Skip to main content
Log in

Fatigue performance on 7050 aluminum alloy by twice hole expansion strengthening of split mandrel

  • ORIGINAL ARTICLE
  • Published:
The International Journal of Advanced Manufacturing Technology Aims and scope Submit manuscript

Abstract

To investigate the impact of various forms of hole expansion strengthening of split mandrel (HESSM) process on the fatigue performance of 7050 aluminum alloy, a 3D finite element simulation analysis model is established for once hole expansion strengthening (OHES) and twice hole expansion strengthening. HESSM experiment is conducted to explore its influence on hole wall stress, microstructure, and fatigue life. The results show that the depth of the plastic deformation layer in the middle area of the hole wall is 1.69 times for specimens by twice hole expansion strengthening than that of OHES. Additionally, residual stress on the hole wall is higher and uniform for compared with OHES, when by twice hole expansion strengthening in opposite directions (THESOD) using split mandrel. The median fatigue life of the specimen by OHES is 1.52 times that of without expansion strengthening (WES). The median fatigue life of the specimen by twice hole expansion strengthening in the same direction using split mandrel is 1.73 times that of WES, and the median fatigue life of the specimen by THESOD using split mandrel is 1.80 times that of WES.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12
Fig. 13
Fig. 14
Fig. 15
Fig. 16
Fig. 17
Fig. 18
Fig. 19
Fig. 20
Fig. 21
Fig. 22
Fig. 23

Similar content being viewed by others

Data availability

All data generated or analyzed during this study are included in the present article.

References

  1. Bugdayci B, Lazoglu I (2015) Temperature and wear analysis in milling of aerospace grade aluminum alloy Al-7050. Prod Eng Res Devel 9:487–494

    Article  Google Scholar 

  2. Ye Z, Wang YG, Yu X (2022) Study on the reaming process of aluminum alloy 7050–T7451 under different cooling conditions. Adv Manufact 10(2):272–286

    Article  Google Scholar 

  3. Yu X, Wang YG, Lv DJ (2020) A novel chip breaker structure of PCD tool for the reaming of 7050 aluminum alloy. Int J Adv Manuf Technol 109:659–672

    Article  Google Scholar 

  4. Wang M (1999) Anti-fatigue manufacture principle and technology. Jiangsu Science and Technology Press, Nanjing

    Google Scholar 

  5. Wang YL, Zhu YL, Cao Q, Zhang XH (2018) Progress and prospect of research on hole cold expansion technique. Acta Aeronautica et Astronautica Sinica 39(02):6–22

    Google Scholar 

  6. Fu YC, Ge ED, Su HH, Xu JH, Li RZ (2015) Cold expansion technology of connection holes in aircraft structures: a review and prospect. Chin J Aeronaut 28(04):961–973

    Article  Google Scholar 

  7. Sticchi M, Schnubel D, Kashaev N, Huber N (2015) Review of residual stress modification techniques for extending the fatigue life of metallic aircraft components. Appl Mech Rev 67(1):010801

    Article  Google Scholar 

  8. Lin ZL, Bai QS, Wang HF, Tang W, Wu BQ (2023) Research progress of strengthening mechanism and fatigue life in cold expansion of bushing for hole. Surf Technol 52(04):1–14+99

    Google Scholar 

  9. Lu SH, Gao Y, Li DC (2021) Research progress of split sleeve cold expansion strengthening technology. Forg Stamp Technol 46(01):1–9

    Google Scholar 

  10. Xue XH (2019) Effect of cold expansion on fatigue behavior of domestic 7050 alloy lugs. Xi’an University of Architecture and Technology, Xi’an

  11. Ge ED (2015) Research on hole expansion strengthening technology of composites and their stacks joint structures. Nanjing University of Aeronautics and Astronautics, Nanjing

    Google Scholar 

  12. Kumar BM, Panaskar NJ, Sharma A (2014) A fundamental investigation on rotating tool cold expansion: numerical and experimental perspectives. Int J Adv Manuf Technol 73:1189–1200

    Article  Google Scholar 

  13. Geng HH, Xu XF, Cao QL, Lai ZP, Li L (2022) Improving the fatigue performance of AZ31 sheet with hole via electromagnetic cold expansion process. Int J Adv Manuf Technol 120:5057–5071

    Article  Google Scholar 

  14. Pan X, Zhang H, Yu JH, Wang C (2021) Effects of roller expansion parameters on residual stress and fatigue life of TA15. Mech Sci Technol Aerosp Eng 40(11):1787–1792

    Google Scholar 

  15. Amrouche A, Su M, Aid A, Mesmacque G (2008) Numerical study of the optimum degree of cold expansion: application for the pre-cracked specimen with the expanded hole at the crack tip. J Mater Process Technol 197:250–254

    Article  Google Scholar 

  16. Liu H, Hu DY, Wang RQ, Wang X, Jin SZ, Gu YX (2020) Experimental and numerical investigations on the influence of cold expansion on low cycle fatigue life of bolt holes in aeroengine superalloy disk at elevated temperature. Int J Fatigue 132:105390

