, homogeneous, and isotropic. The results obtained allowed us to observe the mechanical behavior of the dental implant by means of displacements and von Mises forces. They also show the critical areas where the implant tends to fail due to fatigue. Finally, this type of non-destructive analysis proves to be versatile, avoids experimentation on people and/or animals, and reduces costs, and the iteration is unlimited in evaluating various structural parameters (geometry, materials, properties, etc.). Full article
Show Figures

Figure 1

Figure 1
<p>Dental implant dimensions.</p>
Full article ">Figure 2
<p>(<b>a</b>) Conical implant. (<b>b</b>) Abutments including Snappy, Universal, and Esthetic.</p>
Full article ">Figure 3
<p>Boundary conditions and external load.</p>
Full article ">Figure 4
<p>Discretizing the complete model.</p>
Full article ">Figure 5
<p>Total general displacement for the Snappy abutment type (Ti<sub>6</sub>Al<sub>4</sub>V).</p>
Full article ">Figure 6
<p>Total general displacement for the Snappy abutment type (CFR-PEEK).</p>
Full article ">Figure 7
<p>Total unit deformation for the Snappy abutment: (<b>a</b>) titanium and (<b>b</b>) CFR-PEEK.</p>
Full article ">Figure 8
<p>von Mises stress for the Snappy abutment type (Ti<sub>6</sub>Al<sub>4</sub>V).</p>
Full article ">Figure 9
<p>von Mises stress for the Snappy abutment type (CFR-PEEK).</p>
Full article ">Figure 10
<p>S-N curve of fatigue behavior of titanium and CFR-PEEK.</p>
Full article ">Figure 11
<p>Life cycles and fatigue alternating stress for the Snappy abutment (Ti<sub>6</sub>Al<sub>4</sub>V).</p>
Full article ">Figure 12
<p>Life cycles and fatigue alternating stress for the Snappy abutment (CFR-PEEK).</p>
Full article ">Figure 13
<p>Graph σ<sub>a</sub> vs. σ<sub>m</sub> of fatigue behavior by Goodman’s theory for a lifetime of 1 × 10<sup>6</sup> cycles of titanium (Ti<sub>6</sub>Al<sub>4</sub>V).</p>
Full article ">Figure 14
<p>Graph σ<sub>a</sub> vs. σ<sub>m</sub> of fatigue behavior by Goodman’s theory for a life of 1 × 10<sup>6</sup> cycles of polyether–ether–ketone (CFR-PEEK).</p>
Full article ">Figure A1
<p>Total general displacement for the Universal abutment type (Ti<sub>6</sub>Al<sub>4</sub>V).</p>
Full article ">Figure A2
<p>Total general displacement for the Esthetic abutment type (Ti<sub>6</sub>Al<sub>4</sub>V).</p>
Full article ">Figure A3
<p>Total general displacement for the Universal abutment type (CFR-PEEK).</p>
Full article ">Figure A4
<p>Total general displacement for the Esthetic abutment type (CFR-PEEK).</p>
Full article ">Figure A5
<p>Total unit deformation for the Universal abutment: (<b>a</b>) titanium and (<b>b</b>) CFR-PEEK.</p>
Full article ">Figure A6
<p>Total unit deformation for the Esthetic abutment: (<b>a</b>) titanium and (<b>b</b>) CFR-PEEK.</p>
Full article ">Figure A7
<p>von Mises stress for the Universal abutment type (Ti<sub>6</sub>Al<sub>4</sub>V).</p>
Full article ">Figure A8
<p>von Mises stress for the Esthetic abutment type (Ti<sub>6</sub>Al<sub>4</sub>V).</p>
Full article ">Figure A9
<p>von Mises stress for the Universal abutment type (CFR-PEEK).</p>
Full article ">Figure A10
<p>von Mises stress for the Esthetic abutment type (CFR-PEEK).</p>
Full article ">Figure A11
<p>Life cycles and fatigue alternating stress for the Universal abutment type (Ti<sub>6</sub>Al<sub>4</sub>V).</p>
Full article ">Figure A12
<p>Life cycles and fatigue alternating stress for the Esthetic abutment type (Ti<sub>6</sub>Al<sub>4</sub>V).</p>
Full article ">Figure A13
<p>Life cycles and fatigue alternating stress for the Universal abutment type (CFR-PEEK).</p>
Full article ">Figure A14
<p>Life cycles and fatigue alternating stress for the Esthetic abutment type (CFR-PEEK).</p>
Full article ">
Back to TopTop