Al2O3/ZrB2/ZrO2复合陶瓷材料的制备与性能

将ZrB2和ZrO2添加入到Al2O3基体中,采用熟压法制备了Al2O3/ZrB2/ZrO2复合陶瓷材料,ZrB2和ZrO2的体积含量分别为(92.2±0.1)%和(7.8±0.1)%.对复合材料的硬度、断裂韧性和抗弯强度进行了测试和分析.结果表明:当ZrB2/ZrO2体积分数为20%时,所制备的复合陶瓷的综合力学性能最优,其相对密度,抗弯强度和断裂韧度分别达到96.3%,520.5MPa和6.1 MPa·m1/2.Al2O3/ZrB2/ZrO2复合陶瓷断面的断裂模式为沿晶断裂和穿晶断裂混合模式.通过高温氧化试验发现Al2O3/ZrB2/ZrO2复合材料在500～700℃时开始氧化.     

热压烧结TiB2-ZrB2固溶复合陶瓷的结构研究

以ZrB2作为掺加剂，通过热压烧结制备了TiB2-ZrB2固溶复合陶瓷。采用X射线衍射分析对材料的相组成，晶格常数和晶体结构进行了分析，材料的显微结构分别由EPMA，SEM和TEM测定。研究结果表明，随着ZrB2掺入量的增大，固溶产物的晶格常数会相应增加，当ZrB2的掺加量为8％（摩尔分数）时，产物的晶格常数出现极大值；ZrB2可以与TiB2形成部分固溶的固溶体，在复合材料中存在富Ti和富Zr的两种硼化物；由于固溶反应在界面上进行，有效地降低了烧结过程中的晶界移动速度，从而使材料的大晶粒细化。     

SiCp1/ZrB2超高温陶瓷的制备及性能

研究了碳化硅晶片(SiCp1)增韧二硼化锆(ZrB2)陶瓷的制备及其力学性能.采用热压烧结方法,在烧结温度1950℃、保温时间1h、压力20MPa、流动氩气气氛下,制备了高致密度的SiCp1/ZrB2复合材料.通过X射线衍射分析、扫描电子显微镜、三点弯曲法和单边切口梁法对SiCp1/ZrB2陶瓷复合材料的物相、显微结构和力学性能进行了研究,结果表明:随着SiCp1的加入,SiCp1/ZrB2复合材料的相对致密度和断裂韧性都得到了较大提高,当SiCp1添加量为15%(体积分数)时,相对致密度达到99%,断裂韧性达到(8.35±0.26)MPa·m1/2,抗弯强度达到(522±49)MPa.用轧膜法制备的SiCp1定向排列的SiCp1/ZrB2复合材料的力学性能略有下降.     

二硼化锆超高温陶瓷的强韧化EI北大核心CSCD

以ZrB2为基体材料,分别采用添加SiC颗粒(SiCp)、SiC晶须(SiCw)和SiC晶片(SiCpl)作为增韧相,采用热压烧结技术制备了SiC/ZrB2陶瓷基复合材料,分析了不同增韧相的种类和添加量对ZrB2陶瓷强韧化效果的影响,并通过层状结构设计,采用放电等离子体烧结工艺制备出ZrB2基层状复合陶瓷材料,研究了层状结构对ZrB2陶瓷强韧化效果的影响。结果表明:添加SiC颗粒、晶须或晶片,采用热压烧结可以制备出接近完全致密的SiC/ZrB2陶瓷基复合材料;与单独添加SiC颗粒或晶须相比,同时添加SiC颗粒和晶须的增韧效果更加明显,而SiC晶片也可以起到较好的强韧化效果;通过层状结构设计,能够较大幅度地提高ZrB2陶瓷的断裂韧性,显示了很好的增韧效果。     

ZrB2对Al2O3-ZrB2-SiC复相陶瓷室温力学性能影响

Al2O3陶瓷具有优异的室温和高温性能,但其脆性大,断裂韧性较低,限制了其应用.采用热压烧结工艺制备了应用于不同环境的Al2O3-ZrB2-SiC复相陶瓷(简称AZS),主要研究不同含量的ZrB2对Al2O3-SiC基陶瓷性能的影响.力学性能研究发现,当Al2O3陶瓷中ZrB2和SiC的体积百分比分别为20％和5％时,AZS3陶瓷具有最高的强度和韧性,分别为508.5MPa和6.65MPa· m1/2,相比纯氧化铝陶瓷的468.6MPa和5.56 MPa· m1/22提高了8.5％和19.6％.     

