包覆法制备Gp/SiC复合材料的显微结构和性能

以不同粒径的石墨颗粒和SiC粉体为原料,采用SiC粉体包覆石墨颗粒的方法,于2000℃热压制备了石墨/碳化硅（Gp/SiC）复合材料.利用扫描电子显微镜（SEM,EDS）分析了材料的金相和断口显微结构.研究表明,石墨粒径较小且质量分数较少的复合材料比石墨粒径较大且质量分数较多的复合材料在热压工艺中更致密.石墨颗粒呈岛状紧密地镶嵌在SiC基体中,石墨与SiC界面处C和Si的扩散不明显.复合材料的相对密度、抗折强度,断裂韧性和硬度随石墨粒径和质量分数的减少而增加.断口形貌表明SiC陶瓷基体为脆性,石墨为韧性断裂.当石墨粒径为125μm、SiC与石墨的质量比为3.5时,复合材料的综合性能最佳,开口气孔率为0.3%,相对密度为97.9%,抗折强度为75±15 MPa,断裂韧性为5.4±0.5 MPa.m1/2,硬度为26.8±3GPa.     

Processing and characterization of Cf/SiC composites

Carbon fiber-reinforced SiC composites were prepared by precursor pyrolysis-hot pressing （PP-HP） and precursor impregnation-pyrolysis （PIP）, respectively. The effect of fabrication methods on the microstructure and mechanical properties of the composites was investigated. It was found that the composite prepared by PP-HP exhibits a brittle fracture behavior, which is mainly ascribed to a strongly bonded fiber/matrix interface and the degradation of the fibers caused by a higher processing temperature. On the contrary, the composite prepared by PIP shows a tough fracture behavior, which could be rationalized on the basis of a weakly bonded fiber/matrix interface as well as a higher strength retention of the fibers. As a result, in comparison with the composite prepared by PP-HP, the composite prepared by PIP achieves better mechanical properties with a flexural strength of 573.4 MPa and a fracture toughness of 17.2 MPa.m^1/2.     

包覆工艺制备C—SiC—B4C—TiB2复合材料的组织与性能

以鳞片石墨,B4C,SiC,TiO2为原料,利用包覆工艺在不同热压温度下制备了W（C）=50％的C—SiC—B4C—TiB2复合材料,并详细研究了热压温度对复合材料显微组织和性能的影响规律．结果表明,当热压温度高于1850℃时,复合材料由C,SiC,B4C和TiB2这四相组成;复合材料的体积密度、抗折强度和断裂韧性均随着热压温度的升高而增加．2000oC热压时,复合材料的体积密度、气孔率、抗折强度和断裂韧性分别达到2．41g／cm^3,3．42％,176MPa和6．1MPa·m^1/2;热压温度升高,复合材料的碳相和陶瓷相逐渐致密,碳相最终形成了在陶瓷基体上镶嵌的直径为40μm橄榄球状和条状这两种形貌．碳／陶瓷相的弱界面分层诱导韧化和第二相TiB2与陶瓷基体之间热膨胀系数不匹配所致的残余应力使变形过程中微裂纹的扩展路径发展变化,使复合材料的韧性提高．     

Preparation and properties of multi-wall carbon nanotube/SiC composites by aqueous tape casting

MWCNTS/SiC composites were fabricated by aqueous tape casting. High solid content (50 vol%) SiC slurries with sintering additives and multi-wall carbon nanotubes (MWCNTs) as reinforcements were prepared using Tetramethylammonium hydroxide as the dispersant. The stability of MWCNTs/SiC slur-ries was studied and characterized in terms of zeta potential and rheology measurements. The relative density of the composite was about 98% after hot-pressing at 1850℃ (at 25 MPa in Ar for 30 min). The hardness of the composites decreased with the increase in MWCNTs content. The flexural strength and the fracture toughness were 742.17 MPa and 4.63 MPa·m1/2, respectively when the MWCNTs content was 0.25 wt%. Further increase in MWCNTs content to 0.50 wt% did not lead to the increase in mechanical properties. Most of MWCNTs were found to be located at SiC grain boundaries and the pull out of the MWCNTs was observed.     

