Modeling of Residual Stress and Machining Distortion in Aerospace Components

2010 ◽  
pp. 386-407
2018 ◽  
Vol 764 ◽  
pp. 49-57
Author(s):  
Hun Guo ◽  
Dun Wen Zuo ◽  
Fei Hong Yin ◽  
Ya Feng He ◽  
Ji Xu ◽  
...  

It is one of the difficult problems in the manufacture of the integrated aircraft part of Machining distortion caused by residual stress. According to the characteristics of aluminum alloy pre stretched thick plate, the modified removal method for measuring residual stress in thick pre-stretched aluminum plates is proposed and the stress-strain relation matrix is deduced by elasticity theory. Moreover, the residual stresses in the specimen of 7075T7351 plate is measured by the proposed method, and the results are finally analyzed and compared with the data obtained by other methods. The results indicate that the proposed method is effective in measuring the residual stress in thick pre-stretched aluminum alloy plates. The measurement results can be used for the quantitative analysis of aerospace parts machining distortion caused by residual stress, and it has higher value in engineering application.


2006 ◽  
Vol 315-316 ◽  
pp. 235-238 ◽  
Author(s):  
Q.C. Wang ◽  
Xiao Dong Hu ◽  
W. Li ◽  
Ju Long Yuan

The presence of residual stress in aircraft aluminum components can give rise to distortion after machining. Excessive distortion may result in the rejection of a part or the need for costly and time-consuming rework prior to placement in service. The purpose of this research was to develop a methodology for the prediction of machining-induced distortions of residually stressed aircraft aluminum components. Numerical simulation results show that the magnitude of machining distortion is strongly related to the square root of Stain Energy Density W or Stress Range σ . The experimental results demonstrate good agreement with the predicted machining distortions of 7075T73 bulkheads. It included that the original residual stress in the blocks of aircraft aluminum component is one of key factors to cause machining distortion.


Procedia CIRP ◽  
2021 ◽  
Vol 104 ◽  
pp. 1328-1333
Author(s):  
M. Landwehr ◽  
F. Oehler ◽  
H. Behnken ◽  
H. Holling ◽  
R. Sambathkumar ◽  
...  

2005 ◽  
Vol 18 (2) ◽  
pp. 175-179 ◽  
Author(s):  
Zhao-jun WANG ◽  
Wu-yi CHEN ◽  
Yi-du ZHANG ◽  
Zhi-tong CHEN ◽  
Qiang LIU

2010 ◽  
Vol 33 ◽  
pp. 88-91
Author(s):  
Yuan Wei Liu

Formulae of stress re-distribution and distortion by stress releasing during milling process are deduced by elasticity theory. Theory prediction of milling deformation due to residual stress is finished, and some calculating equation is given for the deformation solution. By means of these researches, the mechanism of the milling deformation due to residual stress is analyzed, the machining distortion caused by residual stress are analyzed and summarized using the analytical method.


2011 ◽  
Vol 381 ◽  
pp. 44-47
Author(s):  
Hun Guo ◽  
Dun Wen Zuo ◽  
Guo Xing Tang ◽  
W.M. Gan

Formulae of stress re-distribution and distortion by stress releasing during milling process are deduced to Initial Residual Stresses. Theory prediction of milling deformation due to residual stress is finished, and some calculating equation is given for the deformation solution. By means of these researches, the mechanism of the milling deformation due to residual stress is analyzed, the machining distortion caused by residual stress are analyzed and summarized using the analytical method.


2012 ◽  
Vol 426 ◽  
pp. 143-146 ◽  
Author(s):  
Jie Chen

When machining multi-frame complex components, more than 90% of the materials would be removed, resulting in severe distortion of the parts due to the weakened rigidity and the release of residual stress. This might also lead to stress concentration and damage of the parts. The effect of material removal from residually stressed billet is simulated using FEA software ANSYS, and the causations of distortion is analyzed. To verify the finite element simulation, a high speed milling test on aluminum alloy 7050T7351 is carried out. The results show that the simulation result is consistent with the experimental one. It included that the original residual stress in the blocks of aero-aluminum component is one of key factors to cause machining distortion.


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