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Hollow core-shell structured Fe3O4@Polypyrrole composites for enhanced electromagnetic wave absorption 用于增强电磁波吸收的空心核壳结构 Fe3O4@Polypyrrole 复合材料
IF 8.3 1区 材料科学 Q1 MATERIALS SCIENCE, COMPOSITES Pub Date : 2024-10-16 DOI: 10.1016/j.compscitech.2024.110917
Jiang Guo , Yukun Sun , Xu Li , Shaohua Xi , Mohamed M. Ibrahim , Hua Qiu , Gaber A.M. Mersal , Zeinhom M. El-Bahy , Vignesh Murugadoss , Waras Abdul , Fujian Zhou , Juanna Ren , Zhanhu Guo , Jianfeng Zhu
Due to the rapid development of electronic devices, the electromagnetic pollution has become increasingly serious. Developing electromagnetic wave absorption (EWA) materials with lightweight, strong absorption capacity and wide effective absorption bandwidth (EAB) becomes a research hotspot. In this work, the hollow-Fe3O4@polypyrrole (HFO@PPy) composites with core-shell structure were successfully synthesized by in situ polymerization method. The electromagnetic parameters could be adjusted by controlling the content of HFO in HFO@PPy. In addition, HFO@PPy composites show both dielectric and magnetic losses. The synergistic effect of both two losses contributes to an enhanced electromagnetic attenuation. The enhanced impedance matching is achieved by the composition (HFO and PPy) and designed unique structure (core-shell and hollow structure). The maximum reflection loss (RL) and EAB are −52.01 dB and 2.72 GHz at 3.1 mm for 60.0 wt% HFO@PPy composites. Therefore, by reasonably regulating the component content and optimizing the structural design, the EWA performance of HFO@PPy composites could be effectively improved, providing a significant inspiration for fabrication of microwave absorbers.
随着电子设备的快速发展,电磁污染日益严重。开发重量轻、吸收能力强、有效吸收带宽宽的电磁波吸收(EWA)材料成为研究热点。本研究采用原位聚合法成功合成了具有核壳结构的空心Fe3O4@聚吡咯(HFO@PPY)复合材料。通过控制 HFO@PPy 中 HFO 的含量可以调节电磁参数。此外,HFO@PPy 复合材料同时具有介电损耗和磁损耗。这两种损耗的协同效应增强了电磁衰减。增强的阻抗匹配是通过成分(HFO 和 PPy)和设计的独特结构(核壳和空心结构)实现的。60.0 wt% HFO@PPy 复合材料在 3.1 mm 时的最大反射损耗 (RL) 和 EAB 分别为 -52.01 dB 和 2.72 GHz。因此,通过合理调节成分含量和优化结构设计,可有效提高 HFO@PPy 复合材料的 EWA 性能,为微波吸收器的制造提供了重要启示。
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引用次数: 0
Multifunctional superhydrophobic composite film with icing monitoring and anti-icing/deicing performance 具有结冰监测和防冰/除冰性能的多功能超疏水复合薄膜
IF 8.3 1区 材料科学 Q1 MATERIALS SCIENCE, COMPOSITES Pub Date : 2024-10-15 DOI: 10.1016/j.compscitech.2024.110916
Chao Yang , Haozhong Ji , Longhai Song , Haoxi Su , Zhengpan Qi , Yao Wang , E. Cheng , Libin Zhao , Ning Hu
Icing can cause damage to outdoor equipment such as airplanes, wind turbine blades and power lines, which poses potential safety hazards. Recently, electrothermal superhydrophobic composite film with the synergistic effect of anti-icing and deicing properties can effectively hinder the formation and accumulation of ice. However, these superhydrophobic composite films have no icing condition monitoring property, which is critical to improve deicing efficiency and reduce energy consumption. In this paper, we have designed a multifunctional superhydrophobic composite film using the combination of laser ablation and spraying method, which exhibits excellent comprehensive anti-icing, deicing and icing monitoring properties. The experimental results demonstrated the icing delay time of the film reached 4.0 min at −20 °C. Meanwhile, taking advantage of the outstanding electrothermal effects of the laser induced graphene/carbon nanotubes (LIG/CNTs) composite conductive network, with DC voltage (5 V) excitation, the film temperature rapidly rose from −20 °C to 107 °C in 90 s, thereby effectively removing the ice. More importantly, due to the temperature sensing performance of the LIG/CNTs composite conductive network, it could monitor whole icing and deicing process of droplet with different volumes and temperatures in real time through the change of film resistance. Therefore, the comprehensive anti-icing, deicing and ice monitoring properties allowed it to effectively reduce icing hazards.
