SiCf/Ti-6Al-4V复合材料界面反应动力学

SiC纤维增强Ti基复合材料（SiCf／Ti）容易发生界面反应，从而影响其力学性能。开展界面反应和动力学的研究，对于SiCdTi复合材料的制备和服役具有指导意义。采用扫描电镜、透射电镜和X射线衍射分析了SICf／Ti-6Al—4V复合材料的界面反应及其动力学，发现SiC纤维的C涂层与Ti-6Al—4V反应形成粗晶粒的和细晶粒的TiC，长期高温热处理使得界面反应加剧，TiC层加厚，当C涂层完全消耗后，界面反应层中除了TiC外，还出现了Ti3SiC2。研究表明，界面反应层的加厚受元素扩散控制，服从抛物线规律，求出的动力学参数Q为268．8kJ／mol，k为0．0057m/s1/2。     

SiCf/Ti-43Al-9V复合材料的界面反应

利用纤维涂层法和真空热压工艺制备SiC纤维增强γ-TiAl金属间化合物(Ti-43Al-9V)复合材料,采用扫描电镜(SEM)、能谱(EDS)、X射线衍射(XRD)仪等研究复合材料的界面反应产物和界面反应产物的生长动力学。结果发现,SiCf/Ti-43Al-9V复合材料的界面反应生成了TiC、Ti2AlC和Ti5Si3,分三层分布。从SiC纤维到Ti-43Al-9V基体,界面反应产物序列为:TiC/Ti2AlC/Ti5Si3+Ti2AlC(颗粒)。界面反应产物的生长受扩散控制并遵循抛物线生长规律,其生长激活能Q和指前因子k0分别为190kJ/mol和2.5×10-5m.s-1/2。与其它Ti合金基的复合材料相比,γ-TiAl基复合材料的界面热稳定性更好。     

SiC_f/Ti6Al4V/Cu复合材料的界面行为及力学性能

采用箔-纤维-箔法制备SiC_f/Ti6Al4V/Cu复合材料,研究Ti6Al4V在连续SiC纤维增强Cu基复合材料中作界面改性涂层时的界面反应结合特征.利用光学显微镜、扫描电镜和能谱仪分析复合材料显微组织、断口形貌以及SiC_f/Ti6Al4V界面和Ti6A14WCu界面的反应扩散特征.结果表明:该复合材料的抗拉强度并没有显著提高;SiC_f/Ti6Al4V界面反应非常微弱;而Ti6Al4V/Cu界面反应非常明显,主要是Ti原子与Cu原子之间的反应,反应层厚度约为20 μm;反应产物主要呈4层分布,分别为CuTi_2、CuTi、Cu_4Ti_3和Cu_4Ti.     

SiCf增强Ti-48Al-1.5Mn复合材料的界面反应

利用透射电子显微镜（TEM）对SiC纤维（SiCf)增强Ti-48Al-1.5Mn复合材料的界面区域进行了分析。结果表明，在材料的复合过程中，SiCf与γ－TiAl基体之间发生了化学反应，形成了TiC1-x,Ti5Si3和Ti2AlC等一系列产物，并对这些产物的形成机制进行了分析。在高温条件下，C，Si原子从纤维向基体扩散和Ti,Al,Mn等原子从基体向纤维扩散，发生了界面反应。     

SiCf/Ti-6Al-4V复合材料的界面研究

采用扫描电镜、透射电镜和X射线衍射仪研究了用中国制备SiC纤维增强的Ti-6Al-4V复合材料的界面反应,发现在SiC纤维的C涂层和Ti-6Al-4V基体之间形成的界面反应产物为细晶粒和粗晶粒的TiC,而无C涂层的SiCf/Ti-6Al-4V的界面反应产物,从SiC纤维到Ti-6Al-4V基体,依次为细晶粒的TiC+Ti5Si3、粗晶粒的TiC和Ti3SiC2.还测量了界面反应区厚度并讨论了界面反应机理.     

连续SiC纤维增强钛基复合材料界面反应研究

针对连续SiC纤维增强钛基复合材料界面反应速率、反应产物进行了研究.采用基体-纤维涂覆法和热等静压工艺,制备了连续W芯SiC纤维增强TC17复合材料.对复合材料进行不同温度、不同时间热暴露,通过SEM、TEM、EDS,表征分析了界面反应层厚度、界面处化学成分及界面反应产物类型.结果表明:C涂层能有效保护SiC纤维;界面反应层处的主要元素为Ti和C;制备状态试样的界面反应产物为TiC1-x,靠近C涂层的TiC1-x晶粒较细小,靠近基体TiC1-x晶粒较粗大;高温热暴露使界面反应加剧,反应层厚度增加,反应层的生长符合抛物线规律,反应的动力学参数为频率因子k0=1.33×10-3m·s-1/2,反应激活能Q=243.22 kJ·mol-1.     

