Al2O3/Cu复合材料的载流摩擦磨损性能

研究了采用内氧化法制备的Al2O3／Cu复合材料在载流条件下的干滑动摩擦磨损性能，结果表明，在相同条件下，Al2O3／Cu复合材料的抗摩擦磨损性能明显优于紫铜；当电流一定时，随着速度与载荷的增加，销试样的磨损率增加，摩擦因数降低。Al2O3／Cu复合材料销试样表层发生了磨粒磨损和粘着磨损，紫铜表层主要发生了粘着磨损。在试验范围内，质量分数为0．60％的Al2O3的Cu肚复介材料比质量分数为0．24％的磨损率和摩擦因数低。     

润滑条件下Mg2B2O5/6061Al基复合材料摩擦磨损性能研究

采用自制的机械-超声混合搅拌设备制备出Mg2B2O5/6061Al铝基复合材料,复合材料的体积分数为2%。研究了载荷和滑动速度对基体以及复合材料的摩擦磨损性能的影响。实验结果表明,基体和复合材料摩擦系数总体上随着载荷和滑动速度的增加而减小。基体和复合材料的磨损率随载荷和滑动速度的增加而明显的增大,且基体和复合材料均存在一个临界载荷和临界滑动速度。当载荷和滑动速度到达临界值后,磨损率均急剧增大,此时试样摩擦磨损机制由微观疲劳磨损和磨粒磨损向粘着磨损与剥离磨损转变。     

增强颗粒对镁基复合材料磨损性能的影响(英文)

研究增强颗粒Mg2Si对镁基复合材料摩擦磨损性能的影响,讨论Si加入量、载荷和滑动速度对Mg2Si/AM60镁基复合材料磨损性能的影响。结果表明,向镁合金中加入合金元素Si,可原位生成增强颗粒Mg2Si,增强颗粒Mg2Si可明显提高AM60镁合金的磨损性能。随着载荷和滑动速度的增加,AM60镁合金和Mg2Si/AM60镁基复合材料的磨损量都增大。AM60镁合金的磨损机制为粘着磨损。随着载荷的增大,Mg2Si/AM60镁基复合材料的磨损由磨粒磨损向粘着磨损转变。     

Ti基内生枝晶非晶复合材料的摩擦磨损性能

采用电弧熔炼-铜模吸铸法制备Ti_(43)Zr_(27)Mo_5Cu_(10)Be_(15)非晶复合材料,利用销-盘式摩擦磨损试验机进行干滑动磨损试验,研究了载荷、转速和时间对非晶复合材料的摩擦磨损性能的影响。利用X射线衍射仪分析物相,扫描电镜观察分析磨损表面的形貌,探讨非晶复合材料的磨损机理。结果表明,在不同载荷、转速条件下摩擦因数比较低且稳定在0.219 0~0.367 5之间,磨损量为2.0~31.9mg;随着转速、载荷的增加,动态摩擦因数波动幅度逐渐减小,磨损量增大。磨损机制由磨粒磨损逐渐转变为粘着磨损,并伴有塑性变形。     

粉煤灰/铝-镁合金复合材料的微观组织及摩擦磨损性能

采用粉末冶金法制得粉煤灰/Al-25%Mg复合材料,研究不同粉煤灰含量对复合材料微观组织、硬度和摩擦磨损性能的影响,采用扫描电子显微镜观察复合材料的磨损表面形貌,并对其磨损机制进行探讨。结果表明:随着粉煤灰含量的增加,复合材料的硬度呈现先增大而后减小的趋势;在较低粉煤灰含量和较低载荷下,该复合材料的摩擦因数均低于基体铝合金的,并且随粉煤灰含量的增加复合材料的耐磨性有所提高,复合材料的磨损机制主要为粘着磨损和磨粒磨损;在较高粉煤灰含量和较高载荷下,该复合材料的磨损机制转化为以剥层磨损和磨粒磨损为主。     

正火温度对高碳钢组织与耐磨性能的影响

在MFT-3000型摩擦磨损试验机测试了经不同正火温度处理后的高碳钢干滑动磨损性能,观察了其在不同摩擦载荷、滑动速度及滑动时间下的磨损形貌,并分析了磨损机制。结果表明:在正火温度在850～1000℃时,高碳钢的组织主要为马氏体,具有较低的摩擦因数和磨损量。随施加载荷、滑动速度和滑动时间增加,磨损量均增加;实验高碳钢在不同载荷下均有粘着磨损,随载荷增大氧化磨损加剧并伴有磨粒磨损,高速滑动下,以磨粒磨损为主,氧化磨损作用变大,随滑动时间延长,磨损机制由磨粒磨损为主向粘着磨损为主转变,还出现了疲劳磨损。     

