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Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (13): 629365-629365.doi: 10.7527/S1000-6893.2023.29365

• special column • Previous Articles     Next Articles

Residual stresses evolution mechanism of thin⁃walled component and deformation control method

Zhongxi ZHANG1, Shuaiqin WANG1, Huijuan ZHAO1(), Dinghua ZHANG2, Longhao WANG1   

  1. 1.School of Mechanical Engineering,Yangzhou University,Yangzhou 225009,China
    2.Key Laboratory of High Performance Manufacturing for Aero Engine,Ministry of Industry and Information Technology,Northwestern Polytechnical University,Xi’an 710072,China
  • Received:2023-07-25 Revised:2023-08-17 Accepted:2023-10-07 Online:2024-07-15 Published:2023-12-01
  • Contact: Huijuan ZHAO E-mail:008370@yzu.edu.cn
  • Supported by:
    National Natural Science Foundation of China(52205501);Key Laboratory of High Performance Manufacturing for Aero Engine (Northwestern Polytechnical University), Ministry of Industry and Information Technology(HPM-2021-04);The High-level Talent Program of Yangzhou University(137012319);Yangzhou-Yangzhou University Cooperative Innovation Technology Platform Support Project(YZ2020266)

Abstract:

Deformation is one of the most important challenges in the machining of the thin-walled component, especially for the complicated thin-walled component with difficult-to-machining material. The internal stress and machining induced residual stress are evolved during the machining process, causing the poor machining accuracy of the final component. To solve this problem, a deformation control method based on the evolution mechanism of residual stress is proposed. Firstly, the simplified model of the component is obtained through the slice method. The equilibrium equation for clamping point is established by analyzing the loads distribution. The geometric equilibrium equation is then obtained according to the deformation superposition principle and micro deformation theory. The distribution of loads at different instants of machining process is analyzed, and the evolution mechanism of the residual stresses and the equivalent loads is revealed. Secondly, a mathematical model is established to regulate the in-process deformation of the thin-walled component. As the result, the evolution of the residual stresses and the deformation of the final component is controlled. Finally, 3 deformation validation experiments are carried out to process the same thin plates, and the deformation of the thin plates are compared. The experimental results indicate that the maximum deformation can be reduced by 82.2%.

Key words: thin-walled component, residual stress, evolution mechanism, equilibrium state, deformation control

CLC Number: