Ceramic matrix composites (CMCs) are the preferred materials for solving advanced aerospace high-temperature structural components;it has the comprehensive advantages of higher temperature (~1500˚C) and low density. I...Ceramic matrix composites (CMCs) are the preferred materials for solving advanced aerospace high-temperature structural components;it has the comprehensive advantages of higher temperature (~1500˚C) and low density. In service environments, CMCs exhibit complex damage mechanisms and failure modes, which are affected by constituent materials, meso-architecture and inhere defects. In this paper, the in-plane tensile mechanical behavior of a plain-woven SiCf/SiC composite at room and elevated temperatures was investigated, and the factors affecting the tensile strength of the material were discussed in depth. The results show that the tensile modulus and strength of SiCf/SiC composites at high temperature are lower, but the fracture strain increases and the toughness of the composites is enhanced;the stitching holes significantly weaken the tensile strength of the material, resulting in the material is easy to break at the cross-section with stitching holes.展开更多
A new standard parametric modeling method of the micro-structure of plain woven composite is proposed. It is based on good analysis of the mechanical property of the yarn, weaving law of plain woven, and other factors...A new standard parametric modeling method of the micro-structure of plain woven composite is proposed. It is based on good analysis of the mechanical property of the yarn, weaving law of plain woven, and other factors. The method implements a woven fabric composite visual engineering modeling process standardization, and it gives five steps to calculate the key micro-structural parameters of the yarn including the cross-section and the trajectory of the central Line. On the basis, the digital model of a plain woven composite has been constructed. The experimental result shows that the forecast for the mechanical property of the model using finite-element simulation analysis is consistent with the actual value. The shape and the structure of the model are also consistent with the solid.展开更多
Due to notable characteristics,sustainability concept and environmental issues,hybridisation natural with synthetic fibres to fabricate composites have been rapidly gaining market share in different applications(struc...Due to notable characteristics,sustainability concept and environmental issues,hybridisation natural with synthetic fibres to fabricate composites have been rapidly gaining market share in different applications(structural,military,aerospace and automotive vehicles).Compression,tension and fatigue tests of various stacking sequences of plain jute/carbon reinforced(PVB)polyvinyl butyral by hot hydraulic press technique were experimentally conducted.Six types of fabricated composites with various constituents(jute,carbon and their hybrids)were fabricated and tested.Notably,fatigue lifetime of hybrids increases with increasing the carbon content relative to the jute fibre content.On the other hand,Jute composites possess high strain compared to pure carbon composite,which gives an overall improvement in mechanical behaviours.Interestingly,H1 hybrid with Carbon/Jute/Carbon sequences offers similar fatigue stiffness behaviour of H3 hybrid with Carbon/Jute/Carbon/Jute sequences when subjected to cyclic loading.Carbon composite(C)exhibited the highest fatigue resistance,whiles jute composite(J)possessed the highest strain and semi brittle trends in both mechanical and fatigue performance.Results concluded that plain jute fibres could partially replace high-cost synthetic carbon fibres to produce more eco-friendly hybrids to be utilised in different composites industries.展开更多
The mechanical behavior of plain woven Carbon Fiber-Reinforced Polymer(CFRP)composites under Three-Point Bending(TPB)is investigated via experimental and numerical approaches.Multiscale models,including microscale,mes...The mechanical behavior of plain woven Carbon Fiber-Reinforced Polymer(CFRP)composites under Three-Point Bending(TPB)is investigated via experimental and numerical approaches.Multiscale models,including microscale,mesoscale and macroscale models,have been developed to characterize the TPB strength and damages.Thereinto,Representative Volume Elements(RVEs)of the microscale and mesoscale structures are established to determine the effective properties of carbon-fiber yarn and CFRP composites,respectively.Aimed at accurately and efficiently predicting the TPB behavior,an Equivalent Cross-Ply Laminate(ECPL)cell is proposed to simplify the inherent woven architecture,and the effective properties of the subcell are computed using a local homogenization approach.The macroscale model of the TPB specimen is constructed by a topology structure of ECPL cells to predict the mechanical behavior.The TPB experiments have been performed to validate the multiscale models.Both the experimental and numerical results reveal that delamination mainly appears in the top and bottom interfaces of the CFRP laminates.And matrix cracking and delamination are identified as the significant damage modes during the TPB process.Finally,the quasi-static and dynamic behaviors of plain woven composites are discussed by comparing the results of Low-Velocity Impact(LVI)and TPB simulations.展开更多
为探究平纹织物复合材料的组分细观强度,笔者基于细观力学失效(micro-mechanics of failure, MMF)理论提出了一种确定平纹织物复合材料细观强度的跨尺度分析方法。建立了单向带复合材料和平纹织物复合材料纤维束的细观尺度代表体积单元...为探究平纹织物复合材料的组分细观强度,笔者基于细观力学失效(micro-mechanics of failure, MMF)理论提出了一种确定平纹织物复合材料细观强度的跨尺度分析方法。建立了单向带复合材料和平纹织物复合材料纤维束的细观尺度代表体积单元有限元模型,并介绍了基于代表体积单元模型的宏-细观应力转换方法;根据单向带复合材料的宏观强度测试结果确定了单向带复合材料的组分细观强度;以单向带复合材料组分细观强度为基础,根据组分强度不变的假设反推了平纹织物复合材料的纤维束强度,并以平纹织物复合材料层板宏观强度试验结果对反推所得的纤维束强度进行了校验与修正;以纤维束强度为基础,结合细观尺度代表体积单元模型,确定了平纹织物复合材料的纤维、基体组分强度。针对T300/环氧复合材料,应用上述方法并结合宏观强度测试,确定了平纹织物复合材料的组分细观强度。研究结果表明所提出的分析方法和计算结果与实验结果较为符合,可应用于实际工程复合材料。展开更多
文摘Ceramic matrix composites (CMCs) are the preferred materials for solving advanced aerospace high-temperature structural components;it has the comprehensive advantages of higher temperature (~1500˚C) and low density. In service environments, CMCs exhibit complex damage mechanisms and failure modes, which are affected by constituent materials, meso-architecture and inhere defects. In this paper, the in-plane tensile mechanical behavior of a plain-woven SiCf/SiC composite at room and elevated temperatures was investigated, and the factors affecting the tensile strength of the material were discussed in depth. The results show that the tensile modulus and strength of SiCf/SiC composites at high temperature are lower, but the fracture strain increases and the toughness of the composites is enhanced;the stitching holes significantly weaken the tensile strength of the material, resulting in the material is easy to break at the cross-section with stitching holes.