(TiB2+Al3Ti)/Al-4.5Cu原位复合材料的高温耐磨性能

本文采用混合盐法制备了(TiB2 Al3Ti)/Al4.5Cu原位复合材料,研究了该复合材料在150℃下的干摩擦滑动磨损行为,并与基体合金进行对比.结果表明,载荷在10～20 N之间时,(TiB2 Al3Ti)/Al-4.5Cu原位复合材料的磨损量低于基体合金,但并不明显;随载荷的增加(特别是当载荷超过30 N之后),复合材料的磨损量仍低于基体合金,且复合材料的磨损量增大的速度小于基体合金磨损量的增长速度.(TiB3 Al3Ti)/Al-4.5 Cu原位复合材料同45钢对磨时的主要磨损机制为粘着磨损和磨粒磨损.随着原位反应体系中混合盐含量的增加,复合材料的耐磨性能提高,并逐渐由粘着磨损向磨粒磨损过渡.     

不同载荷下再生复合辊环耐磨性能研究

通过对回收的废旧复合辊环材料进行重熔和离心铸造,制备了由耐磨WCp颗粒增强的复合层与Fe-C合金基体组成的再生复合材料辊环,并采用MMS-1G高速销-盘摩擦磨损试验机、扫描电镜(SEM),研究了在100、150和200 N载荷下滑动速度对再生复合辊环的摩擦性能的影响.结果表明,在100、150和200 N载荷条件下,随滑动速度的增加,再生复合辊环的磨损率均出现幅度很小的波动现象,而摩擦因数先降低后缓慢增加.在相同滑动速度条件下,磨损率明显随载荷的增加而增大,而摩擦因数随载荷的增加而降低.再生复合辊环在低速条件下的磨损机理主要为犁沟磨损和塑性变形,而当滑动速度较高时,表现为粘着磨损、氧化磨损和磨粒磨损.     

生理盐水润滑下PEEK/WK复合材料的摩擦学性能

为研究生理盐水润滑条件下碳酸钙晶须含量、载荷大小、滑动速度因素对PEEK/CaCO3复合材料摩擦学性能的影响规律,并考察复合材料的摩擦学稳定性,在自制改性偶联剂处理晶须表面的基础上制备了PEEK/CaCO3复合材料,利用MMW1A立式万能摩擦磨损试验机对复合材料的摩擦学性能进行测试,用扫描电子显微镜(SEM)对磨损表面形貌进行扫描分析表征。结果表明,晶须含量对复合材料摩擦学性能影响明显,在0.9%的生理盐水润滑条件下PEEK/CaCO3复合材料随着晶须含量的增加,摩擦因数及比磨损率均呈现先减小后增大现象;当晶须质量分数为15%左右时,复合材料的摩擦因数达到最低值,同时比磨损量相对最低,复合材料与摩擦副的磨合过程相对平稳,具有较好的摩擦学性能,表现为粘着腐蚀磨损特征。外加载荷、滑动速度增大,材料的摩擦因数增大,比磨损率增加。     

不同载荷下碳纤维增强碳基体复合材料的摩擦磨损性能

在Falex摩擦磨损实验机上研究了碳纤维增强碳基体（C／C）复合材料在不同载荷下的摩擦磨损性能,且对摩擦表面进行了SEM观察和分析。研究结果表明：C／C复合材料的摩擦系数随着载荷的增大呈现出先增大后减小的趋势,而磨损量则随着载荷的增大,整体呈现出逐渐增大的趋势;在高载荷下表面形成的磨屑膜,是导致摩擦系数减小的原因之一;随着载荷的逐渐增大,C／C复合材料的磨损由磨粒磨损为主逐渐向粘着磨损为主转变。     

T6态Al-10Si-5Cu-0.75Mg合金干滑动摩擦磨损性能的研究

利用UMT-2 型摩擦磨损试验机研究了T6态Al-10Si-5Cu-0.75Mg 合金的干滑动摩擦磨损性能,采取SEM、XRD、EDS等方法分析了合金在不同转速和载荷下的摩擦磨损行为。结果表明：合金的磨损率随转速和载荷的增加而增大,但在800 r/min的高转速下仍具有良好的耐磨性,15N高载荷时的磨损率相对于5N低载荷时只增加了291%,属于轻微磨损;摩擦系数的平均值在0.35-0.40范围内变化,且随时间的变化不大,具有较高的稳定性;另外,磨损机制由低速轻载时的磨粒磨损、粘着磨损向高速重载时的剥层磨损、氧化磨损转变。     

基于稀土调控的激光熔覆Ni60强化铝合金的高温摩擦磨损性能研究

目的 提高铝合金的综合使用性能。方法 采用激光熔覆技术对6063铝合金表面分别进行了Ni60、Ni60+4%CeO2、Ni60+5%Y2O3和Ni60+5%La2O3激光熔覆处理,然后进行了硬度和高温摩擦磨损实验,通过分析各试样的摩擦系数、磨痕轮廓、磨损量、物相、成分和磨损后微观形貌,进而分析各试样的耐磨性能和磨损机理,以及稀土对熔覆层耐磨性能和磨损机理的影响。结果 熔覆层的硬度呈梯度分布,加入稀土Ni60熔覆层的硬度明显提升。6063铝合金随着载荷和磨损温度的升高,磨损机制从二体磨粒磨损,到粘着磨损,再到严重的熔融磨损和氧化磨损,由轻微向严重磨损转变。Ni60熔覆层的磨损机制主要为剥层磨损、氧化磨损和轻微的犁削磨损,并随着载荷和磨损温度的升高,剥层磨损的程度越来越严重。添加最佳稀土含量的熔覆层随着载荷和磨损温度的升高,磨损机制逐渐由以犁削磨损为主过渡为以剥层磨损为主,并含有氧化磨损和犁削磨损。与Ni60熔覆层相比,加入最佳稀土含量的熔覆层的高温摩擦磨损性能均有明显提高。结论 对比三种稀土熔覆层,高温摩擦磨损性能由好到差的顺序为Ni60+4%CeO2熔覆层>Ni60+5%Y2O3熔覆层>Ni60+5%La2O3熔覆层。     

高硅铝合金及其原位复合材料干滑动磨损性能与机制

采用熔体反应法制备了(Al2O3 Al3Zr)p/Al-22%Si原位复合材料。探讨了高硅铝合金及其原位复合材料的干滑动磨损行为,并对其磨损表面和亚表面形貌进行了观察和分析。试验结果表明:复合材料的磨损量显著低于同条件下高硅铝合金的磨损量,且随颗粒体积分数的增大,复合材料的磨损量减小。磨损表面亚表面的SEM观察分析表明:高硅铝合金磨损表面存在与亚表面相连的撕裂纹和宽大的犁沟,其磨损机制为粘着磨损加磨粒磨损的混合型磨损;复合材料的磨损表面亚表面平整光滑,主要表现为磨粒磨损。     

Fraction and wear performances of 7475 aluminium alloy after anodic oxidation

The layer of oxide film was prepared on the surface of 7475 aluminum alloy by anodic oxidation, and the friction and wear performance under different loads were investigated with the friction and wear test. The atomic binding energy spectrum, wear morphologies, surface hardness and residual stress were analyzed with XPS, SEM, hard meter and XRD stress tester, respectively. The results show that the oxide film on the surface is relatively dense after anodic oxidation, existing in the form of Al2O3, and the form of the diffusion type in the interface is contained. The average friction coefficient is decreased after anodic oxidation, indicating the friction performance improving. The wear mechanism of primitive sample is adhesive wear and tear, accompanying with abrasive wear, and the wear mechanism of the sample after the anodic oxidation is abrasive wear, where high surface hardness is the main factor of the wear resistance.     

银-石墨烯复合材料的滑动摩擦磨损性能

采用球磨混粉、冷等静压和真空烧结的工艺流程制备了含0.5%~2.0%石墨烯的银-石墨烯复合材料,并对复合材料进行销盘式摩擦磨损试验以研究其大气环境滑动摩擦磨损性能。研究结果表明,因石墨烯易团聚,石墨烯含量限于1.5%时能够有效改善复合材料的性能。与未增强的银相比,由于在接触表面形成自润滑碳质膜,银-石墨烯复合材料表现出较低的摩擦系数、较少的磨损量和较低的接触表面温度。随石墨烯含量的增加,复合材料的摩擦系数和磨损量均下降。复合材料的主要磨损机制为粘着磨损和磨料磨损。     

载荷和滑动速度对块体镁基非晶合金干摩擦性能的影响

目的以制备的Mg_(59.5)Cu_(22.9)Ag_(6.6)Gd_(11)块体镁基非晶合金为基础,探索法向载荷和滑动速度影响镁基非晶合金干摩擦行为的规律和机制,为进一步研究镁基非晶合金提供实验依据。方法采用UMT-2多功能摩擦磨损机,改变法向载荷和滑动速度的大小,进行摩擦磨损实验。通过白光干涉轮廓仪测出磨损轨迹的宽度和深度,再根据公式计算出磨损体积和磨损率。利用扫描电镜和EDS能谱分析磨损轨迹,揭示非晶合金的磨损机制。结果随着载荷的增加,磨损率先减小后稳定,摩擦系数略有减小。随着滑动速度的增加,磨损率先减小后增大,在相对滑动速度为120 mm/s时出现最小值。载荷小于20 N时,磨痕表面布满犁沟和小颗粒状磨屑;载荷大于20 N时,磨痕表面出现层叠状非均匀塑性变形层,对磨球表面转移膜粘连明显。滑动速度低时,磨痕表面布满犁沟,随着速度的增加,先是软化均匀流变,接着出现熔化、剥落。结论块体非晶镁基合金在低载荷下以磨粒磨损为主,还伴随着氧化、少量的粘着;载荷大于20 N时,变为粘着磨损为主。低滑动速度下以磨粒磨损为主,当滑动速度为180 mm/s时,试样表面熔化失效,磨损方式为剥落和磨粒磨损的综合。     

