编织复合材料弹性性能的细观力学模型

提出了编织复合材料弹性性能分析的细观力学模型，这个力学模型考虑了实际编织结构中的纬向和经向纤维束的曲屈，相邻纤维束之间的间隙和纤维束的横截面尺寸对编织复合材料弹性性能的影响，并探讨了在纤维束间纯树脂区内孔隙的含量和两种叠层结构对材料弹性性能的影响．理论计算结果与实测值的比较，表明所提出的细观力学模型是合理的．根据理论分析的结果，提出了优化单层和叠层编织结构的结构参数选择方法     

二维三轴编织复合材料的弹性性能分析

提出了二维三轴编织复合材料的几何模型，模型考虑了纤维束的弯曲扭转状态及空间交错特性等几何元素。基于体积平均法，建立了预测二维三轴编织复合材料弹性性能的理论分析模型；通过引入更普遍适用的周期性位移边界条件，结合二维三轴编织复合材料的细观实体结构，建立了分析其力学性能的有限元模型。两种模型预测结果均与试验结果吻合，证明了方法的合理有效性。分析了材料受载下的细观应力分布，并讨论了编织参数对材料性能的影响。研究表明，二维三轴编织复合材料轴向性能得到了增强，应力分布更均匀，编织角以及纤维体积含量对材料弹性性能影响较大。     

三维编织复合材料模量的双尺度有限元计算

针对三维编织复合材料的力学性能进行了双尺度有限元(TSA)数值计算，给出了计算模型和算法过程，并将数值结果与文献中的实验数据进行了比较，验证了算法的物理准确性。编织复合材料的力学性能不仅依赖于材料的基本组份，也与细观构造相关。双尺度有限元计算可以数值模拟出三维编织复合材料的整体力学性能，从而为材料的研发提供指导。本文的双尺度有限元三维数值计算方法可以推广到其他增强／孔隙等多相复合材料的数值模拟。     

三维五向编织复合材料渐进损伤分析及强度预测

基于五向编织复合材料连续体细观结构单胞,提出了材料的三维渐进损伤分析模型,采用非线性有限元方法并结合均匀化平均思想,建立了三维五向编织复合材料的强度预测胞元模型.经研究典型编织角材料在拉伸载荷作用下细观损伤的发生及演化过程,分析了材料的细观失效机理,获得了材料的宏观拉伸应力应变曲线和极限破坏强度,并详细探讨了工艺参数编织角对材料宏观力学性能的影响规律.     

粘弹性树脂基三维编织复合材料的热膨胀性能研究

首先利用均匀化理论并结合有限元法研究了三维编织复合材料的粘弹性效应，根据松弛模量的计算结果研究了材料热膨胀系数随时间的变化关系，在此基础上，给出了编织结构和工艺参数(编织角、纤维体积比)对材料初始热膨胀系数的影响规律，计算结果与实验值吻合较好。本文工作为深入研究三维编织复合材料的热粘弹性能提供了基础。     

Z-pins增强C/SiC复合材料层间I型断裂韧性

提出手工预缝纫方法将3K丝束的T300碳纤维引入预成型体，经过多次反复化学气相渗透工艺，在预成型体和缝线处同时渗透SiC基体，制备Z-pins增强平纹编织C/SiC陶瓷基复合材料。通过双悬臂梁对称弯曲试验测定了层间I型应变能释放率，分析了材料的裂纹扩展行为和Z-pins增强机理，建立了层间I型裂纹扩展预测模型。结果表明：Z-pins植入平纹编织C/SiC陶瓷基复合材料层压板能提高层间I型断裂韧性。Z-pins增强平纹编织C/SiC陶瓷基复合材料层压板I型层间增强机理主要是Z-pins桥连和Z-pins拔出。层间裂纹扩展预测模型的预测结果与试验结果吻合较好。     

2D编织陶瓷基复合材料应力-应变行为的试验研究和模拟

该文对2D编织陶瓷基复合材料的拉伸应力-应变行为进行了试验研究和理论模拟.将2D编织结构简化为:正交铺层结构和纤维束波动结构.基于Curtin和Ahn提出的基体随机开裂、纤维随机断裂的统计分布理论,得到正交铺层结构的应力-应变关系;基于体积平均方法,将纤维束波动部分分割为若干子单元;由于纤维束的波动使各子单元材料方向与加载方向不一致,因此考虑了各子单元的线性行为和非线性行为对材料响应的影响,同时引入强度分析模型,得到纤维束波动部分的应力-应变关系.结合正交铺层部分和纤维束波动部分的应力-应变关系,得到2D编织结构的应力-应变行为,理论与试验结果吻合较好.     

