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
The 3D fine-woven punctured C/C-(PyC/SiC/TaC)composites,composed of PyC/SiC/TaC interphases and pyrocarbon (PyC)matrix,were synthesized by isothermal chemical vapor infiltration(ICVI)methods.The alternating layers and...The 3D fine-woven punctured C/C-(PyC/SiC/TaC)composites,composed of PyC/SiC/TaC interphases and pyrocarbon (PyC)matrix,were synthesized by isothermal chemical vapor infiltration(ICVI)methods.The alternating layers and the structure of these composites were examined by polarized light microscopy(PLM),X-ray diffractometry(XRD)and scanning electron microscopy(SEM).It is found that the PyC matrix has rough laminar(RL)structure,the TaC layer has NaCl-type cubic structure,and the SiC layer has few wurtzite type 10H-SiC besidesβ-SiC structure.The effects of fiber coating and the bulk density on the tensile and flexural properties of composites along X or Y and Z direction were investigated.It is shown that fiber coated 3D woven punctured C/C composites have good tensile and flexural strength,and the maximum of flexural strength is 375 MPa in X or Y direction at density of 1.89 g/cm 3 ,which is about three times higher than that of samples without TaC/SiC fiber coating.The flexural strength and bending strength increase with increasing the density of the composites.The analysis of fracture surfaces reveals that fibers and fiber bundles are pulled out in composites,indicating that the composite exhibits a non-linear failure behavior through propagation and deflection of the cracks.展开更多
通过对平纹编织C/SiC复合材料经向和纬向截面的扫描电子显微镜(Scanning Electron Microscope,SEM)照片的精确测量,获取了纤维束的几何参数和波动曲线,以四参数正弦函数为拟合函数,得到了纤维束纵、横截面的参数化曲线方程。并通过建立...通过对平纹编织C/SiC复合材料经向和纬向截面的扫描电子显微镜(Scanning Electron Microscope,SEM)照片的精确测量,获取了纤维束的几何参数和波动曲线,以四参数正弦函数为拟合函数,得到了纤维束纵、横截面的参数化曲线方程。并通过建立的代表特征体元(representative volume element,RVE)得到纤维体积含量的计算值与试验测定值相比较,来检验模型的精确性。以MSC.PATRAN为平台,采用六面体单元进行分网,得到了RVE的三维有限元模型。通过在RVE模型中预制孔洞的方法,计算了平纹编织C/SiC复合材料的有效弹性模量,其中轴向拉伸模量与轴向剪切模量的计算值与试验值吻合较好,其它3个有效弹性模量还有待试验值的检验。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.
基金Project(50872154)supported by the National Natural Science Foundation of ChinaProject(20080431029)supported by China Postdoctoral Science FoundationProject supported by the Postdoctoral Science Foundation of Central South University,China
文摘The 3D fine-woven punctured C/C-(PyC/SiC/TaC)composites,composed of PyC/SiC/TaC interphases and pyrocarbon (PyC)matrix,were synthesized by isothermal chemical vapor infiltration(ICVI)methods.The alternating layers and the structure of these composites were examined by polarized light microscopy(PLM),X-ray diffractometry(XRD)and scanning electron microscopy(SEM).It is found that the PyC matrix has rough laminar(RL)structure,the TaC layer has NaCl-type cubic structure,and the SiC layer has few wurtzite type 10H-SiC besidesβ-SiC structure.The effects of fiber coating and the bulk density on the tensile and flexural properties of composites along X or Y and Z direction were investigated.It is shown that fiber coated 3D woven punctured C/C composites have good tensile and flexural strength,and the maximum of flexural strength is 375 MPa in X or Y direction at density of 1.89 g/cm 3 ,which is about three times higher than that of samples without TaC/SiC fiber coating.The flexural strength and bending strength increase with increasing the density of the composites.The analysis of fracture surfaces reveals that fibers and fiber bundles are pulled out in composites,indicating that the composite exhibits a non-linear failure behavior through propagation and deflection of the cracks.
文摘通过对平纹编织C/SiC复合材料经向和纬向截面的扫描电子显微镜(Scanning Electron Microscope,SEM)照片的精确测量,获取了纤维束的几何参数和波动曲线,以四参数正弦函数为拟合函数,得到了纤维束纵、横截面的参数化曲线方程。并通过建立的代表特征体元(representative volume element,RVE)得到纤维体积含量的计算值与试验测定值相比较,来检验模型的精确性。以MSC.PATRAN为平台,采用六面体单元进行分网,得到了RVE的三维有限元模型。通过在RVE模型中预制孔洞的方法,计算了平纹编织C/SiC复合材料的有效弹性模量,其中轴向拉伸模量与轴向剪切模量的计算值与试验值吻合较好,其它3个有效弹性模量还有待试验值的检验。
