TiC对C—B4C—SiC复合材料显微结构与性能的影响

本文就烧结助剂ＴｉＣ对Ｃ—Ｂ４Ｃ—ＳｉＣ炭／陶复合材料显微结构与性能的影响进行了研究，结果表明ＴｉＣ在烧结过程中发生了固相反应，在晶界生成了ＴｉＢ２，有效地促进了Ｃ—Ｂ４Ｃ—ＳｉＣ复合材料的烧结，抑制了晶粒的长大，使复合材料密度与强度大幅度地增加，电阻率下降；同时ＴｉＢ２在氧化时生成致密的ＴｉＯ２，包裹了易氧化的Ｂ４Ｃ和Ｃ，使制品难氧化，从而大大提高了制品的抗氧化性能。     

碳相含量对C—SiC—TiB2复合材料结构和力学性能的影响

研究了碳相含量对原位合成的碳／陶复合材料（Ｃ－ＳｉＣ－ＴｉＣ－ＴｉＢ２）的结构和性能的影响。结果表明：随着碳含量的增加,材料的抗弯强度下降。材料的烧结温度应随着碳含量增加相应的提高,才能获得致密的碳／陶复合材料     

C－B_4C－SiC复合材料抗氧化性能的研究

对碳／陶瓷复合材料（Ｃ－Ｂ＿４Ｃ－ＳｉＣ）的抗氧化性能进行了研究，结果表明：Ｃ－Ｂ＿４Ｃ－ＳｉＣ复合材料抗氧化性能比碳素材料大大提高，而且烧结助剂对Ｃ－Ｂ＿４Ｃ－ＳｉＣ复合材料的抗氧化性能影响很大。在复合材料中分别加入了Ａｌ，Ａｌ＿２Ｏ＿３，Ｎｉ，Ｔｉ，ＴｉＣ，Ｓｉ等不同烧结助剂，发现添加Ｎｉ的材料抗氧化性能最佳，经１０００℃氧化１５ｈ后，氧化度小于０．５％；加入Ｔｉ，Ｓｉ和ＴｉＣ的次之，不加烧结助剂的又次之，加入Ａｌ和Ａｌ＿２Ｏ＿３的最差。     

C—B4C—SiC复合材料抗氧化性能的研究

对碳／陶瓷复合材料（Ｃ－Ｂ４Ｃ－ＳｉＣ）的抗氧化性能进行了研究。结果表明：Ｃ－Ｂ４Ｃ－ＳｉＣ复合材料抗氧化性能比碳素材料大大提高，而且烧结助剂对Ｃ－Ｂ４ＣＳｉＣ复合材料的抗氧化性能影响很大。在复合材料中分别加入了Ａｌ，Ａｌ２Ｏ３，Ｎｉ，Ｔｉ，ＴｉＣ，Ｓｉ等不同烧结助剂，发现添加Ｎｉ的材料抗氧化性能最佳，经１０００℃氧化１５ｈ后，氧化度小于０．５％；加入Ｔｉ，Ｓｉ和ＴｉＣ的次之，不加烧结助剂的又次之     

B4C--SiC/C复合材料氧化过程的TG/DTA分析

制备了Ｂ_４Ｃ－ＳｉＣ／Ｃ复合材料,对不同组成的复合材料在２０１５００℃升温氧化过程进行了ＴＧ／ＤＴＡ（热重和差热联用）分析。结果表明,复合材料具有不同的高温抗氧化性能,此差异可归因于以下几方面：复合材料的组成不同（包括陶瓷粒子的种类、含量）,不同种类的陶瓷粒子氧化转变成陶瓷氧化物的温度、速率不同,生成的陶瓷氧化物在高温下的物性（对基体材料的润湿性、粘度及流动性、挥发性和对氧的扩散系数等）不同。通过在炭基体中弥散Ｂ４Ｃ粒子可明显提高炭基体在８５０℃以下的抗氧化性。当复合材料中Ｂ４Ｃ含量较高而ＳｉＣ含量低时,样品表面将趋于形成Ｂ２Ｏ３较为富集的硼硅酸玻璃相,在１５００℃以下具有良好的氧化防护效果;当样品中ＳｉＣ含量较高时,在高温下（＞１２００℃）,随着部分Ｂ２Ｏ３的挥发和大量ＳｉＯ２的生成,样品表面将趋于形成ＳｉＯ２较为富集的硼硅酸盐玻璃相,在高达１４００℃以上仍具有良好的氧化防护效果     