Research of the Tribological Properties of the Surface on 16Mn Steel by Plasma Nitriding and S-N-C Plasmas Composite Treatment

Sulfide layer with certain thickness was made on the nitrided surface of 16Mn steel by means of plasma S-C-N composite treatment. Under half lubricated condition, friction coefficient and wear loss of LY12 aluminum alloy were measured in sliding against samples of 16Mn treated by cubrizing and sulphiding respectively; In order to avoid the transfer of aluminum to the steel that lead to the inaccurate measurement of wear loss of carburized samples, Grl5 steel was adopted as counterpart face to measure the wear loss of them. SEM and EDAX were used for the morphological and chemical characterization of the wear surface and longitudinal cross-sections beneath sliding surface of LY12 aluminum alloy cirque and the wear tacks of the carburized samples and sulphided samples. Results show: The surface roughness,wear rate, average friction coefficient and magnitude of friction fluctuations of LY12 aluminum alloy cirque sliding against sulphided sample were all lower than sliding against carburized sample; Compared with carburized layer, sulfide layer of 16Mn steel can not only efficiently prevent the occurrence of adhesion when sliding against LY12 aluminum alloy, but also greatly lower the wear loss when sliding against Gr15 steel.     

硼酸镁晶须增强6061铝基复合材料的干摩擦磨损行为(英文)

研究搅拌铸造工艺制备的硼酸镁晶须增强6061铝基复合材料在干滑动条件下的摩擦磨损性能。复合材料的体积分数为2%,根据增强体种类,材料分别记为:Al基体、Mg2B2O5w/6061Al、ZnO/Mg2B2O5w/6061Al和CuO/Mg2B2O5w/6061Al;讨论磨损速率和摩擦因数之间的关系。结果表明:在4种材料中,ZnO/Mg2B2O5w/6061Al复合材料的磨损率最低。随着载荷和滑动速度的增大,基体和复合材料的摩擦因数和磨损率降低,摩擦磨损机制由轻微磨损机制转向严重磨损机制。     

Wear and Friction Behavior of the Spray-Deposited SiCp/Al-20Si-3Cu Functionally Graded Material

The spray-deposited SiCp/Al-20Si-3Cu functionally graded material (FGM) can meet the structure design requirements of brake disk. The effects of rotational speed and load on the wear and friction behaviors of the SiCp/Al-20Si-3Cu FGM sliding against the resin matrix friction material were investigated. For comparison, the wear and friction behaviors of a commercially used cast iron (HT250) brake rotor were also studied. The results indicate that the friction coefficient of the SiCp/Al-20Si-3Cu FGM decreases constantly with the increase of load or rotational speed and is affected by the gradient distribution of SiC particles. The wear rate of the SiCp/Al-20Si-3Cu FGM firstly increases, then decreases and finally increases again with increasing load or speed, and is about 1/10 of that of HT250. Based on observations and analyses on the morphology and substructure of the worn surface, the mechanical mixing layer acts as a protective coating and lubricant, and its thickness reduces with the SiC content increasing. Furthermore, it is proposed that the dominant wear mechanism of SiCp/Al-20Si-3Cu FGM changes from the abrasive wear to the oxidative wear and further to the delamination wear with increasing load or speed.     

Abrasive Wear Behavior of In Situ TiC Reinforced with Al-4.5%Cu Matrix

The present work deals with the investigation on weight loss and coefficient of friction of TiC reinforced Al-4.5%Cu in situ metal matrix composites. Experiments were conducted using pin-on-disc apparatus against abrasive paper by varying the applied load, sliding distance, and weight percentage of TiC. The results indicated significant improvement in the mechanical properties and wear resistance of experimental composites as compared to the parent metal matrix. The percentage of porosity though increased with increasing TiC reinforcement. The variation of weight loss of composites increased linearly with increasing applied load and sliding distance, whereas decreased with increasing weight percentage of TiC reinforcement. The coefficient of friction decreased linearly with increasing applied load and TiC reinforcement. SEM micrographs of worn surfaces show a well compacted transfer layer of wear debris along with wear track over the sliding surface. Grooves, delamination, and crack propagation were also observed in all test samples. The effective depth of penetration and size of debris was seen to reduce with increasing wt.% of TiC reinforcement in metal matrix.