Si3N4／SiC纳米复合陶瓷的微观结构

利用ＪＥＭ２０００ＥＸⅡ高分辨电镜和ＨＦ２０００冷场发射枪透射电镜对Ｓｉ３Ｎ４ＳｉＣ纳米笔合陶瓷材料的微观组织，结构和成分进行了研究。结果表明，ＳｉＣ颗粒弥散分布基体相β－Ｓｉ３Ｎ４晶内和晶界，晶内ＳｉＣ颗粒与基体相的界面结构有三种类型；１）直接结合的的界面；２）完全非晶态的界面；３）混合型的界面，晶间ＳｉＣ颗粒与基体相的界面大部分是直接结合的。     

含氮聚硅氧烷配位体及其Cu^2＋络合物的介电性能

研究了ｎ－β（氨乙基）－γ（氨丙基）三乙氧基硅烷（ＮＨ２（ＣＨ２）２ＮＨ（ＣＨ２）３Ｓｉ（ＯＥｔ）３）与二甲基二乙氧基硅烷（ＣＨ３）２Ｓｉ（ＯＥｔ）２）共水解，制备含（ＣＨ２）３ＮＨ（ＣＨ２）２ＮＨ２功能基的聚硅氧烷配位体，用ＩＲ，＾１ＨＮＭＲ和元素分析法对水解产物分析证明，ＮＨ２（ＣＨ２）２ＮＨ（ＣＨ２）３Ｓｉ（ＯＥｔ）３与（ＣＨ３）２Ｓｉ（ＯＥｔ）２进行了共水解反应，而且水解程度随ＮＨ２（ＣＨ     

超细孔二氧化硅膜的制备研究

以正硅酸乙酯（ＴＥＯＳ）为原料，采用溶胶－凝胶技术在多孔陶瓷载体上制备出具有３．０ｎｍ孔径的ＳｉＯ２陶瓷膜。考察了制膜过程中ＴＥＯＳ、乙醇、水的相对量；酸碱催化和ｐＨ值；热处理温度及成膜助剂对膜性能的影响。在自制的单管膜分离器上，测定了Ｏ２、Ｎ２、ＣＯ２和ＣＨ４等气体在ＳｉＯ２陶瓷膜上的渗透性能。     

SiC－AlN－Y_2O_3复相陶瓷的制备与性能

通过热压烧结技术，ＳｉＣ、ＡｌＮ和Ｙ２Ｏ３粉末混合作在１９２０～２０５０℃、Ａｒ气氛下形成了致密的复相陶瓷．在室温下ＳｉＣ－ＡｌＮ－Ｙ２Ｏ３复相材料的抗弯强度和断裂韧性分别达到６００ＭＰａ和７ＭＰａ·ｍ１／２以上运用ＸＲＤ、ＳＥＭ和ＴＥＭ分析致密样品的断裂裂纹、形貌和组成．ＳｉＣ－ＡｌＮ－Ｙ２Ｏ３复相陶瓷在１３７０℃氧化试验３０ｈ，其氧化产物为莫来石．     

SiC—AlN—Y2O3复相陶瓷的制备与性能

通过热压烧结技术，ＳｉＣ、ＡｌＮ和Ｙ２Ｏ３粉末混合体在１９２０￣２０５０℃、Ａｒ气氛下形成了致密的复相陶瓷。在室温下ＳｉＣ－ＡｌＮ－Ｙ２Ｏ３复相材料的抗弯强度和断裂韧性分别达到６００ＭＰａ和７ＭＰａ·ｍ＾１／２以上。运用ＸＲＤ、ＳＥＭ和ＴＥＭ分析致密样品的断裂裂纹、形貌和组成。ＳｉＣ－ＡｌＮ－Ｙ２Ｏ３复相陶瓷在１３７０℃氧化试验３０ｈ，其氧化产物为莫来石。     

LOM技术中的挤制陶瓷片的研究

采用挤出工艺制备了用于ＬＯＭ技术中的Ａｌ２Ｏ３和ＳｉＣ陶瓷片坯件，厚度０．２ｍｍ。有机物载体采用低密聚乙烯，固体粉料占４８ｖｏｌ％，研究了Ａｌ２Ｏ３－ＬＤＰＥ混合物的流变性能，对陶瘊片进行了ＴＧ－ＤＴＡ热分析和ＳＥＭ微观组织分析。     

液态搅拌铸造颗粒增强Al－4％Mg复合材料的微观结构研究

本文以ＴＥＭ和ＥＤＳ为主要分析手段，研究了不同颗粒增强的Ａｌ－４％Ｍｇ复合材料的界面及其基体中的微观结构，探讨了它们的形成原因。结果表明：ＳｉＯ_２颗粒与基体间为反应结合，Ａｌ_２Ｏ_３和ＳｉＣ则基本上为机械结合。     

