SiC颗粒增强PEEK树脂基复合材料的制备与性能EI

以纯PEEK粉,粒径为10μm的SiC粉为原料,在360℃热压制备了纯PEEK树脂和SiC体积比分别为10%,20%及30%的SiC/PEEK复合材料,并测试了材料的硬度、压缩性能、冲击性能以及摩擦磨损性能,用扫描电镜(SEM)观察了复合材料的断口以及磨损表面.实验结果表明:随着SiC添加量的增加复合材料的相对密度和硬度同时下降;SiC/PEEK复合材料的强度以及韧度随着SiC颗粒添加量的增加逐渐提高,当SiC达到某一含量时可以获得最佳的综合力学性能,此后随着SiC含量的进一步增多,复合材料的脆性增大,强度急剧下降;SiC/PEEK复合材料的摩擦系数随SiC的添加先增大后减小,磨损率逐渐变大,磨损机制由粘着磨损转向粘着磨损与犁削磨损共存最后变成全部的犁削磨损.     

SiC颗粒增强PEEK树脂基复合材料的制备与性能

以纯PEEK粉,粒径为10μm的SiC粉为原料,在360℃热压制备了纯PEEK树脂和SiC体积比分别为10%,20%及30%的SiC/PEEK复合材料,并测试了材料的硬度、压缩性能、冲击性能以及摩擦磨损性能,用扫描电镜(SEM)观察了复合材料的断口以及磨损表面.实验结果表明:随着SiC添加量的增加复合材料的相对密度和硬度同时下降;SiC/PEEK复合材料的强度以及韧度随着SiC颗粒添加量的增加逐渐提高,当SiC达到某一含量时可以获得最佳的综合力学性能,此后随着SiC含量的进一步增多,复合材料的脆性增大,强度急剧下降;SiC/PEEK复合材料的摩擦系数随SiC的添加先增大后减小,磨损率逐渐变大,磨损机制由粘着磨损转向粘着磨损与犁削磨损共存最后变成全部的犁削磨损.     

数值模拟SiCp/Al复合材料的微观结构对力学性能的影响

本文运用有限元法模拟了SiC颗粒体积分数和颗粒尺寸对SiCp/Al复合材料弹性模量、屈服强度、延伸率的影响。为了建立与真实显微结构相似的复合材料模型,假定任意尺寸的SiC颗粒随机地分布在SiCp/Al复合材料中。计算结果表明:SiC颗粒体积分数对复合材料的力学性能的影响更加显著。随着体积分数的增加,SiCp/Al复合材料的弹性模量和屈服强度逐渐增加;而其延伸率会相应降低。其应力应变曲线由韧性材料的特性向脆性材料的特性逐渐过渡。相反,当平均颗粒尺寸在一定的范围内变化时,颗粒尺寸对其应力-应变曲线的影响并不显著。     

SiC颗粒体积分数对SiCp/Al复合材料疲劳裂纹扩展的影响

本文通过对疲劳裂纹扩展速率的测试和对疲劳裂纹扩展路径及疲劳断口的观察分析,研完了SiC颗粒体积分数对SiCp/Al复合材料疲劳裂纹扩展的影响.结果表明:随着SiC颗粒体积分数的增加,复合材料疲劳裂纹扩展抗力增加,但只有SiC颗粒体积分数为15％时,复合材料的疲劳裂纹扩展抗力才优于基体.      

粉末冶金法制备CNT和SiC混杂增强铝基复合材料的摩擦磨损性能EI北大核心CSCD

以7055Al为基体,通过粉末冶金法分别制备碳化硅(SiC)颗粒、碳纳米管(CNT)以及SiC和CNT混杂增强7055Al复合材料,并对三种复合材料的干滑动摩擦磨损行为进行研究。结果表明:随着载荷提高,复合材料磨损失重增加,摩擦因数略有降低。在0.5 MPa与1.0 MPa载荷条件下,SiC-CNT/7055Al复合材料磨损失重低于单一SiC/7055Al和单一CNT/7055Al复合材料。2.0 MPa时,SiC-CNT/7055Al复合材料磨损失重急剧增加。随着载荷提高,CNT/7055Al复合材料耐磨性逐渐增加,在中、高载荷下,材料具有更为优异的耐磨性。SiC/7055Al复合材料磨损量则随着载荷提高,磨损失重逐渐增加,当载荷为2.0 MPa时,材料磨损量增加幅度较小。     

碳化硅增强铝基复合材料的力学性能和断裂机制

研究了碳化硅颗粒(SiCp)尺寸对用粉末冶金法制备体积分数为15%的SiCp/2009铝基复合材料力学性能和断裂机制的影响.结果表明,复合材料的强度随着SiCp尺寸的增大而减小,塑性则随着颗粒的增大而增大.当SiCp尺寸为1.5μm时,SiCp/2009A1复合材料的断裂主要以界面处撕裂和基体材料的开裂为主;当SiCp尺寸为20 μm时,复合材料的断裂主要以SiCp断裂为主;当SiCp尺寸处于两者之间时,SiCp/2009A1复合材料界面处撕裂和SiCp断裂的共同作用决定复合材料的断裂.     

