碳纤维增强铜基复合材料摩擦与磨损行为的研究

研究了用热压法制造的碳纤维增强铜—5％锡基复合材料的摩擦磨损行为。对碳纤维的体积分数改变时,复合材料的摩擦系数,磨损速率的变化规律作了分析,进行了磨屑成分分析及磨面的形貌观察,初步提出了这种复合材料的磨损机制。实验结果表明:随着碳纤维含量的增加,复合材料的摩擦系数下降、磨损率减小,认为在给定的实验条件下,“碳纤维/铜—5％锡”复合材料的磨损是粘着和氧化共同作用的结果,在高温下或纤维体积含量较高时,氧化磨损是主要磨损形式。     

不同压力下聚四氟乙烯复合材料的磨损行为

对炭纤维等无机填料增强的聚四氟乙烯(PTFE)复合材料在低、中、高压下的摩擦磨损行为进行了研究。利用扫描电子显微镜分析了材料的磨损状况,利用差热扫描量热分析仅、X射线衍射仪对材料的热性能及结晶性能进行了分析,并与材料的摩擦、磨损性能相联系．研究结果表明．高压摩擦环境中,蠕变的发生是加速PTFE复合材料磨损、恶化材料性能的主要原因;高比表面填料的加入会提高复合材料的熔化热,有助于降低材料的磨损率;结晶度的提高对增强复合材料的耐蠕变性有明显的效果。     

微波烧结原位合成TiC增强钛复合材料的性能

以纳米管(MWCNTs)和纯钛为原料,用微波烧结法原位合成TiC增强钛基复合材料,研究了这种材料的组织和性能并探讨了TiC增强相的生成机理.结果 表明,微波烧结时MWCNTs与Ti原位生成TiC增强相.MWCNTs的添加量(质量分数,下同)低于1％时TiC呈现颗粒状且分布均匀,Ti基体致密;MWCNTs的添加量高于1....     

碳纤维增强TiC复合材料的抗热震性能

通过测量力学性能和热物理性能,研究了热压烧结碳纤维增强TiC复合材料（Cf/TiC,20vo%碳纤维）的抗热震性能。结果表明,碳纤维加入到TiC基体中,提高了复合材料的抗弯强度和断裂韧性,降低了复合材料的弹性模量和热膨胀系数,进而使得复合材料的抗热震断裂参数R,抗热震损伤参数R^TV和裂纹稳定性参数RST都得以提高,复合材料热震残留强度在热震温差超过900℃后迅速下降。复合材料热扩散率的提高有利于抗热稳定性能的提高,复合材料增强机理是纤维承载。韧化机理是纤维桥联和纤维拔出。     

自生TiC颗粒增强钛基复合材料的研究进展

从自生TiC颗粒增强钛基复合材料（PTMCs）的制备方法、微观组织及界面结构、性能和应用与展望4个方面论述了自生TiC颗粒增强钛基复合材料的研究进展。重点介绍了近年来PTMCs的一些制备方法及在室温、高温时的力学性能。     

自生TiC增强钛基复合材料的微观组织

采用反应自生法制备了ＴｉＣ颗粒增强钛合金基复合材料,研究了复合材料的相组成和微观组织。在Ｔｉ－６Ａｌ－２Ｃ合金中存在Ｔｉ和ＴｉＣ两种相。ＴｉＣ权树枝状初生Ｔｉｃ和短棒状共晶ＴｉＣ两种开头存在,其中共晶ＴｉＣ主要存在于晶界,特别是三角晶界处。ＴｉＣ晶格常数的计算结果表明ＴｉＣ的衍射峰存在一定的偏移,主要是由于存在于ＴｉＣ中的Ｃ空位引起晶格畸变。随着Ａｌ含量的增加,初生ＴｉＣ由发达粗大的树枝晶变为不发达的树枝晶,当Ａｌ含量为３５％时变为短棒状和薄片状的ＴｉＣ。基体组织也相应地由单一的Ｔｉ基体变为Ｔｉ和Ｔｉ３Ａｌ的两相基体以及Ｔｉ３Ａｌ和ＴｉＡｌ两相基体。根据相图分析了组织变化的主要原因。     

TiC颗粒增强非晶钛合金基复合材料的热稳定性

用单辊铜轮旋注法制备了TiC颗粒增强Ti45Zr5Cu25Ni20Sn5非晶合金基复合材料.发现在Ti45Zr5Cu25Ni20Sn5非晶合金中加入TiC颗粒可以提高合金的热稳定性.     

