Numerical-Experimental Correlation of Distortions Induced by Machining Process on Thin-Walled Nickel Super Alloy Forged Components

Article Preview

Abstract:

AeroEngines main components made by nickel super alloys are mainly obtained by machining of large forged components. The work piece machining process generates some distortions that may also be relevant. In this contest, in many cases the removed volume in the machining operations represents a large percentage of the forged component in order to obtain the thin-walled wanted geometry. Due to this reason, the residual bulk stresses induced by the process history can lead to significant 3D geometric distortions in the machined component with unacceptable dimensions and shapes of the obtained product for comparison with the wanted geometry. Moreover, it is a matter of fact how, the final component distortions depend by the cutting strategy adopted in the machining process. The experimental study of such cutting strategies on real components are particularly time consuming and costly and for this reason the chance to study the problem using reliable numerical models it is particularly welcome. In the present work authors reports the numerical model development of the forging and machining processes needed for the production of a aircraft engine component and the comparison of the obtained results with the ones physically measured. The objective is to develop and validate a modeling method able to predicts the shape and the magnitude of the distortion induced by the machining operation on the considered component and to establish a possible strategy to suggest machining working steps able to improve the quality of the manufactured component reducing the needed production time.

You might also be interested in these eBooks

Info:

Periodical:

Key Engineering Materials (Volumes 504-506)

Pages:

1299-1304

Citation:

Online since:

February 2012

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] J. Su, Residual Stress Modeling In Machining Processes, Ph D Thesis, Georgia Institute of Technology, (2006).

Google Scholar

[2] G. Shen, D. Furrer, Manufacturing of aerospace forgings, Journal of Materials Processing Technology 98 (2000) 189-195.

DOI: 10.1016/s0924-0136(99)00198-3

Google Scholar

[3] J. Gayda, Effect of heat treatment on residual stress and machining distortions in advanced nichel base disk alloys, NASA/TM (2001).

Google Scholar

[4] M. Zhongyi, W Yunqiao, Analyzing distortion of Aircraft structural part in NC machining based on FEM simulation, International Conference on Mechanical and Electrical Technology (2010).

DOI: 10.1109/icmet.2010.5598480

Google Scholar

[5] O. Pierard, J. Barboza, M. Duflot, L. D'Alvise, A. Perez-Duarte, Distortions prediction during multi-pass machining simulation, Int. J Mater. Form, suppl. 1 (2008) 563-565.

DOI: 10.1007/s12289-008-0318-3

Google Scholar

[6] M, Zhongyi, W. Yunqiao, A. Saleem, Distortion Analysis of Arc Shaped Workpiece in NC Machining, Proceedings of the World Congress on Engineering (2011) Vol III.

Google Scholar

[7] D. Dye, K.T. Conlon, R.C. Reed, Characterization and modeling of quenching-induced residual stresses in the nichel-based superalloy IN718, Metallurgical and Materials Transactions , Vol. 35A, (2004) 1713-1723.

DOI: 10.1007/s11661-004-0079-7

Google Scholar

[8] Lambda Research, Minimizing Distortion in Machining, NUM. 24 (1999).

Google Scholar