结冰会对飞机、风力涡轮机叶片和电线等户外设备造成损坏,从而带来潜在的安全隐患。最近,具有防冰和除冰协同效应的电热超疏水复合膜能有效阻止冰的形成和积聚。然而,这些超疏水复合薄膜没有结冰状态监测性能,而这对于提高除冰效率和降低能耗至关重要。本文采用激光烧蚀和喷涂相结合的方法设计了一种多功能超疏水复合薄膜,该薄膜具有优异的防冰、除冰和结冰监测综合性能。实验结果表明,该薄膜在-20 °C时的结冰延迟时间达到4.0 min。同时,利用激光诱导石墨烯/碳纳米管(LIG/CNTs)复合导电网络的卓越电热效应,在直流电压(5 V)激励下,薄膜温度在 90 秒内从 -20 °C 迅速升至 107 °C,从而有效地清除了冰层。更重要的是,由于 LIG/CNTs 复合导电网络的温度传感性能,它可以通过薄膜电阻的变化实时监测不同体积和温度液滴的整个结冰和除冰过程。因此,其全面的防冰、除冰和冰监测性能可有效降低结冰危害。
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引用次数: 0
Effect of crossing warp arrangements on delamination resistance of 3D woven composite T-joints under in-plane tensile loading 平面拉伸载荷下交叉经纱排列对三维编织复合材料 T 型接头抗分层能力的影响
IF 8.3 1区 材料科学 Q1 MATERIALS SCIENCE, COMPOSITES Pub Date : 2024-10-12 DOI: 10.1016/j.compscitech.2024.110907
Ziyue Wei , Xiaogang Chen , Constantinos Soutis
An experimental study for investigating the delamination behaviour of 3D woven composite T-joints with weave variations and optimising weave architectures is carried out. This study involves 10 types of crossing warp architectures at the junction. Quasi-static tensile load is applied to two flanges of 3D woven composite T-joints to evaluate the in-plane mechanical performance. The crossing warp architecture effectively improves the in-plane mechanical performance. Results indicate a significant influence of crossing warp arrangements on failure modes of the 3D woven composite T-joints. The use of internal crossing warp architectures leads to severe delamination in the 3D woven composite T-joints while the composite T-joints with 3D woven external crossing warps primarily fail due to the debonding of fibres and matrix and fibre breakage. The optimal weave architecture for 3D woven composite T-joints is confirmed by analysing the in-plane mechanical behaviour with different crossing warp arrangements and proportions. Regardless of the crossing warp proportions, the external crossing warp architectures outperformed their internal counterparts in resisting delamination, resulting in a maximum increase of 68.75 %, 30.04 % and 116.81 % in modulus, strength and failure strain respectively.
为研究具有编织变化的三维编织复合材料 T 型接头的分层行为并优化编织结构,我们开展了一项实验研究。这项研究涉及 10 种交接处的交叉经纱结构。对三维编织复合材料 T 型接头的两个翼缘施加准静态拉伸载荷,以评估平面内的机械性能。交叉经纱结构有效地改善了平面力学性能。结果表明,交叉经纱排列对三维编织复合材料 T 型接头的失效模式有重大影响。使用内部交叉经纱结构会导致三维编织复合材料 T 形接头出现严重分层,而使用三维编织外部交叉经纱的复合材料 T 形接头则主要由于纤维与基体脱粘和纤维断裂而失效。通过分析不同交叉经纱排列和比例下的面内机械性能,确认了三维编织复合材料 T 形接头的最佳编织结构。无论交叉经纱比例如何,外部交叉经纱结构在抗分层方面都优于内部交叉经纱结构,其模量、强度和破坏应变的最大增幅分别为 68.75%、30.04% 和 116.81%。
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引用次数: 0
Influence of process parameters on the interlaminar shear strength of CF/PEEK composites in-situ consolidated by laser-assisted automated fiber placement 工艺参数对激光辅助自动纤维铺放原位固结 CF/PEEK 复合材料层间剪切强度的影响
IF 8.3 1区 材料科学 Q1 MATERIALS SCIENCE, COMPOSITES Pub Date : 2024-10-11 DOI: 10.1016/j.compscitech.2024.110902
Ningguo Dong , Congcong Luan , Xinhua Yao , Zequan Ding , Yuyang Ji , Chengcheng Niu , Yaping Zheng , Yuetong Xu , Jianzhong Fu
The influence of process parameters, including placement speed, laser power, tooling temperature, compaction force and tape tension, on the interlaminar shear strength of CF/PEEK components in-situ consolidated by laser-assisted automated fiber placement was systematically investigated. To examine both the individual and interactive effects of these parameters, two sets of orthogonal experiments were formulated and conducted, yielding a maximum ILSS of 70.3 MPa. Analysis of variance revealed that the interaction between laser power and placement speed had the most significant effect, followed by tooling temperature, compaction force and tape tension. Furthermore, the concept of linear energy density of consolidated segments (LEDCS) was introduced to characterize and quantify the relationship between laser power and placement speed. ILSS values exceeding 50 MPa were predicted within the LEDCS range of 1.58 J/mm to 3.75 J/mm. Finally, the failure modes of the samples were elucidated through scanning electron microscopy.