Analytical model of elastic modulus and coefficient of thermal expansion for 2.5D C/SiC composite

To make better use of 2.5D C/SiC composites in industry, it is necessary to understand the mechanical properties. A finite element model of 2.5D composites is established, by considering the fiber undulation and the porosity in 2.5D C/SiC composites. The fiber direction of warp is defined by cosine function to simulate the undulation of warp, and based on uniform strain assumption, analytical model of the elastic modulus and coefficient of thermal expansion (CTE) for 2.5D C/SiC composites were established by using dualscale model. The result is found to correlate reasonably well with the predicted results and experimental results. The parametric study also demonstrates the effects of the fiber volume fraction, distance of warp yarn, and porosity in micro-scale on the mechanical properties and the coefficients of thermal expansion.     

Effects of oxidation treatment on properties of SiO2f/SiO2-BN composites

The silica fiber reinforced silica and boron nitride-based composites (SiO_2f/SiO₂-BN) were prepared firstly via the sol-gel method and then the urea route, and the effects of oxidation treatment on the component, structure, mechanical and dielectric properties of the composites were investigated. The results show that the oxidation treatment at 450 °C will not impair the structure of boron nitride, and carbon is the main impurity with the excessive urea. The density of SiO_2f/SiO₂-BN composites is 1.81 g/cm³, and the flexural strength and elastic modulus are 113.9 MPa and 36.5 GPa, respectively. After oxidation treatment, the density varies to 1.80 g/cm³, and the flexural strength and elastic modulus are decreased to 58.9 MPa and 9.4 GPa, respectively. The mechanical properties of the composites are severely damaged, but they still exhibit a good toughness. The composites show excellent dielectric properties with the dielectric constant and loss tangent being 3.22 and 0.003 9, respectively, which indicates that the oxidation treatment is ineffective to improve the dielectric properties of SiO_2f/SiO₂-BN composites.     

Fracture mechanism of 3D, five-directional braided (SiO2) f /SiO2 composites prepared by silicasol-infiltration-sintering method

Three-dimensional (3D) five-directional braided (SiO₂) _f /SiO₂ composites were prepared by silicasol-infiltration-sintering (SIS) method. The flexural properties and microstructures were studied. The flexural strength and flexural elastic modulus were found to be 73 MPa and 12 GPa, respectively. The results of stress vs deflection curve and SEM examinations revealed that the fracture mechanism of 3D, five-directional braided (SiO₂) _f /SiO₂ composite was a mixture mode of ductile and brittle. The ductile mode was attributed to the weak bonding strength of fiber/matrix at low temperature. The brittle fracture might be caused by the propagation of micro defect or crack, which existed in the as-prepared composites for the ten-cycle process.     

三维连通网状SiC陶瓷/Zr基非晶复合材料单轴压缩性能研究

利用分离式霍普金森压杆(SHPB)装置对三维连通网状SiC陶瓷/Zr基非晶复合材料进行不同应变率下的动态压缩实验,并与准静态压缩实验结果比较.利用X射线衍射仪和扫描电子显微镜研究了复合材料的相组成和断口形貌.结果表明:在压缩条件下三维连通网状SiC陶瓷/Zr基非晶复合材料的断裂发生在弹性变形阶段,断裂前几乎观察不到塑性变形;复合材料的准静态压缩强度达到了1 270 MPa,高于在动态压缩中的断裂强度1 100 MPa.试样发生纵向劈裂和剪切断裂,准静态下试样形成的破片数量较多,动态加载条件下试样破碎成数量较少的较大块体.三维连通网状SiC陶瓷断口形貌为层片状、台阶式的解理断裂,非晶合金发生粘性流动,在变形过程中形成脉状花样,在高应变率加载条件下,非晶热软化严重,断口形貌复杂多样.     

Microstructure and thermal properties of SiCp/Cu composites with Mo coating on SiC particles

SiCp/Cu composites with a compact microstructure were successfully fabricated by vacuum hot-pressing method. In order to suppress the detrimental interfacial reactions and ameliorate the interfacial bonding between copper and silicon carbide, molybdenum coating was deposited on the surface of silicon carbide by magnetron sputtering method and crystallized heat-treatment. The effects of the interfacial design on the thermo-physical properties of Si Cp/Cu composites were studied in detail. Thermal conductivity and expansion test results showed that silicon carbide particles coated with uniform and compact molybdenum coating have improved the comprehensive thermal properties of the Si Cp/Cu composites. Furthermore, the adhesion of the interface between silicon carbide and copper was significantly strengthened after molybdenum coating. Si Cp/Cu composites with a maximum thermal conductivity of 274.056 W/(m·K) and a coefficient of thermal expansion of 9 ppm/K were successfully prepared when the volume of silicon carbide was about 50%, and these Si Cp/Cu composites have potential applications for the electronic packageing of the high integration electronic devices.     

