SiC纳米纤维/C/SiC复合材料拉伸行为的分子动力学研究

本文采用分子动力学计算方法和Tersoff作用势研究了无定型碳(amorphous carbon, a-C) 涂层厚度对SiC纳米纤维/SiC纳米复合材料断裂方式及力学性能的影响. 分析结果发现, 随着涂层厚度的增加, 纳米纤维的平均应力集中系数下降, 即足够厚度涂层可以同时起到增强和补韧的作用. 当a-C涂层厚度t ≤ 0.3 nm时, 裂纹直接穿透纤维, 纳米复合材料表现出典型的脆性断裂方式; t = 4.0 nm时, 裂纹发生偏转, SiC纳米纤维发生拔出现象, 此时纳米复合材料的拉伸强度约为无涂层纳米复合材料的4倍, 断裂能则提高一个数量级. 计算结果表明, a-C涂层的厚度是SiC纳米纤维/SiC纳米复合材料中产生韧性机理的重要因素, 即传统微米级陶瓷基复合材料的增韧理论在纳米复合材料中仍适用. 研究结果可望为设计同时具有高强度、高韧性的陶瓷基纳米复合材料提供理论基础.     

涂层界面结合强度检测研究(Ⅱ)：涂层结合界面应力检测系统

利用X射线衍射技术(XRD)测试了涂层及其基体材料的应力及其变化规律，建立了一种涂层结合界面应力检测系统，进行界面结合状态的检测研究.利用涂层从基体脱粘前后的界面应力变化量，结合涂层材料的物性参数和涂层-基体系统温度场参数，用涂层残余应力衍射峰来表征涂层与基体的结合强度，创立一种研究检测涂层结合强度理论的实验新方法，适用于各种热障涂层的界面结合强度测量. 关键词： X射线衍射法(XRD) 界面结合强度 涂层 残余应力     

石墨颗粒/CuAlMn形状记忆合金复合材料中的位错内耗峰

利用渗流技术制备出了以石墨颗粒为阻尼增强相、以Cu-11.9Al-2.5Mn(wt%)形状记忆合金为基体的复合材料，对该合金的内耗行为进行了研究. 在淬火态样品的内耗-温度曲线上观察到两个内耗峰，分别位于240 ℃和370 ℃附近. 对其中低温峰的变化规律和机理进行了研究. 实验发现，低温峰仅在复合材料中出现，峰位与频率无关，峰高随频率升高而上升；随升温速率增加，峰高增加，峰位移向高温；随石墨颗粒体积分数增加，峰高增加；经多次热循环后该内耗峰消失. 由以上特征和微观观察，可以证明该峰起因于外加交变应力与位错的相互作用.     

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用煅烧石油焦作填料、煤沥青作粘结剂和B4C、Si、Ti作添加剂，利用热压工艺制备了系列重结晶掺杂石墨，并通过化学气相反应法在掺杂石墨表面沉积了有梯度的SiC涂层。对掺杂石墨的热力学性能、微观结构及在HT-7装置的聚变环境中的行为进行了考察。结果表明：与纯石墨材料相比，掺杂了10%的B4C的重结晶石墨力学性能得到明显的改善，抗弯强度达104Mpa，但导热性能较差；掺杂了Si、Ti的重结晶石墨的热导率高，达314W•m-1•K-1，但力学性能较差；掺杂了BSTDG的石墨在聚变环境中的抗等离子体辐照能力明显提高；在HT-7装置中经过一轮实验的辐照后，SiC涂层厚度因等离子体的刻蚀由初期的40～50μm下降至5μm左右，且局部区域涂层剥落。     

硬质合金表面Ti系涂层退除后的界面性能研究

采用电弧离子镀技术(AIP)在YW2合金基体表面制备了TiAlN涂层,通过化学方法退除基体上的涂层,分析了硬质合金表面退除涂层后和镀覆涂层前成分和元素存在形态的变化。发现当样品在30%H₂O₂、草酸钾COOK(1.5mol·L-1)、缓蚀剂葡萄糖酸钠GA和NaOH,V_NaOH溶液∶V_30%H2O2∶V_COOK溶液=1∶1∶1,45 ℃时,45 min可以退除涂层,肉眼未观察到基体表面受腐蚀。涂层退除后样品表面光亮,呈现合金未镀覆涂层前颜色。通过对退镀后YW2基体和基体镀覆涂层前的表面XPS定性及定量分析发现,退除涂层后,基体表面W元素结合能和N元素主峰结合能与XPS结合能与参照表上对应结合能变化很小,元素的价态没有发生变化;镀覆TiAlN涂层时扩散到合金浅表层的Al,Ti,N元素,造成表面Al,Ti,N元素含量较镀覆涂层前增加,结合能位置偏移,形成AlN和TiN,有利于重新镀覆的涂层与合金基体的结合。     

