铝合金熔体氧化制备Al2O3 / SiC/ Ni/ Al-Si多相模糊界面陶瓷基复合材料

针对Al₂O₃ / Al 复合材料中金属相Al 对其高温性能的不利影响, 本试验在高温下将铝合金熔体氧化渗透到注浆成型的SiC/ Ni 多孔预制体中, 制备了Al₂O₃ / SiC/ Ni/ Al-Si 多相陶瓷基复合材料。借助光学显微镜、电子显微镜(SEM) 、X 射线衍射仪(XRD) 、波谱仪( EDS) 等手段分析了预制体和复合材料的相组成、微观结构及界面特征。结果表明, 复合材料的主晶相为Al₂O₃ 与SiC , 相间存在Al (Si) 复合氧化物、NiAl₂O₄ 及Ni 与Al-Si 合金相, 各相界面处成分呈连续过渡变化趋势, 构筑了具有模糊界面特征的多相复合材料。      

连续碳化硅纤维增强钛基(SiCf/Ti)复合材料的制备技术及界面特性研究综述

连续碳化硅纤维(SiCf)由于具有比强度、比模量高,耐磨性、热稳定性好等性能优点,常作为增强体制备SiC纤维增强钛基复合材料。与钛合金基体相比,其具有密度更低、强度更高、疲劳蠕变性能大幅提升等优点,但横向性能却明显下降。因此,该类材料常被设计制作成单向增强性部件,广泛应用在航空航天等领域,如发动机的传动轴、整体叶环、盘类及风扇叶片等多种复合材料的结构件。碳化硅纤维增强钛基复合材料的性能主要由碳化硅纤维的性能、基体性能及纤维与基体之间的结合界面性能决定。目前批量生产的SiC纤维性能较差,界面结合状态与复合材料性能之间关系的研究开展较少,还不能为钛基复合材料构件设计提供足够的数据支持。因此,近年来研究者们主要从SiCf/Ti基复合材料力学行为的研究角度出发,探究不同基体及纤维类型、复合材料制备工艺方法、界面特性及产物对SiCf/Ti基复合材料界面结合力及破坏机制的影响,获得了大量有价值的数据,以期开发出成本低、产物稳定性好、可批量生产SiCf/Ti基复合材料的制造工艺方法。目前较为成熟的碳化硅纤维有英国DERA-Sigma公司提供的Sigma系列SiCf及美国Textron公司提供的SCS系列SiCf,后者强度最高达到6 200 MPa。SiCf/Ti基复合材料的制备工艺包括金属箔-纤维-金属箔工艺(FFF)、单层带工艺(MT)、基体-涂层纤维工艺(MCT)等,制备复合材料的工艺根据零部件的用途来定,FFF适用于制备板材等大尺寸构件,MCT适用于制备叶环、轴、管、叶片等复杂结构件。界面是增强体与基体之间的纽带和桥梁,界面结构设计、界面反应控制及反应产物均影响着界面的力学特性。在SiCf/Ti基复合材料的纤维和基体之间添加过渡层能够减缓它们之间的相互扩散及化学反应,过渡层选用反应层和惰性涂层组成的双层涂层较好。界面反应产物受涂层成分、基体组织、复合和热处理工艺、环境因素等的影响,增强纤维及基体性能、优选制备工艺、控制界面反应及产物有利于提高复合材料的力学性能。本文总结了连续SiC纤维(SiCf)增强钛基复合材料的应用研究现状,详述了SiCf/Ti基复合材料的钛合金基体材料、SiCf的种类及性能,SiCf与SiCf/Ti基复合材料的制备方法,分析了SiCf/Ti基复合材料界面结构设计及反应产物,阐明了界面力学特性与复合材料性能的关系,指出国内SiCf/Ti基复合材料发展的重点应放在高性能SiC纤维的研究与开发、界面层设计及界面与性能的关系以及复合材料分析检测手段三个方面,为SiCf/Ti基复合材料的制备及其今后的实际应用提供了参考。     

