纸制备SiC/Si层状陶瓷复合材料的微观结构和性能

本文以纸为原料,通过叠层设计、低温碳化和高温渗硅制备了具有层状结构特征的SiC/Si陶瓷复合材料。并采用XRD、SEM和三点弯曲等分析测试手段对其相组成、微观结构和力学性能进行了分析。结果表明:纸碳化后为非晶形的碳;渗硅后试样的相组成为β-SiC相、自由Si相和残C相。叠层纸碳化后的微观结构为含有大量扁长空洞的碳骨架,渗硅后得到的SiC陶瓷复合材料具有明显的层状结构特征。三点弯曲实验表明,SiC/Si陶瓷复合材料的强度高达290MPa,达到了常规反应烧结SiC陶瓷的强度水平;且其断裂方式为非灾难性断裂,分析认为这与材料的层状结构形貌有关。     

层状陶瓷复合材料制备技术的研究进展

论述了层状陶瓷复合材料的性能特点以及这种材料的发展现状，从基体及夹层材料的类型选择和匹配、结构及界面的设计、工艺参数的选取、料浆制备、薄层预制、复合成形、排胶烧结等方面介绍了当前层状陶瓷制备工艺技术的研究进展；从性能及结构优化等方面探讨了在复合材料发展中目前存在的不足，指出了进一步研究应该解决的问题和未来的发展前景。     

SiC/β-Sialon装甲陶瓷的制备及性能

采用无压烧结工艺制备高比强度SiC/β-sialon复相陶瓷。研究了原料组成和第一阶段反应温度对合成β-sialon相的影响,分析了氧化物添加剂和第二阶段烧结温度对材料烧结性能和力学性能的影响。利用X射线衍射仪、扫描电子显微镜以及万能试验机表征样品的物相组成、微观结构和力学性能。结果表明：用10%（质量分数,下同）的苏州土部分替代Al2O3和SiO2能有效促进β-sialon相的生成,在1500℃保温2h合成出无杂相的β-sialon相;复合添加5%ZrO2和5%Y2O3可促进样品的烧结致密化。当温度为1650℃时,样品的体积密度为2.90g/cm3,抗弯强度和断裂韧性分别达到375MPa和3.24（MPa·m1/2）,弯曲比强度为1.29×105（N·m）/kg,比Al2O3提高了40%以上。     

层状氮化硅陶瓷的性能与结构

从结构设计的角度出发研究了层状复合Ｓｉ３Ｎ４陶瓷材料，利用轧膜使层内的晶粒，晶须产生定向增韧，通过调整外部层状复合结构得到材料的两级增韧效果，并实验制备了高韧性层状复合Ｓｉ３Ｎ４基陶瓷材料。     

Ti3SiC2陶瓷的制备及性能研究

层状陶瓷材料Ti，SiC2结合了金属和陶瓷的许多优异性质，既具有与金属相似的良好的导热、导电性，良好的可加工性，相对柔软，抗热震性好，可塑性变形等性能，同时又具有与陶瓷相似的抗氧化、耐腐蚀、耐高温等特性；并且还有很好的自润滑性和超低磨擦系数，被认为在许多领域有着广泛的应用前景。     

高可靠性层状复合陶瓷的制备

层状复合陶瓷具有显著的增韧增强效果,其成型工艺具有许多独特的工艺特性,是整个制备技术的关键。本文着重评述了层状复合陶瓷的成型制备技术。     

SiC/W层状复合材料的制备工艺与力学性能

研究了ＳｉＣ陶瓷片为基体层,金属Ｗ（界面层）为软层的仿生层状复合材料的制备及性能。采用凝胶铸（Ｇｅｌ－ｃａｓｔｉｎｇ）方法制备ＳｉＣ陶瓷层,采用喷涂的方法制备金属层,确定了金属喷涂的最佳工艺条件。研究了不同金属层层状复合材料力学性能的影响。并对层状复合材料的成分和微观结构进行分析。     