系统地研究了贴装速度、激光功率、工具温度、压实力和胶带张力等工艺参数对激光辅助自动纤维贴装原位加固 CF/PEEK 组件层间剪切强度的影响。为了研究这些参数的单独效应和交互效应,制定并进行了两组正交实验,得出的最大 ILSS 为 70.3 兆帕。方差分析显示,激光功率和贴片速度之间的交互影响最为显著,其次是工具温度、压实力和胶带张力。此外,还引入了加固段线性能量密度(LEDCS)的概念,以表征和量化激光功率与贴片速度之间的关系。预计在 1.58 J/mm 至 3.75 J/mm 的 LEDCS 范围内,ILSS 值将超过 50 MPa。最后,通过扫描电子显微镜阐明了样品的失效模式。
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引用次数: 0
A novel method for through-thickness reinforcement of laminated composites using discrete micro-polarization-induced fiber injection (DMFI) approach 利用离散微极化诱导纤维注射(DMFI)方法对层状复合材料进行厚度加固的新方法
IF 8.3 1区 材料科学 Q1 MATERIALS SCIENCE, COMPOSITES Pub Date : 2024-10-11 DOI: 10.1016/j.compscitech.2024.110912
Yihan Fu , Shuran Li , Mengze Li , Liang Cheng , Weidong Zhu , Yinglin Ke
Conventional through-thickness reinforcement methods for laminated composites, such as Z-pin, encounter issues with in-plane property degradation and complex fabrication processes. To achieve rapid and low-damage reinforcement, a novel approach using short-chopped carbon fibers (SCFs) to form a micron-diameter interlaminate structure has been proposed. This method employs a discrete micro-polarization-induced fiber injection (DMFI) technique, where polarized SCFs are electrostatically oriented and injected at high speeds into pre-formed holes in the laminates. The insertion process of SCFs was thoroughly investigated, with optimal interlaminate conditions determined using high-speed cameras and other equipment. The toughening mechanism of SCFs was explored through various characterization methods, including metallurgical microscopy. This innovative method offers several advantages over the traditional Z-pin reinforced method. Notably, present method eliminates the need for prefabrication of Z-pins and fully leverages the excellent mechanical properties of individual carbon fiber in short length. It provides superior interlaminar mechanical properties, achieving a 392 % improvement compared to the control group and a 15 % improvement compared to 0.1 mm Z-pin reinforcement at the same insertion volume fraction. Additionally, it has minimal impact on the in-plane properties of the laminates, with only a 3.6 % reduction in tensile strength and a 4.1 % reduction in compression strength. Furthermore, it is environmentally friendly, allowing for the recycling and reuse of waste SCFs.
