Numerical simulation study on rolling-chemical milling process of aluminum-lithium alloy skin panel

0Citations
Citations of this article
5Readers
Mendeley users who have this article in their library.

This article is free to access.

Abstract

Single curvature parts such as aircraft fuselage skin panels are usually manufactured by rolling-chemical milling process, which is usually faced with the problem of geometric accuracy caused by springback. In most cases, the methods of manual adjustment and multiple roll bending are used to control or eliminate the springback. However, these methods can cause the increase of product cost and cycle, and lead to material performance degradation. Therefore, it is of significance to precisely control the springback of rolling-chemical milling process. In this paper, using the method of experiment and numerical simulation on rolling-chemical milling process, the simulation model for rolling-chemical milling process of 2060-T8 aluminum-lithium alloy skin was established and testified by the comparison between numerical simulation and experiment results for the validity. Then, based on the numerical simulation model, the relative technological parameters which influence on the curvature of the skin panel were analyzed. Finally, the prediction of springback and the compensation can be realized by controlling the process parameters.

Cite

CITATION STYLE

APA

Huang, Z. B., Sun, Z. G., Sun, X. F., & Li, X. Q. (2017). Numerical simulation study on rolling-chemical milling process of aluminum-lithium alloy skin panel. In IOP Conference Series: Materials Science and Engineering (Vol. 242). Institute of Physics Publishing. https://doi.org/10.1088/1757-899X/242/1/012040

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free