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采用激光熔覆技术在Q235钢基体上制备Ni60A-30%WC-x%石墨烯(质量分数, x=0.0, 0.1, 0.3, 0.5)涂层, 研究石墨烯对激光熔覆镍基碳化钨涂层组织与性能的影响。结果表明, 涂层物相主要由具有γ相结构的Ni-Cr-Fe固溶体、WC、W2C、Cr7C3、Cr23C6、B4C等组成; 石墨烯改善了激光熔覆镍基碳化钨涂层的组织, 提高了涂层的硬度和抗摩擦磨损性能; 当石墨烯质量分数为0.3%时, 得到了析出相分布均匀且细小的组织, 涂层具有高硬度、良好的抗裂纹扩展能力和耐磨性。 相似文献
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采用半导体激光器在2205双相不锈钢表面激光熔覆Ni基合金涂层.借助扫描电镜、电化学综合测试仪和硬度测试仪等,探讨了激光功率对涂层稀释率、微观组织、耐腐蚀性能及硬度的影响.结果表明:激光功率越大,涂层稀释率越大,熔覆层与基体元素发生更多的对流扩散;熔覆层的耐腐蚀性能随激光功率的增加而降低,当激光功率为2.7 kW时,熔覆层的自腐蚀电位最低,为-0.46 mV,腐蚀电流最小,为3.47×10-5 A/cm2. 硬度测试实验表明,激光熔覆Ni基合金涂层硬度最高达680 HV,约为基体硬度的2.5倍. 相似文献
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紫铜上激光熔覆镍基自熔合金组织和性能研究 总被引:2,自引:0,他引:2
采用万瓦横流CO2激光器在紫铜表面熔覆镍基自熔合金熔敷层,并采用SEM、XRD、OM和显微维氏硬度计进行组织结构和硬度分析。结果表明:在紫铜表面完全可采用激光熔覆的方法制备镍基自熔合金的熔覆层,熔覆层与铜基体形成冶金结合,组织致密、晶粒细小、无裂纹、孔隙夹杂等缺陷,熔敷层内具有等轴晶、树枝晶及胞状晶等不同结构,并有WC、W2C、Ni3B等强化相颗粒。同时,与采用超音速火焰喷涂(HVAF)涂层进行对比,结果表明激光熔覆层硬度虽然低于喷涂涂层,但磨擦系数小,耐磨损性能有明显的提高。 相似文献
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采用激光熔覆技术制备了Ni60B镍基合金涂层以及微米WC、纳米WC和微-纳米WC颗粒增强的Ni60B基复合涂层(分别称为WCm、WCn和WCmn复合涂层).对制备涂层在Amsler200磨损试验机上进行了不同载荷和滑动距离的水润滑滑动磨损试验.结果表明:WC颗粒的加入显著提高了Ni60B涂层的耐磨性.WCm复合涂层和纳米WCn复合涂层的耐磨性差别不大,但磨损形貌不同.涂层在水润滑环境下的磨损量均远远低于干滑动摩擦,其原因是水膜的支撑或隔离作用降低了涂层与磨轮之间的接触应力,水的冷却作用减少了摩擦热引起的温度升高,降低了涂层摩擦表面的温升和热软化.水润滑摩损条件下,WCm和WCn复合涂层中过饱和W元素发生扩散和聚集. 相似文献
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以激光熔覆铁基涂层为研究对象,在MM-P2屏显式摩擦磨损试验机上进行摩擦磨损对比实验,分析了不同工艺参数下熔覆层形貌及熔覆涂层后磨损量的变化关系.结果表明:熔覆涂层后的表面硬度均在62HRC以上,远高于基体的硬度;熔覆层的形貌和质量主要影响因素是扫描速度,激光功率次之,并在此基础上采用能量密度进行表征,能量密度为60 J/mm2左右时的耐磨性最好,其最佳组合工艺参数为激光功率3.2 kW左右、扫描速度300 mm/min左右.激光功率过高,扫描速度过快都会导致熔覆层耐磨性能下降. 相似文献
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Ceramic-MetalCompositeCoatingbyLaserCladdingWangPengzhu;QuJinxing;ShaoHeshengAbstract:Fourkindsofceramics(siliconcarbide,boro... 相似文献
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The Microstructure and room temperature abrasive wear resistance of chromium carbide reinforced NiM3Al matrix composite cladding at different depth on nickel base alloy were investigated. The results showed that there is a great difference in microstructure and wear resistance of the Ni3 Al matrix composite at different depth. Three kinds of tests, designed for different load and abrasive size, were used to understand the wear behaviour of this material. Under all three wear conditions, the abrasion resistance of the composite cladding at the depth of 6 mm, namely NC-M2, was much higher than that of the composite cladding at the depth of 2 mm, namely NC-M1. In addition, the wear-resistant advantage of NC-M2 was more obvious when the size of the abrasive was small. The relative wear resistance of NC-M2 increased from 1.63 times to 2.05 times when the size of the abrasive decreased from 180 μm to 50μm. The mierostructure of the composite cladding showed that the size of chromium carbide particles, which was mainly influenced by cooling rate of melting pool, was a function of distance from the interface between the coating and substrate varied gradually. The chromium carbide particles near the interface were finer than that far from inter-face, which was the main reason for the different wear resistance of the composite cladding at different depth. 相似文献