层压复合材料的传统通厚加固方法(如 Z 形销)存在面内性能下降和制造工艺复杂的问题。为了实现快速、低损伤的加固,有人提出了一种使用短切碳纤维(SCF)形成微米直径层间结构的新方法。这种方法采用了离散微极化诱导纤维注射(DMFI)技术,将极化的 SCF 进行静电定向并高速注射到层压板上预先形成的孔中。对 SCFs 的插入过程进行了深入研究,并使用高速摄像机和其他设备确定了最佳层间条件。通过包括金相显微镜在内的各种表征方法,探索了 SCF 的增韧机制。与传统的 Z 形销加固法相比,这种创新方法具有多项优势。值得注意的是,这种方法无需预制 Z 形钉,并能充分利用短碳纤维的优异机械性能。在相同的插入体积分数下,与对照组相比,层间机械性能提高了 392%,与 0.1 毫米 Z 形钉加固法相比,提高了 15%。此外,它对层压板面内性能的影响极小,拉伸强度仅降低 3.6%,压缩强度降低 4.1%。此外,它还非常环保,可以对废弃的 SCF 进行回收和再利用。
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引用次数: 0
Decreasing propagation rate of interfacial debonding between a single carbon fiber and epoxy matrix under cyclic loading 循环加载下单根碳纤维与环氧树脂基体之间界面脱粘的传播速度降低
IF 8.3 1区 材料科学 Q1 MATERIALS SCIENCE, COMPOSITES Pub Date : 2024-10-11 DOI: 10.1016/j.compscitech.2024.110900
Kosuke Takahashi , Takuma Matsuo , Wataru Sato , Takashi Nakamura
The interfacial debonding of a single carbon fiber transversely embedded in a dumbbell-shaped epoxy sample was generated under cyclic loading, and images were captured using synchrotron radiation X-ray computed tomography. A fatigue testing machine driven by a piezoelectric actuator placed along the beamline for in situ observation was developed for precise alignment. Interfacial debonding was initially observed under a static tensile load and was confirmed to be almost of the same length at both ends of the carbon fiber, implying negligible bending deformation due to inclination. Cyclic loads were then applied to the sample to capture the progressive debonding. The propagation rate of the interfacial debonding decreased as the number of cycles increased. Another sample with a single carbon fiber aligned parallel to the loading direction was prepared following a single-fiber fragmentation test. Interfacial debonding was clearly observed around the fiber breakage. Cyclic loads were also applied to this sample; however, no progression of the interfacial debonding was evident. Degradation of the interfacial strength between the carbon fiber and epoxy matrix was not confirmed under cyclic loading within the elastic deformation range.
在循环载荷作用下,单根碳纤维横向嵌入哑铃形环氧树脂样品中,产生了界面脱粘现象,并利用同步辐射 X 射线计算机断层扫描捕捉到了图像。开发了一种由压电致动器驱动的疲劳试验机,沿光束线放置,用于原位观测,以实现精确对准。最初是在静态拉伸载荷下观察界面脱粘情况,结果证实碳纤维两端的长度几乎相同,这意味着倾斜导致的弯曲变形可以忽略不计。然后对样品施加循环载荷,以捕捉渐进式脱胶。随着循环次数的增加,界面脱粘的传播速度也在下降。在单根碳纤维破碎试验后,制备了另一个与加载方向平行的单根碳纤维样品。在纤维断裂周围明显观察到界面脱粘现象。对该样品也施加了循环载荷,但未发现界面脱粘现象。在弹性变形范围内施加循环载荷时,碳纤维和环氧基体之间的界面强度没有发生退化。
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引用次数: 0
Radiation hardened MOSFETs realized by Al2O3 induced Bi-GdF3 with trapped interfacial electrons located in Ti3C2Tx framework 由 Al2O3 诱导的 Bi-GdF3 实现的辐射硬化 MOSFET,Ti3C2Tx 框架中存在被困的界面电子
IF 8.3 1区 材料科学 Q1 MATERIALS SCIENCE, COMPOSITES Pub Date : 2024-10-11 DOI: 10.1016/j.compscitech.2024.110911
Tianyu Zhang , Yang Hong , Jingyang Li , Yang Li , Huiyang Zhao , Kai Cui , Wenjing Wei , Hongjun Kang , Jinzhu Wu , Wei Qin , Xiaohong Wu
The radiation resistance of Metal-Oxide-Semiconductor Field-Effect Transistors (MOSFETs) is of great significance when applied in aerospace. However, it is still challenging to obtain MOSFETs with excellent radiation resistance. In this work, the radiation hardened MOSFETs were realized by GdF3-Al2O3@Bi-Ti3C2Tx/epoxy (MBAG/EP) polymer-based composite coating with function of trapped interfacial electrons. The radiation resistance of resultant packed MOSFET is significantly improved, showing the lower threshold voltage negative drift value (0.41 V) than the bare MOSFET (7.89 V). This is mainly attributed to the introduction of ultra-thin Al2O3 intermediate layer between Bi and GdF3, which effectively tailor electron dense and distribution for an effective electron attenuation, and thus improve the radiation resistance of the MOSFET. Theoretical calculations further reveal that the packed MOSFETs present the less shifted voltage and trapped charges compared with the pristine one. This work provides an interface engineering strategy for developing radiation hardened MOSFETs.
