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    李勇, 许鹤君, 巴发海, 何贝贝, 李凯. 选区激光熔化制备Hastelloy-X合金的有限元模拟及其高温蠕变性能[J]. 机械工程材料, 2019, 43(9): 60-67. DOI: 10.11973/jxgccl201909012
    引用本文: 李勇, 许鹤君, 巴发海, 何贝贝, 李凯. 选区激光熔化制备Hastelloy-X合金的有限元模拟及其高温蠕变性能[J]. 机械工程材料, 2019, 43(9): 60-67. DOI: 10.11973/jxgccl201909012
    LI Yong, XU Hejun, BA Fahai, HE Beibei, LI Kai. Finite Element Simulation and High-temperature Creep Property of Hastelloy-X Superalloy Prepared by Selective Laser Melting[J]. Materials and Mechanical Engineering, 2019, 43(9): 60-67. DOI: 10.11973/jxgccl201909012
    Citation: LI Yong, XU Hejun, BA Fahai, HE Beibei, LI Kai. Finite Element Simulation and High-temperature Creep Property of Hastelloy-X Superalloy Prepared by Selective Laser Melting[J]. Materials and Mechanical Engineering, 2019, 43(9): 60-67. DOI: 10.11973/jxgccl201909012

    选区激光熔化制备Hastelloy-X合金的有限元模拟及其高温蠕变性能

    Finite Element Simulation and High-temperature Creep Property of Hastelloy-X Superalloy Prepared by Selective Laser Melting

    • 摘要: 基于选区激光熔化(SLM)成型原理,利用体生热率法模拟热源模型,采用ANSYS参数化设计语言实现激光热源的移动加载,通过有限元模型模拟了Hastelloy-X合金在SLM成型过程中单层瞬态温度场和熔池的形貌,并对模拟结果进行了试验验证;研究了SLM成型试样的高温蠕变性能,并与固溶态Hastelloy-X合金热轧棒材的进行对比。结果表明:体生热率法能够较好地模拟SLM成型过程中的单层瞬态温度场,计算得到的熔池尺寸和一次枝晶间距与试验结果吻合较好;在相同蠕变试验条件下,SLM成型试样的稳态蠕变速率远低于固溶态Hastelloy-X合金热轧棒材的,但二者的蠕变应力指数相近,且均主要通过位错的移动和攀移进行蠕变变形。

       

      Abstract: Based on molding principle of selective laser melting (SLM), the heat source model was simulated by body heat generation method, and the load of moving laser heat source was realized by ANSYS parametric design language (APDL); then the single-layer transient temperature field and molten pool morphology of Hastelloy-X superalloy during SLM process were simulated by finite element model. The simulation results were verified by tests. The high temperature creep property of SLM molding specimens was investigated and compared with Hastelloy-X superalloy hot-rolled rods treated by solution. The results show that the body heat generation method could simulate the single-layer transient temperature field during SLM molding well, and the calculated molten pool size and primary dendrite spacing agreed well with the experimental results. Under the same creep test condition, the steady-state creep rate of SLM molding specimen was much lower than that of Hastelloy-X superalloy hot-rolled rods treated by solution; however, the creep stress index of them were similar, and creep deformation were both dominated by movement and climbing of dislocations.

       

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