干摩擦条件下Al_2O_（3f）／ZL109复合材料的磨损行为

用压铸法制备Ａｌ２Ｏ（３ｆ）／ＺＬ１０９复合材料，研究了恢复合材料在干摩擦条件下磨损量与滑动距离的关系，结果表明：复合材料磨损失效的临界值远高于其基体合金．同一时刻对应的耐磨性也明显高于基体合金。借助ＳＥＭ及ＥＰＭＡ等手段对磨损表面及亚表面和粘着磨损的材料转移情况进行了观察和分析，并对磨损机制进行了讨论。     

钛合金材料防微动磨损涂层性能研究

采用超音速火焰喷涂工艺在TC4钛合金基体材料表面制备碳化铬系耐磨涂层,通过自制微动磨损试验设备测试不同对磨副、不同位移副值试验条件下带涂层的TC4钛合金材料的摩擦因数、磨损量等微动磨损性能,利用SEM、EDS、XRD等分析手段,对比分析微动磨损表面形貌、成分和相组成的差异.结果表明:不同摩擦副和位移副值条件下的摩擦因数...     

GF增强尼龙1010复合材料的磨擦学性能研究

制备了玻璃纤维（GF）增强尼龙1010复合材料,在环一块磨损试验机上研究了复合材料的摩擦学性能。结果表明：GF含量对复合材料的摩擦学性能有显著影响,GF质量分数为35％时增强效果较好;随着滑速的增加,GF增强尼龙1010复合材料的摩擦系数和磨损量持续上升。干摩擦下的复合材料磨损以疲劳断裂和粘着为主,且纤维出现磨损、断裂及从基体中剥落的现象。在油润滑下材料向对偶产生轻微的转移,与干摩擦相比复合材料的摩擦系数和磨损量大为降低;水润滑下的尼龙以化学腐蚀磨损和磨粒磨损为主,此时复合材料摩擦系数也有较大程度的降低,但磨损量较干摩擦增大。     

电刷镀Ni - P合金镀层的高温摩擦磨损性能

对电刷镀Ni - P合金镀层的高温摩擦磨损性能进行了研究.实验结果表明,在20CrMo钢基体上,电刷镀Ni - P合金镀层能有效降低试样在高温(450 ℃)下的摩擦因数,减小高温磨损量.其中,12 min电刷镀试样在高温摩擦测试前80 min内,摩擦因数基本维持在平均值约0.30,仅为20CrMo钢基体(0.60)的50%;80～120 min因镀层局部被磨损穿透,其摩擦因数缓慢增长;120 min后,基本维持在平均值约0.50,测试完成后质量磨损量为同等测试条件下20CrMo钢基体的19.99%;24 min电刷镀试样在450℃下摩擦测试180 min的整个过程中,摩擦因数均较稳定,平均值为0.30,高温摩擦磨损测试后的质量磨损量仅为20CrMo钢基体的6.36%.     

稀土镁合金的摩擦磨损性能

采用MMS-2A型环块式摩擦磨损试验机对稀土镁合金GW103K进行了摩擦磨损试验.试验结果表明:GW103K体积磨损量随着磨损时间和外载荷的增大而增大,当磨损时间超过30min,外载荷超过400N时,体积磨损量增大明显;摩擦因数在0.26~0.28之间变化.对摩擦副环块,转速与体积磨损量成正比,与摩擦因数成反比.     

碳化铬-镍铬涂层对几种陶瓷的滑动摩擦磨损

在ＭＭ－２００块－环接触磨损试验机上，测定了等离子喷涂碳化铬－镍铬涂层对烧结Ａｌ２Ｏ３、热压烧结Ｓｉ３Ｎ４、ＳｉＣ和等离子喷涂ＴｉＯ２涂层等四种陶瓷材料在干摩擦条件下的滑动摩擦系数和磨损量；利用ＳＥＭ、ＥＤＡＸ和ＸＲＤ等技术，观察和分析了摩擦副材料在磨损后的形貌、物质转移和物相转变；讨论了摩擦副材料的显微结构和某些物理性能、机械性能对碳化铬－镍铬涂层摩擦磨损行为的影响，结果表明：涂层与不同陶瓷对磨，不仅其磨损量相差很大，而且其摩擦磨损机理也不相同，摩擦磨损过程中对磨材料向涂层表面的转移，有利于提高涂层的耐磨能力。配对陶瓷的显微颗粒尺寸和弹性模量愈小，导热系数愈高，则与碳化铬－镍铬涂层的配对性能愈好。     

