欢迎登录材料期刊网

材料期刊网

高级检索

应用元胞自动机模型对合金钢表面氮化及扩散层中氮化物沉淀过程进行了计算机模拟.考察了过程的动力学和沉淀相尺寸与分布特征,以及氮势和稳定氮化物形成元素含量对它们的影响.结果表明氮化过程动力学为抛物线型,抛物线速率常数k随氮势提高呈线性增大;氮化物形成元素含量XM对氮化速率也有影响,k~XM基本呈线性正比关系;表面渗氮层内的稳定氮化物沉淀相颗粒尺寸与体积分数则随氮势的降低而增大.

参考文献

[1] Bergheau J M;Mangjialenti G;Boitout F.Contribution of numerical simulation to the analysis of heat treatment and surface hardening processes[A].Ohio:ASM International,1999:681-690.
[2] Fortunier R;Leblond J B;Bergheau J M.Computer simulation of thermochemical treatment:Modeling diffusion and precipitation in metals[J].上海交通大学学报(英文版),2000(05):301-309.
[3] Zhou Lang;Wei Xiuqin .A randomwalk-cellular automaton model of precipitation of internal oxides[J].Scripta Materialia,1997,37:1483-1487.
[4] Zhou Lang;Wei Xiuqin .A randomwalk-cellular automaton simulation of internal oxidation and its transition to external oxidation[J].Scripta Materialia,1990,40:365-369.
[5] Zhou Lang;Wei Xiuqin;Deng Zhangming.A simulational study of precipitation kinetics and morphology in nitridation of alloy steels[J].上海交通大学学报(英文版),2000(05):298-301.
[6] Zhou Lang;Deng Zhangming;Wei Xiuqin .A simulation study of the effect of varying nitrogen potential on behaviour of precipitation in nitridation of alloys[J].Computational Materials Science,2002,23:204-208.
[7] 邓章铭,周浪.元胞自动机模型方法及其在材料组织结构模拟中的应用[J].材料科学与工程,2000(03):123-129.
[8] Wolfram S .Statistical mechanics of cellular automata[J].Reviews of Modern Physics,1983,55:601-630.
[9] Brown S G R;Willians T;Spttle J A .A cellular automation model of the steady-state"free"growth of a non-isothermal dendrite[J].冶金材料学报,1994,42:2893-2895.
[10] Zhou Lang;Wei Xiuqin;Zeng Hui.A cellular automaton approach to modeling of phase transformation in quenching[A].Ohio:ASM International,1999:700-704.
[11] Jack K H.Nitriding:Heat Treatment'73[M].London,The Metals Society,1975
[12] Rapp R A;Kinetics .microstructures and mechanism of internal oxidation-its effect and prevention in high temperature alloy oxidation[J].Corrosion,1965,21:382-394.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%