首页/文章/ 详情

【新文速递】2024年7月23日复合材料SCI期刊最新文章

1小时前浏览2

   

今日更新:Composites Part A: Applied Science and Manufacturing 1 篇,Composites Science and Technology 1 篇

Composites Part A: Applied Science and Manufacturing

From virtual to actual assisted tape placement − application of the Frenet frame to robotic steering trajectories

Gregório F.O. Ferreira, David Jones, Aswani Kumar Bandaru, Giovanni Zucco, Paul M. Weaver

doi:10.1016/j.compositesa.2024.108369

从虚拟到实际辅助胶带放置- Frenet框架到机器人转向轨迹的应用

A novel computational tool is presented that integrates the design and manufacturing of variable-angle tow composites for automated tape placement, facilitating the creation of tow-steered trajectories for cut-outs. Steering movements of the robot are planned and executed within a MATLAB virtual environment via short paths and linear commands. Leveraging piecewise-continuous clothoid splines and the Frenet frame, the tool furnishes crucial details on trajectory vectors, steering angles, and curvatures. Via four integrated modules, the user can define input parameters such as the robot’s actuators and structural geometry, allowing for the subsequent visualisation of the steered trajectories as well as the generation of the manufacturing code. Finally, to assess the potential and limitations of this methodology, the file containing all details is integrated into the Kuka KR L240-2 robot model to continuously steer a carbon fibre/PEEK tape around an elliptical cut-out in a composite panel using laser-assisted tape placement, representative of an access hole in an aircraft wing.

提出了一种新的计算工具,该工具集成了用于自动放置胶带的可变角度牵引复合材料的设计和制造,有助于创建用于切割的牵引轨迹。机器人的转向运动是通过短路径和线性命令在MATLAB虚拟环境中规划和执行的。利用分段连续的样条和Frenet框架,该工具提供了关于轨迹矢量、转向角度和曲率的关键细节。通过四个集成模块,用户可以定义输入参数,如机器人的执行器和结构几何形状,从而实现转向轨迹的可视化以及制造代码的生成。最后,为了评估该方法的潜力和局限性,将包含所有细节的文件集成到库卡KR L240-2机器人模型中,使用激光辅助胶带放置,连续地引导碳纤维/PEEK胶带围绕复合材料面板上的椭圆切口,代表飞机机翼的访问孔。


Composites Science and Technology

Experimental and numerical study of the thermomechanical properties of flexible self-reinforced polyimide composite membrane

Cheng Lu, Xin Yang, Huiqi Shao, Siyi Bi, Nanliang Chen, Guangwei Shao, Jinhua Jiang

doi:10.1016/j.compscitech.2024.110775

 

柔性自增强聚酰亚胺复合膜热力学性能的实验与数值研究

Polyimide membranes are favored in the aerospace field for their excellent comprehensive properties, but new application requirements demand higher strength, modulus and thermal expansion properties. Here, self-reinforced polyimide composite membranes (SRPICM) with varying fiber tow arrangement densities were fabricated by unidirectional reinforcement of polyimide fiber tows to enhance the thermomechanical properties of the membranes while maintaining the characteristics of low thickness and flexibility. A micro-scale representative volume element model with interface, and a macro-scale model containing cracks were developed based on the membranes' morphology to investigate the tensile and thermal expansion behavior of SRPICM. Experimental and numerical analyses demonstrated that fiber tows significantly improved the longitudinal tensile properties of SRPICM, with maximum increases in modulus and strength to 34.02 GPa and 1.26 GPa, respectively, over 13 times those of pure PI membranes. Further, the test results, combined with the two-scale finite element model revealed the evolution of longitudinal and transverse tensile deformation and thermal expansion behavior of SRPICM. The validity of the two-scale model was confirmed by experimental results, attributed to the practical consideration of interfacial bonding, prefabricated cracks and thermal residual stress effects during initial modeling. Notably, SRPICM with 10 fiber tows/20 mm arrangement density exhibited excellent longitudinal tensile properties (modulus and strength of 14.01 GPa and 470.89 MPa, respectively) and a longitudinal thermal expansion close to zero (0.03 μm/m°C), making it an ideal material for aerospace applications.