复合材料残余应力的拉曼测定

本文报道在拉曼光谱仪中用拉曼光谱术和荧光光谱术测定复合材料残余应力(应变)的方法和结果。复合材料组分中Al2O3的荧光R1峰、Si晶体和SiC纤维拉曼峰的位置(波数)随应变的偏移与应变值都有近似的线性关系。这种关系可用于确定复合材料中由外负荷力学作用或热学作用引起的残余应变。在显微拉曼系统中测定了ZrO2-Al2O3层状复合材料,Al-Si共晶体和SiC纤维增强玻璃复合材料的残余应变及其空间分布。     

基于XRD的镀锌钝化膜残余应力试验研究

利用XRD技术测试了镀锌钝化膜结合界面的残余应力，同时通过电解抛光法检测了其厚度方向残余应力的分布规律，分析了残余应力对镀锌钝化膜结合强度的影响. 试验结果表明，镀锌钝化膜的残余应力均表现为压应力，并随着基体表面残余应力的增大而减小；钝化膜在2—10μm厚度方向的残应力为-274.5—-428.3MPa，其应力为梯度分布；镀锌钝化膜与基体的界面结合强度与其残余应力成反比，减小薄膜残余应力，有利于提高镀锌钝化膜与基体的结合强度. 关键词： X射线衍射法(XRD) 镀锌钝化膜 结合强度 残余应力     

石墨颗粒／CuAIMn形状记忆合金复合材料中的位错内耗峰

利用渗流技术制备出了以石墨颗粒为阻尼增强相、以Cu-11．9A1-2．5Mn（wt％）形状记忆合金为基体的复合材料，对该合金的内耗行为进行了研究．在淬火态样品的内耗-温度曲线上观察到两个内耗峰，分别位于240℃和370℃附近．对其中低温峰的变化规律和机理进行了研究．实验发现，低温峰仅在复合材料中出现，峰位与频率无关，峰高随频率升高而上升；随升温速率增加，峰高增加，峰位移向高温；随石墨颗粒体积分数增加，峰高增加；经多次热循环后该内耗峰消失．由以上特征和微观观察，可以证明该峰起因于外加交变应力与位错的相互作用．     

碳化硅反射镜坯体光学加工的残余应力测量与分析

测量并分析了碳化硅反射镜坯体光学加工的残余应力。采用X射线衍射法测定了磨削成形、研磨以及抛光过程引入的表面残余应力的性质和大小;采用逐层抛光法测定了在用120#粒度金刚石砂轮磨削时引入的残余应力层厚度。研究结果表明:在用120#金刚石砂轮磨削加工时沿磨削方向和垂直于磨削方向分别引入了残余拉应力和残余压应力,其大小分别为40MPa和70MPa,应力层深度约为60μm,大于裂纹层深度;在用W7金刚石微粉研磨时引入了残余压应力,在其作用范围内残余应力平均值为60～80MPa;在抛光时理论上会引入残余压应力。在此基础上提出了在碳化硅反射镜坯体的光学加工过程中,可以通过研磨消除磨削引入的裂纹层和残余应力层。     

含有缺陷3C-SiC陶瓷拉伸性能的分子动力学模拟

SiC纤维增韧SiC基复合材料(SiC_f/SiC)由于其优越的性能而成为新一代核能系统重要候选材料之一.材料中的缺陷会使材料的力学性能发生变化,本文运用分子动力学程序LAMMPS模拟计算了分别含有空位、微空洞和反位替代三种缺陷的3C-SiC结构体系沿[100]方向的拉伸变形过程,原子间相互作用采用Tersoff多体势描述.通过模拟得到不同缺陷体系的应力—应变曲线和拉伸过程中体系能量,通过分析应力-应变曲线,得到了不同缺陷体系的杨氏模量、断裂应变、拉伸强度随缺陷"浓度"的变化关系,最后分析了3C-SiC拉伸断裂机理.研究结果表明,空位和微空洞对杨氏模量、拉升强度的影响类似,都是随着缺陷"浓度"的增加而减小,反位替代缺陷使体系的杨氏模量随缺陷"浓度"的增加而增大.     