炭陶瓷复合材料中铝添加剂抗氧化机理

Ａｌ添加剂在热处理过程中生成Ａｌ４Ｃ３，和ＣＯ反应生成Ａｌ２Ｏ３．与复合材料氧化过程中生成的Ｂ２Ｏ３，ＳｉＯ２形成Ｂ２Ｏ３－ＳｉＯ２─Ａｌ２Ｏ３玻璃系薄膜，有效地抑制了炭陶瓷制品中碳的氧化。     

Si－C－O－N系统相稳定性及反应烧结制备原位SiC（p）复合ZAS材料

给制了Ｓｉ－Ｃ－Ｏ－Ｎ系统平衡状态下相稳定性与Ｎ２分压和Ｏ２分压以及相稳定性与Ｎ２分压和ＳｉＯ分压的关系图；以此为指导，将原位复合引入到反应烧结锆莫来石（ＺＡＳ）材料中，制备了含原位（ｉｎ－ｓｉｔｕ）ＳｉＣ（ｐ）的ＺｒＯ２ＳｉＣ（ｐ）、ＺｒＯ２－３Ａｌ２Ｏ３·ＺＳｉＯ２－ＳｉＣ（ｐ）－ＳｉＣ（ｐ）复合材料。研究了烧结温度、时间、碳添加量、成型压力等工艺因素对烧结ＺｒＳｉＯ４－Ｃ体系中原位ＳｉＣ生成量的影响，并观察了试样的显微结构。     

烧结温度对C—B4C—SiC复合材料显微结构与性能的影响

本文就烧结温度对Ｃ－Ｂ４Ｃ－ＳｉＣ炭／陶复合材料显微结构与性能影响进行了研究，发现复合材料密度、强度随烧结温度的升高而明显提高，电阻率随烧结温度的升高而下降，这和烧结体显微结构密切相关。     

炭／陶复合材料的研究

采用高温热压法，制备了炭／Ｂ．ｃ，炭／金属钛及炭／Ｂ４Ｃ／金属钛三种炭／陶复合材料。着重研究了Ｂ４Ｃ、Ｔｉ的掺杂量对复合材料抗氧化能力的影响。结果表明，随着掺杂量的增加，复合材料的抗氧化能力提高。其中Ｂ４Ｃ的影响更显著。且炭、Ｂ４Ｃ、Ｔｉ三组份炭陶复合材料的抗氧化性较双组份复合材料更好一些。     

SiCw增韧Al2O3／TiB2陶瓷复合材料的研究

根据对晶须与基体材料的热胀失配的分析，计算得出了Ａｌ２Ｏ３／ＴｉＢ２／ＳｉＣｗ三元复合材料中ＳｉＣｗ的临界体积分数。采用ＴｉＢ２颗粒增韧和ＳｉＣｗ增韧两种途径来改善Ａｌ２Ｏ３的脆性，得到此复合材料的抗弯强度为７４０ＭＰａ，断裂韧性为７．７ＭＰａ·ｍ＾１／２。分析表明：当ＳｉＣｗ含量大于临界体积分数时，强度大幅降低的主要原因是由于致密度的降低和热残余拉应力的增大。     

硅液相浸渍反应制备TiC/SiC和TiN/SiC复相陶瓷

以滤纸、酚醛树脂和氧化钛为原料,经过模压成型、固化、碳化及不同条件下渗硅制备了TiC/SiC和TiN/SiC复相陶瓷。通过X射线衍射和扫描电子显微镜研究了TiC/SiC和TiN/SiC复相陶瓷的微观结构和物相组成,测量了复相陶瓷的弯曲强度和断裂韧性。结果表明:真空条件下液态渗硅获得的TiC/SiC复相陶瓷具有多孔的微观结构,其弯曲强度和断裂韧性较小。氮气气氛下液态渗硅制备的TiN/SiC复相陶瓷结构致密,有较高的弯曲强度和断裂韧性。不同反应生成的TiC,TiN陶瓷颗粒对液态硅的润湿性不同,使得生成的复相陶瓷具有不同的微观结构。TiN/SiC复相陶瓷中TiN颗粒的引入,在基体与第二相颗粒间的界面上产生拉应力和压应力,使达到这一区域的裂纹偏转,从而获得增韧效果。     