三维编织复合材料剪切性能分析

根据三维四向编织复合材料的结构特点，提出了刚度合成法预测编织复合材料剪切弹性模量，比较了整体编织试件和裁剪所得试件理论剪切性能差别，分析了三维编织T300／QY9512复合材料的剪切性能随试件沿宽度和厚度两个方向内部单胞数目的变化规律。结果表明，三维编织复合材料剪切弹性模量是与试件尺寸相关的，只有当试件尺寸较大、沿宽度和厚度两个方向内部单胞数目较多时，试件尺寸的影响可以忽略。当沿宽度方向单胞数目较大时，整体编织试件和裁剪所得试件的剪切模量相近。本文还得到了在复合材料板的纤维体积含量不变的情况下，剪切模量随编织角的变化规律。     

二维编织陶瓷基复合材料应力-应变行为

对二维编织陶瓷基复合材料拉伸应力-应变行为进行了试验研究和理论模拟. 将二维 编织结构简化为：正交铺层结构和纤维束波动结构. 基于基体随机开裂、纤维随机断裂分布 理论，得到正交铺层结构的应力-应变关系；基于体积平均方法，将纤维束波动部分进行分割， 引入强度分析模型，得到纤维束波动部分的应力-应变关系. 结合正交铺层部分和纤维束波动 部分的应力-应变关系，得到二维编织结构的应力-应变行为，理论与试验吻合较好.     

PAN炭纤维预制体对C/C复合材料滑动摩擦磨损行为的影响

以二维平纹编织叠层炭纤维坯体(2D)、二维无纬布/炭毡混合叠层针刺毡坯体(2DN)、三维正交编织炭纤维坯体(3D)为预制体,采用化学气相渗透结合树脂浸渍炭化技术进行增密,制备了4种C/C复合材料.在室温干态条件下测试4种C/C复合材料与表面镀Cr的40Cr钢配副时的滑动摩擦行为.结果表明:在试验载荷下,采用2D坯体增强的C/C复合材料摩擦系数最高;随载荷增加,其摩擦系数和磨损体积的波动幅度最大,分别为0.17和1.22mm3;采用2DN坯体的2种C/C复合材料摩擦系数较低,在0.13～0.17之间,且随时间延长呈下降趋势;其余2种坯体的C/C复合材料摩擦系数则上升.4种材料摩擦系数的波动幅度均逐渐降低.SEM观察表明:采用2D坯体C/C复合材料在低载荷下的摩擦表面粗糙,充满磨屑,高载荷下能形成了较松散的摩擦膜.而采用2DN、3D坯体的C/C复合材料摩擦表面部分形成了较完整、致密的摩擦膜,部分呈现显著的纤维磨损和摩擦膜大块剥落形貌.     

三维编织复合材料渐进损伤的非线性数值分析

基于考虑纤维束相互挤压的八边形纤维束截面单胞模型，引入周期性位移边界条件，采用 细观非线性有限元方法，建立了三维四向编织复合材料的渐进损伤拉伸强度模型. 该模型考 虑了增强体纤维束纵向非线性剪切应力-应变关系，采用Hashin型损伤失效准则定义了纤维 束的典型损伤类型，并根据纤维束和纯基体相应损伤类型所造成的材料性能退化，模拟了不 同编织角试件各类损伤产生、扩展及材料最终破坏的整个过程. 模型数值结果与实验数据吻 合较好，证明了该模型的合理有效性. 探讨了组分材料剪切非线性、损伤对材料宏观非线性 本构行为的影响，结果表明：随着编织角增大，纤维束剪切非线性效应和累积损伤对材料非 线性力学行为的影响明显增强.     

