Numerical Analysis of Residual Stresses in Quenched High-Strength Aluminum Alloy Ultra-Thick Plates and their Reduction through Single-Side Cold Compression Method

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Abstract:

Residual stresses developed after quenching of high-strength aluminum alloy ultra-thick plates have an important effect on the quality and reliability of parts, and should be reduction to meet the requirement. In this investigation, numerical techniques of SIMUFACT software are used to simulate residual stresses in quenched 340mm×127mm×124mm Al-Zn-Mg-Cu high-strength aluminum alloy ultra-thick plate, and the results have been verified. On the basis of verified simulation parameters, residual stresses in quenched 4000mm×720mm×285mm ultra-thick plate and their reduction through single-side cold compression method were simulated by SIMUFACT software. After quenching, the value of maximum tension stress located at the interior center of the plate is 200MPa, and the value of maximum compression stress located on the surface of the plate is-169MPa. Through analysis of single-side cold compression processes, it can be concluded that more than 90% quenching residual stresses can be reduced by 1% upsetting ratio and 75% feed of the top die. Residual stresses after compression can be reduced down to the range of-25~9MPa. Mean residual stress values of simulation after compression are identical to the XRD testing data.

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Advanced Materials Research (Volumes 887-888)

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400-406

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February 2014

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© 2014 Trans Tech Publications Ltd. All Rights Reserved

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[1] P. Lequeu, P. Lassince, T. Warner, and G.M. Raynaud. Engineering for the future: weight saving and cost reduction initiative. Aircraft Engr Aerospace Tech. 73 (2001) 147-158.

DOI: 10.1108/00022660110386663

Google Scholar

[2] Z.D. Huda, E. Prasetyo. Materials selection in design of structures and engines of supersonic aircrafts: A review. Materials and Design 46 (2013) 552-560.

DOI: 10.1016/j.matdes.2012.10.001

Google Scholar

[3] S.Y. Chen, K.H. Chen, G.S. Peng, X. Liang, X.H. Chen. Effect of quenching rate on microstructure and stress corrosion cracking of 7085 aluminum alloy. Trans. Nonferrous Met. Soc. China 22 (2012) 47-52.

DOI: 10.1016/s1003-6326(11)61138-2

Google Scholar

[4] J.S. Robinson, S. Hossain, C.E. Truman, A.M. Paradowska, D.J. Hughes, R.C. Wimpory, M.E. Fox. Residual stress in 7449 aluminium alloy forgings. Materials Science and Engineering A 527 (2010) 2603-2612.

DOI: 10.1016/j.msea.2009.12.022

Google Scholar

[5] J.S. Robinson, D.A. Tanner, C.E. Truman, A.M. Paradowska, R.C. Wimpory. The influence of quench sensitivity on residual stresses in the aluminium alloys 7010 and 7075. Materials characterization 65 (2012) 73-85.

DOI: 10.1016/j.matchar.2012.01.005

Google Scholar

[6] A.K. Nallathambi, Y. Kaymak, E. Specht, A. Bertram. Sensitivity of material properties on distortion and residual stresses during metal quenching processes. Journal of Materials Processing Technology 210 (2010) 204-211.

DOI: 10.1016/j.jmatprotec.2009.09.001

Google Scholar

[7] X. Yang, J. Zhu, Z. Lai, Y. Liu, H.E. Dong, Z. Nong. Finite element analysis of quenching temperature field, residual stress and distortion in A357 aluminum alloy large complicated thin-wall workpieces. Trans. Nonferrous Met. Soc. China 23(2013).

DOI: 10.1016/s1003-6326(13)62657-6

Google Scholar

[8] C.J. Lammi, D.A. Lados. Numerical predictions and experimental measurements of residual stresses in fatigue crack growth specimens. Engineering Fracture Mechanics 78 (2011) 1114-1124.

DOI: 10.1016/j.engfracmech.2011.01.029

Google Scholar

[9] K. Mori, Y. Abe, T. Kato. Mechanism of superiority of fatigue strength for aluminium alloy sheets joined by mechanical clinching and self-pierce riveting. Journal of Materials Processing Technology 212 (2012) 1900-(1905).

DOI: 10.1016/j.jmatprotec.2012.04.017

Google Scholar

[10] D.A. Tanner, J.S. Robinson. Modelling stress reduction techniques of cold compression and stretching in wrought aluminium alloy products. Finite Elements in Analysis and Design 39 (2003) 369-386.

DOI: 10.1016/s0168-874x(02)00079-3

Google Scholar

[11] S. Zhang, Y.X. Wu, H. Gong. A modeling of residual stress in stretched aluminum alloy plate. Journal of Materials Processing Technology 212 (2012) 2463-2473.

DOI: 10.1016/j.jmatprotec.2012.06.019

Google Scholar

[12] Q.C. Wang. The study of residual stress relief and its evaluation in aviation aluminum alloy parts. In Chinese. Zhejiang University. 2003. 1-136.

Google Scholar

[13] X.W. Yang, J.C. Zhu, Z.S. Nong, Z.H. Lai, D. He. FEM simulation of quenching process in A357 aluminum alloy cylindrical bars and reduction of quench residual stress through cold stretching process. Computational Materials Science 69 (2013).

DOI: 10.1016/j.commatsci.2012.11.024

Google Scholar

[14] G.Y. Lin. The basic research of process technology in high performance 7x75 aluminum alloy thick plate. In Chinese. Central South University. (2006) 1-176.

Google Scholar

[15] M. Koc, J. Culp, T. Altan. Prediction of residual stresses in quenched aluminum blocks and their reduction through cold working processes. Journal of Materials Processing Technology 174 (2006) 342-354.

DOI: 10.1016/j.jmatprotec.2006.02.007

Google Scholar