期刊文献+

TC11钛合金多道次镦拔工艺三维有限元模拟 被引量:4

3D FEM simulation of multi-pass upsetting and stretching for TC11 alloy
下载PDF
导出
摘要 采用三维有限元模拟软件DEFORM-3D,对片层态TC11钛合金在近β区多道次反复镦拔过程进行了数值模拟。分析了在不同火次、不同变形阶段时锻件中的温度场、应变场。通过模拟研究得到TC11钛合金多道次镦拔的最佳镦粗比为41%。每次拔长分两次压下,每次压下量为总变形量的50%。最后一火先镦粗到210 mm,将坯料翻转180°再镦粗到140 mm。采用多道次反复镦拔工艺可使初始态为粗大片层态的TC11钛合金转变为均匀的等轴态,能为后续的锻造提供合格的坯料。 The finite element software DEFORM-3D was employed to simulate multi-pass upsetting and stretching of TCll alloy in near β zone. The distribution of temperature and effective strain fields were investigated. Simulation results show that the optimal compression ratio of TC11 is 41% during multi-pass upsetting and stretching. The process of stretching is divided into two steps, and in each step, compression ratio is 50%. In the last pass, the workpiece should be upset to 210 mm first and rotated 180°, then upset to 140 mm, The initial coarse lamellar structure can be transferred to refined equaxied structure through multi-pass upsetting and stretching, which can provide eligible workpiece for the next forging process.
出处 《锻压技术》 CAS CSCD 北大核心 2009年第1期1-5,共5页 Forging & Stamping Technology
基金 国家自然科学基金资助项目(50775211)
关键词 钛合金 多道次镦拔 数值模拟 titanium alloy multi-pass forming numerical simulation
  • 相关文献

参考文献9

二级参考文献41

共引文献87

同被引文献30

  • 1马小怀.钛合金超声波检测中杂波产生原因分析[J].无损检测,2006,28(12):649-651. 被引量:12
  • 2吕成,张立文,牟正君,裴继斌.TC4钛合金锻件锻造过程三维热力耦合有限元模拟[J].锻压技术,2007,32(1):28-31. 被引量:21
  • 3Rebelo N, Rydstad H, Schroder G. Simulation of Material Flow in Closed-die Forging by Model Techniques and Rigidplastic FEM [ M ]. Num. Meth. Ind. Form. Prec. Swansea. U K: Pineridge Press, 1982.
  • 4Hu Z M, Brook J W, Dean T A. Experimental and theoretical a- nalysis of deformation and micrestruetural evolution in the hot - die forging of titanium alloy aerefoil sections [ J]. Journal of Materials Processing Technology, 1999, 88 ( 1 - 3 ) : 251 - 265.
  • 5Argyris J H, Doltsinis J S, Luginsland J. Three-dimension thermomechanical analysis of metal forming processes [ A ]. Proc. Int. Workshop Simulation of Metal Forming Processes by the Finite Element Method [ C]. Stuttgart, 1985.
  • 6Yang D Y, Lee N K, Yoon J H. A three-dimension of isothermal turbine blade forging by the rigid-viscoplastic finite-element method [ J]. Journal of Material Engineering and Performance, 1993, (2): 119-124.
  • 7Zhan Mei, Yang He, Liu Yu -li. Deformation characteristic of the precision forging of a blade with a damper platform using 3D FEM analysis [ J ]. Journal of Materials Processing Technology,2004, 150 (3): 290 -299.
  • 8《中国航空材料手册》编辑委员会.中国航空材料手册:铜合金及钦合金[M].北京:中国标准出版社,2001:147-173.
  • 9刘艳.叶片制造技术[M].北京:科学出版社,2002..
  • 10粟祜.叶片精锻[M].北京:国防工业出版社,1984.

引证文献4

二级引证文献8

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部