碳纤维增强TiC复合材料的制备与高温强度

采用热压烧结工艺制备了碳纤维增强 Ti C复合材料 (2 0 vol%碳纤维 ) ,研究了热压烧结温度对力学性能的影响和碳纤维对复合材料高温强度的增强作用。结果表明 :采用球磨湿混工艺将易于团聚的短碳纤维均匀地分散在 Ti C基体中 ,Cf/ Ti C复合材料最佳热压烧结温度为 2 10 0℃ ,Cf/ Ti C复合材料的室温抗弯强度为 5 93MPa,断裂韧性为 6 .87MPa· m1 / 2 ,140 0℃时的高温抗弯强度为 439MPa。定量分析了碳纤维对复合材料的增强和增韧效果     

原位合成TiC颗粒增强铁基复合材料的微观结构研究

采用不同化学成分基体制备了原位合成ＴｉＣ颗粒增强铁基复合材料,并以透射电镜为手段对其微观结构进行了分析研究,结果表明,ＴｉＣ增强相周围基体组织与基体含碳量有关,基体中较高的含碳量有助于抑制Ｆｅ２Ｔｉ相的形成,在含钼基体中ＴｉＣ增强相与基体之间存在一富钼的包覆层,进一步改善了基体对碳化钛的润湿性,有利于增强体在基体中的均匀分布。     

聚八钛酸钾晶须增强ZL109复合材料的润滑磨损行为

本文研究了聚八钛酸钾晶须增强ＺＬ１０９复合材料的润滑磨损行为。研究发现，聚八钛酸钾晶须增强铝合金复合材料和ＺＬ１０９的磨损量随负荷的增加而增加在较低负荷的条件下，两种材料的耐磨性大致相当；在较高负荷的条件下该复合材料的耐磨性高于ＺＬ１０９。     

苎麻纤维/聚乳酸复合材料在不同pH环境下的水解行为

以生物基树脂聚乳酸为基体,以植物纤维苎麻为补强剂,利用熔融共混法制备了苎麻纤维/聚乳酸(RF/PLA)复合材料,考查了RF/PLA复合材料在不同pH环境下的水解行为,并以力学性能测试、SEM、DSC和维卡软化温度检测为手段对其降解行为进行了评估。结果表明:RF/PLA复合材料在碱性(pH=12.0)环境中的降解比在酸性(pH=2.0)和中性(pH=7.0)环境中的更快,界面侵蚀空化是其性能劣化的主要原因。RF的加入提高了PLA的结晶度和维卡软化温度,同时也加快了PLA的降解速度,降解导致材料的力学强度下降。随着降解过程的加剧,RF/PLA复合材料的结晶度和维卡软化温度因材料内部产生缺陷而有所降低;而纯PLA树脂的结晶度却随碱液处理时间的延长而增加,但其维卡软化温度没有发生明显的变化。     

Wear characteristics of hybrid aluminium matrix composites reinforced with graphite and silicon carbide particulates

This investigation studies the dry sliding wear behaviour of Al matrix composites reinforced with Gr and SiC particulate up to 10%, to study the effect of % reinforcement, load, sliding speed and sliding distance on stir cast Al–SiC–Gr hybrid composites, Al–Gr and Al–SiC composites. Parametric studies indicate that the wear of hybrid composites has a tendency to increase beyond% reinforcement of 7.5% as its values are 0.0242 g, 0.0228 g and 0.0234 g respectively at 3%, 7.5% and 10% reinforcement. The corresponding values are 0.0254 g, 0.0240 g and 0.0242 g in Al–Gr composites and 0.0307 g, 0.0254 g and 0.0221 g in Al–SiC composites, clearly indicating that hybrid composites exhibit better wear characteristics. Increase of speed reduces wear and increase of either load or sliding distance or both increases wear. Statistical analysis has revealed interactions among load, sliding speed and sliding distance in composites with Gr particulates.     