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Li Shang-Ping He-Li Luo Di Feng Xu Cao Xi-e Zhang 《钢铁研究学报(英文版)》2009,16(5):87-87
The Microstructure and room-temperature abrasive wear resistance of chromium carbide reinforced Ni3Al matrix composite cladding in different depth on nickel base alloy were investigated. The results showed that there is a great difference in microstructure and wear resistance of the Ni3Al matrix composite in different depth. Three kinds of tests, designed for different load and abrasive’ size, were utilized to understand the wear behaviour of this material. Under all three wear conditions, the abrasion resistance of the composite cladding in the depth of 6mm, namely NC-M2, was much higher than that of the composite cladding in the depth of 2mm, namely NC-M1. In addition, the wear-resistant advantage of NC-M2 was more obvious when the size of the abrasive was small. The relative wear resistance of NC-M2 increased from 1.63 times to 2.05 times when the size of the abrasive decreased from 180μm to 50μm. The microstructure of the composite cladding showed that the size of chromium carbide particles, which was mainly influenced by cooling rate of melting pool, as a function of distance from the interface between the coating and substrate was gradual. The chromium carbide particles near the interface were finer than that away from interface, which was the main reason for the different wear resistance of the composite cladding in different depth. 相似文献
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真空液相烧结法制备三元硼化物硬质合金覆层材料 总被引:3,自引:0,他引:3
采用液相烧结法在钢基体表面制备三元硼化物硬质合金覆层,将三元硼化物硬质合金的优异性能赋予钢基体表面,获得了耐磨抗蚀、界面结合强度高的新型硬质覆层材料。同时确定了硬质合金覆层的化学配比(B、Fe、Mo元素成分的配比)和C、Cr、Ni合金元素的添加量。对硬质合金覆层的洛氏硬度的测量结果表明,覆层的硬度明显高于钢基体的硬度,其中5Cr2Ni0.8C材料试样的硬度最大;对硬质合金覆层以及覆层与钢基体的界面结合处的扫描电镜观察和能谱分析表明,铬加入后部分进入陶瓷硬质相,加强了其硬度,而镍元素只在铁基粘结相中存在,并且覆层与钢基体之间形成了致密的冶金结合。 相似文献
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为了得到耐磨损的表面涂层,用真空熔烧方法制成与钢基休牢固结合的镍基自熔合金—碳化铬复合涂层。用扫描电子显微镜及X射线衍射仪对涂层的组织和结构进行了观察和分析。应用环块磨损试验机,对具有不同碳化铬含量的镍基复合涂层对金属的摩擦副进行了磨损试验。试验结果指出,在同样条件下,在涂层对金属副中的复合涂层的磨损抗力比在金属对金属副中的GCr15钢要好。复合涂层的磨损率比GCr15钢及纯镍基合金涂层降低约一个数量级,并且复合涂层的磨损率是随碳化铬含量增加而下降的。根据试验结果,对在复合涂层中合理的碳化铬含量也进行了讨论。 相似文献
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以Ni60为粘结金属,在其中分别加入5%(质量分数,下同)、10%和15%的超微碳化钼粉体,利用等离子喷涂方法在40Cr钢基体表面形成热喷涂层。通过对涂层在300 N压力、干磨2 h的试验条件下进行磨损试验,研究了超微碳化钼涂层的耐磨性能。试验结果表明,超微碳化钼粉体的加入显著提高了涂层的耐磨性,并且涂层的耐磨性随碳化钼粉体加入量的增加而提高,其原因主要在于超微碳化钼颗粒在涂层中的弥散强化和自润滑作用。 相似文献
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钴作为硬质合金应用最广泛的黏结剂,存在资源稀缺、成本高昂以及WC-Co硬质合金耐腐蚀性能较差等问题,综合考量生产成本与改善性能,本研究采用铁镍部分代替钴组成复合黏结剂,以其制备超细硬质合金,研究其显微组织和力学、耐蚀耐磨性能的关系。结果表明,黏结相中Fe/Ni质量分数比增加,使得合金WC晶粒细化和黏结相分布不均,合金的硬度和抗弯强度分别提高与降低。合金在中性NaCl溶液中的耐腐蚀性能评估采用极化曲线测试与浸泡实验,黏结相添加Ni能提高合金耐蚀性,归因于Ni的钝化特性与促进腐蚀产物膜的形成。硬质合金摩擦系数和磨损率与Fe/Ni质量比呈负相关,合金耐磨性的提高主要归因于黏结相的强度增强和WC晶粒细化合金硬度提高。 相似文献
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激光熔敷Ni60/WC合金层的腐蚀磨损特性 总被引:6,自引:1,他引:5
研究了45钢表面激光熔敷镍基WC合金层的耐蚀性及在不同冲击速度和不同浓度酸性介质下的腐蚀磨损特性。结果表明,激光熔敷Ni60/WC合金层不论耐蚀性还是抗腐蚀磨损性能同于2Cr13不锈钢。应用微机对试验结果进行逐步回归分析,得出了影响因素与腐蚀磨损速度的害量关系,并探讨了熔敷层的腐蚀磨损过程。 相似文献