Improved mechanical properties of reaction-bonded SiC through in-situ formation of Ti3SiC2

Reaction-bonded SiC is a ceramic with excellent thermal properties, good corrosion resistance and the characteristic of near-net-shape manufacturing. However, the poor fracture toughness of free Si limits the applications of reaction-bonded SiC. In this study, TiC was added to reaction-bonded SiC and reacted with free Si to form Ti₃SiC₂. The effects of TiC and carbon black on the mechanical properties of reaction-bonded SiC were investigated. The results demonstrated that the in-situ formation of Ti₃SiC₂ and decrease in the content and size of free Si improved the mechanical properties of reaction-bonded SiC ceramics. The mechanical properties of TiC-added reaction-bonded SiC with 17.5 wt% carbon black were superior to those of TiC-added reaction-bonded SiC with 15 wt% carbon black. Moreover, increasing the TiC content of reaction-bonded SiC with 17.5 wt% carbon black from 0 to 7.5 wt% caused an increase in its bending strength from 183.92 to 424.43 MPa and an increase in fracture toughness from 3.7 to 5.24 MPa m^1/2.     

碳纤维增强碳复合材料表面多层复合涂层中SiC和TiC内层的比较(英文)

采用包埋法制备了碳纤维增强碳(carbon fiber reinforced carb on composites,C/C)复合材料表面多层涂层,包括SiC,TiC内层,SiC,TiC中间层以及SiC+TiC复合外层。利用场发射扫描电镜和X射线衍射对其表面和断面的结构进行研究。结果显示:和TiC内层相比较,SiC内层较厚而且致密,具多孔结构且和C/C复合材料结合紧密;TiC内层较薄且和C/C复合材料结合松散。制备的SiC+TiC复合外层由SiC,TiC和Ti3SiC2组成。     

Properties of (Y)ZrO2–Al2O3 and (Y)ZrO2–Al2O3–(Ti or Si)C Composites

The effect of Al₂O₃ and (Ti or Si)C additions on various properties of a (Y)TZP (yttria-stabilized tetragonal zirconia polycrystal)–Al₂O₃–(Ti or Si)C ternary composite ceramic were investigated for developing a zirconia-based ceramic stronger than SiC at high temperatures. Adding Al₂O₃ to (Y)TZP improved transverse rupture strength and hardness but decreased fracture toughness. This binary composite ceramic revealed a rapid loss of strength with increasing temperature. Adding TiC to the binary ceramic suppressed the decrease in strength at temperatures above 1573 K. The residual tensile stress induced by the differential thermal expansion between ZrO₂ and TiC therefore must have inhibited the t - → m -ZrO₂ martensitic transformation. It was concluded that a continuous skeleton of TiC prevented grain-boundary sliding between ZrO₂ and Al₂O₃. In contrast, for the ternary material containing β-SiC in place of TiC, the strength decreased substantially with increasing temperature because of incomplete formation of the SiC skeleton.     

Microstructure and mechanical properties of in situ produced SiC/TiSi2 nanocomposites

The microstructure and mechanical properties of in situ produced SiC/TiSi₂ nanocomposites have been studied. The results indicate that SiC/TiSi₂ composites can be fabricated by reactively hot pressing mixed powders of TiC, elemental Si and elemental Ti. The in situ produced SiC particles are close to nanosize. Without elemental Ti powder, the composite obtained consists of TiSi₂ 66 vol% and SiC 34 vol% without residual Si or TiC. At ambient temperature, the highest bending strength of SiC/TiSi₂ composites was 400 MPa, twice that of monolithic TiSi₂. Also fracture toughness of SiC/TiSi₂ composites exceeds that of pure TiSi₂. At 1200°C, the yield strength of composites was improved due to the presence of the SiC particles.     

