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采用非平衡磁控溅射技术,在高淬火高回火H13钢及再加氮化的H13钢表面沉积CrN及CrMoN涂层,分析和测试涂层的微观结构和形貌、纳米硬度和弹性模量、摩擦学性能,以及涂层对两种基体热疲劳性能的影响.结果表明,CrN和CrMoN涂层均匀致密,呈FCC结构,有效地强化了H13钢表面.与CrN涂层相比,CrMoN涂层有着更高的纳米硬度(21.73GPa)、弹性模量(268.34 Ga)以及更低的摩擦系数(0.37),从而更有效地改善了H13钢的摩擦学性能.此外,CrMoN涂层大大改善了H13钢抗热疲劳性能,经1 000次热疲劳实验,表面无明显的宏观裂纹,损伤因子近似为零.其次,CrN涂层也显示了较低的表面损伤因子(0.009),裂纹数量明显减少.然而,CrMoN和CrN涂层难以缓解氮化H13钢表面粗大的网状裂纹,表面损伤因子(0.032,0.104)明显高于H13钢(0.012).

参考文献

[1] 王孟,刘宗德,宝志坚.H13钢汽车热锻模具失效机理分析[J].锻压技术,2008(04):83-86.
[2] 夏立芳;高彩桥.钢的渗氮[M].北京:机械工业出版社,1989
[3] 黄艳,魏仕勇,蒋庐珍.物理气相沉积TiN涂层的研究现状与展望[J].江西科学,2009(03):466-471.
[4] 李钦虎,王军.磁控反应溅射沉积CrN薄膜的抗氧化性研究[J].表面技术,2005(06):40-41,44.
[5] Eun Young Choi;Myung Chang Kang;Dong Hee Kwon;Dong Woo Shin;Kwang Ho Kim .Comparative studies on microstructure and mechanical properties of CrN, Cr-C-N and Cr-Mo-N coatings[J].Journal of Materials Processing Technology,2007(0):566-570.
[6] S.H. Yao;Y.L. Su;W.H. Kao .Effect of Ag/W addition on the wear performance of CrN coatings prepared by RF unbalanced magnetron sputtering[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,2005(1/2):88-92.
[7] Yau BS;Chu CW;Lin D;Lee W;Duh JG;Lin CH .Tungsten doped chromium nitride coatings[J].Thin Solid Films: An International Journal on the Science and Technology of Thin and Thick Films,2008(8):1877-1882.
[8] P. Hones;R. Sanjines;F. Levy .Sputter deposited chromium nitride based ternary compounds for hard coatings[J].Thin Solid Films: An International Journal on the Science and Technology of Thin and Thick Films,1998(1/2):240-246.
[9] Oliver W C;Pharr G M .An improved technique for deter mining hardness and elastic modulus using load and displacement sensing indentation exper iments[J].Journal of Materials Research,1992,7(06):1564-1583.
[10] Kim KH;Choi EY;Hong SG;Park BG;Yoon JH;Yong JH .Syntheses and mechanical properties of Cr-Mo-N coatings by a hybrid coating system[J].Surface & Coatings Technology,2006(7):4068-4072.
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