金属氧化物半导体场效应晶体管(MOSFET)的抗辐射性能在航空航天领域的应用中具有重要意义。然而,要获得具有优异抗辐射性能的 MOSFET 仍然是一项挑战。在这项工作中,通过 GdF3-Al2O3@Bi-Ti3C2Tx/epoxy (MBAG/EP) 聚合物基复合涂层实现了具有捕获界面电子功能的辐射硬化 MOSFET。与裸 MOSFET(7.89 V)相比,封装后的 MOSFET 的抗辐射能力明显提高,阈值电压负漂移值(0.41 V)更低。这主要归功于在 Bi 和 GdF3 之间引入了超薄 Al2O3 中间层,从而有效地调整了电子密度和分布,实现了有效的电子衰减,从而提高了 MOSFET 的辐射阻抗。理论计算进一步表明,与原始 MOSFET 相比,填料 MOSFET 的偏移电压和俘获电荷更少。这项研究为开发抗辐射 MOSFET 提供了一种界面工程策略。
{"title":"Radiation hardened MOSFETs realized by Al2O3 induced Bi-GdF3 with trapped interfacial electrons located in Ti3C2Tx framework","authors":"Tianyu Zhang ,&nbsp;Yang Hong ,&nbsp;Jingyang Li ,&nbsp;Yang Li ,&nbsp;Huiyang Zhao ,&nbsp;Kai Cui ,&nbsp;Wenjing Wei ,&nbsp;Hongjun Kang ,&nbsp;Jinzhu Wu ,&nbsp;Wei Qin ,&nbsp;Xiaohong Wu","doi":"10.1016/j.compscitech.2024.110911","DOIUrl":"10.1016/j.compscitech.2024.110911","url":null,"abstract":"<div><div>The radiation resistance of Metal-Oxide-Semiconductor Field-Effect Transistors (MOSFETs) is of great significance when applied in aerospace. However, it is still challenging to obtain MOSFETs with excellent radiation resistance. In this work, the radiation hardened MOSFETs were realized by GdF<sub>3</sub>-Al<sub>2</sub>O<sub>3</sub>@Bi-Ti<sub>3</sub>C<sub>2</sub>T<sub><em>x</em></sub>/epoxy (MBAG/EP) polymer-based composite coating with function of trapped interfacial electrons. The radiation resistance of resultant packed MOSFET is significantly improved, showing the lower threshold voltage negative drift value (0.41 V) than the bare MOSFET (7.89 V). This is mainly attributed to the introduction of ultra-thin Al<sub>2</sub>O<sub>3</sub> intermediate layer between Bi and GdF<sub>3</sub>, which effectively tailor electron dense and distribution for an effective electron attenuation, and thus improve the radiation resistance of the MOSFET. Theoretical calculations further reveal that the packed MOSFETs present the less shifted voltage and trapped charges compared with the pristine one. This work provides an interface engineering strategy for developing radiation hardened MOSFETs.</div></div>","PeriodicalId":283,"journal":{"name":"Composites Science and Technology","volume":"258 ","pages":"Article 110911"},"PeriodicalIF":8.3,"publicationDate":"2024-10-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"142434330","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":1,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Effects of SiO2-coated CNTs on the directional formation of SiC whiskers and improvement in the ablative resistance of polymer-matrix composites 涂覆 SiO2 的 CNT 对定向形成 SiC 晶须和提高聚合物基复合材料抗烧蚀性的影响
IF 8.3 1区 材料科学 Q1 MATERIALS SCIENCE, COMPOSITES Pub Date : 2024-10-11 DOI: 10.1016/j.compscitech.2024.110904
Li Wang, Jiang Li, Yiwei Wang, Shihui Cheng, Chenyang Ma
As the development of hypersonic aerospace technology progresses, greater challenges are presented for solid rocket motors (SRMs) thermal protection, and the ablation performance of insulation materials needs to be further improved. Carbon nanotubes (CNTs) as a new type of reinforcing nano-filler, readily react with the oxidative components in the working gas during SRMs operation, limiting their excellent performance. In this study, we propose to coat the commonly used reinforcing filler, SiO2, on the surface of CNTs to suppress their susceptibility to oxidation and investigate the effects of adding CNTs, SiO2, and CNTs@SiO2 to the matrix on material properties. The results show that the addition of CNTs@SiO2 significantly improves the ablation resistance of the insulation material, with the linear ablation rate of M-@SiO2-2 being 56 % lower than that of M-SiO2-2. Based on the analysis of the material's antioxidation performance and the strength of the resulting char layer after ablation, the reasons for the improvement of ablation performance are discussed. By conducting high-temperature tube furnace tests, the composition and structure of the char layer at different temperatures are studied, and it is found that CNTs in the CNTs@SiO2 formulation can directly provide the carbon source required for the carbon thermal reduction reaction, promoting the directional growth of SiC whiskers. Based on these findings, an ablation mechanism is proposed.
