Chinese Journal of Mechanical Engineering >

2021 , Vol. 34 >Issue 6: 90 - 90

DOI: https://doi.org/10.1186/s10033-021-00611-1

Research article

Influence of Ultrasonic Surface Rolling Process and Shot Peening on Fretting Fatigue Performance of Ti-6Al-4V

  • Ning Wang ,
  • Jinlong Zhu ,
  • Bai Liu ,
  • Xiancheng Zhang ,
  • Jiamin Zhang ,
  • Shantung Tu
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  • Key Laboratory of Pressurized System and Safety, East China University of Science and Technology, Shanghai, 200237, China
Ning Wang, born in 1980, is currently an associate professor at Key Laboratory of Pressurized System and Safety, East China University of Science and Technology, China. She received her PhD degree from East China University of Science and Technology, in 2013. Her research interests include structural integrity, metal corrosion, creep and fretting fatigue of components;
Jinlong Zhu, born in 1995, is currently a master candidate at Key Laboratory of Pressurized System and Safety, East China University of Science and Technology, China.;
Bai Liu, born in 1996, is currently a master candidate at Key Laboratory of Pressurized System and Safety, East China University of Science and Technology, China.;
Xiancheng Zhang, born in 1979, is currently a professor at Key Laboratory of Pressurized System and Safety, East China University of Science and Technology, China. He received his PhD degree from Shanghai Jiao tong University, China, in 2008. His main research interests include fatigue fracture theory of multi-component structures, the design method and theory of material safety tolerance under extreme environment;
Jiamin Zhang, born in 1994, is currently a master candidate at Key Laboratory of Pressurized System and Safety, East China University of Science and Technology, China.;
Shantung Tu, born in 1961, is currently an academician of Chinese Academy of Engineering and a professor at Key Laboratory of Pressurized System and Safety, East China University of Science and Technology, China. His main research interests include chemical equipment safety, high temperature strength, advanced energy materials and equipment

收稿日期: 2020-12-29

  修回日期: 2021-08-07

  网络出版日期: 2022-04-03

基金资助

Supported by National Key Research and Development Project (Grant No.2018YFC1902400) and Natural Science Foundation of Shanghai (Grant No. 20ZR1415300).

收起

Influence of Ultrasonic Surface Rolling Process and Shot Peening on Fretting Fatigue Performance of Ti-6Al-4V

  • Ning Wang ,
  • Jinlong Zhu ,
  • Bai Liu ,
  • Xiancheng Zhang ,
  • Jiamin Zhang ,
  • Shantung Tu
Expand
  • Key Laboratory of Pressurized System and Safety, East China University of Science and Technology, Shanghai, 200237, China

Received date: 2020-12-29

  Revised date: 2021-08-07

  Online published: 2022-04-03

Supported by

Supported by National Key Research and Development Project (Grant No.2018YFC1902400) and Natural Science Foundation of Shanghai (Grant No. 20ZR1415300).

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摘要

At present, there are many studies on the residual stress field and plastic strain field introduced by surface strengthening, which can well hinder the initiation of early fatigue cracks and delay the propagation of fatigue cracks. However, there are few studies on the effects of these key factors on fretting wear. In the paper, shot-peening (SP) and ultrasonic surface rolling process (USRP) were performed on Ti-6Al-4V plate specimens. The surface hardness and residual stresses of the material were tested by vickers indenter and X-ray diffraction residual stress analyzer. Microhardness were measured by HXD-1000MC/CD micro Vickers hardness tester. The effects of different surface strengthening on its fretting fatigue properties were verified by fretting fatigue experiments. The fretting fatigue fracture surface and wear morphology of the specimens were studied and analyzed by means of microscopic observation, and the mechanism of improving fretting fatigue life by surface strengthening process was further explained. After USRP treatment, the surface roughness of Ti-6Al-4V is significantly improved. In addition, the microhardness of the specimen after SP reaches the maximum at 80 μm from the surface, which is about 123% higher than that of the AsR specimen. After USRP, it reaches the maximum at 150 μm from the surface, which is about 128% higher than that of AsR specimen. It is also found that the residual compressive stress of the specimens treated by USRP and SP increases first and then decreases with the depth direction, and the residual stress reaches the maximum on the sub surface. The USRP specimen reaches the maximum value at 0.18 mm, about -550 MPa, while the SP specimen reaches the maximum value at 0.1 mm, about -380 MPa. The fretting fatigue life of Ti-6Al-4V effectively improved after USRP and SP. The surface integrity of specimens after USRP is the best, which has deeper residual compressive stress layer and more refined grain. In this paper, a fretting wear device is designed to carry out fretting fatigue experiments on specimens with different surface strengthening.

