journal article·2025-08-19

Assembly interface accuracy prediction model considering stress release

Niu Nana, Zhao Yongsheng, Liu Zhifeng, Cheng Qiang

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Abstract

Due to the effects of vibration, shock and alternating loads, uneven stress release and stress redistribution occur in the large bolt connection structure of the machine tool. This will lead to deformation of the assembly structure under the combined action of assembly stress and residual stress. This will result in a decline in the assembly performance of the bolt connection structure. This paper proposes a prediction model for the connection state of the machine tool bed- guideway assembly interface considering stress release, and obtains the interface accuracy and stiffness losses caused by stress release. The installation base plane of the bed- guideway is simplified as a beam model, and the coupling relationship between assembly stress and residual stress is considered, obtaining the evolution law of the force balance system caused by stress release, and finally, the deflection deformation curve of the base plane in the time domain is obtained through the stress release law. This method will provide new methods and ideas for the accuracy prediction of the assembly interface.
Source: openalex_inverted_index · Quality: baseline

Research context

OpenAlex topics: Manufacturing Process and Optimization · Adhesion, Friction, and Surface Interactions · Additive Manufacturing Materials and Processes

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Beijing University of Technology

Jilin University

Funding

National Natural Science Foundation of China

References (22)

Show source-provided references
1. 10.1016/j.jmps.2019.10372410.1016/j.jmps.2019.103724 ↗
2. Greenwood J, Williamson J. Contact of nominally flat surfaces. Proc R Soc Lond. 1966;295(1442):300–319.
3. 10.3901/JME.2007.03.09510.3901/JME.2007.03.095 ↗
4. 10.1177/0954405424131033010.1177/09544054241310330 ↗
5. 10.1016/j.cirp.2017.04.09710.1016/j.cirp.2017.04.097 ↗
6. 10.1177/0954405421101965510.1177/09544054211019655 ↗
7. Gu B, Tao X, Zhao Y. Residual stress inversion and deformation calculation based on elastic theory. J Solid State Mech. 2024;45(2):188–200.
8. Wang S. Research on prediction of residual stress in milling of aviation structural components and control of machining deformation. Harbin Institute of Technology; 2025.
9. Liu X, Wang Y, Li C, et al. Research on deformation simulation and deformation control technology of guideway beam processing based on residual stress redistribution. Aeronaut Manuf Technol. 2023;66(13):102–112.
10. Feng Z, Ou Y, Bao Y, et al. Study on defect-free hole making method for aviation carbon fiber composite components. Aeronaut Manuf Technol. 2010(6):32–34.
11. Sun G. Research on repeated positioning error mechanism, suppression technique and error evaluation method of precision machine tool linear shaft. Tianjin University; 2023 Dev 07.
12. 10.1007/s00158-019-02356-x10.1007/s00158-019-02356-x ↗
13. 10.1177/095440621561590910.1177/0954406215615909 ↗
14. 10.1016/j.precisioneng.2024.11.01110.1016/j.precisioneng.2024.11.011 ↗
15. 10.1109/TIA.2025.353255810.1109/TIA.2025.3532558 ↗
16. 10.1186/s10033-025-01184-z10.1186/s10033-025-01184-z ↗
17. 10.1109/TMECH.2023.329350510.1109/TMECH.2023.3293505 ↗
18. 10.1016/j.triboint.2023.10827510.1016/j.triboint.2023.108275 ↗
19. 10.1108/AA-04-2020-005810.1108/AA-04-2020-0058 ↗
20. 10.1002/qre.283610.1002/qre.2836 ↗
21. 10.1007/s00170-021-07957-910.1007/s00170-021-07957-9 ↗
22. Li G, Lin X, Xie T, et al. Numerical simulation and experimental analysis of beam residual stress in CNC gantry boring and milling machine. Hot Work Technol. 2019;48(22):6.