颗粒尺寸对B4C增强铝基中子吸收材料界面反应与力学性能的影响

采用粉末冶金真空热压法制备了B₄C质量分数为31%、平均颗粒尺寸分别为6.5 μm、9.3 μm、17.3 μm、28 μm、39.5 μm的纯Al和6061Al基体的复合材料。对复合材料进行微观结构和力学性能检测,结果表明:所有复合材料的B₄C颗粒在基体中都均匀分布,且致密度都达到99%以上;对于纯Al基复合材料,随着颗粒尺寸增加,其致密度和塑性逐渐增加,强度逐渐下降;对于6061Al基复合材料,致密度随着颗粒尺寸的增加稍有降低,其强度和塑性受颗粒尺寸和热压温度共同影响,当热压温度610℃时,界面反应严重,随B₄C颗粒尺寸增加,强度先下降后上升,塑性先上升后下降;当热压温度580℃时,界面反应轻微,复合材料强度逐渐下降,塑性逐渐上升。颗粒尺寸、界面反应和基体材料等均影响B₄C增强铝基复合材料的力学性能。      

Ca含量对SiC/Al泡沫复合材料性能和结构的影响

研究了SiC颗粒增强铝基（SiC/Al）复合材料中Ca含量对SiC分散性的影响以及Ca含量对注气法制备的SiC/Al泡沫复合材料的压缩性能和结构的影响。首先,制备不同Ca含量的SiC/Al复合材料,用来制备SiC/Al泡沫复合材料的基本材料,并对不同Ca含量的SiC/Al泡沫复合材料进行压缩实验;然后,利用OM、SEM和XRD研究了SiC/Al复合材料及泡沫结构中Ca含量对SiC分散性的影响。结果表明:Ca的加入会明显影响SiC/Al复合材料中SiC的分布,且存在Ca含量临界值。当Ca含量小于1.5wt%时,SiC在基体中分布较均匀;当Ca含量达到或超过1.5wt%时,熔体中生成一种富含Al、Ca和Si的金属间化合物Ca₂Al₄Si₃,且其体积分数和尺寸随Ca含量的提高而显著增大,SiC集聚在这些金属间化合物区域内及其边界上而影响SiC分布的均匀性。压缩实验表明,SiC/Al泡沫复合材料压缩应力-应变曲线的平台应力和抗压屈服强度随着Ca含量的增加有提高的趋势。相应的SiC/Al泡沫复合材料的胞壁厚度随着Ca含量的提高明显增加,这不仅与金属间化合物的形成提高了熔体黏度相关,更可能是与金属间化合物在熔体中尺寸随Ca含量提高而明显增大相关。      

短切碳纤维含量对Csf/SiC复合材料摩擦磨损性能的影响

采用热压烧结法制备短切碳纤维增强碳化硅(short carbon fiber reinforced SiC composite,Csf/SIC)复合材料.采用销一盘式摩擦磨损试验测试不同短切碳纤维(Csf)含量的复合材料的干摩擦磨损性能,借助扫描电镜观察其磨痕形貌,分析不同Csf体积分数对复合材料摩擦磨损性能的影响.研究表明:由于碳纤维在复合材料中具有增强基体和固体润滑的作用,以及其自身良好的热传导性和低摩擦系数,因此,Csf/SiC复合材料的摩擦系数随Csf体积分数增大而不断降低;当Csf含量在42 vol.%以内时,复合材料的磨损率比无纤维SiC材料有大幅度减少,并且随着Csf体积分数增大而降低;但当Csf含量达到53 vol.%时,由于Csf含量高,导致纤维和基体之间的结合强度有所降低,造成复合材料的磨损率急剧增大.在本文研究范围内,含30 vol.% Csf复合材料具有最佳的摩擦磨损性能.     