关键词： Ti-6Al-4V; Fretting fatigue; Residual stress; Ultrasonic surface rolling process; Surface strengthening

本文引用格式

Ning Wang , Jinlong Zhu , Bai Liu , Xiancheng Zhang , Jiamin Zhang , Shantung Tu . Influence of Ultrasonic Surface Rolling Process and Shot Peening on Fretting Fatigue Performance of Ti-6Al-4V[J]. Chinese Journal of Mechanical Engineering, 2021 , 34(6) : 90 -90 . DOI: 10.1186/s10033-021-00611-1

Abstract

At present, there are many studies on the residual stress field and plastic strain field introduced by surface strengthening, which can well hinder the initiation of early fatigue cracks and delay the propagation of fatigue cracks. However, there are few studies on the effects of these key factors on fretting wear. In the paper, shot-peening (SP) and ultrasonic surface rolling process (USRP) were performed on Ti-6Al-4V plate specimens. The surface hardness and residual stresses of the material were tested by vickers indenter and X-ray diffraction residual stress analyzer. Microhardness were measured by HXD-1000MC/CD micro Vickers hardness tester. The effects of different surface strengthening on its fretting fatigue properties were verified by fretting fatigue experiments. The fretting fatigue fracture surface and wear morphology of the specimens were studied and analyzed by means of microscopic observation, and the mechanism of improving fretting fatigue life by surface strengthening process was further explained. After USRP treatment, the surface roughness of Ti-6Al-4V is significantly improved. In addition, the microhardness of the specimen after SP reaches the maximum at 80 μm from the surface, which is about 123% higher than that of the AsR specimen. After USRP, it reaches the maximum at 150 μm from the surface, which is about 128% higher than that of AsR specimen. It is also found that the residual compressive stress of the specimens treated by USRP and SP increases first and then decreases with the depth direction, and the residual stress reaches the maximum on the sub surface. The USRP specimen reaches the maximum value at 0.18 mm, about -550 MPa, while the SP specimen reaches the maximum value at 0.1 mm, about -380 MPa. The fretting fatigue life of Ti-6Al-4V effectively improved after USRP and SP. The surface integrity of specimens after USRP is the best, which has deeper residual compressive stress layer and more refined grain. In this paper, a fretting wear device is designed to carry out fretting fatigue experiments on specimens with different surface strengthening.

Key words： Ti-6Al-4V; Fretting fatigue; Residual stress; Ultrasonic surface rolling process; Surface strengthening

