WC／Cu复合材料的研究

探讨了用常规粉末冶金固相烧结法制备ＷＣ颗粒增强铜基复合材料的可行性。研究了不同ＷＣ体积含量复合材料的显微组织和性能，试验了复压轧制对颗粒分布和基体经的的影响。并对相应的断口形貌进行了分析。     

WC_p/2024Al复合材料疲劳性能研究

利用粉末冶金法制备了WC颗粒体积分数分别为8.0%,11.8%,16.7%的WCp/2024Al复合材料,采用PQ1-6纯弯曲疲劳试验机对其进行高周疲劳性能测试,通过扫描电镜观察复合材料疲劳试验后的疲劳断口。结果表明:WCp/2024Al复合材料疲劳极限和疲劳寿命随着WC体积分数的增加而升高;复合材料的疲劳源产生于试样表面有缺陷或表面附近颗粒团聚的薄弱部位;随着WC体积分数的增加,WCp/2024Al复合材料的疲劳断口韧窝组织呈减少的趋势,脆性断裂特征逐渐明显;由空洞形核与长大造成的界面脱粘和基体相破坏是WCp/2024Al复合材料疲劳断裂的主要形式。     

ARZ陶瓷颗粒增强316L不锈钢复合材料的制备及性能

采用粉末冶金工艺制备了Al₂O₃增强ZrO₂(alumina reinforced zirconia,ARZ)陶瓷颗粒增强316L不锈钢(316L不锈钢/ARZ)复合材料，研究了ARZ陶瓷颗粒体积分数对316L不锈钢/ARZ复合材料的微观组织、相对密度、硬度、耐磨性的影响。结果表明：当ARZ陶瓷颗粒体积分数为20%时，复合材料的相对密度达到97.53%，与不锈钢基体相当；继续加入ARZ陶瓷，陶瓷颗粒发生团聚降低了复合材料相对密度。316L不锈钢/ARZ复合材料的硬度随着ARZ陶瓷颗粒体积分数的增高而增大，当ARZ陶瓷颗粒的体积分数为60%时，复合材料的硬度达到最大值HRB 96.8。复合材料耐磨性优于不锈钢基体，其中含有体积分数为60%ARZ陶瓷颗粒的复合材料体积磨损率较基体减少了4.2倍；随着ARZ陶瓷颗粒含量的增加，复合材料的耐磨性提高，复合材料的磨损机理主要为316L不锈钢的剥落。     

显微组织结构对GJW35钢结硬质合金热疲劳性能的影响

分析了热处理后ＧＪＷ３５钢结硬质合金的显微组织结构，研究了显微组织对合金的热疲劳裂纹萌生及扩展的影响。结果表明，热疲劳裂纹优先在硬质相区中萌生、扩展，钢基体相阻碍裂纹的萌生及扩展。改善显微组织结构，可提高合金的抗热疲劳性能     

喷射成形WC颗粒增强高速钢基复合材料中WC的颗粒行为

研究了喷射成形制备的ＷＣ颗粒增强Ｍ２高速钢复合材料中ＷＣ颗粒瓣形貌变化、成分变化。结果表明，ＷＣ颗粒的形貌、成分发生了较大的变化，但是微硬度并没有发生明显的下降。ＷＣ颗粒增强ＭＭＣｓ的硬度明显高于喷射成形高速钢和铸锻高速钢。     

SiC颗粒强化铝基复合材料及其断裂韧性

介绍了ＳｉＣ颗粒强化铝基复合材料的性能及一些应用，阐述了ＳｉＣ颗粒的体积百分比对ＳｉＣ颗粒强化的６０６１铝合金复合材料的断裂韧性及断裂机理的影响。     

纳米SiC增强纯Al基复合材料的微观组织和力学性能

与采用微米尺度SiC颗粒为增强相制备的Al基复合材料相比,以纳米SiC颗粒为增强相制备的Al基复合材料具有更加优异的力学性能,可极大提高SiC增强Al基复合材料的服役可靠性及应用范围。采用传统粉末冶金方法制备纳米SiC颗粒增强纯Al基复合材料,研究烧结温度和增强相体积分数对复合材料微观结构和力学性能的影响。研究表明,烧结温度和增强相体积分数均对复合材料的微观结构和力学性能有重要影响。随烧结温度升高,复合材料中的残留微孔减少,密度和强度均得到显著提高。含体积分数为3%纳米SiC颗粒的复合材料在610℃具有最高的强度,进一步提高纳米SiC颗粒的含量并不能提高材料的力学性能,这主要是由于当纳米SiC颗粒的体积分数超过3%时将出现明显的团聚,从而降低强化效应。     