聚酰亚胺膜以其优异的综合性能在航空航天领域受到青睐,但新的应用要求对其强度、模量和热膨胀性能提出了更高的要求。本文通过单向增强聚酰亚胺纤维束,制备了具有不同纤维束排列密度的自增强聚酰亚胺复合膜(SRPICM),以提高膜的热机械性能,同时保持膜的低厚度和柔韧性。基于膜的形貌,建立了含界面的微尺度代表性体积元模型和含裂纹的宏观尺度模型,研究了SRPICM的拉伸和热膨胀行为。实验和数值分析表明,纤维束显著改善了SRPICM的纵向拉伸性能,模量和强度的最大增幅分别达到34.02 GPa和1.26 GPa,是纯PI膜的13倍以上。结合双尺度有限元模型,揭示了SRPICM纵向和横向拉伸变形及热膨胀行为的演变规律。由于在初始建模时实际考虑了界面结合、预制裂纹和热残余应力效应,实验结果证实了双尺度模型的有效性。值得注意的是,具有10根纤维束/20 mm排列密度的SRPICM具有优异的纵向拉伸性能(模量和强度分别为14.01 GPa和470.89 MPa),纵向热膨胀接近于零(0.03 μm/m°C),使其成为航空航天应用的理想材料。



来源:复合材料力学仿真Composites FEM
ACTMechanicalDeform复合材料航空航天MATLABUM裂纹材料机器人
著作权归作者所有,欢迎分享,未经许可,不得转载
首次发布时间:2024-11-21
最近编辑:1小时前
Tansu
签名征集中
获赞 3粉丝 0文章 679课程 0
点赞
收藏
作者推荐