纳米SiO2填充尼龙PA10101的摩擦磨损性能实验研究

用纳米SiO2填充PAl010制备了尼龙复合材料，并用MM—200磨损试验机对尼龙复合材料与45钢在干摩擦条件下的摩擦磨损实验进行了实验．研究表明，纳米SiO2填充PAl010大幅度提高了尼龙复合材料的耐磨性，降低了摩擦系数。纳米SiO2填充量在10％左右时，尼龙复合材料达到最低摩擦系数O.32和最低磨损量O．2mg，磨损量比纯PAl010降低了60多倍，摩擦系数降低了1倍．对纳米Si02填充尼龙的磨损机理研究发现，纳米Si02填充尼龙复合材料的磨损机理受滑动速度和接触载荷影响比较大。当摩擦副PV值小于60Nm／s时，尼龙复合材料的磨损机理主要是切削和粘着磨损。当摩擦副PV值大于60Nm／s时，磨损机理转变为疲劳剥层或熔融流变，导致磨损量急剧增长。     

纳米SiO2增强尼龙摩擦学性能的影响因素研究

使用MM-200磨损实验机在干摩擦条件下研究了偶副表面粗糙度对质量分数为10%的纳米SiO2增强尼龙1010复合材料与45号钢对磨时摩擦学性能的影响,并利用光学显微镜和扫描电子显微镜对纳米SiO2-PA1010复合材料的转移膜和磨损机理进行了观察和分析.结果表明,随着偶副表面粗糙度的增加,纳米SiO2-PA1010复合材料的摩擦系数和磨损量均呈先下降达到一个最低值后又上升的趋势.说明存在一个最佳表面粗糙度,使材料的磨损最小.本实验中这个最佳粗糙度为Ra＝0.22μm.     

纳米SiO2填充尼龙PA1010的摩擦磨损性能实验研究

用纳米 Si O2 填充 PA1 0 1 0制备了尼龙复合材料 ,并用 MM- 2 0 0磨损试验机对尼龙复合材料与 45钢在干摩擦条件下的摩擦磨损实验进行了实验 .研究表明 ,纳米 Si O2 填充 PA1 0 1 0大幅度提高了尼龙复合材料的耐磨性 ,降低了摩擦系数 .纳米 Si O2 填充量在 1 0 %左右时 ,尼龙复合材料达到最低摩擦系数 0 .32和最低磨损量 0 .2 mg,磨损量比纯 PA1 0 1 0降低了 60多倍 ,摩擦系数降低了 1倍 .对纳米 Si O2 填充尼龙的磨损机理研究发现 ,纳米 Si O2 填充尼龙复合材料的磨损机理受滑动速度和接触载荷影响比较大 .当摩擦副 PV值小于 60 Nm/ s时 ,尼龙复合材料的磨损机理主要是切削和粘着磨损 .当摩擦副 PV值大于 60 Nm/ s时 ,磨损机理转变为疲劳剥层或熔融流变 ,导致磨损量急剧增长 .     

SiCp含量与粒径对SiCp-Al/无石棉有机摩擦材料摩擦学特性的影响

对不同体积含量（１０％,１５％,２０％）和不同粒径（６,１３μｍ）的ＳｉＣｐ增强Ａｌ９Ｓｉ铝基复合材料与无石棉有机摩擦材料组成的摩擦副的摩擦磨损特性进行了试验研究．试验表明：该摩擦副具有较稳定的摩擦系数;ＳｉＣｐ的含量和粒径对摩擦副的摩擦系数影响不大．摩擦材料的磨损量随ＳｉＣｐ含量和粒径的增大而减小．     

Wear mechanism for spray deposited Al-Si/SiC_p composites under dry sliding condition

Al-Si/15%SiCp(volume fraction) composites with different silicon contents were fabricated by spray deposition technique, and typical microstructures of these composites were studied by optical microscopy(OM). Dry sliding wear tests were carried out using a block-on-ring wear machine to investigate the effect of applied load range of 10-220 N on the wear and friction behavior of these composites sliding against SAE 52100 grade bearing steel. Scanning electron microscopy(SEM) and energy-dispersive X-ray microanalysis(EDAX) were utilized to examine the morphologies of the worn surfaces in order to observe the wear characteristics and investigate the wear mechanism. The results show that the wear behavior of these composites is dependent on the silicon content in the matrix alloy and the applied load. Al-Si/15%SiCp composites with higher silicon content exhibit better wear resistance in the applied load range. Under lower loads, the major wear mechanisms are oxidation wear and abrasive wear for all tested composites. Under higher loads, severe adhesive wear becomes the main wear mechanisms for Al-7Si/15%SiCp and Al-13Si/15%SiCp composites, while Al-20Si/15%SiCp presents a compound wear mechanism, consisting of oxidation, abrasive wear and adhesion wear.     

Wear behavior of Cu matrix composites reinforced with mixture of carbon and carbon nanotubes

In order to improve wear resistance and decrease the cost, carbon and carbon nanotubes reinforced copper matrix composites were fabricated by the power metallurgy method. The effects of carbon (carbon and carbon nanotubes) volume fraction and applied load on the friction coefficient and wear rate under dry sliding of the composites were investigated at room temperature. By scanning electron microscopy (SEM), the worn surfaces and debris were observed, and wear mechanism was also analyzed and discussed. The experimental wear process consists of the run-in, steady wear and severe wear process with the increasing of sliding distance. Both the friction coefficient and wear rate of the composites first decrease and then increase with the increasing of carbon volume fraction. The minimum friction coefficient and wear rate are obtained when carbon is 4.0vol%. The wear mechanisms of the composites change from the adhesive wear and delamination wear to abrasive wear with the increasing of carbon volume fraction. Funded by the National Natural Science Foundation of China (50873047) and the Natural Science Foundation of Gansu Province (3ZS061-A25-039)     

In situ prepared Al-Si alloy matrix composites reinforced by γ-Al2O3p

A γ-Al2O3 particles reinforced Al-Si alloy matrix composite was fabricated by adding NH4Al(SO4)2 to molten aluminum alloy. TEM observation shows that in-situ γ-Al2O3 particles are generally spherical and uniformly distributed in the matrix. The results of dry sliding wear tests show that the wear resistance of the composites increases with increasing mass fraction, and the volume loss is considerably lesser than that of the matrix and is lesser than that of the composites by adding γ-Al2O3 particles directly.     

Microstructural characterization and mechanical property of Fly Ash/Al-25Mg composites

Fly ash/Al-Mg composites are fabricated by powder metallurgical method. The morphology and structure of fly ash/A l-Mg composites are characterized by scanning electron microscope （SEM） and X-ray diffraction, respectively. The influences of different fly ash content on the friction and wear behavior of the composites are investigated at a constant sliding velocity of 400 r/min and the worn mechanism of composites is discussed. The results indicate that the friction coefficient is steadily lower than that of Al alloy matrix at the lower fly ash content and loads. For the fly ash/Al-Mg composites, the wear mechanism is characterized as abrasive wear and adhesive wear under small normal load and at low fly ash content, and it is characterized as delamination wear and abrasive wear transferred onto the counterpart under high normal load and at high fly ash content.     

Fabrication and properties of Al matrix composites strengthened by in situ alumina particulates

New aluminum matrix composites strengthened by Al2O3 particulates through stirring cast by adding NH4Al（SO4）2 to the molten aluminum have been fabricated. TEM observation shows that in-situ Al2O3 particulates are generally spherical and they are uniformly distributed in the Al matrix. Dry sliding wear test results show that the volume loss of the unreinforced Al matrix is about three times that of the Al2O3 reinforced metal matrix composite （MMC） and the volume loss of the MMC fabricated by adding Al2O3 is larger than that of the MMC by adding NH4Al（SO4）2. Lubricating sliding wear test results show that the volume loss of the MMCs increases more slowly than that of the matrix with the increasing of the load.     

指尖密封用炭-炭复合材料摩擦磨损性能

为确定指尖密封用炭-炭(炭纤维增强炭基体)复合材料的摩擦学性能,针对指尖密封的轻载使用条件,应用UMT-2摩擦磨损测试仪进行炭-炭复合材料摩擦磨损性能试验,测量摩擦系数与磨损率,并采用扫描电子显微镜(SEM)分析材料的摩擦磨损机理.结果表明,无纬布层垂直于摩擦平面时,材料的摩擦系数和磨损率较低.载荷增加,较高密度材料的磨损率增加缓慢,摩擦系数减小.与载荷相比,材料磨损率受频率的影响较小,且随频率升高摩擦磨损性能越好.磨损表面的SEM分析表明:低频、低载条件下材料发生磨粒磨损;频率的提高加快磨屑膜的成形,自润滑能力增强;载荷的增加虽使磨屑快速被挤压形成磨屑膜,但磨屑膜被不断挤出剥落,纤维裸露断裂产生严重磨损,这一点在材料密度较低时表现更为显著.选用较高密度的材料以及布置无纬布层垂直于摩擦平面可以有效缓解密封材料的磨损.     

Tribological Behavior of Nano-ZrO_2 Reinforced PTFE-PPS Composites

Polytetrafluoroethylene(PTFE) is a commonly used seal material for oil-free engine that is well known for its excellent tribological properties. In this work, the nano-ZrO_2 particles were used as the friction modifiers to improve the friction and wear performance of PTFE-PPS composites. The friction and wear characteristics of PTFE/PPS-nano-ZrO_2 composites were investigated by a block-on-ring tester under dry friction sliding condition. The worn surfaces, counterpart transfer films and wear debris were studied by scanning electron microscopy and X-ray photoelectron spectroscopy. It was found that the increase of nanoZrO_2 content could effectively reduce the coefficient of friction and enhance the anti-wear ability of PTFEPPS composites. Especially, the best tribological properties of the composites were obtained when the particle content of nano-ZrO_2 was 10 vol%, the anti-wear performance of composite is 195 times better than that of the unfilled PTFE-PPS composite. Under different conditions, the coefficient of friction of PTFE/PPS-nano-ZrO_2 composites was more affected by the applied load while the wear rate was more affected by the sliding velocity.     

Surface functionalized carbon nanofibers and their effect on the dispersion and tribological property of epoxy nanocomposites

Surface functionalization of carbon nanofibers (CNFs) was carried out, i e, CNFs were firstly oxidized and then the surface was silanized by 3-Aminopropyltriethoxysilane (APTES) via an assembly method. A new kind of high wear resistance s-CNFs/epoxy composite was fabricated by in-situ reaction. FTIR spectroscopy was used to detect the changes of the functional groups produced by silane on the surface of CNFs. The tribological properties and microstructures of modified and unmodified CNFs/epoxy composites were studied, respectively. The expremental results indicate that APTES is covalently linked to the surface of CNFs successfully and improves the dispersion of CNF in epoxy matrix. The friction coefficients and the wear rates of s-CNFs/epoxy composites are evidently lower than those of u-CNFs/epoxy composites under the same loads. Investigations also indicate that abrasive wear is the main wear mechanism for u-CNFs/epoxy composite, with slight adhesive wear for s-CNFs/epoxy composite under the same sliding wear condition.     

In situ prepared Al-Si alloy matrix composites reinforced by γ-Al2O3p

A γ-Al2O3 particles reinforced Al-Si alloy matrix composite was fabricated by adding NH4Al（SO4）2 to molten aluminum alloy. TEM observation shows that in-situ γ-Al2O3 particles are generally spherical and uniformly distributed in the matrix. The results of dry sliding wear tests show that the wear resistance of the composites increases with increasing mass fraction, and the volume loss is considerably lesser than that of the matrix and is lesser than that of the composites by adding γ-Al2O3 particles directly.     

PTFE和MoS_2填充尼龙复合材料摩擦行为研究

以注塑成型法制备了聚四氟乙烯(PTFE)和MoS2填充PA1010复合材料,采用M-2000磨损试验机考察了复合材料与45钢对摩时的摩擦磨损性能,并利用扫描电子显微镜(SEM)分析了PA复合材料磨损表面及其偶件表面转移膜形貌。研究结果表明:PTFE填充PA1010可显著改善尼龙复合材料的摩擦磨损性能。PTFE质量分数为25%时,复合材料的摩擦学综合性能最佳。PTFE和MoS2共同填充PA1010时,复合材料的摩擦因数和磨损率随着PTFE含量的减少、MoS2含量的增加,整体呈现增大趋势,其中PA+20%PTFE+5%MoS2复合材料的减摩抗磨性能较好。在正常工作条件下(0.21-0.42 m/s,100-300 N),PA+25%PTFE复合材料的抗磨性优于相同条件下PA+20%PTFE+5%MoS2复合材料,但PA+20%PTFE+5%MoS2复合材料具有更宽的速度适用范围。PA复合材料的摩擦磨损性能与其在偶件表面形成的转移膜的特性有重要关系,转移膜的厚度大小、分布均匀状况以及和偶件的结合强度都会对复合材料的减摩抗磨性能产生影响。