（CH3）2SiCl2和N2H4反应产物裂解逸出气体与粉体组成关系的研究

采用（ＣＨ３）２ＳｉＣｌ２和Ｎ２Ｈ４反应产物为先驱体，在Ｈ２，ＮＨ３气条件下，用ＣＶＤ法制备Ｓｉ／Ｃ／Ｎ的纳米微粉，在制备Ｓｉ／Ｃ／Ｎ纳米微粉的过程中通过高温炉－气相色谱联用技术分析了裂解逸出的气体，用化学法分析了微粉中元素组成变化，讨论了先驱体Ｈ２，ＮＨ３气体条件下的裂解机理及微粉的形成机理。     

液态搅拌铸造颗粒增强Al－4％Mg复合材料的微观结构研究EI

本文以ＴＥＭ和ＥＤＳ为主要分析手段，研究了不同颗粒增强的Ａｌ－４％Ｍｇ复合材料的界面及其基体中的微观结构，探讨了它们的形成原因。结果表明：ＳｉＯ_２颗粒与基体间为反应结合，Ａｌ_２Ｏ_３和ＳｉＣ则基本上为机械结合。     

核壳结构型纳米CaCO3-SiO2.nH2O复合粒子的制备

在搅拌槽式反应器中,以用超重力法合成的纳米 ＣａＣＯ３和 Ｎａ２ＳｉＯ３为原料,用溶胶－凝胶技术制备具有核壳结构的纳米 ＣａＣＯ３－ＳｉＯ２·ｎＨ２Ｏ复合粒子　用 ＸＰＳ、 ＴＥＭ、 ＸＲＤ等方法对粒子的化学组成、形貌、晶型等作了分析和表征     

用CVI工艺制备碳纤维增强C－SiC梯度热结构材料

用化学气相渗（ＣＶＩ）工艺，分别用分段沉积和共沉积方法制取了Ｃ／Ｃ－ＳｉＣ梯度热结构材料，并比较了二者的成分梯度、性能与组织结构特征。     

旋转CVI制备C/SiC复合材料

旋转 ＣＶＩ是在 ＣＶＩ原理基础上发展的一种制备 Ｃ／ＳｉＣ复合材料的新工艺,通过石墨衬底的旋转,使预制体的制备与基体的沉积同步进行,能有效消除一般ＣＶＩ工艺过程中存在的“瓶颈”效应．在自制的旋转 ＣＶＩ设备上实验,探索了旋转 ＣＶＩ工艺参数中 ＣＨ_３ＳｉＣｌ_３（ＭＴＳ）的流量与浓度、沉积温度和Ｃ布缠绕线速度对ＳｉＣ基体沉积速度,以及沉积温度对基体结构的影响．并在低压（５ｋＰａ）、高温 （１１００℃）、 ４００ ｍＬ·ｍｉｎ^－１ Ｈ_２、 ２００ ｍＬ·ｍｉｎ^－１Ａｒ、 ＭＴＳ４０℃与Ｃ布以１．１～３．５ｍｍ·ｍｉｎ^－１的线速度连续旋转的沉积条件下,实现了单丝纤维间微观孔隙、纤维束之间以及Ｃ布层间宏观孔隙的致密化同步完成．     

On the CVD of MoSi2: an experimental study from the MoCl4–SiCl4–H2–Ar precursor with a view to the preparation of C/MoSi2/SiC and SiC/MoSi2/SiC microcomposites

The chemical vapour deposition of MoSi2 on plane substrates (graphite or sintered-SiC) and ceramic fibres has been studied from MoCl4–SiCl4–H2–Ar gas mixtures at 900相似文献   

3D C/SiC复合材料喷管在小型固体火箭发动机中的烧蚀规律研究

采用小型固体火箭发动机研究了3D C/SiC复合材料喷管的烧蚀性能,分析了3D C/SiC的烧蚀机理及燃气参数对烧蚀性能的影响.结果表明,喷管喉部线烧蚀率为0.128±40.088mm/s,质量烧蚀率为0.166kg/(m2.s);受喷管内燃气组分、温度、压强和流速等环境参数的影响,3D C/SiC的烧蚀涉及不同机理的非均匀烧蚀.喉部及其上下游过渡区域烧蚀最严重,收敛段其次,扩散段烧蚀最弱.烧蚀过程是热物理化学侵蚀和机械剥蚀综合作用的结果:涉及SiC的分解流失,SiC和碳纤维的氧化烧蚀,还涉及低速Al2O3大粒子的机械化学侵蚀,高速Al2O3小粒子的机械侵蚀等.     