Preparation and properties of C/C-SiC brake composites fabricated by warm compacted-in situ reaction

Carbon fibre reinforced carbon and silicon carbide dual matrix composites(C/C-SiC) were fabricated by the warm compacted-in situ reaction.The microstructure,mechanical properties,tribological properties,and wear mechanism of C/C-SiC composites at different brake speeds were investigated.The results indicate that the composites are composed of 58wt%C,37wt%SiC,and 5wt%Si.The density and open porosity are 2.0 g.cm~(-3) and 10%,respectively.The C/C-SiC brake composites exhibit good mechanical properties.The ...     

Si对热压法制备Ti3SiC2/SiC复合材料的影响

通过热压法制备了Ti3SiC2／SiC复合材料,并通过扩散偶实验及组织观察,探讨了Si元素对热压制备Ti3SiC2／SiC复合材料的反应过程及组织的影响．结果表明,Si元素在反应过程中起主要作用,决定着反应进行的速度与方向．而且随着反应物中Si量的增加,更有利于Ti3SiC2／SiC复合材料的形成．     

原位合成SiCp/(Mo,W)Si2复合材料的组织与性能

以Mo粉、W粉、Si粉和C粉为原料,采用原位反应高温热压一次复合工艺制备了不同配比的SiCp/(Mo,W)Si2复合材料。采用光学显微镜、扫描电镜和X射线衍射仪研究了其显微结构,并测定了其力学性能。结果表明,SiCp/(Mo,W)Si2复合材料中的增强相SiC颗粒分布在基体MoSi2的晶界和晶内,WSi2固溶于MoSi2,起到了协同强化的作用,强化效果比单独加入SiC或WSi2更为显著。该种复合材料的抗弯强度最高达到592 MPa,断裂韧性达到5.9 MPa.m1/2,维氏硬度达到19.4 GPa,分别比相同工艺制备的纯MoSi2提高了约5倍、2.1倍和2.2倍。     

Fabrication of high performance 3D SiO<Subscript>2</Subscript>/Si<Subscript>3</Subscript>N<Subscript>4</Subscript> composite via perhydropolysilazane infiltration and pyrolysis

The continuous fiber reinforced ceramic matrix composites have received consider-able attention for structural applications because of their excellent thermal stability, light weight, and damage tolerance imparted by the reinforcing fibers. Silica fibers, with ex-cellent ablative resistance, thermal shock damage resistance, dielectric properties, chemical stability and flexibility, are suitable for fabricating high temperature antenna window materials to meet the requirements of communication, …     

Microstructure characterization of 3D C/SiC composites in combustion gas environments

C/SiC composites prepared by chemical vapor infiltration(CVI) were subjected to a stationary loading of 160 MPa in a combustion gas environment with flame temperature of 1300 ℃.Lifetime of C/SiC composites in such environment was measured.Microstructures of the composites after the testing were also characterized by SEM.The experimental results indicate the lifetime of C/SiC composites is average 2.3 hours in combustion gas environments.The combustion gas flow accelerates the damage of carbon fibers and the failure of the composites by speeding up the diffusion of gas reactants and products,destroying the layer of SiO2 on the surface of SiC coating and bringing fused SiO2 inside the composites.The fracture face of C/SiC is uneven,i e,a flat area close to the windward side and a pulling-out of long fibers near the leeward side,which results from the directionality effect of the combustion gas flow.     

SiC/Cu纳米包裹粉体及其复合材料的制备

选用工业生产的SiC亚微米粉体,利用置换反应制备纳米Cu.采用直接还原-旋转沉淀工艺制备SiC/Cu包裹粉体.采用气氛烧结获得金属陶瓷复合材料.分别通过AES、XRD、SEM等分析方法对原始SiC粉体、包裹复合粉体和烧成样品进行表征.结果表明:包裹复合粉体具有"核-壳"结构,由于Cu的自发氧化使得复合粉体中出现Cu2O.包裹结构中SiC颗粒抑制了烧结过程中Cu的晶粒生长,从而使烧结样品呈现纳米结构.     