常规铸造工艺条件下SiCp/Al-Si复合材料中的界面反应

采用搅拌复合法制备了10%SiC／Al—5Si—Mg，10%SiC／Al—7Si—Mg(体积分数)复合材料，研究了在常规铸造工艺条件下重熔后复合材料中的界面反应。通过透射电镜和能谱分析可知，SiC界面基本上都是单一的SiC／Al及SiC／Si界面，部分界面上有MgAl2O4颗粒相形成，由于基体合金中Si的存在，生成Al2C3的有害界面化学反应得到了抑制。对不同文献中抑制Al4C3产生所需临界Si含量实验测定结果的差异进行了分析。     

A functionally gradient coating on carbon fibre for C/Al composites

A functionally gradient coating on carbon fibre for casting C/Al composites with an ultimate tensile strength up to 1250 MPa (V _f=0.35) has been produced. The coating consisted of three layers: an inner pyrocarbon layer, an outer silicon layer and an intermediate gradient layer C/SiC/Si, and their optimum thicknesses were 0.1–0.15, 0.1 and 0.2 m, respectively. This coating was fabricated by chemical vapour deposition and the C/Al composite was performed by pressure-regulated infiltration. Auger electron spectroscopy and X-ray diffraction analyses confirmed that the structure of the coating was in keeping with its design. The excellent ultimate tensile strength of the C/Al composite also proves that the functionally gradient coating has many functions, including wetting agent, diffusion and reaction barrier, releaser of residual thermal stresses, and tailor of interfacial shear strength. According to the mechanical, physical and chemical coordination between fibre and matrix, the functionally gradient coating can solve nearly all the problems of the interface during fabrication and service.     

用Raman光谱研究纤维复合材料

本文以Raman光谱方法的基本原理为依据,结合纤维复合材料研究对结构表征和性能测试技术的要求,评述了Raman光谱在本领域中应用所取得的成果。通过分析在测定界面应力分布、评价界面性质、表征界面和基体结构、测量残留应力等方面应用Raman光谱所遇到的问题,探讨了在研究纤维复合材料本构关系和跟踪复合材料加工过程等领域采用现代Raman光谱技术的前景。     

反应热压(Al2O3+TiB2+Al3Ti)/Al复合材料的低周疲劳行为

采用反应热压法以Al、B₂O₃、TiO₂粉和Al、B、TiO₂粉为原料制备了两种(Al₂O₃+TiB₂+Al₃Ti)/Al复合材料。后一种原料粉制备的复合材料从基体中析出了细小的Al₃Ti相。研究了应变控制原位生成复合材料的室温低周疲劳行为。结果表明,在应变幅较小时(ε_</em>t≤0.3%),不含Al₃Ti析出相的材料表现为循环稳定;而在应变幅较大时(ε_</em>t≥0.4%), 则表现为第一周的循环硬化和随后的循环软化。在所采用的应变幅下,含Al₃Ti析出相的材料均表现为循环稳定。疲劳裂纹萌生部位为Al₃Ti相断裂、Al₃Ti相与基体的界面开裂和基体中微裂纹。疲劳裂纹穿过基体,绕过Al₂O₃、TiB₂质点扩展。两种复合材料的疲劳寿命均符合Coffin-Manson公式。      

Tunable strength of SiCf/β-Yb2Si2O7 interface for different requirements in SiCf/SiC CMC:Inspiration from model composite investigation

Model composites consisting of Si C fiber embedded inβ-Yb₂Si₂O₇ matrix were processed by Spark Plasma Sintering method and the feasibility of tunable Si Cf/Yb₂Si₂O₇ interface in Si C-based CMCs were estimated.Weak and strengthened Si Cf/Yb₂Si₂O₇ interfaces were achieved by adjusting sintering temperatures.The indentation crack test and fiber push out experiments clearly demonstrated the different debonding mechanisms in the samples.Weak interfaces sintered at 1200 and 1250℃exhibited crack deflection at interface in indentation test.Their low debond energy at the interface,which were comparable to those of Py C or BN,satisfied the well-recognized interfacial debond and crack deflection criteria for CMCs.The interface was strengthened by atomic bonding in model composite sintered at 1450℃,leading to crack penetrating into Si C fiber and high debond energy.The strong interface may be promising in Si Cf/Si C CMC to withstand higher combustion temperature,because Yb₂Si₂O₇ will provide plastic deformation capacity,which would serve as weak interphase for crack deflection and energy dissipation.Therefore,it is possible to design the capability of Si C_f/RE₂Si₂O₇ interface for different requirements by adjusting interfacial strength or debond energy to reach optimal mechanical fuse mechanism in SiC_f/SiC CMC.     

