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A prediction model of the extrusion deformation with residual stress on 6063 aluminum alloy aeronautical plate considering different extrusion parameters

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Abstract

The deformation of aluminum alloy aeronautical plate is a common problem in the processing. The machining deformation can usually be predicted by the initial residual stress in the aluminum alloy plate. In this study, a prediction model considering the extrusion parameters for predicting the machining deformation of aluminum alloy plate is proposed. The FEM simulations and experiments are conducted to validate the accuracy of the prediction model, and not only the residual stress results but also the deformation results show good agreements. In addition, the other four groups of experiments are performed to obtain the results of machining deformation under different extrusion parameters. Finally, the relationship between machining deformation and extrusion parameters is discussed. The extreme values and their positions of the deformations under different parameters are given.

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Funding

This work was supported by the National Natural Science Foundation of China (number 51875024), the Defense Industrial Technology Development Program (number JCKY2018601C002), the Civil Aerospace Technology Pre-research Project (number B0109), and the State Key Laboratory of Virtual Reality Technology Independent Subject (number BUAA-VR-16ZZ-07).

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Authors and Affiliations

  1. State Key Laboratory of Virtual Reality Technology and Systems, Beihang University, Beijing, 100191, People’s Republic of China

    Qiong Wu, Nian-Pu Xue, Yi-Du Zhang, Han-Jun Gao & Jian Wu

  2. School of Mechanical Engineering and Automation, Beihang University, Beijing, 100191, People’s Republic of China

    Qiong Wu, Nian-Pu Xue, Yi-Du Zhang, Han-Jun Gao & Jian Wu

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  1. Qiong Wu
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  2. Nian-Pu Xue
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Correspondence to Qiong Wu.

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Wu, Q., Xue, NP., Zhang, YD. et al. A prediction model of the extrusion deformation with residual stress on 6063 aluminum alloy aeronautical plate considering different extrusion parameters. Int J Adv Manuf Technol 107, 1671–1681 (2020). https://doi.org/10.1007/s00170-020-05102-6

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