Theoretical prediction of stiffness and strength of three-dimensional and four-directional braided composites

Based on unit cell model, the 3D 4-directional braided composites can be simplified as unidirectional composites with different local axial coordinate system and the compliance matrix of unidirectional composites can be defined utilizing the bridge model. The total stiffness matrix of braided composites can be obtained by the volume average stiffness of unidirectional composites with different local axial coordinate system and the engineering elastic constants of braided composites were computed further. Based on the iso-strain assumption and the bridge model, the stress distribution of fiber bundle and matrix of different unidirectional composites can be determined and the tensile strength of 3D 4-directional braided composites was predicted by means of the Hoffman＇s failure criterion for the fiber bundle and Mises＇ failure criterion for the matrix.     

三维四向编织复合材料的拉伸尺寸效应研究

通过对三维四向碳/环氧编织复合材料的拉伸实验,观测了不同几何尺寸的试件的破坏模式和断口形貌,得到了材料在拉伸载荷下不同的破坏机理以及材料的力学性能与试件几何尺寸的相关性,研究表明材料随着内部单胞数量的增加材料的弹性模量递减,而剪切模量和泊松比递增的变化规律,通过体积平均法从理论上预报了材料的弹性性能,预报结果与实验结果相符,实验和理论所获结论为进一步进行材料的刚度和强度预报以及强度准则的建立奠定了必要的实验和理论基础.     

三维编织复合材料几何建模及数值分析

论文根据三维编织复合材料的结构特点,把整体结构分为内部单胞、表面单胞和角单胞三种类型的子单胞,考虑空间纤维束的相互扭结和挤压所造成的纤维束的弯曲和截面变形,针对每种类型的子单胞,建立了相应的几何分析模型.引入周期性位移边界条件,建立了材料的弹性性能预报模型,得到了三维编织复合材料的工程弹性常数.通过数值比较可以看出,论文所给出的数值计算结果与实验结果吻合较好,从而验证了本文模型的有效性.     

Modeling of particle–resin suspension impregnation in compression resin transfer molding of particle-filled,continuous fiber reinforced composites

A particle–resin suspension impregnation model is used for analyzing the mold filling process in compression resin transfer molding (CRTM) of particle-filled, continuous fiber composites. The model is based on Darcy flow coupled with particle filtration and is applicable to two-dimensional impregnation through isotropic/anisotropic fiber preforms. Comparisons with simple analytical solutions and experimental results from the literature were made to validate the numerical solution. Simulations showed that CRTM was advantageous over resin transfer molding (RTM) for smaller non-homogeneity in composite microstructure, when particle filtration was high. Limits on certain process parameters were observed beyond which molding pressures in CRTM became comparable with those in RTM. The preform anisotropy was effective in the particle distribution profile. The choice of inlet gate configuration in CRTM was found influential in the particle distribution homogeneity and molding pressures. The developed modeling tool can be extended to analyze any composite liquid molding process involving particle fillers.     

Microstructure and mechanical properties of three-dimensional five-directional braided composites

Three-dimensional (3D) five-directional braided composites are significant structural materials in the fields of astronauts and aeronautics. On the basis of the 3D five-directional braiding process, three types of microstructural unit cell models are established with respect to the interior, surface and corner regions. The mathematical relationships among the structural parameters, such as fiber orientation, fiber volume fraction, the yarn packing factor, are derived. By using these three unit cell models, a micromechanical prediction procedure is described to simulate the stiffness and strength properties of 3D five-directional braided composites. Only the in situ constituent fiber and matrix properties of the composites and the fiber volume proportion are required in the simulation. The stress states generated in the constituent fiber and matrix materials are explicitly correlated with the overall applied load on the composites. The predictive stiffness and strength are in good agreement with available experimental data, which demonstrates the applicability of the present analytical model.     

Influences of reinforcing particle and interface bonding strength on material properties of Mg/nano-particle composites

In the present study, an effective model is proposed to predict the effective elastic behavior of the three-phase composite containing spherical inclusions, each of which is surrounded by an interphase layer. The constitutive equations are derived for the stress and strain of each phase of the composite subjected to a far-field tension. Based on these constitutive laws, the effective bulk, shear and Young’s modulus are obtained. A statistical debonding criterion is adopted to characterize the varying probability of the evolution of interphase debonding. Influences of debonding damage, particle volume fraction, interphase properties and bonding strength on overall mechanical behavior of composites are also discussed. Numerical analyses are carried out on particle-reinforced composites and the predictions have a good agreement with the experimental results.