随着高超音速航空航天技术的发展,固体火箭发动机(SRM)的热防护面临着更大的挑战,绝热材料的烧蚀性能需要进一步提高。碳纳米管(CNTs)作为一种新型的增强纳米填料,在 SRM 运行过程中容易与工作气体中的氧化成分发生反应,限制了其优异性能的发挥。在本研究中,我们提出在 CNT 表面包覆常用的增强填料 SiO2,以抑制其易氧化性,并研究了在基体中添加 CNT、SiO2 和 CNTs@SiO2 对材料性能的影响。结果表明,添加 CNTs@SiO2 能显著提高绝缘材料的抗烧蚀性,M-@SiO2-2 的线性烧蚀率比 M-SiO2-2 低 56%。根据对材料抗氧化性能和烧蚀后产生的炭层强度的分析,讨论了烧蚀性能改善的原因。通过进行高温管式炉试验,研究了不同温度下炭层的组成和结构,发现 CNTs@SiO2 配方中的 CNTs 可直接提供碳热还原反应所需的碳源,促进 SiC 晶须的定向生长。基于这些发现,提出了一种烧蚀机制。
{"title":"Effects of SiO2-coated CNTs on the directional formation of SiC whiskers and improvement in the ablative resistance of polymer-matrix composites","authors":"Li Wang,&nbsp;Jiang Li,&nbsp;Yiwei Wang,&nbsp;Shihui Cheng,&nbsp;Chenyang Ma","doi":"10.1016/j.compscitech.2024.110904","DOIUrl":"10.1016/j.compscitech.2024.110904","url":null,"abstract":"<div><div>As the development of hypersonic aerospace technology progresses, greater challenges are presented for solid rocket motors (SRMs) thermal protection, and the ablation performance of insulation materials needs to be further improved. Carbon nanotubes (CNTs) as a new type of reinforcing nano-filler, readily react with the oxidative components in the working gas during SRMs operation, limiting their excellent performance. In this study, we propose to coat the commonly used reinforcing filler, SiO<sub>2</sub>, on the surface of CNTs to suppress their susceptibility to oxidation and investigate the effects of adding CNTs, SiO<sub>2</sub>, and CNTs@SiO<sub>2</sub> to the matrix on material properties. The results show that the addition of CNTs@SiO<sub>2</sub> significantly improves the ablation resistance of the insulation material, with the linear ablation rate of M-@SiO<sub>2</sub>-2 being 56 % lower than that of M-SiO<sub>2</sub>-2. Based on the analysis of the material's antioxidation performance and the strength of the resulting char layer after ablation, the reasons for the improvement of ablation performance are discussed. By conducting high-temperature tube furnace tests, the composition and structure of the char layer at different temperatures are studied, and it is found that CNTs in the CNTs@SiO<sub>2</sub> formulation can directly provide the carbon source required for the carbon thermal reduction reaction, promoting the directional growth of SiC whiskers. Based on these findings, an ablation mechanism is proposed.</div></div>","PeriodicalId":283,"journal":{"name":"Composites Science and Technology","volume":"258 ","pages":"Article 110904"},"PeriodicalIF":8.3,"publicationDate":"2024-10-11","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"142434258","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":1,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
An ANN-based concurrent multiscale damage evolution model for hierarchical fiber-reinforced composites 基于 ANN 的分层纤维增强复合材料并发多尺度损伤演变模型
IF 8.3 1区 材料科学 Q1 MATERIALS SCIENCE, COMPOSITES Pub Date : 2024-10-10 DOI: 10.1016/j.compscitech.2024.110910
Xiaojian Han, Kai Huang, Tao Zheng, Jindi Zhou, Hongsen Liu, Zhixing Li, Li Zhang, Licheng Guo
In this paper, an ANN-based concurrent multiscale damage evolution model is proposed, which is able to investigate the complex failure behaviors of hierarchical fiber-reinforced composites. In the framework of the proposed model, yarn damage evolution laws at the mesoscale are indirectly derived from the microscale representative volume element (RVE), using artificial neural networks (ANNs) as a surrogate model. A homogenized characterization method is proposed to derive the homogenized damage variables. The homogenized strain and damage variables of the microscale RVE are taken as inputs and outputs in ANNs, respectively. The dataset is generated by combining clustering with the finite element simulation. A typical kind of plain-woven composite is adopted as a benchmark material for numerical implementation and experimental verification. The numerical predictions, including the tensile properties and damage evolution, are consistent with the results from quasi-static tension experiments.
