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Surface integrity of high strength aviation aluminum alloy in CURP treatment

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Abstract

In order to explore the influence of cutting process (CP) pretreatment on surface integrity in ultrasonic rolling process (URP), we build a composite cutting–ultrasonic rolling process (CURP) model of 7N01 aluminum alloy based on finite element (FE) software and obtain the deformation mechanism of surface material in CURP treatment through plane ultrasonic rolling experiments. The results show that under CP pretreatment at different feed rates, after URP treatment, surface roughness is reduced by more than 70% compared to after CP treatment; after CURP treatment, surface roughness increases with increasing feed rate; maximum surface microhardness reaches 185 HV, and hardened depth rises to 500 μm. Cutting depth makes the greatest difference to residual stress in CURP; both the amount and depth of residual stress increase with increasing cutting depth; when the cutting depth is 0.6 mm, the residual stress after CURP treatment reaches – 350 MPa. FE analysis reveals that during URP, the surface micro-elements will pass through three deformation zones—extrusion, impact, and recovery. The coupling of mechanical stress and thermal stress will turn the residual tensile stress caused by CP treatment into a compressive stress.

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Funding

This study was funded by the National Natural Science Foundation of China (NO.51575289), the Key Research and Development Project of Shandong Province (No. 2019GHY112068), and the Natural Science Foundation of Shandong Province (NO. ZR2019PEE028).

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Authors and Affiliations

  1. School of Mechanical and Automotive Engineering, Qingdao University of Technology, Shandong, Qingdao, 266520, China

    Xiao Yu, Youqiang Wang & Xuezhao Wang

  2. Key Lab of Industrial Fluid Energy Conservation and Pollution Control, Ministry of Education Qingdao Shandong, Shandong, Qingdao, 266520, China

    Xiao Yu, Youqiang Wang & Xuezhao Wang

  3. School of Mechanical and Electronic Engineering, Shandong University of Science and Technology, Shandong, Qingdao, 266590, China

    Ping Zhang

  4. School of Intelligent Manufacturing, Qingdao Huanghai University, Shandong, Qingdao, 266427, China

    Xiujie Yue

Authors
  1. Xiao Yu
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  2. Youqiang Wang
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  3. Ping Zhang
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  4. Xuezhao Wang
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Contributions

The first author Xiao Yu has been responsible for writing this paper, drawing up the experimental scheme, establishing the finite element model, and analyzing all the obtained raw data. The corresponding author Youqiang Wang directed the analysis of experiment and simulation data. Ping Zhang was mainly responsible for the residual stress test in this paper. Xuezhao Wang and Xiujie Yue assisted in CURP processing.

Corresponding author

Correspondence to Youqiang Wang.

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Yu, X., Wang, Y., Zhang, P. et al. Surface integrity of high strength aviation aluminum alloy in CURP treatment. Int J Adv Manuf Technol 119, 6135–6146 (2022). https://doi.org/10.1007/s00170-021-08499-w

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  • DOI: https://doi.org/10.1007/s00170-021-08499-w

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