Analysis on Milling Deformation of 7022 Aluminum Alloy Blank Jointed by FSJ

Dun Wen Zuo; Hong Feng Wang; Hong Miao; H.J. Wang

doi:10.4028/www.scientific.net/KEM.499.27

Paper Titles

Accuracy Synthesis of Redundant Parallel Kinematic Mechanism with Weighted Least Square Method
p.3

Advances in High-Speed Milling of Metal Matrix Composites
p.9

Analysis and Prediction Approach to the Thin-Walled Workpiece Deformation with Thermo-Mechanical Couple Consideration
p.15

Analysis of Structural Parameters of Grooved-Wicksin Micro Heat Pipes Based on Capillary Limits
p.21

Analysis on Milling Deformation of 7022 Aluminum Alloy Blank Jointed by FSJ
p.27

Chemical Mechanical Polish of Potential New Barrier Material Ruthenium (Ru) in ULSI Copper Interconnects
p.33

Computer Simulation of AISI D2 Orthogonal Cutting Using Finite Element Method
p.39

Deposition and Application of CVD Diamond Films on the Interior-Hole Surface of Silicon Carbide Compacting Dies
p.45

Design and Simulation of the Hydraulic System for the Disc Cutter of the Rock Hob Test-Bed
p.51

HomeKey Engineering MaterialsKey Engineering Materials Vol. 499Analysis on Milling Deformation of 7022 Aluminum...

Analysis on Milling Deformation of 7022 Aluminum Alloy Blank Jointed by FSJ

Abstract:

Milling process of jointing blank of 7022 aluminum alloy was simulated by ANSYS. The results show that the maximum residual tensile stress and pressure stress are mainly concentrated in the jointing seam zone when the jointing blank is milled. The milling deformation of jointing blank is shown as “wave” shape. The milling deformation of key eye side is shown upwarp. The jointing initiating terminal is shown downward displacement. The maximum downward displacement is present to the middle of jointing seam central line. In additional, the milling deformation along sheet length direction is shown outward extension.

You might also be interested in these eBooks

Anti-Fatigue Design and Manufacturing Technologies I

View Preview

Info:

Periodical:

Key Engineering Materials (Volume 499)

Pages:

27-32

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.499.27

Citation:

Cite this paper

Online since:

January 2012

Authors:

Dun Wen Zuo, Hong Feng Wang, Hong Miao, H.J. Wang

Keywords:

7022 Aluminum Alloy, Friction Stir Jointing, Milling Deformation, Milling Process, Residual Stress

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] G Y Li: Aeronautical Manufacturing Technology, Vol. (9) (2005), pp.36-43.

Google Scholar

[2] Y F Pu: Aviation Industry Forum, Vol. (1) (2009), pp.16-23.

Google Scholar

[3] H F Wang, D W Zuo, D L Shao, et al.: Journal of Shenzhen University Science and Engineering, Vol. 27(2) (2010), pp.172-177.

Google Scholar

[4] D Joeli: Weiding Journal Vol. 80(5) (2001), pp.30-34.

Google Scholar

[5] G H Luan, T H North, D L Guo, et al.: Transactions of the China Jointing Institution Vol. 23(6) (2002), pp.62-66.

Google Scholar

[6] W M Thomas, Nicholas E D: Materials and Design Vol 18(6) (1997), pp.269-273.

Google Scholar

[7] M Guerra, C Schmidt, J C Mcclure, et al: Materials Characterization Vol 49(2003), pp.95-101.

Google Scholar

[8] A P Reynolds, F Duvall: Jointing Journal Vol 78(10) (1999), pp.355-360.

Google Scholar

[9] H W Zhang, Z Zhang and J T Chen: Materials Science and Engineering Vol A403 (2005) , pp.340-348.

Google Scholar

[10] H Guo.: Study on mechanism and prediction analysis of machining distortion for aero-multi-frame monolithic structure parts(Ph. D dissertation of Nanjing University of Aeronautics and Astronautics, China, 2005).

Google Scholar