放电等离子烧结法制备金刚石/Cu复合材料

通过真空镀铬对金刚石颗粒进行表面改性,采用放电等离子烧结法(SPS)制备改性金刚石/Cu复合材料;研究金刚石的体积分数、工艺参数以及金刚石颗粒表面改性对复合材料导热性能的影响。结果表明,烧结温度、混料时间以及金刚石颗粒的体积分数都会影响材料的致密度,金刚石颗粒的体积分数还会影响材料的界面热阻,而致密度和界面热阻是影响该复合材料导热性能的2个重要因素;对金刚石颗粒进行真空镀铬表面改性,可改善颗粒与铜基体的润湿性,降低界面热阻。在一定的工艺条件下,镀铬金刚石体积分数为60%时,改性金刚石/Cu复合材料具有很高的致密度,其热导率达到503.9W/(m.K),与未改性的金刚石/Cu复合材料相比,热导率提高近2倍,适合做为高导热电子封装材料。     

热等静压法制备SiC_p/Al复合材料的组织及性能研究

采用热等静压法制备SiC颗粒增强铝基复合材料,研究其显微组织和力学性能,分析复合材料的断口形貌及断裂机制,测定了其热膨胀系数。结果表明:热等静压后,复合材料中的SiC颗粒会出现颗粒团聚,形成硬质的SiC骨架。对于20%SiC_p/6061Al(体积分数)复合材料,其抗拉强度能达到304 MPa,而20%SiC_p/2024Al(体积分数)的抗拉强度为276 MPa,两种复合材料的抗拉强度都达到或超过其他制备方法的水平。复合材料的断裂方式为基体的韧性断裂、SiC颗粒的解理断裂、SiC颗粒与基体的界面脱粘3种方式并存的混合断裂形式。对比复合材料热膨胀系数的实际测量值和Turner、Kerner模型理论值,Turner模型理论值更接近实测值。     

12%SiCp/Al复合材料制备工艺及力学性能研究

对碳化硅颗粒进行表面氧化酸洗处理，采用粉末冶金加热挤压工艺制备了12％SiCp／Al（体积分数）复合材料。利用金相显微镜和电镜对微观组织进行了观测，拉伸试验测试复合材料的力学性能。试验结果表明：SiC颗粒在铝基体中分布比较均匀；T6热处理条件下12％SiCp／Al复合材料的屈服强度和抗拉强度分别约为472．4MPa、525．7MPa，伸长率为6．5％，弹性模量为92．7GPa。     

Effect of SiC volume fraction and particle size on the fatigue resistance of a 2080 Al/SiC p composite

The effect of SiC volume fraction and particle size on the fatigue behavior of 2080 Al was investigated. Matrix microstructure in the composite and the unreinforced alloy was held relatively constant by the introduction of a deformation stage prior to aging. It was found that increasing volume fraction and decreasing particle size resulted in an increase in fatigue resistance. Mechanisms responsible for this behavior are described in terms of load transfer from the matrix to the high stiffness reinforcement, increasing obstacles for dislocation motion in the form of S’ precipitates, and the decrease in strain localization with decreasing reinforcement interparticle spacing as a result of reduced particle size. Microplasticity was also observed in the composite, in the form of stress-strain hysteresis loops, and is related to stress concentrations at the poles of the reinforcement. Finally, intermetallic inclusions in the matrix acted as fatigue crack initiation sites. The effect of inclusion size and location on fatigue life of the composites is discussed.     

表面镀钨金刚石/铜复合材料的有限元模拟

利用有限元分析软件ANSYS,对表面镀钨金刚石/铜复合材料进行了数值模拟,研究了金刚石体积分数、金刚石粒径及镀层厚度对表面镀钨金刚石/铜复合材料导热系数和热膨胀系数的影响。结果表明:随着金刚石体积分数的增加、金刚石粒径的增大、镀层厚度的减小,复合材料的导热系数呈现出增加的趋势,与文献数据的变化趋势相符,热膨胀系数受金刚石体积分数影响最大,金刚石粒径选在150~200 μm较为合适。     

Fatigue crack growth resistance of unidirectional fiber-reinforced titanium metal-matrix composites under transverse loading

The transverse fatigue crack growth resistance of unidirectional 8 and 35 pct 1140+/Ti-6-4 fiber-reinforced composites has been investigated. It has been found that, at a low fiber volume fraction, the transverse fatigue crack growth resistance of metal-matrix composites (MMCs) is improved with respect to the monolithic matrix alloy. This occurs because “holes” from debonded interfaces can trap the crack and reduce the average fatigue crack growth rates by periodically increasing the effective crack-tip radius. However, an increase of fiber volume fraction from 8 to 35 pct decreases the fatigue crack growth resistance dramatically, due to the significant increase of the frequency of interaction and coalescence between the main crack, the debonded interfaces, and microcracks.     

