欢迎登录材料期刊网

材料期刊网

高级检索

为了减少挤压过程中金属的非均匀流动而导致的AZ31挤压棒的表面裂纹,用三维有限元模拟了其挤压过程,并进行了实验的验证.研究表明:与锥角模具相比,流线模产生死区的倾向大大降低.由于表面附加拉伸应力的降低,使用流线模避免了表面裂纹的产生,而锥模将使挤压过程裂纹的形成趋向增加.结果表明,锥角模将导致连续的裂纹.采用流线模大约能够减少15t的挤压力.用DeformTM-3D模拟得到的理论结果和实验结果吻合.

参考文献

[1] 谢建新;刘静安.金属挤压理论及技术[M].北京:冶金工业出版社,2001
[2] 彭大暑.金属塑性加工原理[M].长沙:中南大学出版社,2004
[3] 刘建生;陈慧琴;郭晓霞.金属塑性加工有限元模拟技术与应用[M].北京:冶金工业出版社,2003
[4] 马怀宪.金属塑性加工学-挤压、拉拔与管材冷轧[M].北京:冶金工业出版社,1997
[5] LOF J .Elasto-viscoplastic FEM simulations of the aluminum flow in the bearing area for extrusion of thin-walled sections[J].Journal of Materials Processing Technology,2001,114:174-183.
[6] QI Le-hua;LI He-jun;GUI Pei-ling;SHI Zhong-ke .Forming of tubes and bars of alumina/LY12 composites by liquid extrusion process[J].Transactions of Nonferrous Metals Society of China,2003(4):803-808.
[7] Qi LH.;Shi ZK.;Li HJ.;Cui PL.;Han HM. .Simulation of liquid infiltration and semi-solid extrusion for composite tubes by quasi-coupling thermal-mechanical finite element method[J].Journal of Materials Science,2003(17):3669-3675.
[8] Suo, T;Li, YL;Deng, Q;Liu, YY .Optimal pressing route for continued equal channel angular pressing by finite element analysis[J].Materials Science & Engineering. A, Structural Materials: Properties, Microstructure and Processing,2007(1-2):166-171.
[9] ROUSSE D R .Numerical predictions of two-dimensional conduction,convection,and radiation heat transfer.I.Formulation[J].International Journal of Thermal Sciences,2000,39(03):315-31.
[10] LEWIS R W;RANSING R S .A correlation to describe interfacial heat transfer during solidification simulation and its use in the optimal feeding design of castings[J].Metallurgical and Materials Transactions B:Process Metallurgy and Materials Processing Science,1998,29:437-448.
[11] Dyi-Cheng Chen;Sheng-Kai Syu;Cing-Hong Wu;Sin-Kai Lin .Investigation into cold extrusion of aluminum billets using three-dimensional finite element method[J].Journal of Materials Processing Technology,2007(0):188-193.
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%