扭转圈数对高压扭转SiC_P/Al复合材料界面扩散行为和组织性能的影响

采用OM和EDS研究不同扭转圈数下高压扭转法制备SiC_P/Al复合材料的显微组织和界面扩散行为,并结合组织特点和界面特征分析扭转圈数对复合材料拉伸性能和断裂机理的影响。结果表明:扭转圈数的增加可以有效提高SiC颗粒分布的均匀性,闭合孔隙,界面处Al元素扩散能力增强,扩散距离增大,Al扩散系数实际计算值较理论值增大了10~(17)倍,形成以元素扩散和界面反应为主的强界面结合,试样抗拉强度和伸长率不断提高,少量的SiC颗粒均匀分布在断口韧窝中,断裂主要以基体的韧性断裂为主;当扭转圈数较大时,SiC颗粒在剧烈剪切作用下破碎加剧,颗粒"再生团聚"导致孔隙率增大,潜在裂纹源增多,形成大量结合强度较低的断裂新生界面,试样抗拉强度和伸长率显著降低,在团聚位置易形成尺寸较大的深坑韧窝,复合材料断裂呈现韧性断裂与脆性断裂的混合模式。     

碳化硅颗粒增强2124Al复合材料特性研究

本文对粉末冶金法制备的SiCp/2124Al复合材料进行了不同温度的拉伸试验和物理性能测试,对并其时效析出特性和磨损性能进行了研究。结果表明,这种复合材料不仅具有高的室温强度、模量和低的热膨胀系数,而且表现出良好的高、低温性能和抗磨损性能。SiC颗粒加入铝合金显著加速了其时效析出过程。     

碳化硅颗粒增强2124Al复合材料特性研究

本文对粉末冶金法制备的SiCp/2124Al复合材料进行了不同温度的拉伸试验和物理性能测试,对并其时效析出特性和磨损性能进行了研究。结果表明,这种复合材料不仅具有高的室温强度、模量和低的热膨胀系数,而且表现出良好的高、低温性能和抗磨损性能。SiC颗粒加入铝合金显著加速了其时效析出过程。      

Influence of fillers on abrasive wear of short glass fibre reinforced polyamide composites

Various composites of polyamide 6 filled with short glass fibre, polytetrafluoroethylene and metal powders viz. copper and bronze were formulated in the laboratory and characterised for their various mechanical properties such as tensile strength, tensile elongation, flexural strength, hardness and impact strength. Compositional analysis was done with gravimetry, solvent extraction and differential scanning calorimetry (DSC) techniques followed by tribo-performance evaluation in abrasive wear mode by abrading a sample against silicon carbide (SiC) abrasive paper in a single pass condition under various loads. It was observed that the fibre reinforcement deteriorated the abrasive wear resistance of virgin polymer. Combination of fibre and particulate filler was more detrimental in this respect. Efforts were made to correlate the wear performance with the appropriate mechanical properties. Under selected loading condition, wear as a function of product of hardness, elongation to break (e) and ultimate tensile strength (S) showed better correlation than Ranter-Lancaster plot. Scanning electron microscopy (SEM) was used to analyse the worn surfaces of the samples.     

增强颗粒含量和尺寸对SiCp/Fe复合材料性能的影响

利用电流直加热动态热压烧结工艺,分别制备了增强颗粒体积含量从5%到15%,尺寸从3 μm到45 μm的SiCp/Fe复合材料,研究了粒子含量与尺寸对复合材料硬度、强度、延伸率和耐磨性能的影响.研究表明:增强颗粒的体积含量从5%提高到10%,可以明显提高材料的性能;随着增强颗粒含量进一步提高,颗粒团聚将导致材料性能降低;...     

Crack and wear behavior of SiC particulate reinforced aluminium based metal matrix composite fabricated by direct metal laser sintering process

In this investigation, crack density and wear performance of SiC particulate (SiCp) reinforced Al-based metal matrix composite (Al-MMC) fabricated by direct metal laser sintering (DMLS) process have been studied. Mainly, size and volume fraction of SiCp have been varied to analyze the crack and wear behavior of the composite. The study has suggested that crack density increases significantly after 15 volume percentage (vol.%) of SiCp. The paper has also suggested that when size (mesh) of reinforcement increases, wear resistance of the composite drops. Three hundred mesh of SiCp offers better wear resistance; above 300 mesh the specific wear rate increases significantly. Similarly, there has been no improvement of wear resistance after 20 vol.% of reinforcement. The scanning electron micrographs of the worn surfaces have revealed that during the wear test SiCp fragments into small pieces which act as abrasives to result in abrasive wear in the specimen.     