SiC纤维增强钛基复合材料的界面反应

采用真空热压工艺制备了界面结合良好的SiC纤维增强钛基复合材料,并对其界面和SiC纤维进行了透射电镜分析.结果表明,针状β-SiC晶粒沿纤维径向生长,呈辐射状分布;在复合材料的热压制备过程中,Si和C由SiC纤维向钛基体扩散,Ti则向SiC纤维扩散,形成了TiC和Ti5Si3等产物.     

SiC/Ti-6Al-4V复合材料界面反应的扫描电镜分析

采用扫描电镜分析了国产SiC纤维增强Ti-6Al-4V复合材料的界面反应,发现不带C涂层的SiC纤维与Ti-6Al-4V反应形成TiC和钛的硅化物,带有C涂层的SiC纤维与Ti-6Al-4V反应仅形成TiC。观察表明C涂层的厚度差别较大。     

SiC/Ti基复合材料界面反应的研究现状及发展趋势

综述了SiC连续纤维增强Ti基复合材料界面反应现状和存在的问题，介绍了本课题组在TMC面反应研究上的最新进展，预测了TMC界面反应研究的趋势。     

SiCf/Ti65复合材料界面反应与基体相变机理

采用磁控溅射先驱丝法并结合热等静压技术制备了SiC_f/Ti65复合材料,对其在650、750、800和900℃进行了长时间热暴露实验。结果表明,热等静压和热暴露过程中,SiC_f/Ti65复合材料内部各元素同时参与界面互扩散和基体相变扩散。热等静压后,SiC_f/Ti65复合材料界面反应层产物主要为TiC,基体中相变产物为等轴的(Zr, Nb)_5Si_4。热暴露过程中,界面反应逐渐生成了Ti_5Si_3和(Zr, Nb)_5Si_4,基体相变则有了Ti_3(Al, Sn)C和TiC生成。SiC_f/Ti65复合材料反应层长大激活能为93 kJ/mol,该材料界面可以在650℃及以下温度长时间保持稳定。     

Chemical kinetic studies on interfacial reaction in SCS-6 SiC/Ti matrix composites

Interfacial reaction and its mechanism of SiC/Ti composite were revealed by chemical kinetic studies. A two-step dynamic model of interfacial reaction in SCS-6 SiC/Ti composites was built up, and the rate constant and the activation energy of the interfacial reactions were obtained based on the quantum chemistry calculation. The results show that the first step, in which the atomic Ti, C and Si are decomposed from Ti matrix and SiC fiber, respectively, is a rate-determined step because the activation energy of the step is much larger than that of the second one in which deferent interfacial reaction products form. The theoretically predicted result of the interfacial reaction is coincident with that of experimental observation.     

Process study, microstructure, and matrix cracking of SiC fiber reinforced MoSi2 based composites

SiC fiber reinforced SiAlON-MoSi₂ composites have been manufactured by a concurrent fiber winding and low pressure plasma spraying (LPPS) technique to produce a multilayer, circumferentially fiber reinforced composite ring. The LPPS parameters for SiAlON-MoSi₂ powder were optimized by a two-level experimental design approach followed by further optimization, which provided a smooth sprayed surface, low matrix porosity, and high deposition efficiency. The microstructure of SiAlON-MoSi₂ matrix consisted of a lamellar structure built up of individual splats and a uniform distribution of discontinuous SiAlON splats throughout the MoSi₂ matrix. The spray/wind composites exhibited 2% porosity and well-controlled fiber distribution. High temperature consolidation led to the formation of a thick reaction zone at the fiber-matrix interface by a chemical reaction between C coating and MoSi₂. Matrix cracking occurred in SiC _f (15 vol.%)/MoSi₂ after cooling from 1500 to 25 °C and was attributed to the large tensile residual stresses in the matrix developed on cooling because of coefficient of thermal expansion (CTE) mismatch between matrix and fiber. The addition of 40 vol.% SiAlON into the MoSi₂ effectively eliminated the matrix cracking by reducing the matrix-fiber CTE mismatch. Predictions of matrix cracking stress on the basis of residual stresses in the composites showed that the maximum permissible fiber volume fraction to avoid matrix cracking was 6% for SiC _f /MoSi₂ and 23% for SiC _f /SiAlON(40 vol.%)-MoSi₂.     

