Research on Overall Aluminum Alloy Flange Machining Deformation

Article Preview

Abstract:

Machining deformation has been a bottle-neck issue in aeronautical manufacturing field. Due to the large amount of material removal and other issues, machining deformation is predicted more difficultly during the process of 2026-T3511 aluminum alloy rim. Hence a simple full-size model of margin monolithic was built to study the deformation under the influence of residual stress releasing. The process of the structural parts was simulated and the deformation law of overall structure considering residual stress releasing only was revealed. Through the comparative study of different machining processing, control strategy reducing the final part machining deformation and optimum machining allowance range were proposed.

You might also be interested in these eBooks

Info:

Periodical:

Materials Science Forum (Volumes 836-837)

Pages:

436-443

Citation:

Online since:

January 2016

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2016 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] S. l. Dai, K. Zhang, S.J. Yang, Advanced Areanautical Aluminum Alloy Materials Technology and Application, Beijing: National Defend Industry Press, (2012).

Google Scholar

[2] G.L. Zhang, Study on the machinability of aero-aluminum alloy and distortion prediction and control of the aerospace beam, Shanghai: Shanghai Jiao Tong University, (2010).

Google Scholar

[3] S. Antonio, G. Niccolò, FEM based cutting velocity selection for thin walled part machining, Procedia CIRP 14(2014)287 – 292.

DOI: 10.1016/j.procir.2014.03.023

Google Scholar

[4] R.A. Izamshah, P.T. John, Finite element analysis of machining thin-wall parts. Key Engineering Materials. 458(2010)283-288.

DOI: 10.4028/www.scientific.net/kem.458.283

Google Scholar

[5] S. Bolsunovskiy, V. Vermel, G. Gubanov, Thin-Walled Part Machining Process Parameters Optimization based on Finite-Element Modeling of Workpiece Vibrations, Procedia CIRP 8 (2013) 276 – 280.

DOI: 10.1016/j.procir.2013.06.102

Google Scholar

[6] R. Seshadri, I. Naveen, S. Sharan, Finite Element Simulation of the Orthogonal Machining Process with Al 2024 T351 Aerospace Alloy, Procedia Engineering . 64 (2013) 1454 – 1463.

DOI: 10.1016/j.proeng.2013.09.227

Google Scholar

[7] T.T. Chen, B. Rong, Y.F. Yang, FEM-based Prediction and Control of Milling Deformation for a Thin-wall Web of Ti-6Al-4V Alloy. Materials Science Forum Vols. 800-801 (2014) 368-373.

DOI: 10.4028/www.scientific.net/msf.800-801.368

Google Scholar

[8] Y. Wang, X.F. WU, H.Z. Zhang, Finite Element Simulation of Deformation in Machining Large Thin-walled Aluminum Alloy Ring, Journal of Wuhan University of Technolotgy-Mater. S1(2009)95-99.

Google Scholar

[9] G.Y. Wang, Y.X. Wu, P.F. Yan, Prediction model for machining deformation of aeronautical aluminum alloy thin-walled workpiece, Journal of Central South University (Science and Technology). 43(2012)1696-1702.

Google Scholar

[10] G. Li, W.Y. Chen, P. Zhang, Analysis and Calculation on Machining Deformation of Parameterized Thin-Wall Workpiece Based on ANSYS, Aeronautical Manufacturing Technology . 19(2011)76-79.

Google Scholar