基于激光闪射法测量某内燃机铝合金活塞的热物性参数

基于激光闪射法,采用闪射法导热仪测量了不同温度下某内燃机铝合金活塞的比热容、热扩散系数及导热系数。结果表明：随着温度的升高,该内燃机铝合金活塞的热扩散系数逐渐减小,比热容逐渐升高,导热系数在一定温度范围内呈逐渐增大的趋势。     

陶瓷/纤维/树脂超混杂复合材料的力学性能

以泡沫SiC陶瓷为基本骨架,以改性酚醛树脂为基体,加入短切高硅氧玻璃纤维制备出陶瓷/纤维/树脂超混杂复合材料(SHCM),研究了泡沫陶瓷骨架和高硅氧纤维对材料力学性能的影响.结果表明,泡沫陶瓷骨架有利于材料的刚度和尺寸稳定性提高.加入泡沫陶瓷骨架后,纤维/树脂/陶瓷超混杂复合材料的压缩强度和压缩模量增大,随着泡沫陶瓷骨架含量的提高,弯曲模量大幅度提高而弯曲强度略有下降;随着高硅氧纤维含量的提高,材料的弯曲强度及弯曲模量均明显提高.     

一维高导热C/C复合材料的制备研究

以三种沥青作为基体前驱体, 实验室自制的AR中间相沥青基纤维为增强体, 通过500℃热压成型, 随后经炭化和石墨化处理制备出一维炭/炭(C/C)复合材料。研究了前驱体沥青种类和热处理温度对复合材料导热性能的影响, 并采用扫描电子显微镜和偏光显微镜对其石墨化样品的形貌和微观结构进行表征。结果表明; C/C复合材料在沿纤维轴向的室温热扩散系数和导热率均随热处理温度的升高而逐渐增大; 由AR沥青作为基体前驱体所制备的C/C复合材料具有更加明显的沿纤维轴向取向的石墨层状结构以及最好的导热性能, 其3000℃石墨化样品沿纤维轴向的室温热扩散系数和导热率分别达到594.5 mm²/s和734.4 W/(m·K)。     

SiC泡沫陶瓷/Fe基双连续相复合材料的制备和性能

将SiC泡沫陶瓷氧化,用挤压铸造法制备SiC泡沫陶瓷/Fe基双连续相复合材料并对其退火,研究了制备工艺和SiC泡沫陶瓷的体积分数对其微观组织和力学性能的影响。结果表明,在1250℃氧化48 h后在SiC泡沫陶瓷表面生成了厚度为1 mm的SiO2反应阻挡层。在双连续相复合材料的制备过程中,SiO2反应阻挡层抑制Fe与SiC的化学反应,避免了脆性化合物Fe3Si的生成,改善了基体与增强体的界面,使复合材料的抗弯强度提高2倍,压缩强度提高18%。当SiC泡沫陶瓷的氧化时间增至72 h时,SiC泡沫陶瓷表面SiO2的厚度过大。SiO2与基体和增强体热膨胀系数不匹配,使复合材料内相界面间的残余应力增加,导致其性能下降。将SiC泡沫陶瓷/Fe基双连续相复合材料在600℃退火4 h,可降低复合材料中的残余应力,提高复合材料的性能。SiC的体积分数较低时,金属基体的桥接、偏转裂纹的作用比较大,复合材料的弯曲强度高,变形程度大。随着复合材料中SiC体积分数的增大,SiC骨架筋增粗,其承载能力加强,复合材料的压缩强度呈提高的趋势。     

填充颗粒导热性对复合材料导热性能的影响

基于ANSYS Workbench稳态热分析模块,利用均匀化方法,研究了填充颗粒导热性对填充型复合材料导热性能的影响。结果表明,依靠增大填充颗粒导热系数来提高复合材料整体的导热性能有一定局限性,填料导热系数与基体材料导热系数之比存在一个临界值。在相同体积分数下,随着比值的增大复合材料导热系数增加,当达到临界值后继续增大比值复合材料的导热系数基本不变。不同形状的填充颗粒有不同的临界值,圆柱形颗粒的临界值略大于正方体形和球形,而且对于同一种形状的填充颗粒,随着填充分数的增大临界值略有增加。     

膨胀石墨/石蜡相变复合材料有效导热系数的数值计算

通过膨胀石墨粉与石蜡混合制备相变复合材料可有效提高该储能材料的传热性能。为研究膨胀石墨/石蜡相变复合材料的导热机制,提出了膨胀石墨粉与石蜡混合后的3尺度层次固体有效导热系数计算方法。然后,通过数值模拟计算得到了具有不同体积分数和不同导热系数的膨胀石墨导热颗粒的膨胀石墨/石蜡相变复合材料的有效导热系数。结果表明:膨胀石墨能够有效地提高石蜡的导热性能,当膨胀石墨的体积分数为10%时,膨胀石墨/石蜡相变复合材料的有效导热系数是纯石蜡的9倍。此外,提高底层尺度的石墨片与石蜡的混合程度及降低底层尺度石墨的体积分数都能有效提高膨胀石墨/石蜡相变复合材料的有效导热系数。所得结论为探究膨胀石墨粉提高相变复合材料导热系数的机理奠定了基础。     