掺杂改性C/C复合材料研究进展

陶瓷掺杂改性碳/碳(C/C)复合材料在保持C/C复合材料原有优异高温力学性能及尺寸稳定性等特性的前提下,显著提高了C/C复合材料的高温抗氧化、抗烧蚀性能,且其具有可设计性和良好的抗热震性能等优势,是新型高超声速飞行器和新一代高性能发动机热防护部件的理想候选材料。综述了国内外在SiC陶瓷掺杂改性C/C复合材料,ZrC,ZrB2超高温陶瓷掺杂改性C/C复合材料以及TaC,HfC超高温陶瓷掺杂改性C/C复合材料等方面的最新研究进展和应用情况,并分析了陶瓷掺杂改性C/C复合材料目前研究及应用中存在的主要问题和今后潜在的研究发展方向。     

MoSi2-SiC 抗氧化涂层对碳/碳复合材料弯曲性能的影响

在C/C 复合材料表面制备了MoSi₂-SiC 抗氧化涂层, 分析了涂层工艺对C/C 复合材料组织的影响, 测试了材料的室温弯曲力学性能。结果表明, 该工艺在C/C 复合材料表面生成抗氧化涂层的同时, 基材内部的层间和纤维束界面, 以及孔隙周围也被硅化。C/C 复合材料经涂层工艺处理后, 弯曲断裂行为发生改变, 弯曲强度明显升高,塑性有一定程度的降低。      

Oxidation behaviour of three-dimensional woven C/SiC composites

Abstract

The oxidation behaviour of a three-dimensional woven C/SiC composite protected with an SiC seal coating and with an SiC coating combined with an SiO₂–B₂O₃ glassy coating have been respectively investigated through an experimental approach based on mass and flexural strength changes. Three main temperature domains exist for C/SiC composites protected with an SiC seal coating. At low temperatures (<700°C), the mechanisms of reaction between carbon and oxygen control the oxidation kinetics. At an intermediate temperatures (between 700 and 1100°C), the oxidation kinetics are controlled by gas phase diffusion through a network of microcracks in the SiC matrix and coating. At high temperatures (>1100°C), the oxidation kinetics are controlled by oxygen diffusion through the SiO₂ scale formed on the SiC coating. Composites of C/SiC with an SiC/(SiO₂–B₂O₃) coating exhibit better oxidation resistance. The filling of the pores and the microcracks and the flow of the glassy coating at higher temperatures result in a global decrease of mass loss in the composites. By researching the relationship between the residual flexural strength and the mass variation in different temperature ranges, it is shown that the change in the residual flexural strength is dominated by the degradation of carbon phase.     

C(B) materials as interphases in SiC/SiC model microcomposites

A specific test procedure has been developed to compare the high temperature lifetimes of SiC/SiC microcomposites with various interphases in air and under mechanical loading. The interphases, namely pure pyrocarbon (PyC) or C(B) materials with uniform or variable boron contents in the thickness, were prepared by chemical vapour deposition (CVD). Uniform addition of boron in PyC interphases improved their oxidation resistance and consequently the lifetimes of the microcomposites. However, room temperature tensile tests have shown that this improvement occurs to the detriment of the mechanical properties even when a non-brittle behaviour is maintained. In the case of variable boron contents, compositional gradient interphases (CGI) in which boron content increases from the fibre interface to the matrix interface allow the mechanical fuse properties of PyC to be combined with the oxidation resistance of a C(B) material. This revised version was published online in November 2006 with corrections to the Cover Date.     

高温氧化及热震对SiC/ZrB2-SiC/SiC涂层炭/炭复合材料力学行为的影响

为提高炭/炭(C/C)复合材料的高温抗氧化性能,同时分析涂层制备及高温氧化对涂层材料力学行为的影响,在C/C复合材料表面采用反应熔渗、料浆涂刷结合化学气相沉积工艺制备了SiC/ZrB2-SiC/SiC三层高温抗氧化涂层。利用SEM和XRD分析复合涂层的微观结构和相组成,考察涂层复合材料1500℃高温抗氧化和1500℃-室温的抗热震性能,研究高温氧化及热震对涂层C/C复合材料力学行为的影响。结果表明,复合涂层试样1500℃静态空气环境下具有优异的抗氧化及抗热震性能:1500℃氧化20 h后试样保持增重,1500℃至室温热震50次后增重为0.69%。因涂层制备过程中粉料的渗入反应,复合材料弯曲强度增长了7.08%。在经历1500℃氧化20 h和1500℃至室温50次热震后,涂层复合材料弯曲强度有所下降,且因材料界面结合力的减弱使得纤维拔出特征明显,材料塑性断裂特征增强。     

The nanostructured phase transition of superhard Ti-Si-C-N coatings

Ti-Si-C-N coatings with different Si contents were synthesized by means of pulsed direct current plasma-enhanced chemical vapor deposition using a TiCl(4), SiCl(4), CH(4), N(2), H(2) and Ar gas mixture. A complex phase transition has been identified which is strongly controlled by the silicon content in the coatings. Transmission electron microscopy (TEM) and x-ray diffraction (XRD) results indicate that increasing Si content leads to a phase transition from a solid solution (Ti, Si)(C, N) to a dual-phase Ti?(C,N)+TiSi(2) structure, and then to a two-phase Ti?(C,N)+SiC structure, and that the changes in grain size and lattice parameter coincide with the phase transition. The Ti-Si-C-N coatings with high Si contents (≥4.3?at.%) possess a superhigh hardness (43-52?GPa) due to grain refinement/grain boundary hardening and compressive stress/dispersion hardening of the hard, nanosized crystalline TiSi(2) or SiC dispersed in the matrix.