【新文速递】2024年7月28日复合材料SCI期刊最新文章

今日更新:Composite Structures 1 篇,Composites Part A: Applied Science and Manufacturing 1 篇,Composites Part B: Engineering 1 篇,Composites Science and Technology 1 篇Composite StructuresExperimental behaviour and design model of FRP-UHPC-steel tubular columns under monotonic axial compressionZhang Bing, Zhou Chong, Zhang Sumei, Lin Shuhong, Fan Zhihong, Peng Yutao, Sun Jiaming, Lin Guandoi:10.1016/j.compstruct.2024.118416frp - uhpc -钢管柱在单调轴压作用下的试验性能及设计模型By integrating structural steel with Fiber-Reinforced Polymer (FRP) and Ultra-High Performance Concrete (UHPC), FRP-UHPC-steel tubular columns (FUSTs) emerge as innovative composite members that offer exceptional corrosion resistance and lightweight properties. FUSTs hold significant potential for use as thin-walled tubular columns working in harsh environments, such as wind turbines and high-voltage transmission towers. To obtain in-depth understanding of key parameters including the steel fiber ratio of UHPC, the specimen void ratio and the FRP thickness, this paper tested 24 specimens to evaluate their compressive behaviour, including 18 FUSTs and 6 UHPC-filled FRP tubes (UCFFTs). Experimental results showed that: (1) FUSTs demonstrated ductile behavior with significant strain enhancement and notable strength improvement; (2) the steel fibers in UHPC had marginal influences on the ultimate condition of FUSTs; (3) a larger inner void had a general effect to lead to more localized rupture for the FRP tube; (4) the FRP thickness was the predominant influencing factor on both the general shape and the ultimate point of the normalized axial stress–strain curves. Finally, a design model was proposed, which was able to capture the general shape of the axial load–strain curves, and could generate reasonably accurate predictions for the peak load.通过将结构钢与纤维增强聚合物(FRP)和超高性能混凝土(UHPC)相结合,FRP-UHPC钢管柱(FUSTs)成为创新的复合材料构件,具有卓越的耐腐蚀性和轻质性能。fsts在恶劣环境中作为薄壁管柱,如风力涡轮机和高压输电塔,具有巨大的应用潜力。为了深入了解UHPC的钢纤维比、试件空隙率和FRP厚度等关键参数,本文对24个试件进行了压缩性能评估,其中包括18个FUSTs和6个UHPC填充FRP管(UCFFTs)。试验结果表明:(1)FUSTs具有显著的应变增强和强度提高的延性;(2) UHPC中钢纤维对fsts极限状态的影响较小;(3)较大的内空隙对玻璃钢筒的局部破裂有普遍影响;(4) FRP厚度是影响归一化轴向应力-应变曲线总体形状和终点的主要因素。最后,提出了一个设计模型,该模型能够捕捉轴向载荷-应变曲线的一般形状,并能够合理准确地预测峰值载荷。Composites Part A: Applied Science and ManufacturingRevolutionizing textile: Advanced techniques for superior thermal conductivityYang Hong, Zhanxiao Kang, Jintu Fandoi:10.1016/j.compositesa.2024.108380革命性的纺织品:先进的技术,优越的导热性Improving thermal conductivity in textile/composites is crucial for heat dissipation in apparel and engineering. Apparel textiles’ thermal conductivities rarely exceed 1.0 W/(m·K), limiting efficient personal thermal management. Advances in silver conductive yarn and heat-stretched polyethylene show promise for ultra-high thermal conductivity materials. In electronic packaging, materials’ thermal conductivities rarely exceed 40 W/(m·K), causing overheating and reduced reliability. Techniques like freeze-drying and templating can enhance boron nitride composites’ thermal conductivity. Aerospace and automotive composites with mechanical and flame-retardant properties rarely exceed 120 W/(m·K), leading to potential safety hazards. Recent advancements indicate that mechanical structure enhancement and chemical surface modification can improve carbon composites’ thermal conductivity. Understanding existing enhancement techniques and mechanisms is essential. This paper reviews these techniques, discussing their potentials and limitations for future high thermal conductive textiles and composites development.提高纺织/复合材料的导热性是服装和工程散热的关键。服装纺织品的热导率很少超过1.0 W/(m·K),限制了有效的个人热管理。银导电纱和热拉伸聚乙烯的进展显示出超高导热材料的前景。在电子封装中,材料的热导率很少超过40 W/(m·K),导致过热和可靠性降低。冷冻干燥和模板等技术可以提高氮化硼复合材料的导热性。具有机械和阻燃性能的航空航天和汽车复合材料很少超过120 W/(m·K),从而导致潜在的安全隐患。近年来的研究进展表明,机械结构增强和化学表面改性可以提高碳复合材料的导热性。理解现有的增强技术和机制是必要的。本文综述了这些技术,讨论了它们在未来高导热纺织品和复合材料发展中的潜力和局限性。