Numerical Simulation of Hot Die Forging Process of Ti-6Al-4V Alloy Blade

Article Preview

Abstract:

Ti-6Al-4V alloy is used extensively in aerospace industries due to its excellent properties. In this paper, the hot die forging process of the Ti-6Al-4V alloy blade was simulated by using 3D finite element method. Based on the model, the effect of process parameters on the deformation was investigated. The results show that the increase of temperature is beneficial to improving the uniformity of stress distribution. The slower the declining velocity of upper die is, the larger the strain gradient of severe deformation area will be. In addition, the stress distribution gets uniform with velocity decreasing. The large friction coefficient can make strain distribution uneven and cause symmetry of stress distribution. The proposed numerical simulation of hot die forging of blade in the present work may yield important information for the development of hot die forging techniques and the manufacture of blade.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

1325-1331

Citation:

Online since:

June 2017

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2017 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] R. Boyer, G. Welsch, E.W. Collings, Materials Properties Handbook: Titanium Alloys, ASM International, USA, (1994).

Google Scholar

[2] R.R. Boyer. An overview on the use of titanium in the aerospace industry. Materials Science and Engineering A, 213(1996): 103~114.

Google Scholar

[3] V. Alimirzaloo, M.H. Sadeghi, F.R. Biglari. Optimization of the forging of aerofoil blade using the finite element method and fuzzy-Pareto based genetic algorithm. Journal of Mechanical Science and Technology, 26(2012): 1801~1810.

DOI: 10.1007/s12206-012-0429-0

Google Scholar

[4] M. Zhan, H. Yang and Y. Liu. Deformation characteristic of the precision forging of a blade with a damper platform using 3D FEM analysis. Journal of Materials Processing Technology, 150(2004): 290~299.

DOI: 10.1016/j.jmatprotec.2004.02.062

Google Scholar

[5] C. Lv, L. Zhang, Z. Mu, and et al. 3D FEM simulation of the multi-stage forging process of a gas turbine compressor blade. Journal of Materials Processing Technology, 198(2008): 463~470.

DOI: 10.1016/j.jmatprotec.2007.07.032

Google Scholar

[6] Z.M. Hu, T.A. Dean. Aspects of forging of titanium alloys and the production of blade forms. Journal of Materials Processing Technology, 111(2001): 10~19.

DOI: 10.1016/s0924-0136(01)00510-6

Google Scholar

[7] B. Zhao, Z. Li, H. Hou, et al. Three dimensional FEM simulation of titanium hollow blade forming process. Rare Metal Materials & Engineering, 39(2010): 963~968.

DOI: 10.1016/s1875-5372(10)60106-3

Google Scholar

[8] A. Kocanda, P. Czyzewski, K.H. Mehdi. Numerical analysis of lateral forces in a die for turbine blade forging. Archives of Civil & Mechanical Engineering, 9(2009): 49~54.

DOI: 10.1016/s1644-9665(12)60068-5

Google Scholar

[9] L. Huang, R. Zeng, X.T. Zhang, et al. Study on plastic deformation behavior of hot splitting spinning of TA15 titanium alloy. Materials & Design, 58(2014): 465~474.

DOI: 10.1016/j.matdes.2014.02.007

Google Scholar

[10] G. Zhou, L. Hua, D.S. Qian, et al. Effects of axial rolls motions on radial-axial rolling process for large-scale alloy steel ring with 3D coupled thermo-mechanical FEA. International Journal of Mechanical Sciences, 59(2012): 1~7.

DOI: 10.1016/j.ijmecsci.2012.01.002

Google Scholar

[11] F. Chen, F.C. Ren, J. Chen, et al. Microstructural modeling and numerical simulation of multi-physical fields for martensitic stainless steel during hot forging process of turbine blade. The International Journal of Advanced Manufacturing Technology, 82(2016).

DOI: 10.1007/s00170-015-7368-8

Google Scholar

[12] C.L. Hu, H.G. Ou, Z. Zhao. An alternative evaluation method for friction condition in cold forging by ring with boss compression test. Journal of Materials Processing Technology, 30(2015): 18~25.

DOI: 10.1016/j.jmatprotec.2015.04.010

Google Scholar

[13] Y. Shao, B. Lu, H. Ou, et al. A new approach of preform design for forging of 3D blade based on evolutionary structural optimization. Structural & Multidisciplinary Optimization, 51(2015): 199~211.

DOI: 10.1007/s00158-014-1110-2

Google Scholar

[14] Q.A. Tai, X.G. Li, Z.H. Li, et al. On the measurement of friction coefficient of Ti-6Al-4V titanium alloy utilizing the hot compression test of ring and FE simulation. Journal of Materials Engineering, 1(2011): 23~26.

DOI: 10.1016/j.triboint.2011.07.001

Google Scholar

[15] J.P. Wang. A new evaluation to friction analysis for the ring test, New Park Publications, UK, (1973).

Google Scholar

[16] J.P. Wang, F.L. Lin, B.C. Huang, et al. A new experimental approach to evaluate friction in ring test. Journal of Materials Processing Technology, 197(2008): 68~76.

DOI: 10.1016/j.jmatprotec.2007.06.017

Google Scholar

[17] S.Y. Luo, D.H. Zhu, L Hua, et al. Effects of process parameters on deformation and temperature uniformity of forged Ti-6Al-4V turbine blade. Journal of Materials Engineering & Performance, 25(2016): 1~13.

DOI: 10.1007/s11665-016-2320-0

Google Scholar