BN/PA66导热复合材料制备与研究

采用熔融挤出法制备了BN/PA66导热复合材料,通过导热性能测试、力学性能测试、耐热性能测试和DSC等方法研究了BN含量对BN/PA66复合材料的导热性能、力学性能、耐热性能和结晶性能等的影响。结果表明:在实验范围内,当BN体积分数达到24.8%时,BN/PA66复合材料导热系数λ为0.751W/(m.K),约为纯PA66的2.2倍。随BN含量增加,BN/PA66复合材料刚性增加,其热形变温度大幅度提高。     

基于Lattice-Boltzmann方法的填充型复合导热材料的导热性能数值分析

陶瓷被广泛用作催化燃烧的催化剂载体。为及时将反应热导出,避免催化剂烧结、失活,需提高陶瓷导热能力。针对通过填充高导热性的金属或无机填料的方法制成的陶瓷复合导热材料,引入二维九速度不可压格子多相Lattice-Boltzmann模型,对构造的5种规则填充形状(圆形、正八边形、正六边形、正四边形和正三角形)的陶瓷基复合材料进行了完整的二维导热过程的数值分析。结果表明,在相同的填料和填充体积分数下,三角形填充的复合材料有效导热系数最大,填充形状愈趋近圆形则有效导热系数越小。同时模拟了各填充形状下,填充材料与基体材料的导热系数之比kp/km对复合材料有效导热系数的影响。研究结果表明,孤立的导热填料对于复合材料导热系数的提高作用是有限的,当kp/km增大到一定程度,有效导热系数不再明显增加。     

陶瓷/树脂/纤维超混杂复合材料的界面控制

以具有不同表面状态的泡沫SiC陶瓷为基本骨架,以改性酚醛树脂为基体,加入短切高硅氧玻璃纤维制备了陶瓷/纤维/树脂超混杂复合材料,研究了界面控制对超混杂复合材料界面粘结强度的影响.结果表明,对于泡沫SiC陶瓷骨架,在表面生长多孔过渡层或表面堆积SiC颗粒等方法可提高树脂陶瓷之间界面的粘结强度.通过良好的界面控制,可显著提高复合材料的弯曲强度和弯曲模量,模量的提高比强度的提高幅度更大.偶联剂处理使高硅氧纤维与树脂基体的粘结强度增加,从而提高复合材料的弯曲强度.     

骨架表面改性对SiC/Al复合材料性能的影响

采用挤压铸造法制备了SiC/Al双连续相复合材料,并对增强体SiC泡沫陶瓷骨架进行了表面改性处理,研究了网络骨架的表面粗化和表面涂覆K2ZrF6对骨架和双连续相SiC/Al复合材料性能的影响.结果表明:随着粗化时间的增加,SiC陶瓷骨架表面的粗化程度增大.粗化时间为12 min时骨架表面粗化最佳,而且保持了骨架的致密结构.SiC陶瓷骨架表面粗化增加了骨架筋的表面积,加强了界面的机械结合;SiC陶瓷骨架表面涂覆K2ZrF6,提高了基体纯铝对SiC陶瓷骨架的润湿,改善了复合材料中增强体与基体间界面的结合,增强了材料的三维连续性,提高了复合材料的力学性能.骨架表面涂覆K2ZrF6的复合材料的界面结合得最好,复合材料的强度最高,为纯铝基体的5倍.     

CVD SiC涂层SiC纤维增强SiC复合材料的研究

本文采用CVD技术对KD-1 SiC纤维作涂层处理,再通过聚碳硅烷浸渍裂解法制备单向SiCf/SiC复合材料.研究了不同沉积时间的CVDSiC涂层对SiCf/SiC复合材料性能的影响,同时运用SEM研究了SiC纤维表面SiC涂层的形貌.结果表明:经过5小时CVDSiC涂层SiCf/SiC复合材料具有良好的力学性能和抗氧化性能.     

泡沫碳化硅陶瓷表面纳米多孔碳化硅涂层的制备

利用硅改性树脂中硅元素和碳元素分子级均匀分散的特征,以硅改性树脂为涂层原料,在泡沫碳化硅陶瓷表面原位生成了多孔碳化硅活性涂层。在加入适量活性炭颗粒的条件下,在泡沫碳化硅陶瓷表面得到了性能良好的纳米碳化硅涂层,适合作为催化剂载体。相反,在没有活性炭颗粒加入的情况下,所得涂层龟裂、结合强度低,且碳化硅团聚成片,比表面积小。     

Growth of SiC particles in reaction sintered SiC

For reaction sintered SiC (RSSC) prepared at 1600°C by conventional melt infiltration technique, experimentation with two different particle sizes of initial SiC, viz., 0.2 and 23.65 μm, showed that the large SiC particles remained unaltered and the sizes of the fine-grained SiC increased several times yielding well-developed faceted crystals in the final material. To study the process further, compacts of SiC powder of particle sizes varying between 0.20 and 8.99 μm were reacted with pure Si at 1600°C and the resulting SiC–Si boundaries were studied by optical microscopy. A distinct boundary layer with no penetration of Si in the compact of SiC of 0.2 μm was observed and the width of the SiC–Si boundary was found to be increasing linearly with time. Detailed SEM examination establishes the growth of the SiC upto around 4 μm from 0.2 μm starting powder. No such growth was observed in the case of starting SiC powder coarser than 0.2 μm. The growth of SiC is explained in terms of solution-reprecipitation mechanism.     