本文提出了一种基于人工神经网络的并发多尺度损伤演化模型,该模型能够研究分层纤维增强复合材料的复杂失效行为。在所提模型的框架内,利用人工神经网络(ANN)作为代理模型,从微观代表体积元素(RVE)间接推导出中观尺度的纱线损伤演化规律。提出了一种同质化表征方法来推导同质化损伤变量。微尺度 RVE 的均质化应变和损伤变量分别作为人工神经网络的输入和输出。数据集是通过聚类与有限元模拟相结合生成的。采用一种典型的平织复合材料作为基准材料,进行数值计算和实验验证。数值预测结果(包括拉伸性能和损伤演变)与准静态拉伸实验结果一致。
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引用次数: 0
Domain generalization-based damage detection of composite structures powered by structural digital twin 基于领域泛化的复合材料结构损伤检测,由结构数字孪生提供动力
IF 8.3 1区 材料科学 Q1 MATERIALS SCIENCE, COMPOSITES Pub Date : 2024-10-10 DOI: 10.1016/j.compscitech.2024.110908
Cheng Liu, Yan Chen, Xuebing Xu, Wangqian Che
This research addresses the challenge of generalizing deep learning models for different CFRP composite structures in the task of fatigue damage detection. To overcome this challenge, knowledge distillation is employed to enhance the generalizability of deep learning models. A teacher network processes continuous wavelet transform images using Fourier transform and neural networks, while a student network distills the teacher network. This framework improves the models' generalization performance by transferring knowledge from the teacher network to the student network. Additionally, soft gradient boosting is utilized to further enhance the generalizability. By constructing a main sub-network and multiple parallel auxiliary sub-networks within the teacher network, the student network mimics the main sub-network to achieve improved accuracy in the target domain and prevent overfitting. To augment limited datasets of real CFRP monitoring signals and help to learn domain-invariant features, structural digital twin technology is leveraged to generate simulated monitoring signals, which enables the models to capture domain invariant information, significantly enhancing its performance of fatigue damage detection across different structures. Damage detection based on the generalization results between multiple Layups demonstrates a test accuracy exceeding 80 % when the monitoring data of the target CFRP structure is unavailable during training. Therefore, the cross-structure damage detection ability of the proposed approach is well proved.
本研究解决了在疲劳损伤检测任务中针对不同 CFRP 复合材料结构推广深度学习模型的难题。为了克服这一挑战,我们采用了知识提炼的方法来增强深度学习模型的通用性。教师网络利用傅立叶变换和神经网络处理连续小波变换图像,而学生网络则对教师网络进行提炼。这一框架通过将知识从教师网络转移到学生网络,提高了模型的泛化性能。此外,还利用软梯度提升技术来进一步增强泛化能力。通过在教师网络中构建一个主子网络和多个并行辅助子网络,学生网络可以模仿主子网络,从而提高目标领域的准确性,并防止过拟合。为了扩充有限的真实 CFRP 监测信号数据集并帮助学习域不变特征,利用结构数字孪生技术生成模拟监测信号,从而使模型能够捕获域不变信息,显著提高其在不同结构中的疲劳损伤检测性能。当训练过程中无法获得目标 CFRP 结构的监测数据时,基于多层结构间泛化结果的损伤检测显示出超过 80% 的测试精度。因此,该方法的跨结构损伤检测能力得到了很好的证明。
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引用次数: 0
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Composites Science and Technology
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