先驱体浸渗裂解法制备C/C-SiC复合材料的烧蚀性能

用先驱体浸渗裂解法制备了碳纤维增强碳(carbon fiber reinforced carbon,C/C)-SiC复合材料,用H2-D2火焰法检测其烧蚀性能.结果表明:C/C-SiC复合材料的烧蚀率随复合材料中的Si含量的增加而呈下降趋势;经过5次浸渍,C/C-SiC复合材料的密度从1.46 g/cm3增加到1.75 g/cm3,Si含量从5.06%增加到13.8%,线烧蚀率和质量烧蚀率分别下降474%和34.5%.密度为1.75g/cm3的C/C-SiC复合材料,其线烧蚀率和质量烧蚀率分别为2.22 μm/s和1.289 mg/s,其线烧蚀率和质量烧蚀率分别为密度1.78 g/cm3的C/C复合材料的21.7%和78.6%.基体中SiC的引入明显提高了C/C复合材料的抗氧化烧蚀性能.     

Tough and wear-resistant carbon fiber reinforced TiC-based composite prepared by alloyed melt infiltration at low temperatures

To improve the toughness and friction properties of carbon fiber reinforced ceramic matrix composite, a Cu alloy modified carbon fiber reinforced TiC based ceramic matrix composite was designed and prepared by TiCu alloy melt infiltration at low temperatures up to 1100 °C. The as-produced composite was mainly composed of carbon, TiC, Ti₃Cu₄, TiCu₄ and Cu phases. Due to the ductile Cu alloy introduced into the matrix, the composite showed good mechanical performance especially the fracture toughness. The flexural strength reached about 248.36 MPa while the fracture toughness was up to 15.78 MPa·m^1/2. The high toughness of the composite was mainly attributed to the fiber bridging, fiber pull-out, interface debonding, crack propagation and deflection. The tribological performance of the as-produced composite was measured using SiC and 440C stainless steel balls as counterparts, respectively. The as-prepared composite exhibited good wear resistance and the wear mechanism was discussed based on the microstructural observations.     

真空原位合成SiC-TiC复合粉末及其氧化性能研究

以碳化硅、二氧化钛和炭黑为原料,在真空条件下原位合成SiC-TiC复合粉末。采用XRD、SEM等测试手段对合成SiC-TiC复合粉末的物相组成和显微形貌进行表征,同时对合成的粉末样品的氧化性能进行探讨。实验结果表明:在本实验条件下,SiC-TiC复合粉末适宜的合成条件为在1350℃保温1h。在SiC粉末中原位生成的TiC,以粒径为0.1～0.2μm左右的小颗粒存在。SiC-TiC复合粉末在氧化过程中,在较低温度下TiC优先氧化生成TiO2,在较高温度下(1100℃左右)SiC才开始氧化生成SiO2。     

Ultra-high-temperature ablation behavior of SiC–ZrC–TiC modified carbon/carbon composites fabricated via reactive melt infiltration

To improve the ablation resistance under the ultra-high temperature, the matrix of the carbon/carbon (C/C) composite was modified with a ternary ceramic of SiC–ZrC–TiC via reactive melt infiltration. The obtained ceramic matrix was composed of Zr-rich and Ti-rich solid solution phases of Zr_1−xTi_xC and SiC. This composite exhibited an excellent ablation property at 2500 °C with low mass and linear ablation rates of 0.008 mg s⁻¹ cm⁻² and 0.000 μm s⁻¹, respectively. The ablation mechanism was revealed with various microstructure characterizations and compared with those of C/C–SiC and C/C–TiC composites. Results showed that the degradations of these composites were primarily caused by the loss of the protective oxide scale via volatilization under the ultra-high temperature and flushing by high-speed airflow. The high ablation resistance of the C/C–SiC–ZrC–TiC composite was attributed to the protection of a multiphase oxide scale with high viscosity and low volatility.     

原位合成板晶增强复相陶瓷

首次通过ＴｉＨ２、ｓＩ,ｂｎ,Ｂ４Ｃ和Ｃ之间的原位化学反应采用反应热压工艺制备出了ＴｉＢ２板晶或ＳｉＣ板晶增强复相陶瓷,初步探讨了影响板晶生长的各种因素。通过原位化学反应热压制备出的复相陶瓷具有较满意的力学性能。