Graphene oxide effects on the properties of Al_2O_3-Cu/35W5Cr composite

Graphene oxide(GO) nanosheets were dispersed into premixed powders(Cu-0.4 wt% Al/35W5Cr) by wet grinding and vacuum freeze-drying process. The 0.3 wt% GO/Al_2O_3-Cu/35W5Cr and 0.5 wt%GO/Al_2O_3-Cu/35W5Cr composites, used for electrical contacts, were fabricated by vacuum hot-pressing sintering.The microstructure was analyzed by field emission scanning electron and transmission electron microscopy. In addition, the Raman spectroscopy and X-ray photoelectron spectroscopy were used to investigate the structural changes of GO before and after sintering. The arc erosion behavior was investigated by the JF04 C electrical contact testing apparatus. Consequently, the Al_2O_3 nanoparticles were evenly dispersed in the matrix, causing dislocation tangles. GO was converted to reduced graphene oxide after sintering. A group of carbon atoms combined with Cr forming Cr_3C_2 in situ during sintering, which enhanced the interface bonding. Compared with the Al_2O_3-Cu/35W5Cr composite, the tensile strength of the two contact materials containing 0.3 wt% GO and 0.5 wt% GO was increased by 45% and 34%, respectively. Finally, pips and craters were present on the anode and cathode surfaces, respectively.Tungsten has undergone re-sintering during arcing and formed needle-like structures. Compared with Al_2O_3-Cu/35W5Cr, the GO/Al_2O_3-Cu35W5Cr composites have better welding resistance. The final mass transfer direction of the two composites was from the cathode to anode.     

铝合金表面覆盖SiO2直接氧化生长的反应机理

通过热力学计算和XRD分析,确定了Al-Mg-Si合金熔体与SiO2表面覆盖反应的生成物相为Al2O3,Al,Si和MgAl2O4,直接金属氧化动力学实验表明,SiO2与熔体的接触反应加快了初期的传质过程,使微观传输通道始终处于活性状态,生成的Al2O3构筑了材料的初始骨架,Al2O3/Al复合材料氧化生长的孕育消失。     

对非连续增强铝基复合材料的腐蚀、应力腐蚀断裂与氢脆研究的评述

本文就国内外对非连续增强铝基复合材料,主要是SiC、Al_2O_3颗粒和晶须增强铝基复合材料的腐蚀、应力腐蚀断裂和氢脆的研究现状和主要结论进行了介绍和评价,并为今后的进一步研究提供了一些思路。复合材料的腐蚀形态与铝合金相似,但复合材料的增强体对应力腐蚀断裂和氢脆的、作用不同研究者有不同的结论。     

熔体浸渗法制备Al/Al2O3复合材料中界面的研究进展

界面是复合材料特有的而且及其重要的组成部分,形成更稳定的界面结合是复合材料研究的重点.理想平面间润湿行为的研究对优化复合材料的制备方法以及提高复合材料的结合性能有重要意义.综述了Al和Al2O3异质材料平面间润湿行为的研究现状,并按界面结合机理对Al2O3复合材料现有制备方法进行了归纳.Al2O3复合材料凸显的性能优势和潜在的商业前景将鼓励人们对这一领域展开更深入的研究.     

Determination of residual stresses in SiC monofilament reinforced metal-matrix composites using Raman spectroscopy

Raman spectroscopy has been used to follow the deformation of chemical vapour deposition type SCS-6 and Sigma 1140+ SiC monofilaments and to determine residual stresses in these SiC monofilaments reinforced metal-matrix composites. Raman bands at 1330 and 1600 cm⁻¹ due to carbon have been observed on the monofilament surface and it has been shown that both bands shift linearly to lower wavenumbers during tensile deformation. The residual stresses in SiC monofilament reinforced composites arising from thermal expansion mismatch have also been determined by measuring the shifts of carbon bands from the same monofilaments embedded in a Ti–6Al–4V matrix. The axial residual stresses in the carbon coating are found to be around −850 MPa for the SCS-6 composite and −540 MPa for the Sigma 1140+ composite.     