Composites Part B: EngineeringRecent Approaches of Interfaces Strengthening in Fibre Metal Laminates: Processes, Measurements, Properties and Numerical AnalysisUmut Bakhbergen, Fethi Abbassi, Gulnur Kalimuldina, Reza Montazami, Essam Shehab, Sherif Arabydoi:10.1016/j.compositesb.2024.111744金属纤维层合板界面强化的新方法:工艺、测量、性能和数值分析Recently, there is a pressing need for high-performance and lightweight structural materials in aircraft and automobile industry; fibre metal laminates (FMLs) are suggested ideal candidates for aviation industry. FMLs are hybrid composite material comprised thin-metal sheets and fibre-reinforced polymers (FRPs). By combining the features of both components, FMLs possess high tolerance to fatigue damage, exceptional impact resistance and an outstanding weight-to-strength ratio. However, maintaining high structure integrity of FML layers – without debonding – remains the primary challenge in FMLs-based structures. The present review explores the recent developments in manufacturing techniques and surface treatments aimed at enhancing the interfacial strength between FML layers. Recently, adding nanofillers into FRPs and FMLs is gaining attention. These nanofillers can enhance mechanical performance of FRPs/FMLs, strengthen the interface in FMLs; and add functionalities such as gas and water impermeability. The article discusses the recent studies on employing nanofillers in FMLs and adhesively bonded structures; and their role (nanofillers) in enhancing the crack resistance of FMLs. It also explores failure mechanisms in FMLs through experimental methods and advanced numerical simulations. A comprehensive review of the existing studies assists in understanding the complex failure mechanisms, aiming to find optimal input conditions that yield desired mechanical performance. Furthermore, the article introduces machine learning techniques in adhesively bonded structures and potential application in FMLs-related research. The article concludes with perspectives on the limitations, current challenges, and future prospects for FMLs and nanofiller-reinforced FMLs.近年来,飞机和汽车工业对高性能、轻量化结构材料的需求日益迫切;金属纤维层压板(FMLs)是航空工业的理想选择。FMLs是由金属薄板和纤维增强聚合物(frp)组成的杂化复合材料。结合这两种成分的特点,FMLs具有高的疲劳损伤耐受性,卓越的抗冲击性和出色的重量强度比。然而,保持FML层的高结构完整性(不脱粘)仍然是基于FML结构的主要挑战。本文综述了旨在提高FML层间界面强度的制造技术和表面处理的最新进展。近年来,在frp和fml中添加纳米填料的研究日益受到关注。这些纳米填料可以提高frp /FMLs的力学性能,增强FMLs中的界面;并增加诸如气体和水的不渗透性等功能。本文综述了近年来纳米填料在FMLs和粘接结构中的应用研究进展;以及它们(纳米填料)在增强FMLs抗裂性中的作用。通过实验方法和先进的数值模拟,探讨了FMLs的破坏机制。对现有研究的全面回顾有助于理解复杂的失效机制,旨在找到产生理想力学性能的最佳输入条件。此外,本文还介绍了机器学习技术在粘合结构中的应用以及在fml相关研究中的潜在应用。文章最后对FMLs和纳米填料增强FMLs的局限性、当前挑战和未来前景进行了展望。Composites Science and TechnologyFacile Chemical Surface Modification of Boron Nitride Platelets and Improved Thermal and Mechanical Properties of Their Polymer Compounds for 2.5D/3D Packaging ApplicationsZihao Lin, Jiaxiong Li, Zhijian Sun, Andrew D. Fang, Keyi Han, Shu Jia, Yao-Hao Liu, Michael J. Adams, Kyoung-sik Moon, Ching-Ping Wongdoi:10.1016/j.compscitech.2024.110778 用于2.5D/3D包装的氮化硼薄片的简单化学表面改性及其聚合物化合物的热力学性能的改善Thermally conductive yet electrically insulative epoxy composites are sought after as encapsulation materials to tackle the heat dissipation challenges in modern electronics. In this work, we developed a novel one-step and facile solvothermal reflux method using a high-boiling-point solvent to surface-modify hexagonal boron nitride (h-BN) with glycine. By refluxing glycine at high temperature, amino functional groups are grafted onto the BN surface, which can enhance the affinity of fillers for epoxy and reduce the interfacial thermal resistance of the filler/epoxy composites. We investigated the mechanism of glycine-grafted layer formation, optimizing reactant mass ratios for enhanced interfacial thermal transport. The resulting BN@G11/epoxy composites exhibit a remarkable thermal conductivity of 1.04 W/mK at 30 wt% modified-BN loading, representing a 477.8% increase over neat epoxy and 57.5% higher than h-BN/epoxy composites at equivalent BN filler loading. Additionally, these composites demonstrate improved thermomechanical properties, confirming the strengthened BN/epoxy interface bonding using modified BN fillers. Compared to other surface treatment methods, this solvothermal reflux approach stands out for its scalability and cost-effectiveness. This scalable and eco-friendly innovation presents a competitive strategy for designing polymer-based composites for thermal management, catering to the demands of future 2.5D/3D semiconductor packaging.导热且绝缘的环氧复合材料作为封装材料受到追捧,以解决现代电子产品中的散热挑战。在这项工作中,我们开发了一种新的一步和简单的溶剂热回流方法,使用高沸点溶剂对六方氮化硼(h-BN)进行甘氨酸表面改性。通过高温回流甘氨酸,将氨基官能团接枝到BN表面,增强填料对环氧树脂的亲和力,降低填料/环氧复合材料的界面热阻。我们研究了甘氨酸接枝层形成的机制,优化了反应物质量比以增强界面热传递。所得BN@G11/环氧复合材料在30 wt%的改性BN载荷下的导热系数为1.04 W/mK,比纯环氧提高了477.8%,比同等BN填料载荷下的h-BN/环氧复合材料高57.5%。此外,这些复合材料表现出改善的热机械性能,证实了改性BN填料增强了BN/环氧界面结合。与其他表面处理方法相比,溶剂热回流法因其可扩展性和成本效益而脱颖而出。这种可扩展且环保的创新为设计用于热管理的聚合物基复合材料提供了一种具有竞争力的策略,以满足未来2.5D/3D半导体封装的需求。来源:复合材料力学仿真Composites FEM

未登录
还没有评论
课程
培训
服务
行家
VIP会员 学习 福利任务 兑换礼品
下载APP
联系我们
帮助与反馈