参考文献

[1] M J He. Fretting fatigue of mechanical components. Beijing:National Defense Industry Press, 1994. (in Chinese)
[2] M Ciavarella, G Demelio. A review of analytical aspects of fretting fatigue, with extension to damage parameters, and application to dovetail joints. International Journal of Solids and Structures, 2001, 38(10-13):1791-1811.
[3] J K Duan, X Y Yang, L W Dong, et al. Research on fracture of compressor blade dovetail from fretting wear. Gas Turbine Experiment and Research, 2009, 22(3):28-32.
[4] P Arnaud, S Fouvry. Modeling the fretting fatigue endurance from partial to gross slip:The effect of debris layer. Tribology International, 2020, 143:106069.
[5] R Rajasekaran, D Nowell. Fretting fatigue in dovetail blade roots:Experiment and analysis. Tribology International, 2006, 39(10):1277-1285.
[6] G Chen, J Yan, T Tian, et al. Effect of wet shot peening on Ti-6Al-4V alloy treated by ceramic beads. Transactions of Nonferrous Metals Society of China, 2014, 24(3):690-696.
[7] S Bagherifard, S Slawik, I Fernández-Pariente, et al. Nanoscale surface modification of AISI 316L stainless steel by severe shot peening. Materials & Design, 2016, 102:68-77.
[8] J Z Lu, L J Wu, G F Sun, et al. Microstructural response and grain refinement mechanism of commercially pure titanium subjected to multiple laser shock peening impacts. Acta Materialia, 2017, 127:252-266.
[9] S Srinivasan, D B Garcia, M C Gean, et al. Fretting fatigue of laser shock peened Ti-6Al-4V. Tribology International, 2009, 42(9):1324-1329.
[10] P J Golden, M J Shepard. Life prediction of fretting fatigue with advanced surface treatments. Materials Science and Engineering:A, 2007, 468:15-22.
[11] Y Zhang, S Descartes, P Vo, et al. Cold-sprayed Cu-MoS2 and its fretting wear behavior. Journal of Thermal Spray Technology, 2016, 25(3):473-482.
[12] Q Yang, W Zhou, X Zheng, et al. Investigation of shot peening combined with plasma-sprayed CuNiIn coating on the fretting fatigue behavior of Ti-6Al-4V dovetail joint specimens. Surface and Coatings Technology, 2019, 358:833-842.
[13] C Tang, Liu D Liu, B Tang, et al. Influence of plasma molybdenizing and shot-peening on fretting damage behavior of titanium alloy. Applied Surface Science, 2016, 390:946-958.
[14] Z R Zhou, L Vincent. Fretting wear. Beijing:Science Press, 2002.
[15] Z Ren, F Lai, S Qu, et al. Effect of ultrasonic surface rolling on surface layer properties and fretting wear properties of titanium alloy Ti5Al4Mo6V2Nb1Fe. Surface and Coatings Technology, 2020, 389:125612.
[16] K Li, X Fu, R Li, et al. Fretting fatigue characteristic of Ti-6Al-4V strengthened by wet peening. International Journal of Fatigue, 2016, 85:65-69.
[17] J Liu, X Zhang, Z Cui, et al. Effects of ultrasonic surface rolling processing and plasma nitriding on the fretting wear behavior of Inconel 690TT. Surface and Coatings Technology, 2020, 402:126312.
[18] D Liu, B Tang, X Zhu, et al. Improvement of the fretting fatigue and fretting wear of Ti6Al4V by duplex surface modification. Surface and Coatings Technology, 1999, 116:234-238.
[19] C Liu, D Liu, X Zhang, et al. Fretting fatigue characteristics of Ti-6Al-4V alloy with a gradient nanostructured surface layer induced by ultrasonic surface rolling process. International Journal of Fatigue, 2019, 125:249-260.
[20] L X Lu, J Sun, L Li, et al. Study on surface characteristics of 7050-T7451 aluminum alloy by ultrasonic surface rolling process. The International Journal of Advanced Manufacturing Technology, 2016, 87(9-12):2533-2539.
[21] Z Wang, Z Xiao, C Huang, et al. Influence of ultrasonic surface rolling on microstructure and wear behavior of selective laser melted Ti-6Al-4V alloy. Materials, 2017, 10(10):1203.
[22] H Wang, G Song, G Tang. Effect of electropulsing on surface mechanical properties and microstructure of AISI 304 stainless steel during ultrasonic surface rolling process. Materials Science and Engineering: A, 2016, 662:456-467.
[23] Y S Zeng. Application of shot peening technology in the development of integral panels of civil aircraft. Aeronautical Manufacturing Technology, 2008(1):54-55.
[24] E Maleki, Okan Unal, Kazem Reza Kashyzadeh, et al. A systematic study on the effects of shot peening on a mild carbon steel:Microstructure, mechanical properties, and axial fatigue strength of smooth and notched specimens. Applied Surface Science Advances, 2021, 4:100071.
[25] J Huang. Effect of low parameters ultrasound-aided deep rolling on the high cycle fatigue performance of Ti-6Al-4V alloy. Shanghai:East China University of Science And Technology, 2019. (in Chinese)
[26] T Wang, D P Wang, G Liu, et al. Investigations on the nano crystallization of 40Cr using ultrasonic surface rolling processing. Applied Surface Science, 2008, 255(5):1824-1829.
[27] Z Cai. Effect of surface ultrasonic rolling on multi-scale fatigue crack growth behavior of Ti-6Al-4V Alloy. Shanghai:East China University of Science and Technology Press, 2017. (in Chinese)
[28] M D Mao. Effect of ultrasonic rolling on high and low cycle fatigue properties of Ti-6Al-4V Alloy. Shanghai:East China University of Science and Technology Press, 2018. (in Chinese)
[29] Q Zhang, Z Hu, W Su, et al. Microstructure and surface properties of 17-4PH stainless steel by ultrasonic surface rolling technology. Surface and Coatings Technology, 2017, 321:64-73.
[30] K Dalaei, B Karlsson, L E Svensson. Stability of shot peening induced residual stresses and their influence on fatigue lifetime. Materials Science and Engineering:A, 2011, 528(3):1008-1015.
[31] H Wohlfahrt. Shot peening and residual stresses. Residual Stress and Stress Relaxation. Springer, Boston, MA, 1982:71-92.
[32] Y K Gao, X R Wu, L M Lei. Influence of laser peening and shot peening on fatigue properties of FGH97 superalloy. Rare Metal Materials and Engineering. 2016, 45(5):1230-1234.
[33] A L M Tobi, J Ding, G Bandak, et al. A study on the interaction between fretting wear and cyclic plasticity for Ti-6Al-4V. Wear, 2009, 267(1-4):270-282.
[34] X L Liu, Z Zhang, C H Tao. Fatigue fractegraphy quantitative analysis. Beijing:National Defense Industry Press, 2010. (in Chinese)
[35] Q Yang, W Zhou, Z Niu,, et al. Effect of different surface asperities and surface hardness induced by shot-peening on the fretting wear behavior of Ti-6Al-4V. Surface and Coatings Technology, 2018, 349:1098-1106.
[36] R B Waterhouse, A J Trowsdale. Residual stress and surface roughness in fretting fatigue. Journal of Physics D:Applied Physics, 1992, 25(1A):A236.
[37] Z Y Li, X L Liu, G Q Wu, et al. Observation of fretting fatigue cracks of Ti6Al4V titanium alloy. Materials Science and Engineering:A, 2017, 707:51-57.
[38] S Bagherifard, I Fernandez-Pariente, R Ghelichi, et al. Effect of severe shot peening on microstructure and fatigue strength of cast iron. International Journal of Fatigue, 2014, 65:64-70.
[39] L B Zheng. The effect of shot peening residual stress and roughness on fatigue life of 2024 aluminum alloy by simulation and experimental study. Shandong:Shandong University, 2017. (in Chinese)
[40] Charles S Montross, Tao Wei, Lin Ye, et al. Laser shock processing and its effects on microstructure and properties of metal alloys:A review. International Journal of Fatigue, 2002, 24(10):1021-1036.
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