界面过渡层对SiC/Al双连续相复合材料性能的影响

研究了界面过渡层对SiC/Al双连续相复合材料性能的影响.结果表明,界面过渡层降低了复合材料中的残余应力,改善了界面的结合,提高了复合材料的压缩性能.当界面过渡层中SiC的体积分数接近50%时,复合材料的压缩强度最高,塑性最好,但弹性模量较低.界面过渡层的存在改变了复合材料的弯曲断裂机制.SiC原始泡沫增强的复合材料在断裂时,增强体SiC泡沫先断裂,基体后破坏,断裂表面凹凸不平;含界面过渡层的复合材料断裂时,过渡层的外侧界面先被撕开,内侧界面结合良好,基体与增强体同时断裂,断口平整.     

Interfacial reaction kinetics of SiC fiber-reinforced Ti3Al matrix composites

• 1.(1) SiC fibers reacted with Ti₃Al + Nb to form multilayer reaction products during consolidation and extended isothermal exposure. Complex carbides and silicides genertated from the reactions between Ti, Nb, Al and SiC appears to be the major components in the reaction zone. The C-rich layer on the surface of a SiC fiber affects the development of the reaction zone and the distribution of the reaction products.
• 2.(2) The fiber/matrix interfacial reaction is diffusion-controlled with an activation energy of 271.49 KJ/mole and 218.11 KJ/mole for the SCS-6/Ti-24A1-11Nb and Sigma/Ti-24Al-11Nb composites, respectively, at the early stage of reaction.
• 3.(3) The results of this study indicate that in the SCS-6/Ti-24Al-11Nb composite, the activation energy is higher, the growth rate of reaction zone is slower, and the consumption of C-rich layer is much slower than that in the SCS-6/Ti-6Al-4V composite.

     

电热作用对碳纤维/树脂复合材料界面应力的影响电热作用对碳纤维/树脂复合材料界面应力的影响

碳纤维/树脂复合材料广泛应用于民用航空器结构中,在服役期间会受到复杂环境（湿热、腐蚀、复杂应力和电热作用等）的作用,低强度电流对碳纤维/树脂复合材料的影响受到的关注较少。以碳纤维/树脂复合材料为研究对象,根据碳纤维的温敏效应和通电时的电阻变化规律,计算出碳纤维单丝/环氧树脂复合试样的界面温度范围,之后采用拉曼光谱测试和单丝断裂实验研究了低强度电流对单丝复合体系界面应力和界面剪切强度的影响。结果表明:随着电流强度的提高,单丝复合体系的界面温度随之升高,电流为8 mA时,界面温度高达约200℃。随着电流强度的增大,单丝复合体系的界面压缩应力表现为先增大后减小的趋势,电流高于7 mA后,界面处树脂出现烧蚀降解破坏;单丝断裂实验结果表明随着电流强度增大,单丝复合体系的界面剪切强度呈现先升后降的趋势,在6 mA时界面剪切强度达到最大值62.39 MPa,而8 mA时界面剪切强度仅为34.95 MPa。      

界面结构对SiCf／Al复合材料性能和声发射行为的影响

运用高分辨场发射扫描电镜（ＦＥ－ＳＥＭ）和声发射（ＡＥ）测试研究了ＳｉＣ纤维铝基复合材料的不同界面组成和界面产物及其对复合材料性能和ＡＥ行为的影响发现富碳自理的ＳｉＣｆ／Ａｌ生成Ａｌ４Ｃ３脆性界面,在伸过程中界面脆断产生许多中幅ＡＥ信号,而富ＳｉＯ２处理的ＳｉＣｆ／Ａｌ生成韧工较高的富氧产物,界面强度较高,在形变过程中不易发生界面断裂,不产生中幅ＡＥ信号。     