Long-term strength of SiC fibers with nanocrystalline SiC coatings

The long-term strength σ_t of SiC fibers coated with SiC nanoparticles is approximately equal to30·10 ⁷ pa for t=200h at 1500K. The long-term strength of coated fibers is lower than for fibers without coatings by 25–50%. Owing to their enhanced reaction characteristics, the nanocrystalline SiC coatings are sintered at T<1500K, which is lower than the temperature of sintering of self-bonded SiC by 500 K. For this reason, we can recommend coated SiC fibers for manufacturing SiC/SiC composites by sintering at a temperature of 1500K because, at this temperature, SiC fibers do not degrade. Shevchenko National University, Kiev, Ukraine. Translated from Problemy Prochnosti, No. 1, pp. 95 – 99, January – February, 1998.     

Fatigue behaviour of 3-d SiC/SiC Composites

A tension–tension fatigue damage analysis was performed using 3-d silicon carbide fibre reinforced (orthogonal) silicon carbide matrix (SiC/SiC) composites. Two groups of SiC/SiC specimens were tested. The first group consisted of samples without any oxidation protective top layer coating, whilst the latter one contained samples covered with a well fitting, chemical vapour deposited (CVD) SiC system. This coating is necessary for the material to sustain high temperatures. Both the coated and uncoated material had a fibre volume fraction of about 36% equally distributed in three rectangular directions. Load control fatigue tests were conducted at room temperature. The fatigue life was found to decrease by increasing the cyclic stress level. A power-law equation is proposed, which correlates the applied maximum stress during the fatigue test with the number of cycles to failure. In general, the presence of the coating layer decreases the static strength of the material. However, the nominal maximum cyclic stress for which the endurance fatigue limit appeared, remained unaffected by the presence of the oxidation protective SiC coating. Microstructural examination has also been performed on the fractured specimens and it reveals some of the failure mechanisms of the composite that appeared under quasi-static and dynamic loading.     

不同界面SiC/SiC复合材料的断裂行为研究

碳化硅纤维增强碳化硅复合材料(SiC/SiC)是极具前景的高温结构材料。通过先驱体浸渍裂解(PIP)工艺分别制备了PyC界面和CNTs界面SiC/SiC复合材料, 对两种SiC/SiC复合材料的整体力学性能以及界面剪切强度等进行了测试表征, 并对材料中裂纹的产生与扩展进行了原位观测。结果表明, 两种界面SiC/SiC复合材料弯曲强度相近, 但PyC界面SiC/SiC复合材料的断裂韧性约为CNTs界面SiC/SiC复合材料的两倍。在PyC界面SiC/SiC复合材料中, 裂纹沿纤维-基体界面扩展, PyC涂层能够偏转或阻止裂纹, 材料呈现伪塑性断裂特征; 而在CNTs界面SiC/SiC复合材料中, 裂纹在扩展路径上遇到界面并不偏转, 初始裂纹最终发展为主裂纹, 材料呈现脆性断裂模式。     

SiC及a-SiC：H薄膜的辐照及其进展

SiC是一种宽带隙半导体材料,在高温,高频在,大功率,光电子及抗辐射等方面具有巨大的应用潜力,介绍了国外对该材料及其薄膜进行辐照的一些结果,并指出开展SiC及其薄膜辐照效应研究的重要意义,预测了其发展方向和应用前景。     

Localized mechanical property assessment of SiC/SiC composite materials

SiC fiber-reinforced SiC matrix composites (SiC/SiC) are under consideration as a structural material for a range of nuclear applications. While these materials have been studied for decades, recently new small scale materials testing techniques have emerged which can be used to characterize SiC/SiC materials from a new perspective. In this work cross section nanoindentation was performed on SiC/SiC composites revealing that both the hardness and Young’s modulus was substantially lower in the fiber compared to the matrix despite both being SiC. Using scanning electron microscopy it was observed that the grain growth of the matrix during formation was radially out from the fiber with a changing grain structure as a function of radius from the fiber center. Focused ion beam machining was used to manufacture micro-cantilever samples and evaluate the fracture toughness and fracture strength in the matrix as a function of grain orientation in the matrix. Additionally microstructural characterization techniques like Raman spectroscopy, X-ray diffraction, and microtomography were used to evaluate differences in the matrix and fibers of the composite.