Microstructure and thermal residual stress analysis of SiC fiber through Raman spectroscopy

SiC fiber‐reinforced metal matrix composite is an interesting material for aerospace industry because of its excellent properties. However, these properties are greatly influenced by fiber microstructure and thermal residual stresses introduced by the preparation of the composites. Due to complicated preparation technology, microstructure and thermal stress along SiC fiber radius varies, which makes characterization difficult. Raman spectroscopy is a non‐destructive technique which provides information, at micrometer scale, on the phase composition and the crystalline state (structure and texture) of materials. Line scanning was used to assess microstructure along SiC fiber radius embedded in Ti64. The SiC coating is subdivided into three concentric parts across the fiber diameter, according to the differences in intensity and width of SiC transverse optical phonon (TO) band. Part 2 is considered to be a buffer zone connecting Part 1 and Part 3 with different deposition conditions, respectively. Amorphous Si is detected throughout fiber radius, while crystalline Si is only detected in the outer part. Thermal residual stress along fiber radius in the composite was calculated by using SiC TO band shifts with a bare fiber as reference. A cylindrical model was also used to compare with the stress data obtained from Raman shift. Copyright © 2013 John Wiley & Sons, Ltd.     

脉冲磁控溅射MoS2-Ti涂层常温及高温真空摩擦磨损性能

利用脉冲磁控溅射法，以铝青铜合金(C63200)和硅片为基底，制作不同Ti含量的MoS₂-Ti复合涂层。通过XRD、SEM、EDS、光学显微镜、多环境摩擦试验机等表征了涂层的结构成分和摩擦性能。结果表明：随Ti含量的增加，涂层致密度提升，S、Mo原子比上升。Ti的掺入使涂层由高度结晶态向非晶态转变。Ti含量增加，涂层摩擦磨损性能先上升再下降，常温真空下含3%Ti的涂层拥有稳定和低至0.015的摩擦系数，23%Ti的涂层失去润滑性。温度升高到400℃，涂层摩擦系数由0.015~0.04上升至0.07~0.1，含13%Ti的涂层高温真空下在800s后润滑失效。磨痕形貌显示，含3%Ti的涂层磨痕最窄，温度升高宽度增加不大，含13%Ti的涂层磨损严重，400℃真空环境下很快磨穿，纯MoS₂和13%Ti涂层摩擦时发现大量磨粒和破碎磨屑。     

Comparison of the properties of Nextel 720/SiC composites at room temperature and 1300°C

Continuous Nextel 720 fibers reinforced SiC composites with PyC interface are fabricated by LPCVI at 1000°C for 200 h using SiCH₃Cl₃ as precursor. The mechanical properties at RT and 1300°C are measured by three-point bending. The microstructures of the interface are characterized by TEM. The results indicate the composites have the metal-like behavior of fracture, whether they are at RT or high temperature. The RT and 1300°C strengths are 310 MPa and 140 MPa, respectively. The RT and 1300°C strains are 0.32% and 0.12%, respectively. The loss of flexural strength and strain of the Nextel 720/SiC composites at high temperature result from stronger residual thermal stress caused by the mismatch of CTE between fibers and matrix. A gap appears between fibers and PyC interface after the 1300°C test, which could be resulted from 7.7% compressive strain of PyC interface caused by the residual thermal stress and 0.1% sintering shrinkage of Nextel 720 fiber.     

Investigation of interfacial stress transfer in a PBO/polypropylene microdroplet composite using synchrotron microfocus X-ray diffraction

The micromechanics of stress transfer in a PBO/polypropylene system were followed using a microdroplet model composite and a synchrotron microfocus X-ray diffraction technique. High quality X-ray diffraction patterns were obtained from both the PBO-HM fiber and the polypropylene matrix. Diffraction patterns were obtained from the fiber inside the PP droplet by subtraction of a PP diffraction pattern from that of the composite. It was found that there was good stress transfer at the fiber–matrix interface and that significant residual stresses occurred in the fiber inside the droplet due to the cooling and crystallization of the polypropylene. The maximum residual stress of 0.55 GPa measured corresponded to an axial fiber strain of 0.2% compressive strain, similar to the literature values for compressive fiber failure.     

