4.6 Article

Springback prediction of thick-walled high-strength titanium tube bending

期刊

CHINESE JOURNAL OF AERONAUTICS
卷 26, 期 5, 页码 1336-1345

出版社

ELSEVIER SCIENCE INC
DOI: 10.1016/j.cja.2013.07.039

关键词

Bending; Finite element method; High strength; Numerical parameters; Solid elements; Springback; Titanium alloys; Tube

资金

  1. National Natural Science Foundation of China [51275415]
  2. Program for New Century Excellent Talents in University
  3. State Key Laboratory of Solidification Processing in NWPU
  4. Natural Science Basic Research Plan in Shaanxi Province [2011JQ6004]
  5. 111 Project [B08040]

向作者/读者索取更多资源

Significant springback occurs after tube rotary-draw-bending (RDB), especially for a high-strength Ti-3Al-2.5V tube (HSTT) due to its high ratio of yield strength to Young's modulus. The combination scheme of explicit and implicit is preferred to predict the springback. This simulation strategy includes several numerical parameters, such as element type, number of elements through thickness (N-EL), element size, etc. However, the influences of these parameters on springback prediction accuracy are not fully understood. Thus, taking the geometrical specification 9.525 mm x 0.508 mm of a HSTT as the objective, the effects of numerical parameters on prediction accuracy and computation efficiency of springback simulation of HSTT RDB are investigated. The simulated springback results are compared with experimental ones. The main results are: (1) solid and continuum-shell elements predict the experimental results well; (2) for C3D8R elements, N-EL of at least 3 is required to obtain reliable results and a relative error of 29% can occur as N-EL is varied in the range of 1-3; (3) specifying damping factor typically works well in Abaqus/Emplicit simulation of springback and the springback results are sensitive to the magnitude of damping factor. In addition, the explanations of the effect rules are given and a guideline is added. (C) 2013 Production and hosting by Elsevier Ltd. on behalf of CSAA & BUAA.

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