水基冷冻干燥工艺制备层状结构多孔SiC陶瓷

以微米级SiC粉体为原料,利用冷冻干燥和原位反应烧结制备了具有层状孔道结构的SiC多孔陶瓷.XRD分析表明多孔陶瓷的主相是α-SiC,结合相是方石英;SEM观察到多孔陶瓷具有相互连通的开孔结构;多孔SiC陶瓷的总孔隙率和开孔隙率随固相含量和烧结温度的增加而下降.多孔陶瓷的孔径分布呈现双峰分布特点,大孔孔径峰值介于20～80 μm,小孔孔径峰值为0.5～0.9 μm.在原位反应烧结过程中,在1100℃以上SiC开始发生氧化形成SiO2结合的多孔SiC陶瓷,显著提高了陶瓷的压缩强度.随着烧结温度从1000℃提高到1500℃,固相含量为30vol%的多孔SiC陶瓷开孔率从68.9%下降到61.8%,压缩强度由5.5 MPa升至25.5 MPa.     

层状复合陶瓷制备技术与界面特性

本文综合评述了层状复合陶瓷研究现状，分析了层状复合陶瓷的制备工艺和界面结合情况以及界对对层状复合陶瓷性能的影响。     

陶瓷器的抗冲击性能

一、前言 陶瓷器的抗冲击强度和抗磕碰性能是陶瓷制品的主要指标之一,随着科学技术的发展,机械化供餐、蒸洗消毒设备广泛应用,人们对陶瓷制品的抗冲击强度和磕碰性能提出了更高的要求。陶瓷器的抗冲击强度不仅取决于材料的性能和坯釉的结合状态,而且和制     

陶瓷制件层合速凝快速成型技术研究进展

着重介绍了层合速凝快速成型技术的原理及应用于陶瓷制件制造的研究现状,比较分析了其优缺点,并对今后该技术的发展作了展望.     

基于冻结浆料的分层实体制造法加工陶瓷坯体

提出了一种新型陶瓷增材制造方法,浆料由陶瓷粉末、有机粘结剂和去离子水构成,单层生坯的加工过程包括:铺料、冷冻和激光扫描,层层累积成型后,将冻结状态坯体置于冷冻干燥机中干燥,得到陶瓷生坯;分析了激光加工参数和浆料固含量对于激光扫描过程的影响.结果表明:采用激光扫描图形轮廓的方式,避免了激光辐照对材料内部结构的破坏;通过与冷冻干燥技术的结合,充分保留了片层状的孔隙结构;随着激光能量密度的增大,激光扫描线的宽度和激光切割的深度增大;随着浆料固含量的增加,受陶瓷颗粒对激光能量产生散射作用的影响,激光的切割深度减小.     

Fabrication and performance of mini SiC/SiC composites with an electrophoresis-deposited BN fiber/matrix interphase

The feasibility of fabricating a BN matrix/fiber interphase of SiC/SiC composites via electrophoresis deposition (EPD) was investigated based on the simplicity and non-destructiveness of the process and the excellent interfacial modification effects of BN. The BN suspension and SiC fiber surface properties were both adjusted to generate suitable conditions for the EPD process of the BN interphase. Next, the deposition dynamics and mechanism were studied under different deposition voltages and time, and the relationship between the deposition morphology of the BN interphase and mechanical properties of the fabricated mini SiC/SiC composites were also discussed. After oxidation at high temperature (600–1000 ℃), the mechanical properties of the mini SiC/SiC composites were studied to verify the oxidation resistance effect of the EPD-deposited BN interphase, whose oxidation resistance mechanism was briefly analyzed as well.     

Insights into internal oxidation of SiC/BN/SiC composites

The article presents new observations of the physical manifestations of internal oxidation and volatilization in SiC/BN/SiC composites. The observations are made on both unbroken and broken minicomposite specimens before and after 12 h exposures at 1000°C in dry air with 10 ppm water vapor. The observations are enabled by a sample preparation method involving ion-mill sectioning and polishing. Complementary analyses of volatilization and closure of resulting gaps are also presented. The observations show that BN is generally consumed in two stages: (i) through reaction with oxygen along the interfaces with both the fiber and the matrix, producing two concentric annular pockets of borosilicate glass and an intervening annulus of progressively thinning BN; and (ii) subsequent volatilization, through the reaction of boria with trace amounts of water vapor in the environment to form borohydroxide gases. The spatial extent to which these processes proceed is governed by a competition between the outward diffusion of reaction gases through both matrix cracks and interface gaps produced by boria volatilization, and the formation of oxides on the newly exposed surfaces of fibers, matrix, and coating.     