二硼化锆系复合材料研究进展

ZrB2系复合材料具有高熔点、高硬度、高导热率等优良性能，是一种性能优异的高温结构材料，具有广泛的应用前景。本文概述了ZrB2基复合材料．如：ZrB2-Ni，ZrB2-SiC，ZrB2／B4C-Ni等的研究现状，并对其力学性能进行了评价；总结了近年来国内外在ZrB2基复合材料烧结工艺方面的研究进展。     

ZrB2-SiC复合材料凝胶注模成型初探

研究了ZrB2-SiC复合材料的凝胶注模成型技术。着重讨论了分散剂、pH值、固相体积含量、有机单体等对ZrB2-SiC复合材料料浆的影响;分析了凝胶注模成型后,排胶前复合材料素坯断面的显微结构以及相对应的烧结体的显微结构。结果表明:当分散剂用量为8.74‰(质量分数),pH为10.8,有机单体含量为3.1%时,可制得固相体积含量为40%,粘度为610mPa.s的ZrB2-SiC复合浆料,此时烧结体的断面主要以穿晶断裂为主;凝胶注模成型的坯体内部的有机聚合物网络因高温而完全分解,使素坯的气孔分布较均匀,利于烧结体致密度的提高。     

Mo–Si–B对ZrB_2超高温陶瓷烧结工艺和性能的影响

针对ZrB2陶瓷材料的断裂韧性低及抗氧化性能差等问题,选择Mo粉、Si粉和B粉为第二相添加物,借助Mo–Si–B间的原位反应生成Mo5SiB2等三元或二元化合物与ZrB2复合,提高ZrB2陶瓷的断裂韧性与抗氧化性能。将混合粉体在1900℃、20MPa的条件下经热压烧结制备出致密的ZrB2陶瓷复合材料,所烧结样品的抗弯强度和断裂韧性随着Mo–Si–B含量的增加呈现先增加再降低再增加的趋势,当Mo–Si–B含量为20%(体积分数)时所得样品的断裂韧性最大,其值为(5.55±0.11)MPa·m1/2,当Mo–Si–B含量为30%时所得样品的抗弯强度最大,其值为(500±40)MPa。所烧结的样品都具有良好的抗氧化性能,其主要机理是在复合材料表面形成一定数量的玻璃相,阻止氧气向材料内部扩散。     

CaZrO3/ZrB2复合材料的无压烧结试验研究

CaZrO3与（0-30vol.%）ZrB2在常压下可以直接烧结。CaZrO3基质中引入ZrB2,降低了材料的相对密度,不利于材料的致密化烧结。但ZrB2的引入抑制了CaZrO3晶粒度的长大,提高了材料的抗折强度。通过显微结构观察,认为其强化机制是ZrB2颗粒的弥散强化作用。CaZrO3/ZrB2复合材料的显微结构特征为粒状堆积结构。     

Mo–Si–B对ZrB_2超高温陶瓷烧结工艺和性能的影响

针对ZrB2陶瓷材料的断裂韧性低及抗氧化性能差等问题,选择Mo粉、Si粉和B粉为第二相添加物,借助Mo–Si–B间的原位反应生成Mo5SiB2等三元或二元化合物与ZrB2复合,提高ZrB2陶瓷的断裂韧性与抗氧化性能。将混合粉体在1900℃、20MPa的条件下经热压烧结制备出致密的ZrB2陶瓷复合材料,所烧结样品的抗弯强度和断裂韧性随着Mo–Si–B含量的增加呈现先增加再降低再增加的趋势,当Mo–Si–B含量为20%(体积分数)时所得样品的断裂韧性最大,其值为(5.55±0.11)MPa·m1/2,当Mo–Si–B含量为30%时所得样品的抗弯强度最大,其值为(500±40)MPa。所烧结的样品都具有良好的抗氧化性能,其主要机理是在复合材料表面形成一定数量的玻璃相,阻止氧气向材料内部扩散。     

