中国机械工程 ›› 2024, Vol. 35 ›› Issue (09): 1653-1658,1709.DOI: 10.3969/j.issn.1004-132X.2024.09.015

• 增材制造 • 上一篇    下一篇

激光选区熔化成形大尺寸薄壁件变形控制仿真与试验研究

张珞1;刘明明2;陈锐敏1;但鹏1;郭楠1   

  1. 1.江西昌河航空工业有限公司,景德镇,333000
    2.航发优材(镇江)增材制造有限公司,镇江,212001
  • 出版日期:2024-09-25 发布日期:2024-10-23
  • 作者简介:张珞,男,1991年生,高级工程师、博士。主要研究方向为金属增材制造。

Simulation and Experimental Study of Deformation Control of Large-size and Thin-wall Parts by SLM

ZHANG Luo1;LIU Mingming2;CHEN Ruimin1;DAN Peng1;GUO Nan1   

  1. 1.Jiangxi Changhe Aviation Industries Co.,Ltd.,Jingdezhen,Jiangxi,333000
    2.HFYC(Zhenjiang)Additive Manufacturing Co.,Ltd.,Zhenjiang,Jiangsu,212001

  • Online:2024-09-25 Published:2024-10-23

摘要: 采用Simufact Additive软件对典型大尺寸薄壁件——排气管进行了增材制造过程工艺仿真分析。结果显示,无约束下的排气管零件在激光选区熔化(SLM)成形后具有较高的残余应力,并存在较大变形;后处理释放了零件残余应力,但零件整体形变量进一步增至3.5 mm,最大形变量高达9 mm。通过引入具有高比强度、高比刚度的晶格结构作为控形辅助结构,设计了一种既具有足够抵抗变形能力又能够后处理去除的晶格工艺方案:单元格类型为QuadDiametral,杆径1.3 mm,杆长19 mm,晶格区域宽度约60 mm。晶格约束下的排气管零件SLM成形试验结果与数值模拟结果相当吻合,三维扫描云图结果显示,零件整体变形量在1 mm左右,最大变形量不超过2.5 mm,满足零件的使用要求。上述结果验证了晶格结构用于SLM成形大尺寸薄壁件变形控制的有效性。

关键词: 增材制造, 激光选区熔化, 大尺寸薄壁件, 仿真分析, 变形控制, 晶格结构

Abstract: Simulate Additive software was used to simulate and analyze the additive manufacturing processes of a typical large-sized thin-walled component—exhaust pipe. The results show that the SLM formed exhaust pipe parts without constraints have high residual stress and significant deformation. The post-processing releases residual stress in the parts, but the overall deformation of the parts further increases to 3.5 mm, with a maximum deformation of 9 mm. A lattice structure was introduced with high specific strength and stiffness as an auxiliary structure for controlling deformations, and a lattice processing scheme was designed with sufficient resistance to deformation and may be removed through post-processing. The cell type is QuadDiamond, the rod diameter is  as 1.3 mm, the rod length is as 19 mm, and the width of the lattice region is about 60 mm. The SLM test results of the exhaust pipe parts under lattice constraints are quite consistent with the numerical simulation results. The cloud image results of the three-dimensional scanning show that the overall deformation of the part is about 1 mm, and the maximum deformation does not exceed 2.5 mm, meeting the requirements for the part use. The above results show the effectiveness of using lattice structure in deformation control of large-sized thin-walled parts formed by SLM. 

Key words:  , additive manufacturing, selective laser melting(SLM), large-size and thin-wall part, simulation analysis, deformation control, lattice structure

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