含有压电陶瓷颗粒的结构陶瓷基复合材料的制备与性能

为了研究压电陶瓷颗粒对结构陶瓷力学性能的影响,把不同的压电陶瓷 颗粒加入到Al2O3结构陶瓷,发现LiTaO3与Al2O3在烧结时能稳定共存,烧结温度高于1400℃时,LiTaO3发生化,冷却后呈网状分布在AlO3基体晶界;低于1400℃烧结,LiTaO3颗粒弥散分布在Al2O3基体中,采用200MPa冷等静压成型,1300℃（保温3小时）空气气氛下无压烧结,最后于1300℃,150MPa（保温保压1h)氩气气氛下热等静压制备了LiTaO3/Al2O3陶瓷复合材料,对其显微结构与力学性能进行了研究,结果表明,LiTaO3体积分数为5％的陶瓷复合材料具有最高的抗弯强度与断裂韧性值,分别达到438．7MPa和5．4MPa.m^1/2,电畴运动和／或压电 应引起的能量耗散是一种新的陶瓷强韧化机制。     

Mode I Fracture Resistance of a Laminated Fiber-Reinforced Ceramic

The mode I fracture resistance of a ceramic matrix composite has been measured. Simultaneous observations have revealed that the resistance is dominated by frictional dissipation upon the pullout of fibers that fracture in the crack wake off the crack plane. Numerical and analytical crack growth simulations have been compared with the experimental results. One important feature in this comparison concerns the occurrence of large-scale bridging. With these effects taken into account, the simulations and the experiments are found to be in good correspondence for acceptable magnitudes of the interface sliding stress.     

Short SiC fiber/Ti3SiC2 MAX phase composites: Fabrication and creep evaluation

The compressive creep of silicon carbide fiber reinforced Ti₃SiC₂ MAX phase with both fine and coarse microstructure was investigated in the temperature range of 1000-1300°C. Comparison of only steady-state creep was done to understand the response of fabricated composite materials toward creep deformation. It was demonstrated that the fibers are more effective in reducing the creep rates for the coarse microstructure by an increase in activation energy compared to the variant with a finer microstructure, being partly a result of the enhanced creep rates for the microstructure with larger grain size. Grain boundary sliding along with fiber fracture appears to be the main creep mechanism for most of the tested temperature range. However, there are indications for a changed creep mechanism for the fine microstructure for the lowest testing temperature. Local pores are formed to accommodate differences in strain related to creeping matrix and predominantly elastically deformed fibers during creep. Microstructural analysis was done on the material before and after creep to understand the deformation mechanics.     

Multiple ballistic damage of segmented SiC/BN laminated ceramic composite armor

This article investigated the structure of the laminated ceramics to improve the multiple ballistic performance of segmented ceramic composite armors. The multiple ballistic experiments were conducted with 5.8 mm caliber steel core bullets at the impact velocity of about 920 m/s. The experiments verified that two laminated SiC/BN structures (GLC and ULC) exhibit higher residual ballistic performances than the monolithic SiC structure (MC). Moreover, through damage evolution analysis, two laminated SiC/BN structures (GLC and ULC) exhibit less sensitivity to the multiple ballistic impacts damages, and possess more energy absorption mechanisms than the monolithic ceramics. The structure design of the laminated of ceramics is beneficial for improving the multiple ballistic performances of composite armors and reducing the crater deformation.     

连续碳化硅纤维增强碳化硅陶瓷基复合材料研究进展

碳化硅纤维增强碳化硅陶瓷基(SiC/SiC)复合材料具有轻质、耐高温、抗氧化的优异特性,在航空领域,如航空发动机的热端构件、高温结构功能一体化构件,航天及空天飞行器热防护结构部件、动力系统热端部件等领域具有广泛的应用前景,受到美国、欧洲、日本等国研究人员的广泛关注。本文从组成、制备工艺、加工工艺和考核应用等方面,综述了SiC/SiC复合材料的国内外研究进展,并指出了目前面临的问题和机遇。     

陶瓷复合装甲材料的研究和发展

陶瓷复合装甲由于在防护领域的应用背景而引起人们的广泛关注,本文综述了陶瓷复合装甲材料的研究和发展方向.