Fatigue in selectively fiber-reinforced titanium matrix composites

Many applications of the Ti alloy matrix composites (TMCs) reinforced with SiC fibers are expected to use the selective reinforcement concept in order to optimize the processing and increase the cost-effectiveness. In this work, unnotched fatigue behavior of a Ti-6Al-4V matrix selectively reinforced with SCS-6 SiC fibers has been examined. Experiments have been conducted on two different model panels. Results show that the fatigue life of the selectively reinforced composites is far inferior to that of the all-TMC panel. The fatigue life decreases with the decreasing effective fiber volume fraction. Suppression of multiple matrix cracking in the selectively reinforced panels was identified as the reason for their lack of fatigue resistance. Fatigue endurance limit as a function of the clad thickness was calculated using the modified Smith-Watson-Topper (SWT) parameter and the effective fiber volume fraction approach. The regime over which multiple matrix cracking occurs is identified using the bridging fiber fracture criterion. A fatigue failure map for the selectively reinforced TMCs is constructed on the basis of the observed damage mechanisms. Possible applications of such maps are discussed.     

SPS法制备SiC_P/Cu复合材料的研究

为了开发高导热低成本电子封装材料与器件,采用SPS方法制备了SiC/Cu复合材料,研究了SiC的粒径和体积分数对材料致密度和热导率的影响.结果表明:随着SiC体积分数的减少(从70%到50%),材料致密度逐渐提高;随着SiC粒径从40μm变化到14μm,材料的致密度提高.在材料未达到完全致密的情况下,材料的热导率主要受致密度的影响,SiC粒径的减小和体积分数的适宜降低对材料热导率的提高有利.此外,研究了对SiC进行化学镀铜对复合材料的影响.SiC化学镀铜改善了复合材料两相界面的润湿性,与未镀铜SiC相比,使样品相对密度提高了3%,热扩散系数提高了60%,热导率为167 W/(m·K).     

放电等离子烧结法制备高导热金刚石/Al复合材料

以金刚石颗粒和铝粉为原料,通过放电等离子烧结(spark plasma sintering,SPS)制备高导热金刚石/Al复合材料,在烧结前采用真空微蒸发镀钛工艺对金刚石颗粒进行表面金属化,以降低复合材料的界面热阻.研究SPS工艺参数、铝粉粒度搭配以及复合材料中金刚石含量(体积分数)等对该复合材料致密度及热导率的影响....     

SiC粒度及粉末装载量对SiCp/Al复合材料热循环行为及力学性能的影响

选用4种不同粒度的SiC分别与平均粒度为14 μm的SiC粉末混合,混炼后得到4种不同粉末装载量(体积分数)的喂料,采用粉末注射成形方法制备成SiC坯体,再无压熔渗Al～12%Si～8%Mg合金,获得高体积分数SiCp/Al复合材料,研究SiC粉末粒度及SiCp/Al复合材料中SiC的体积分数(即注射成形喂料中SiC粉...     

Effect of Volume Fraction of Particle on Wear Resistance of Al2O3／Steel Composites at Elevated Temperature

Inpreviouswork,heat resistingsteelwithlow carboncontentandhighoxidationresistanceatele vatedtemperaturewastakenasthematrixmaterial. AndAl2O3ceramicparticleswereutilizedasrein forcedphasefortheirgreatstabilityandhighrigidi tyatelevatedtemperature.Inorde…     

Ductile-reinforcement toughening in γ-TiAl intermetallic-matrix composites: Effects on fracture toughness and fatigue-crack propagation resistance

The influence of the type, volume fraction, thickness and orientation of ductile phase reinforcements on the room temperature fatigue and fracture resistance of γ-TiAl intermetallic alloys is investigated. Large improvements in toughness compared to monolithic γ-TiAl are observed in both the TiNb- and Nb-reinforced composites under monotonic loading. Toughness increases with increasing ductile phase content, reinforcement thickness and strength; orientation effects are minimal. Crack-growth behavior is characterized by steep resistance curves primarily due to crack trapping/renucleation and extensive crack bridging by the ductile-phase particles. In contrast, under cyclic loading the influence of ductile phases on fatigue resistance is strongly dependent upon reinforcement orientation. Compared to monolithic γ-TiAl, improvements in fatigue-crack growth resistance are observed in TiNb-reinforced composites only in the face (C-L) orientation; crack-growth rates for the edge (C-R) orientation are actually faster in the composite. In comparison, Nb-particle reinforcements offer less toughening under monotonic loading but enhance the fatigue properties compared to TiNb reinforcements under cyclic loading.