燃烧合成ZrB2 / Al2O3 复合粉体及其界面分析

采用燃烧还原合成技术, 以还原体系(B₂O₃ + ZrO2 + Al) 为反应体系制备了ZrB₂ / Al₂O₃ 复合粉体。利用X射线衍射(XRD) 、X 射线光电子能谱(XPS) 和透射电镜( TEM、HRTEM) 对复合粉体的物相组成、化学组成及界面结构进行了表征分析。结果表明, 复合粉体中存在Zr 、B、Al 和O 元素且它们分别以ZrB₂ 和Al₂O₃ 为主要存在形式, ZrB₂ 和Al₂O₃ 为复合粉体的主晶相。复合粉体中有少量ZrO2 的存在, 分析认为是合成反应过程中未参加反应的ZrO2 。ZrB₂ 和Al₂O₃ 颗粒间形成了结合良好的界面, 这主要与ZrB₂ 的结晶过程有关。      

高温热曝露对3D-C/SiC复合材料弯曲性能的影响

3D-C/SiC复合材料试样在空气介质中600℃、900℃和1300℃热曝露不同时间后,采用三点弯曲法测试了以室温弯曲弹性模量表征的损伤变化规律,并进行了SEM和EDS分析.结果表明:3D-C/SiC在热曝露15 h后,损伤变化可分为急剧上升(阶段Ⅰ)和平稳上升(阶段Ⅱ)两个阶段.阶段Ⅰ归因于炭纤维和炭层界面在空气中的直接氧化,阶段Ⅱ由复合材料内部氧的扩散所致.在复合材料制备过程的冷却阶段,因基体和炭纤维热膨胀系数不同所产生的基体微裂纹提供了氧化反应的表面与氧扩散的途径.在同一热曝露时间下,损伤随温度的上升而减少的原由可能是由于高温下裂纹收缩导致氧化表面减少,并降低氧向复合材料内扩散所致.     

Comparing single-walled carbon nanotubes and samarium oxide as strain sensors for model glass-fibre/epoxy composites

The study of the interfacial stress transfer for glass fibres in polymer composites through the fragmentation test requires certain assumptions, such as a constant interfacial shear stress. In order to map the local interfacial properties of a composite, both Raman spectroscopy and luminescence spectroscopy have been independently used. Unlike other polymer fibre composites, the local strain state of a glass fibre cannot be obtained using Raman spectroscopy, since only very broad and weak peaks are obtainable. This study shows that when single-walled carbon nanotubes (SWNTs) are added to the silane sizing as a strain sensor, it becomes possible to map the local fibre strain in glass fibres using Raman spectroscopy. Moreover, if this model glass fibre contains a small amount of Sm₂O₃, as one of the components, luminescence spectroscopy can be simultaneously used to confirm this local fibre strain. A combined micromechanical properties study of stress transfer at the fibre–matrix interface using luminescence spectroscopy, together with Raman spectroscopy, is therefore reported. The local strain behaviour of both Sm³⁺ doped glass and SWNTs in the silane coating are shown to be consistent with a shear-lag model. This indicates that Sm³⁺ dopants and SWNTs are excellent sensors for the local deformation of glass fibre composites.     

Interfacial stress transfer in an aramid reinforced thermoplastic elastomer

The interfacial micromechanics of Twaron 2200 aramid fibers in an engineering thermoplastic elastomer (Pebax 7033, polyether amide block co-polymer) has been investigated by determining the distribution of interfacial shear stress along fibers in single-fiber model composites using Raman spectroscopy. The effects of various fiber surface treatments on the interfacial shear stress and fragmentation of the aramid fibers are discussed. The fiber average stress increased linearly with applied matrix stress up to first fracture. Each composite was subjected to incremental tensile loading up to full fragmentation, while the stress in the fiber was monitored at each level of the applied stress. It was shown that the experimental approach allowed us to discriminate between the strengths of the interfaces in the different surface-treated aramid fiber Pebax matrix systems, but also to detect different phenomena (interfacial debonding, matrix yielding and fiber fracture) related intimately to the nature of stress transfer in composite materials. The efficacy of the surface treatments was clear by comparing the maximum interfacial shear stress with the fragment lengths of the modified aramid fibers. The fiber breaks observed using Raman spectroscopy were not clean breaks as observed with carbon or glass fibers, but manifested themselves as apparent breaks by fiber skin failure. The regions of fiber fracture were also investigated using optical microscopy.