Sliding friction and wear behaviour of vinylester and its composites under dry and water lubricated sliding conditions

In this paper, we studied and explored the tribological performance of pure vinylester (V), glass fiber reinforced (GFR), SiC filled glass fiber reinforced vinylester composite under dry and water lubricated sliding conditions. Friction and wear tests were carried out with configuration of a pin on a rotating disc under ambient conditions. Tests were conducted at normal load 10, 30 and 50 N and under sliding speed of 1.6 m/s, 2.8 m/s and 4 m/s. The results showed that the coefficient of friction decreases with the increase in applied normal load values both under dry and water lubricated conditions. On the other hand for pure vinylester specific wear rate increases with increase in applied normal load under dry sliding condition and decreases with increase in applied normal load under water lubricated conditions. However the specific wear rate for GFR vinylester composite and SiC filled GFR vinylester composite decreases with the increase in applied normal load both under dry and water lubricated conditions. Moreover, for the range of load and speeds used in this investigation the coefficient of friction and specific wear rates using water lubricant registered lower values than that of the dry condition. The specific wear rates for pure vinylester and vinylester + 50 wt.% GFR and SiC filled GFR vinylester composite under dry and water lubricated sliding condition were in the order of 10⁻⁷ mm³ N⁻¹ mm⁻¹.     

Investigation of microstructure and wear behaviors of al matrix composites reinforced by carbon nanotube

In this study, the effect of CNT amount in Al-CNT composites produced by adding carbon nanotube (CNT) to 7075 Al alloy in various amounts on microstructure and wear behaviors of aluminum matrix composites was investigated. CNT was added to 7075 Al alloy powder at five different amounts. The powders were mechanically milled for 2 hours. Mechanical milled powders were cold pressed and then pre-shaped by hot pressing. Pre-shaped samples were sintered for 1 hour under 10^?6 millibar in 580°C. Microstructure examinations, hardness measurements, and wear tests were carried out. The results show that CNT's in the microstructure were agglomerated as nanotube amount increases and there was no uniform distribution. The highest hardness value was obtained in AMC reinforced with 1% CNT while it is seen that hardness of the composite decreases and weight loss increases as CNT amount increases.     

炭/炭复合材料高温力学行为研究

借助三点弯曲试验和扫描电镜观察,对层压结构C C(2D)、三维整体编织结构C C(3D)在高温1700℃及室温下的弯曲力学行为进行了研究,总结了各自性能及损伤破坏的特点。试验结果表明:3DC C以纤维断裂的形式发生弯曲破坏,其弯曲强度、模量均远大于2DC C;对于2DC C,其弯曲破坏模式为基体的层间开裂,材料性能在很大程度上受到炭基体以及界面状态的控制;C C复合材料在高温下弯曲力学性能大幅提高,强度增加幅度高达45%以上,模量增加幅度达15.3%;高温下界面粘结强度增加,导致3DC C的损伤破坏模式有所变化。     

非连续增强金属基复合材料剧烈塑性变形行为研究进展

综述了非连续增强金属基复合材料剧烈塑性变形(SPD)行为的研究进展,系统阐述了等径弯曲通道变形(ECAP)、高压扭转(HPT)、多向锻造(MF)、累积叠轧(ARB)和循环挤压压缩(CEC)5种SPD的加工原理和方法。集中介绍了这些方法在铝基、镁基、铜基和钛基等金属基复合材料方面应用的研究进展。重点介绍了金属基复合材料SPD的微观组织演化和变形力学行为,详细阐明了金属基复合材料SPD机制以及超细晶形成机理,指出了金属基复合材料在SPD中存在的深层次问题及发展趋势,展望了利用SPD方法制备超细晶非连续增强金属基复合材料的应用前景。     

