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高熵合金氮化物薄膜性能优异,目前国内对Al0.3CrFe1.5MnNi0.5高熵合金的研究主要是对块体,对薄膜研究较少.采用直流磁控溅射技术在硅片上沉积了Al0.3CrFe1.5MnNi0.5高熵合金氮化物薄膜.利用X射线衍射仪(XRD)、扫描电子显微镜(SEM)、纳米压痕仪等分析了基板偏压对薄膜的晶体结构、溅射效率、硬度和摩擦磨损性能的影响.结果表明:基板偏压为-50 V时,薄膜的晶体结构为面心立方结构(FCC),薄膜截面有明显的柱状结构;随着偏压幅值的增加,衍射峰的强度降低,晶粒尺寸减小,薄膜的溅射效率降低,硬度提高;基板偏压为-150 V时薄膜硬度最高,为13.74 GPa,此时薄膜的抗摩擦磨损性能最好.

参考文献

[1] Haitao Duan;Yong Wu;Meng Hua;Chengqing Yuan;Ding Wang;Jiesong Tu;Hongchao Kou;Jian Li.Tribological properties of AlCoCrFeNiCu high-entropy alloy in hydrogen peroxide solution and in oil lubricant[J].Wear: an International Journal on the Science and Technology of Friction, Lubrication and Wear,20131/2(1/2):1045-1051.
[2] Jien-Min Wu;Su-Jien Lin;Jien-Wei Yeh;Swe-Kai Chen;Yuan-Sheng Huang;Hung-Cheng Chen.Adhesive wear behavior of Al{sub}xCoCrCuFeNi high-entropy alloys as a function of aluminum content[J].Wear: an International Journal on the Science and Technology of Friction, Lubrication and Wear,20065/6(5/6):513-519.
[3] Chin-You Hsu;Tsing-Shien Sheu;Jien-Wei Yeh;Swe-Kai Chen.Effect of iron content on wear behavior of AlCoCrFe_xMo_(0.5)Ni high-entropy alloys[J].Wear: an International Journal on the Science and Technology of Friction, Lubrication and Wear,20105/6(5/6):653-659.
[4] Y.L. Chou;Y.C. Wang;J.W. Yeh;H.C. Shih.Pitting corrosion of the high-entropy alloy Co_(1.5)CrFeNi_(1.5)Ti_(0.5)Mo_(0.1) in chloride-containing sulphate solutions[J].Corrosion Science: The Journal on Environmental Degradation of Materials and its Control,201010(10):3481-3491.
[5] Praveen, S.;Murty, B.S.;Kottada, R.S..Alloying behavior in multi-component AlCoCrCuFe and NiCoCrCuFe high entropy alloys[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,2012:83-89.
[6] Chen TK;Wong MS.Structure and properties of reactively-sputtered AlxCoCrCuFeNi oxide films[J].Thin Solid Films: An International Journal on the Science and Technology of Thin and Thick Films,20072/4(2/4):141-146.
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