Surface Integrity of TA19 Notched Simulated Blades with Laser Shock Peening and Its Effect on Fatigue Strength

被引:19
作者
Wu, Junfeng [1 ]
Che, Zhigang [1 ]
Zou, Shikun [1 ]
Cao, Ziwen [1 ]
Sun, Rujian [1 ]
机构
[1] AVIC Mfg Technol Inst, Sci & Technol Power Beam Proc Lab, Beijing 100024, Peoples R China
基金
中国国家自然科学基金;
关键词
compressive residual stresses; fatigue strengthening mechanism; laser shock peening (LSP); refined grains; TA19 notched simulated blades; FOREIGN OBJECT DAMAGE; CRACK GROWTH; TITANIUM-ALLOY; MICROSTRUCTURAL RESPONSE; GRAIN-REFINEMENT; RESIDUAL-STRESS; TI-6AL-4V ALLOY; ALUMINUM-ALLOY; LIFE; EVOLUTION;
D O I
10.1007/s11665-020-05025-z
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
To reveal the fatigue strengthening mechanism of TA19 notched simulated blades with laser shock peening (LSP), surface integrity and fatigue strength were investigated. The surface morphology, residual stress, near-surface microstructure, fatigue strength and fatigue fracture morphology were analyzed by surface profiler, x-ray diffraction (XRD), transmission electron microscopy (TEM), QRG-100 servo-hydraulic fatigue test machine and scanning electron microscope (SEM). Results indicated that LSP induced surface micro-dents plastic deformations with a few microns in depth, surface compressive residual stresses and surface nano-grains of TA19 notched simulated blades. Compared with the as-received material, fatigue strengths of TA19 notched simulated blades were improved by 162% for LSP-1 and 218% for LSP-3. In addition, fatigue crack initiation (FCI) locations reduced after LSP, fatigue crack growth (FCG) rate decreased after LSP, and secondary cracks were observed in the FCI and FCG regions of fatigue fracture morphologies after LSP. Fatigue strengthening mechanism of TA19 notched simulated blades with LSP was compressive residual stresses and refined grains. Results could be beneficial to the application of LSP process in civil engines blades.
引用
收藏
页码:5184 / 5194
页数:11
相关论文
共 38 条
[1]  
[Anonymous], 2012, MAT SCI ENG A
[2]   The role of microtexture on the faceted fracture morphology in Ti-6Al-4V subjected to high-cycle fatigue [J].
Bantounas, Ioannis ;
Dye, David ;
Lindley, Trevor C. .
ACTA MATERIALIA, 2010, 58 (11) :3908-3918
[3]   An overview on the use of titanium in the aerospace industry [J].
Boyer, RR .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 1996, 213 (1-2) :103-114
[4]   Investigation of Surface Integrity on TC17 Titanium Alloy Treated by Square-spot Laser Shock Peening [J].
Cao Ziwen ;
Xu Haiying ;
Zou Shikun ;
Che Zhigang .
CHINESE JOURNAL OF AERONAUTICS, 2012, 25 (04) :650-656
[5]   Fatigue crack growth from foreign object damage under combined low and high cycle loading. Part 1: Experimental studies [J].
Ding, J. ;
Hall, R. F. ;
Byrne, J. ;
Tong, J. .
INTERNATIONAL JOURNAL OF FATIGUE, 2007, 29 (07) :1339-1349
[6]   Effect of laser shock peening on residual stress and fatigue life of clad 2024 aluminium sheet containing scribe defects [J].
Dorman, M. ;
Toparli, M. B. ;
Smyth, N. ;
Cini, A. ;
Fitzpatrick, M. E. ;
Irving, P. E. .
MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2012, 548 :142-151
[7]   NUMERICAL ANALYSIS OF CRACK PROPAGATION IN CYCLIC-LOADED STRUCTURES [J].
FORMAN, RG ;
KEARNEY, VE ;
ENGLE, RM .
JOURNAL OF BASIC ENGINEERING, 1967, 89 (03) :459-&
[8]   Studies on fatigue life enhancement of pre-fatigued spring steel specimens using laser shock peening [J].
Ganesh, P. ;
Sundar, R. ;
Kumar, H. ;
Kaul, R. ;
Ranganathan, K. ;
Hedaoo, P. ;
Raghavendra, G. ;
Kumar, S. Anand ;
Tiwari, P. ;
Nagpure, D. C. ;
Bindra, K. S. ;
Kukreja, L. M. ;
Oak, S. M. .
MATERIALS & DESIGN, 2014, 54 :734-741
[9]   Influence of foreign object damage on fatigue crack growth of gas turbine aerofoils under complex loading conditions [J].
Hall, R. ;
Byrne, J. ;
Zhao, T. ;
Tong, J. .
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2008, 31 (05) :386-397
[10]   Laser peen forming induced two way bending of thin sheet metals and its mechanisms [J].
Hu, Yongxiang ;
Xu, Xiaoxia ;
Yao, Zhenqiang ;
Hu, Jun .
JOURNAL OF APPLIED PHYSICS, 2010, 108 (07)