Chinese Journal of Lasers, Volume. 48, Issue 22, 2202009(2021)

Low Cycle Fatigue Behavior of GH3536 Alloy Formed via Laser Additive Manufacturing

Lairong Xiao1, Wei Tan1, Liming Liu2, Xiaoxuan Tu1, Zhenwu Peng1, Huan Wang2, and Xiaojun Zhao1、*
Author Affiliations
  • 1School of Materials Science and Engineering, Central South University, Changsha, Hunan 410083, China
  • 2Beijing Power Machinery Research Institute, Beijing 100074, China
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    Figures & Tables(13)
    GH3536 alloy powder. (a) Powder morphology; (b) size distribution
    Shape and dimension of low cycle fatigue specimen (unit: mm)
    Cyclic stress response curves of GH3536 alloy formed by selective laser melting (SLM) at different strain amplitudes. (a) Room temperature (RT); (b) 800 ℃
    Hysteresis loops at half-life of GH3536 alloy formed by SLM at different strain amplitudes. (a) Room temperature; (b) 800 ℃
    Cyclic stress-strain relationship of GH3536 alloy formed by SLM at room temperature and 800 ℃
    Strain-life curves of GH3536 alloy formed by SLM. (a) Room temperature; (b) 800 ℃
    Low cycle fatigue fracture morphologies of GH3536 alloy formed by SLM tested at room temperature. (a) Macro-fracture at 0.4% strain amplitude; (b) amplified view of crack initiation site at 0.4% strain amplitude; (c) fatigue striations at 0.4% strain amplitude; (d) macro-fracture at 1.2% strain amplitude; (e) amplified view of crack initiation site at 1.2% strain amplitude; (f) fatigue striations at 1.2% strain amplitude
    Low cycle fatigue fracture morphologies of GH3536 alloy formed by SLM tested at 800 ℃. (a) Macro-fracture at 0.4% strain amplitude; (b) amplified view of crack initiation site at 0.4% strain amplitude; (c) fatigue striations at 0.4% strain amplitude; (d) macro-fracture at 1.2% strain amplitude; (e) amplified view of crack initiation site at 1.2% strain amplitude; (f) fatigue striations at 1.2% strain amplitude
    Microstructures of GH3536 alloy formed by SLM after low cycle fatigue fracture at room temperature. (a) 0.4% strain amplitude; (b) 0.4% strain amplitude; (c) 0.8% strain amplitude; (d) 1.2% strain amplitude
    Microstructures of GH3536 alloy formed by SLM after low cycle fatigue fracture at 800 ℃. (a) 0.25% strain amplitude; (b) 0.4% strain amplitude; (c) 0.8% strain amplitude; (d) 1.2% strain amplitude
    Plastic strain energy life prediction model and prediction results. (a) Relationship between plastic strain energy at half-life and cyclic number to failure; (b) the results of fatigue life prediction
    • Table 1. Main chemical composition of GH3536 alloy powder

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      Table 1. Main chemical composition of GH3536 alloy powder

      ElementCrFeMoCoSiWAlMnCNi
      Mass fraction/%21.5318.749.101.720.610.530.300.0250.062Bal.
    • Table 2. Low cycle fatigue parameters of GH3536 alloy formed by SLM at room temperature and 800 ℃

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      Table 2. Low cycle fatigue parameters of GH3536 alloy formed by SLM at room temperature and 800 ℃

      Temperature /℃σ'f /MPabε'fcE /GPa
      RT1369.12-0.09950.1115-0.3748199
      800797.50-0.16800.5859-0.7352110
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    Lairong Xiao, Wei Tan, Liming Liu, Xiaoxuan Tu, Zhenwu Peng, Huan Wang, Xiaojun Zhao. Low Cycle Fatigue Behavior of GH3536 Alloy Formed via Laser Additive Manufacturing[J]. Chinese Journal of Lasers, 2021, 48(22): 2202009

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    Paper Information

    Category: laser manufacturing

    Received: May. 6, 2021

    Accepted: Jun. 2, 2021

    Published Online: Nov. 2, 2021

    The Author Email: Zhao Xiaojun (zhaoxj@csu.edu.cn)

    DOI:10.3788/CJL202148.2202009

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