文摘A new standard parametric modeling method of the micro-structure of plain woven composite is proposed. It is based on good analysis of the mechanical property of the yarn, weaving law of plain woven, and other factors. The method implements a woven fabric composite visual engineering modeling process standardization, and it gives five steps to calculate the key micro-structural parameters of the yarn including the cross-section and the trajectory of the central Line. On the basis, the digital model of a plain woven composite has been constructed. The experimental result shows that the forecast for the mechanical property of the model using finite-element simulation analysis is consistent with the actual value. The shape and the structure of the model are also consistent with the solid.
基金I would like to thank the Ministry of Higher Education&Scientific Research of Iraq and to Mustansiriyah University,College of Engineering,Mechanical Engineering Department,for the support for the work contained in this study in Iraq.
文摘Due to notable characteristics,sustainability concept and environmental issues,hybridisation natural with synthetic fibres to fabricate composites have been rapidly gaining market share in different applications(structural,military,aerospace and automotive vehicles).Compression,tension and fatigue tests of various stacking sequences of plain jute/carbon reinforced(PVB)polyvinyl butyral by hot hydraulic press technique were experimentally conducted.Six types of fabricated composites with various constituents(jute,carbon and their hybrids)were fabricated and tested.Notably,fatigue lifetime of hybrids increases with increasing the carbon content relative to the jute fibre content.On the other hand,Jute composites possess high strain compared to pure carbon composite,which gives an overall improvement in mechanical behaviours.Interestingly,H1 hybrid with Carbon/Jute/Carbon sequences offers similar fatigue stiffness behaviour of H3 hybrid with Carbon/Jute/Carbon/Jute sequences when subjected to cyclic loading.Carbon composite(C)exhibited the highest fatigue resistance,whiles jute composite(J)possessed the highest strain and semi brittle trends in both mechanical and fatigue performance.Results concluded that plain jute fibres could partially replace high-cost synthetic carbon fibres to produce more eco-friendly hybrids to be utilised in different composites industries.
基金financial supports from the National Natural Science Foundation of China (No. 52005451)the China Postdoctoral Science Foundation (No. 2022M712876)+1 种基金supported by the Joint Fund of Research and Development Program of Henan Province, China (No. 222301420033)the Foundation of Henan Center for Outstanding Overseas Scientists, China (No. GZS2021001)
文摘The mechanical behavior of plain woven Carbon Fiber-Reinforced Polymer(CFRP)composites under Three-Point Bending(TPB)is investigated via experimental and numerical approaches.Multiscale models,including microscale,mesoscale and macroscale models,have been developed to characterize the TPB strength and damages.Thereinto,Representative Volume Elements(RVEs)of the microscale and mesoscale structures are established to determine the effective properties of carbon-fiber yarn and CFRP composites,respectively.Aimed at accurately and efficiently predicting the TPB behavior,an Equivalent Cross-Ply Laminate(ECPL)cell is proposed to simplify the inherent woven architecture,and the effective properties of the subcell are computed using a local homogenization approach.The macroscale model of the TPB specimen is constructed by a topology structure of ECPL cells to predict the mechanical behavior.The TPB experiments have been performed to validate the multiscale models.Both the experimental and numerical results reveal that delamination mainly appears in the top and bottom interfaces of the CFRP laminates.And matrix cracking and delamination are identified as the significant damage modes during the TPB process.Finally,the quasi-static and dynamic behaviors of plain woven composites are discussed by comparing the results of Low-Velocity Impact(LVI)and TPB simulations.
文摘为探究平纹织物复合材料的组分细观强度,笔者基于细观力学失效(micro-mechanics of failure, MMF)理论提出了一种确定平纹织物复合材料细观强度的跨尺度分析方法。建立了单向带复合材料和平纹织物复合材料纤维束的细观尺度代表体积单元有限元模型,并介绍了基于代表体积单元模型的宏-细观应力转换方法;根据单向带复合材料的宏观强度测试结果确定了单向带复合材料的组分细观强度;以单向带复合材料组分细观强度为基础,根据组分强度不变的假设反推了平纹织物复合材料的纤维束强度,并以平纹织物复合材料层板宏观强度试验结果对反推所得的纤维束强度进行了校验与修正;以纤维束强度为基础,结合细观尺度代表体积单元模型,确定了平纹织物复合材料的纤维、基体组分强度。针对T300/环氧复合材料,应用上述方法并结合宏观强度测试,确定了平纹织物复合材料的组分细观强度。研究结果表明所提出的分析方法和计算结果与实验结果较为符合,可应用于实际工程复合材料。