Deposition of BN interphase coatings from B-trichloroborazine and its effects on the mechanical properties of SiC/SiC composites

Boron nitride thin films were deposited on silicon carbide fibers by chemical vapor deposition at atmospheric pressure from the single source precursor B-trichloroborazine (Cl₃B₃N₃H₃, TCB). The film growth and structure, as a function of deposition temperature, hydrogen gas flow rate, and deposition time, were discussed. The deposition rate reaches a maximum at 1000 °C, then decreases with the increasing of temperature, and the apparent activation energy of the reaction is 127 kJ/mol. Above 1000 °C, gas-phase nucleation determines the deposition process. The deposited BN films were characterized by Raman spectroscopy, X-ray diffraction (XRD) and scanning electron microscopy (SEM). The effect of BN interphase on the mechanical properties of the unidirectional SiC fiber-reinforced SiC matrix (SiC/SiC) composites was also investigated. The results show that the flexural strength of SiC/SiC composites with and without coating is 276 MPa and 70 MPa, respectively, which indicates that BN interphase coating deposited from B-trichloroborazine precursor can effectively adjust the fiber/matrix interface, thus causing a dramatic increase in the mechanical properties of the composites.     

Raman investigation of chemical reaction product in thermal‐treated SiCf/C/Mo/Ti6Al4V composite

SiC fiber‐reinforced titanium matrix composite (TMC) is an interesting material for aerospace industry because of its excellent properties. Characterization of their interfacial reaction product is principal to further optimization of the TMCs. Here we report application of Raman spectroscopy to identify reaction products and their microstructural details in thermal‐treated SiC_f/C/Mo/Ti6Al4V composite. Meanwhile TEM is performed to help explain phenomena in Raman result. Raman line scanning along interface indicates thickness of two sublayers (Ti₅Si₃(C_x) layer next to SiC fiber and TiC_x layer next to matrix). The main Raman result of phase distribution is confirmed by TEM. While a 300‐nm Ti₃SiC₂ layer whose Raman features are similar with nearby Ti₅Si₃(C_x) layer is also detected. Raman peakshift in Ti₅Si₃(C_x) layer possibly results from residual stress or/and microstructural evolution caused by carbon solution. No evidence indicates Mo participation of interfacial reactions. However, Mo diffusion changes phase distribution of matrix alloy and affects interfacial reaction indirectly. Meanwhile, TEM and Raman results indicate that particles are TiC_x and defective Ti₃AlC₂. Raman features of Ti₃AlC₂ particles differ from that of bulk material, which is attributed to defects. Although Ti₃AlC₂ formation mechanism is ambiguous, it possibly relates to TiC_x formation nearby. Copyright © 2014 John Wiley & Sons, Ltd.     

SiC/C界面辐照性能的分子动力学研究

本文通过分子动力学模拟的方法,研究了5种含不同空间结构的SiC/C界面的材料受辐照后的缺陷分布随时间以及PKA位置的变化关系,并与单质SiC中缺陷分布情况进行对比.利用径向分布函数分析了辐照对界面原子排列情况的影响.研究结果表明,SiC/C界面的抗辐照能力明显低于SiC内部,不同的空间结构对界面缺陷数量存在一定影响.由径向分布函数推得界面区域石墨原子密度高则界面原子排列情况受辐照影响越大.     

激光熔覆Al+SiC涂层对镁合金表面耐磨性能的改性

通过脉冲激光器(Nd-YAG)在AZ91D镁合金基底上熔覆Al+SiC粉体。采用扫描电子显微镜、能量色散谱(EDS)和X-射线衍射测定分析熔覆层的显微组织、化学成分和物相组成。研究表明:Al+SiC涂层主要由SiC,β-Mg_(17)Al_(12)及Mg和Al相组成,激光熔覆层与镁合金基底表现出良好的冶金结合。所有样品都具有树枝状结构,且随着SiC质量分数的增大,树枝状和胞状结构的间隔变得更大。熔覆涂层的表面硬度高于基底,并且随着熔覆层中的SiC质量分数的增加而增大,SiC质量分数为40%的熔覆层具有最大的显微硬度,达到180 HV,然而质量分数为10%的熔覆层硬度为136 HV。销盘滑动磨损试验表明,复合涂层中的SiC颗粒和原位合成的Mg_(17)Al_(12)相显著提高了AZ91D镁合金的耐磨损性,其中,SiC质量分数从10%增加到30%过程中磨损体积损失逐渐减少,SiC质量分数在20%~30%时熔覆层具有最好的耐磨性。     

CVD-SiC纤维的拉曼光谱研究

采用激光拉曼光谱对单根CVD-SiC纤维进行了研究,并与SiCf/Ti-6A1-4V复合材料中SiC纤维的拉曼光谱进行对比分析.发现SiC纤维的第一沉积层的TO峰峰形尖锐,表明SiC晶粒较大,第二沉积层的晶粒较小,在二个沉积层中分别检测到碳和硅的拉曼峰.在复合材料中,SiC纤维的TO峰向高波数偏移,表明复合材料在制备过...