    Article  Google Scholar 

  17. Hou S, Zhu YL, Cai ZH, Wang YL, Ni YH, Du XK (2019) Effect of hole cold expansion on fatigue performance of corroded 7B04-T6 aluminum alloy. Int J Fatigue 126:210–220

    Article  Google Scholar 

  18. Jose CC, Marta MM, Eva MR, Roberto T, Tiziana S (2019) Parametric analysis of the mandrel geometrical data in a cold expansion process of small holes drilled in thick plates. Materials 12:4150

    Google Scholar 

  19. Karabin ME, Barlat F, Schultz RW (2007) Numerical and experimental study of the cold expansion process in 7085 plate using a modified split sleeve. J Mater Process Technol 189(1–3):45–57

    Article  Google Scholar 

  20. Lv HQ, Fan ZY, Xu X, Huang X (2022) Simulation research on cold extrusion strengthening and reaming of 7050 aluminum alloy plate hole. Key Eng Mater 921:109–115

    Article  Google Scholar 

  21. Giovanni PP, Alessandro C, Stefano C, Adam E, Michele M (2021) Cold expansion of rail-end-bolt holes: finite element predictions and experimental validation by DIC and strain gauges. Int J Fatigue 149:106275

    Article  Google Scholar 

  22. Liu KY, Zhou L, Yang XS, Li M, Wang WW, Zhu WJ (2021) Finite element simulation of the cold expansion process with split sleeve in 7075 aluminum alloy. J Inst Eng India Ser C 102(2):361–374

    Article  Google Scholar 

  23. David CC, Jose CC, Pedro MBD, Mónica PC, Maria JGT (2020) Cold expansion process with multiple balls-numerical simulation and comparison with single ball and tapered mandrels. Materials 13:5536

    Article  Google Scholar 

  24. Yan WZ, Wang XS, Gao HS, Yue ZF (2012) Effect of split sleeve cold expansion on cracking behaviors of titanium alloy TC4 holes. Eng Fract Mech 88:79–89

    Article  Google Scholar 

  25. Su M, Amrouche A, Mesmacque G, Benseddiq N (2008) Numerical study of double cold expansion of the hole at crack tip and the influence on the residual stresses field. Comput Mater Sci 41(3):350–355

    Article  Google Scholar 

  26. Stefanescu D (2003) Experimental study of double cold expansion of holes. J Strain Anal Eng Des 38(4):339–347

    Article  Google Scholar 

  27. Sasan F, Sugrib KS, Seyed BB, Hamid J (2020) Split sleeve cold expansion of AZ31B sheet: microstructure, texture and residual stress. Mater Des 186:108213

    Article  Google Scholar 

  28. Yang GY, Li M, Song YG, Lu GX, Huang LJ (2016) Effect of twice hole expansion on fatigue property of Ti1023 alloy. J Aeronaut Mater 36(06):68–73

    Google Scholar 

  29. Luo XK, Ai YJ, Wang X, Wang Q, Song YG, Tang ZH, Zhao ZY (2017) Effect of double cold expansion of hole on fatigue property of TB6 titanium alloy. J Aeronaut Mater 37(06):88–94

    Google Scholar 

  30. Yasniy P, Glado S, Iasnii V (2017) Lifetime of aircraft alloy plates with cold expanded holes. Int J Fatigue 104:112–119

    Article  Google Scholar 

  31. Wang YL, Fu B, Nie L, Sun TP (2019) Fatigue nucleation site of cold expansion hole varying as fatigue load level varies. SN Appl Sci 867:1–10

    Google Scholar 

Download references

Funding

This work was financially supported by the National Natural Science Foundation of China for Creative Research Groups (No. 51921003), the financial support for this work by the Innovation Fund of National Commercial Aircraft Manufacturing Engineering Technology Research Center (No. COMAC-SFGS-607), and the Jiangsu Scientific Research and Practice Innovation Program (No. KYCX21_0196).

Author information

Authors and Affiliations

Authors

Contributions

Fei Liu: experimentation, data curation, and writing the original draft. Honghua Su: supervision, conceptualization, and methodology. Jiuhua Xu: supervision, and methodology. Yongnan Liang: experimentation.

Corresponding author

Correspondence to Honghua Su.

Ethics declarations

Ethics approval and consent to participate

The article follows the guidelines of the Committee on Publication Ethics (COPE) and involves no studies on human or animal subjects.

Consent to participate

Not applicable.

Consent for publication

Not applicable.

Competing interests

The authors have no conflicts of interest to declare that they are relevant to the content of this article.

Additional information

Publisher's Note

Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

Rights and permissions

Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law.

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Liu, F., Su, H., Xu, J. et al. Fatigue performance on 7050 aluminum alloy by twice hole expansion strengthening of split mandrel. Int J Adv Manuf Technol 129, 2241–2256 (2023). https://doi.org/10.1007/s00170-023-12416-8

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s00170-023-12416-8

Keywords

Navigation