短切碳纤维含量对Csf/SiC复合材料力学性能的影响

以Si作为主要烧结助剂,采用热压烧结法制备了短切碳纤维-碳化硅(short carbon fiber reinforced SiC composite,Csf/SiC)复合材料.采用X射线衍射仪、扫描电镜、硬度仪以及力学性能试验机等,研究了Csf含量对所制备材料的结构、组成、形貌及复合材料的弯曲强度、Vickers硬度和断裂韧性的影响.结果表明:采用热压法能制备出致密且Csf分布均匀的Csf/SiC复合材料.Csf/SiC复合材料的弯曲强度随Csf含量增加先增大后减小,含15%(体积分数,下同)Csf的Csf/SiC样品强度最高,达到466MPa,并且Csf含量小于30%的Csf/SiC样品强度高于无纤维SiC材料.材料的Vickers硬度随Csf含量增加而降低.Csf/SiC样品的断裂韧性随Csf含量增加而逐渐增大,Csf含量为53%时,达到最大为5.5MPa·m1/2,与无纤维SiC样品相比,增加近2倍.     

纤维氧化处理对SiCsf/SiC复合材料力学性能的影响

以Y2O3、Al2O3为烧结助剂,采用无压烧结法制备短碳化硅纤维(2～4mm)增强碳化硅(ShortSiCfiberreinforcedSiCcomposite,SiCsf/SiC)复合材料,研究了纤维氧化处理对SiCsf/SiC复合材料结构及力学性能的影响。采用X射线衍射(XRD)、扫描电镜(SEM)以及力学性能试验机对材料进行结构表征和力学性能测试。结果表明:纤维氧化处理后,复合材料的弯曲强度和断裂韧性均有大幅提高。当纤维含量达到5wt%时,复合材料断裂韧性为5.41MPa.m1/2,与原始纤维增强SiC样品相比,提高了6.5%;与无纤维增强SiC样品相比,提高了27%。扫描电镜显示纤维氧化处理后,纤维与基体结合紧密。     

Determination of mechanical properties of Al2O3/Y-TZP ceramic composites: Influence of testing method and residual stresses

A series of Al₂O₃/Y₂O₃-stabilized zirconia (Y-TZP) ceramic composites with different zirconia contents (5 and 40 vol% Y-TZP) and fabricated by different green processing techniques (a novel tape casting and conventional slip casting) were studied. The microstructure and mechanical properties of the composites were investigated systematically, by means of scanning electron microscopy, Vickers indentation, depth-sensing nanoindentation, and single-edge laser-notched beam (SELNB) techniques. The indentation fracture method was found to be unsuitable for fracture toughness determination in this work. Reliable values of fracture toughness were obtained by the SELNB method with an almost atomically sharp laser-machined initial notch. The microstructure and mechanical properties of the ceramic composites mainly depended on the Y-TZP content. No significant differences were induced by the choice of green processing technique. The contribution of residual stresses to fracture toughness in Al₂O₃/Y-TZP ceramic composites was investigated. To this end, a theoretical model was applied to estimate the increase in fracture toughness due to the measured residual stresses in the samples. It was found that in this case, residual stresses were not the main factor responsible for the toughening in Al₂O₃/Y-TZP composites.     

无压烧结硼化锆基ZrB2-SiC复相陶瓷的结构与性能

以钇铝石榴石-YAG为烧结助剂,通过无压烧结制备了ZrB2-SiC复相陶瓷。研究了烧结助剂含量对烧结材料力学性能和显微结构的影响,材料的显微结构由扫描电镜SEM及其能谱分析EDS测定。研究结果表明,烧结助剂(YAG)和原料中的杂质形成玻璃相填充在晶界上,显著促进了硼化锆基ZrB2-SiC复相陶瓷的致密化。     

Fabrication and Properties of Ti3SiC2/SiC Composites

Ti3SiC2/SiC composites were fabricated by reactive hot pressing method. Effects of hot pressing temperature, the content and particle size of SiC on phase composition, densification, mechanical properties and behavior of stress-strain of the composites were investigated. The results showed that ： （ 1 ） Hot-pressing temperature influenced the phase composition of Ti3SiC2/SiC composites. The flexural strength and fracture toughness of composites increased with hot pressing temperature. （2） It became more difficult for the composites to densify when the content of SiC in composites increased. It need be sintered at higher temperature to get denser composite. The flexural strength and fracture toughness of composites increased when the content of SiC added in composites increased. However, when the content of SiC reached 50 wt%, the flexural strength and fracture toughness of composites decreased due to high content of pore in composites. （3） When the content of SiC was same, Ti3SiC2/SiC composites were denser while the particle size of SiC added in composites is 12. 8 μm compared with the composites that the particle size of SiC added is 3 μm. The flexural strength and fracture toughness of composites increased with the increase of particle size of SiC added in composites. （4） Ti3SiC2/SiC composites were non-brittle fracture at room temperature.     

基体改性对碳纤维增韧碳化硅复合材料结构与性能的影响

采用化学气相浸渗法对2D C/SiC复合材料进行基体改性,制备了二维碳纤维增韧碳-碳化硅二元基复合材料(two dimensional carbon fiber reinforced C-SiC binary matrix composites,2D C/C-SiC).2D C/C-SiC复合材料的基体为热解碳和碳化硅交替叠层的多层基体.研究了2D C/C-SiC复合材料的微观结构,比较了2DC/SiC复合材料和2DC/C-SiC复合材料的力学性能及断口形貌.结果表明:2DC/C-SiC复合材料可在基本保持2DC/SiC复合材料抗弯强度的基础上,其断裂韧性得到显著提高.基体改性的效果明显.纤维的逐级拔出是断裂韧性提高的原因.     

ZrB2-Al2O3复合粉体的自蔓延高温还原合成与表征

用自蔓延高温还原合成制备了ZrB2-Al2O3复合粉体。用X射线衍射仪、扫描电镜和透射电镜等分析测试手段,对所制得的复合粉体的相组成、相貌及微观组织进行了表征。结果表明：ZrB2和Al2O3以主晶相的形式存在于复合粉体之中,二者存在良好的界面结合,这主要与ZrB2在Al2O3颗粒表面结晶生长有关。     

Microstructure and mechanical properties of SiC platelet reinforced BaOAl2O32SiO2 (BAS) composites

BaOAl₂O₃2SiO₂ (BAS) glass–ceramic powders were prepared by sol–gel technique. SiC platelet reinforced BAS glass–ceramic matrix composites with high density and uniform microstructure were fabricated by hot-pressing. The effect of additional crystalline seeds on hexagonal to monoclinic phase transformation of Barium aluminosilicate was studied. The effects of SiC platelet content on the microstructure and mechanical properties of the composites were also investigated. The results showed that the flexural strength and fracture toughness of the BAS glass–ceramic matrix composites can be effectively improved by the addition of silicon carbide platelets. The main toughening mechanism was crack deflection, platelets' pull-out and bridging. The increased value of flexural strength is contributed to the load transition from the matrix to SiC platelets.     

Microstructure and Fracture Toughness of Hot-Pressed Zirconia-Toughened Sialon

Zirconia-toughened sialon composites have been fabricated using conventional hot-pressing techniques. The fracture toughness and microstructure were determined for CeO₂-and Y₂O₃-stabilized ZrO₂ additives and also as a function of volume percent ZrO₂. The yttria system showed a linear increase in fracture toughness with increasing volume fraction zirconia content while the ceria-stabilized system exhibited a peak in fracture toughness at 20 vol % ZrO₂ content. The fracture toughness at 800°C was measured and correlated with the microstructure. High-temperature stability was determined and it was found that the deleterious nitride phases of zirconium could be precluded from the microstructure.     

Mechanical and tribological properties of TiB2-SiC and TiB2-SiC-GNPs ceramic composites

TiB₂-SiC and TiB₂-SiC-graphene nanoplatelets (GNPs) composites were prepared using field-assisted sintering technology at 2100 °C in argon atmosphere, and the influence of the SiC and different GNPs addition on microstructure development, mechanical and tribological properties has been investigated. Instrumented hardness, bending strength, chevron-notched fracture toughness and ball-on-flat tribological tests were used for the testing and characterization of the composites. The addition of SiC significantly improved the bending strength and elastic modulus with values of 601 MPa and 474 GPa, respectively, but decreased the fracture toughness with a value of 4.8 MPa.m^1/2. The addition of GNPs has a positive effect on fracture toughness and flexural strength but a negative one on the hardness. The increasing amount of both GNPs has a positive influence on wear characteristics of the composites thanks to the described wear mechanisms.