• Laser & Optoelectronics Progress
  • Vol. 56, Issue 22, 221401 (2019)
Yang Tang1, Maozhong Ge1、*, Taiming Wang2, and Jianyun Xiang3
Author Affiliations
  • 1School of Mechanical Engineering, Jiangsu University of Technology, Changzhou, Jiangsu 213001, China
  • 2China Airlines Changzhou Lanxiang Machinery Co., Ltd., Changzhou, Jiangsu 213022, China
  • 3School of Mechanical Engineering and Technology, Changzhou Institute of Industry Technology, Changzhou, Jiangsu 213164, China
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    DOI: 10.3788/LOP56.221401 Cite this Article Set citation alerts
    Yang Tang, Maozhong Ge, Taiming Wang, Jianyun Xiang. Effect of Laser Shock Peening on Fatigue Life of GH3039 Superalloy[J]. Laser & Optoelectronics Progress, 2019, 56(22): 221401 Copy Citation Text show less
    Shape and size of fatigue specimen
    Fig. 1. Shape and size of fatigue specimen
    Fatigue sample after LSP and laser scanning direction
    Fig. 2. Fatigue sample after LSP and laser scanning direction
    Cross-sectional microstructure of original sample of GH3039 superalloy
    Fig. 3. Cross-sectional microstructure of original sample of GH3039 superalloy
    Microstructure of GH3039 superalloy after LSP. (a) Cross section; (b) local magnification in Fig. 4(a)
    Fig. 4. Microstructure of GH3039 superalloy after LSP. (a) Cross section; (b) local magnification in Fig. 4(a)
    Residual stress state at tested point for different sample surfaces. (a) Original sample; (b) sample after LSP
    Fig. 5. Residual stress state at tested point for different sample surfaces. (a) Original sample; (b) sample after LSP
    Three-dimensional topographies of different sample surfaces. (a) Original sample; (b) sample after LSP
    Fig. 6. Three-dimensional topographies of different sample surfaces. (a) Original sample; (b) sample after LSP
    Morphologies of fatigue fractures of different samples
    Fig. 7. Morphologies of fatigue fractures of different samples
    ElementCCrAlTiMoNbFeSiSMnPNi
    Mass fraction /%≤0.0819-220.35-0.750.35-0.751.8-2.30.90-1.303.00≤0.80≤0.0120.400.02Bal.
    Table 1. Chemical composition of GH3039 superalloy
    Tested point No.123456
    Original sample70.862.35.623.765.460.1
    Laser peened sample-217.1-202.4-269.7-255.3-287.5-298.4
    Table 2. Surface residual stress of original sample and sample after LSP
    No.123456
    Original sample353543429735067334573611834196
    Laser peened sample805418636983142840698502383661
    Table 3. Fatigue cycles of GH3039 superalloy before and after LSP
    Yang Tang, Maozhong Ge, Taiming Wang, Jianyun Xiang. Effect of Laser Shock Peening on Fatigue Life of GH3039 Superalloy[J]. Laser & Optoelectronics Progress, 2019, 56(22): 221401
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