Ti3SiC2/TiB2复合材料的制备及其组织和力学性能

以2TiC／Ti／Si／0．2Al／TiB2粉为原料，采用热压烧结工艺成功制备了Ti3SiC2／TiB2复合材料。结果表明：不同TiB2含量的试样中主晶相为Ti3siC2与TiB2两相，没有发现其它杂质相；当复合材料中TiB2的体积分数为10％时，其硬度、抗压强度、弯曲强度、断裂韧性都有显著的提高。经热处理后，Ti3SiC2／10％TiB2复合材料的弯曲强度由367．5MPa     

Ballistic Performance and Damage Characteristics of Chemical Vapor Infiltration Quasi 3D-Cf/SiC Composites

To investigate the ballistic performance and damage characteristics of quasi threedimensional(3D) needle-punched Cf/SiC composites prepared by chemical vapor infiltration(CVI),penetration experiments were conducted by using 7.62 mm armor piercing incendiary(API).Macro and micro fracture morphologies were then observed on recycled targets.The results show that the protection coefficient of 3D Cf/SiC composites is 2.54.High porosity and many micro thermal stress cracks may directly lead to the lower ballistic performance.Flat fracture morphology was observed on the crater surface.The low dynamic fracture strength along layer direction may be attributed to the voids and microcracks caused by residual thermal stress.The damage characteristics of Cf/Si C composites include matrix cracking,fiber bundle cracking,interfacial debonding,fiber fracture,and fiber bundle pull-out.And interfacial debonding and fiber fracture may play major roles in energy absorption.     

材料参数对短纤维增强金属基复合材料变形行为和性能的影响

运用大应变弹塑性有限元方法和修正混合律,研究了材料参数（纤维长径比、体积分数、根间距）对短纤维金属基复合材料变形行为和性能（弹性模量和屈服应力）的影响。研究结果表明,低应变阶段的应力应变分配系数与复合材料弹性模量之间存在确定的关系,预测的弹性模量与试验结果及Ｅｓｈｅｌｂｙ模型吻合得很好,屈服应力明显小于基体屈服强度。     

SiC颗粒对铝基合金摩擦磨损性能的影响

研究了ＳｉＣ颗粒增强铝基复合材料的摩擦磨损特性，结果表明：ＳｉＣ特性的加入提高了材料的耐磨性，并随ＳｉＣ粒子加入量的增加耐磨性增大     

Interface Stability of the SiC Particles/Fe Matrix Composite System

The interface reaction between the SiC particles （ SiCp ） and Fe was stndicd during sintering the SiCp reinforced Fe matrix composites at 1423 K for 1 h. In the composite having 3wt% （weight ratio） SiCp （the 3SiCp/ Fe composite）, the interface reaction products of Fe3 Si, the carbon precipitates, and Fe3 C or pearlite were generated. Fe3 Si coustructs the bright matrix of the reaction zone in the original situation of the SiCp. The carbon precipitates are randondy embedded in the reaction zone. Fe3 C or pearlite exists at the grain boundaries of the Fe matrix. As increasing the SiCp concentration in the SiCp/ Fe composite, the inteusity of the interface reaction between SiCp and Fe iacreases. After the 10SiCp/ Fe composite （ having 10wt .% SiCp ） sintered at 1423 K for 1 h, all of SiCp are decomposed, and replaced by the reaction zone composed of Fe3 Si and the carbon precipitates. No Fe3 C or pearlite was genertaed during the reaction. The effects of the techniques of oxidizing of SiCp , coating SiCp by interaction with the Cr powder, and alloying the Fe matrix by adding the Cr element on the interface stability of the SiCp/ Fe composite system were also investigated, respectitely. The oxide membrane and the coating layer on SiCp can inhibit the interface reaction between SiCp and Fe by isolating SiCp from the Fe matrix during sintering. The interface reaction does not occur in the 3 SiCp/ Fe- 10 Cr composite but in the 3 SiCp/ Fe-5 Cr composite. In the SiCp/ Fe-Cr alloy composites, the interface reaction between SiCp and the Fe- Cr alloys is weaker than that between SiCp and Fe . The Cr element behaves as a diluent, it causes a redaction in the interface reaction, which is proportional to the amount of the element added.