Study on Prediction of Machining Distortion for Titanium Alloy Aircraft Monolithic Component by FEM

被引:0
|
作者
Yang, Yong [1 ]
Li, Huihui [1 ]
Meng, Guangyao [1 ]
机构
[1] Qingdao Technol Univ, Sch Mech Engn, Qingdao 266033, Shandong, Peoples R China
关键词
Aircraft monolithic component; Titanium alloy; Machining distortion; FEM;
D O I
10.4028/www.scientific.net/AMR.97-101.2951
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A physics-based material processing simulation is approached to research the machining distortion for titanium alloy aircraft monolithic component by the finite element method (FEM). Several key technologies, such as material constitutive model, material removal methodology of machining process, determination and application of cutting loads, have been implemented to improve the accuracy of finite element simulation. To verify the FEM result, an experiment is carried out. The distortion position and dimension of aircraft monolithic component resulting from FEM show a good agreement with the experiment result, which indicates that the key technologies presented in the paper are practicable and can be used to simulate the machining process of monolithic component to predict its distortion.
引用
收藏
页码:2951 / 2954
页数:4
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