激光熔覆原位自生TiC颗粒增强镍基复合涂层的组织与耐磨性

采用预置粉末法在45钢表面进行激光熔覆镍基Ni60A+x%(SiC+Ti)(质量分数,下同)复合粉末涂层的实验研究。使用往复式磨损试验机对不同涂层材料的熔覆层进行干摩擦磨损实验,利用金相显微镜、扫描电镜(SEM)观察和分析熔覆层的显微组织与磨损形貌。结果表明:复合粉末通过原位反应生成弥散分布的TiC颗粒增强复合涂层,随着(SiC+Ti)含量的增加,颗粒状TiC的尺寸和数目逐渐增加;复合粉(SiC+Ti)含量达到60%时,微观组织有气孔和夹杂缺陷;复合粉(SiC+Ti)含量为48%时,熔覆层耐磨性最佳;复合涂层的磨损主要为磨粒磨损,机理为微观切削和挤压剥落。     

Abrasive wear of FeCr (M7C3–M23C6) reinforced iron based metal matrix composites

Abstract

The effects of volume fraction, particle size, and sintered porosity of FeCr (M₇C₃–M₂₃C₆) particulates on the abrasive wear resistance of powder metallurgy (PM) Fe alloy metal matrix composites have been studied under different abrasive conditions. It was seen that the abrasive wear rate of the composites increased with an increase in the FeCr volume fraction in tests performed with 80 grade SiC abrasive paper, but it decreased for tests conducted with 220 grade SiC abrasive paper. Furthermore, the wear rates decreased with an increase in FeCr size for composites containing the same amount of FeCr. Hence it is deduced that Fe alloy composites reinforced with larger size FeCr particles are more effective against abrasive wear than those reinforced with smaller ones. At the same time the results show that the beneficial effects of hard FeCr particulates on wear resistance far outweighed the detrimental effects of sintered porosity in the PM metal matrix composites. In addition, the fabrication of composites containing soft particles such as graphite or copper favours a reduction in the coefficient of friction, and increases the matrix hardness of the composite. For this reason graphite and copper were used in the matrix in different amounts to test their effect on the wear resistance. Increase in graphite and copper volume fraction allowed the formation of additional phases, which had high hardness and wear resistance. It was also found that the wear rate of the composites decreased considerably with graphite and copper addition.     

Investigation of the abrasive wear behaviour of ZA-27 alloy and CuSn10 bronze

In this study, abrasive wear behaviours of ZA-27 alloy and CuSn10 bronze were investigated using a purpose-built wear tester. The ZA-27 alloy was produced by permanent mould casting. The abrasive SiC particles having 63 μm grit size was added to the lubricant oil. The wear rate and friction coefficient of alloys were determined at the different test conditions such as sliding distance, applied load, linear velocity and percentage SiC weight content. The wear surfaces of alloys were examined using SEM and EDS analysis. The results showed that the wear rate of alloys decreased with the increasing of applied load and increased with the increasing linear velocity and abrasive SiC content. It was found that the SiC particle fracture was an important mechanism determining the friction and the wear rate of alloys. CuSn10 bronze showed higher wear resistance than ZA-27 alloy under abrasive test conditions except at high linear velocities.     

Surface modification of an aluminium 2124 composite by eutectic alloying

The incorporation of a hard particular dispersion in a metal matrix results in a composite material with unique mechanical and tribological properties. However, once the composite has been fabricated the particular dispersion cannot be rearranged or modified. In this study, the surface of a 2124 aluminium metal matrix composite is modified by eutectic alloying with copper. The results show that by heat treating the composite at a temperature above the eutectic temperature for the Al-Cu system, the distribution of SiC particles can be altered. There is a significant movement of particles towards the surface of the composite and abrasive wear tests show better wear resistance than the unmodified surfaces. This change in wear behaviour is attributed to the absence of severe plastic deformation due to the increase in concentration of hard SiC particles within the surface.     

Microstructure and abrasive wear behaviour of B<Subscript>4</Subscript>C particle reinforced 2014 Al matrix composites

In this study, the microstructure and abrasive wear properties of varying volume fraction of particles up to 12% B₄C particle reinforced 2014 aluminium alloy metal matrix composites produced by stircasting method was investigated. The density, porosity and hardness of composites were also examined. Wear behaviour of B₄C particle reinforced aluminium alloy composites was investigated by a block-on-disc abrasion test apparatus where the samples slid against the abrasive suspension mixture (contained 10 vol.% SiC particles and 90 vol.% oil) at room conditions. Wear tests performed under 92 N against the abrasive suspension mixture with a novel three body abrasive. For wear behaviour, the volume loss and specific rate of the samples have been measured and the effects of sliding time and the content of B₄C particles on the abrasive wear properties of the composites have been evaluated. The dominant wear mechanisms were identified using SEM. Microscopic observation of the microstructures revealed that dispersion of B₄C particles was generally uniform while increasing volume fraction led to agglomeration of the particles and porosity. The density of the composite decreased with increasing reinforcement volume fraction but the porosity and hardness increased with increasing particle content. Moreover, the specific wear rate of composite decreased with increasing particle volume fraction. The wear resistance of the composite was found to be considerably higher than that of the matrix alloy and increased with increasing particle content.