铜基复合材料干湿条件下的摩擦学行为

采用粉末冶金技术制备铜基复合材料,在制动压力0. 5～1. 2 MPa 范围内,通过定速摩擦试验机研究了干、湿条件下,速度、压力与材料摩擦磨损性能的关系,结果表明:影响摩擦磨损性能的重要因素在于载荷性质和第三体状态。在干摩擦条件下,处于低摩擦速度范围时,摩擦力的静载荷性质使第三体呈疏松状态,这增加了微凸体间的啮合程度而使摩擦系数处于较高值。随第三体致密性增加,其润滑作用增强,微凸体间的机械啮合程度减弱,使材料的摩擦系数和磨损量降低。在高速摩擦时,微凸体间的冲击作用使处于摩擦表层的硬质颗粒容易发生粉碎性破损而弥散分布,这强化了表面强度而使摩擦系数有所增加。摩擦压力对高速摩擦性能影响明显,原因在于高负荷加剧了摩擦面的变形和损伤程度。湿摩擦条件下,水膜的润滑和流动具有降低摩擦系数和增加磨损率的作用主要体现在低速低压条件下。在高摩擦速度和高压力条件下,水分的高温蒸发与离心作用明显,破坏了水膜的存在条件,从而使材料的摩擦磨损性能与干摩擦状态相近。      

低能载条件下C/C复合材料滑动摩擦磨损性能

采用MM-200型环-块摩擦磨损试验机测试了针刺碳毡增强C/C复合材料试样在不同载荷和转速条件下的摩擦磨损性能,借助数码显微镜和扫描电镜观察分析了摩擦表面形貌。结果表明:当转速较低时,摩擦系数比较稳定,磨损率随载荷提高而增大;当转速较高时,低载荷试样摩擦系数不大,磨损率有所增加,而高载荷试样的摩擦系数在5分钟左右时出现峰值然后回落并保持稳定,磨损率急剧增加,说明磨损机制发生变化;摩擦面平行于X-Y向的C/C复合材料磨损率较小,具有较好的摩擦磨损性能。     

Tension behavior of unidirectional glass/epoxy composites under different strain rates

By considering wide applications of composite materials, having a proper knowledge of them under dynamic loading is necessary. In order to study the effects of strain rates on the behavior of the materials, special testing machines are needed. Most of the research in this field is focused on applying real loading and gripping boundary conditions on the testing specimens. In this study, behavior of unidirectional glass fiber reinforced polymeric composites under uni-axial loading is determined at quasi-static and intermediate strain rates of 0.001–100 s⁻¹. The tests were performed using a servo-hydraulic testing apparatus equipped with a strain rate increase mechanism. For performing the tests, a jig and a fixture are designed and manufactured. The performance of the test jig was evaluated and found to be adequate for testing of composites. Dynamic tests results are compared with the results of static tensile tests carried out on specimens with identical geometry. Experimental results show a significant increase of the tensile strength by increasing the strain rate. The tensile modulus and strain to failure are also observed to increase slightly by increasing the strain rate.     

连续制动条件下泡沫陶瓷/金属双连续相复合材料的摩擦磨损性能EI北大核心CSCD

为解决履带式特种车辆机械制动器过热失效问题,采用挤压铸造法制备SiC/Cu和SiC/Fe双连续相复合材料,研究两种材料在连续紧急制动工况和连续高温制动工况下的摩擦磨损性能。结合扫描电子显微镜(SEM)、X射线能谱分析(EDS)、三维形貌仪等手段分析摩擦因数、温度和磨损率的变化规律,揭示相应的磨损机理。结果表明:在连续紧急制动实验中,接触表面经历了摩擦膜形成和层间断裂过程,摩擦因数随接合次数增加略微下降,并趋于稳定。在前40次接合中,SiC/Cu和SiC/Fe摩擦副的磨损率整体下降。在40~60次接合中,SiC/Cu摩擦副黏着磨损、氧化磨损和疲劳磨损加剧,磨损率升高。而SiC/Fe摩擦副以磨粒磨损为主,磨损率较低。在连续高温制动实验中,摩擦因数在前6次接合中逐渐升高,制动时间逐渐缩短。在第6次接合后,摩擦副边缘区域出现的黏着磨损和疲劳磨损导致力矩下降,摩擦因数和制动时间均呈先降后升趋势。连续高温制动过程中以严重的黏着磨损为主,SiC/Cu和SiC/Fe摩擦副的磨损率均随接合次数增加而升高。