SiC界面涂层对碳纤维针刺毡增强Al2O3复合材料力学性能的影响(英文)

分别采用3D碳纤维针刺毡为增强体以及聚碳硅烷(PCS)衍生SiC涂层为界面相,通过溶胶-浸渍-干燥-热处理(SIDH)技术制备C/Al₂O₃复合材料,研究SiC界面涂层对C/Al₂O₃复合材料力学性能、抗氧化性能和抗热震性能的影响。结果表明,C/Al₂O₃复合材料的断裂韧性显著优于Al₂O₃单体陶瓷,引入SiC界面涂层后,尽管断裂功有一定程度下降,但C/Al₂O₃复合材料的强度得到明显提高;得益于SiC涂层和C纤维之间的强结合,C/SiC/Al₂O₃复合材料在静态空气中表现出明显优于C/Al₂O₃复合材料的抗氧化和抗热震性能。     

Effects of SiC volume fraction and aluminum particulate size on interfacial reactions in SiC nanoparticulate reinforced aluminum matrix composites

The SiC nanoparticulate reinforced Al-3.0 wt.% Mg composites were fabricated by combining pressureless infiltration with ball-milling and cold-pressing technology at 700 °C for 2 h. The effects of SiC nanoparticulate volume fractions (6%, 10% and 14%) and Al particulate sizes (38 μm and 74 μm) on interfacial reactions were investigated by SEM, TEM and X-ray diffraction. The results show that the MgO at the interface between SiC nanoparticulate and molten Al can provide a barrier for the diffusion of Si, C and Al. Using Al particulate (74 μm) as raw material, the Al₄C₃ phase was not found in the composites containing 6 vol.% and 10 vol.% SiC, but presented in the composites containing 14 vol.% SiC. When SiC content up to 14 vol.%, the products of MgO around SiC nanoparticulate are not enough to provide effective protection from the reaction between SiC and molten Al, therefore the diffusion of Si, C and Al can take place to produce Al₄C₃ and Si phases. Using 38 μm Al particulate as raw material, the fine Al particulate possesses the high reaction activity and can easily be embedded into the gap among the big Mg particulate segregated at the interface, resulting in the appearance of exposure surface of SiCp to the Al and the forming of diffusion channels for the atomics C, Si and Al. So, the formations of Al₄C₃ and Si phases were occurred.     

Corrosion behavior of SiC reinforced magnesium composites

The corrosion behavior of two SiC reinforced Mg-based metal matrix composites, Mg-6SiC and Mg-16SiC (in volume percent), has been studied in freely aerated 1 M NaCl solution and compared with that of pure Mg. The presence of SiC particles deteriorated the corrosion resistance of magnesium. Corrosion resistance decreased with increasing SiC volume fraction. The galvanic corrosion current density between pure SiC and pure Mg has been experimentally measured using zero resistance ammeter technique and theoretically determined using mixed potential theory. Galvanic corrosion between Mg matrix and SiC reinforcement in the composites did not contribute significantly to the overall corrosion rate. Electrochemical impedance spectroscopy indicated that the higher corrosion rates for the composites could be related to the defective nature of surface film.     

纤维及颗粒增强Al/Ti叠层复合材料制备方法和性能研究

Al/Ti叠层复合材料具有低密度、高比强度、高比刚度和高抗冲击性的优异性能,是一种理想的轻质高强材料,但是金属间化合物Al3Ti的脆性限制了其实际应用。通过复合纤维、陶瓷颗粒可以降低Al3Ti的脆性,提高Al/Ti叠层复合材料的强度和韧性,使其在航空航天、武器装甲等领域具有广阔的应用前景。本文简述了部分典型纤维、陶瓷颗粒增强Al/Ti叠层复合材料的制备方法,比较了不同材料和制备方法的优缺点。提出了碳化硼(B4C)增强Al/Ti叠层复合材料的可行方法,并采用真空热压法制备了0.2 mm厚的B4C薄片强化的Al/Ti叠层复合材料,该方法通过B4C薄片直接承载吸能和形成硬度梯度诱导裂纹偏转的方式强化基体,使其冲击韧性达到89 J/cm2,抗弯强度可达756 MPa,相较基体分别提高51%和38%。     

A new fracture mechanics model for multiple matrix cracks of SiC fiber reinforced brittle-matrix composites

A new model is proposed for multiple matrix cracking in order to take into account the role of matrix-rich regions in the cross section in initiating crack growth. The model is used to predict the matrix cracking stress and the total number of matrix cracks. The model converts the matrix-rich regions into equivalent penny shape crack sizes and predicts the matrix cracking stress with a fracture mechanics crack-bridging model. The estimated distribution of matrix cracking stresses is used as statistical input to predict the number of matrix cracks. The results show good agreement with the experimental results by replica observations. Therefore, it is found that the matrix cracking behavior mainly depends on the distribution of matrix-rich regions in the composite.     

SiCw和纳米SiCp混杂增强铝基复合材料的制备与评价

采用湿成型法制备了体积分数可以调节的碳化硅晶须与纳米碳化硅颗粒混杂的预制块,确定了挤压铸造法制备混杂增强铝基复合材料的工艺参数.通过扫描电镜和透射电镜分析发现:复合材料中晶须与纳米颗粒分布均匀,并与基体合金的界面结合良好,无界面反应物和孔洞;与基体合金相比,混杂增强复合材料的抗拉强度和弹性模量明显增高,延伸率降低;在晶须体积分数一定时,随纳米SiC颗粒体积分数的增加,复合材料的抗拉强度升高.