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Low-cycle Fatigue Behavior of Ni-based Superalloy GH586 with Laser Shock Processing 被引量:3

Low-cycle Fatigue Behavior of Ni-based Superalloy GH586 with Laser Shock Processing
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摘要 Low-cycle fatigue behavior of Ni-based superalloy GH586 with laser shock processing(LSP) was investigated. The residual stress of the specimens treated with LSP was assessed by X-ray diffraction method. The microstructure and fracture morphology were characterized by using an optical microscope(OM), a scanning electron microscope(SEM), and a transmission electron microscope(TEM). The results indicated that the maximum residual compressive stress was at about 1 mm from the shocking spot center, where the residual compressive stress was slightly lower. High density tangling dislocations, dislocation walls, and dislocation cells in the microstructure of the specimens treated with LSP effectively prevented fatigue cracks propagation. The fatigue life was roughly twice as long as that of the specimens without LSP. The fatigue crack initiation(FCI) in specimens treated with LSP was observed in the lateral section and the subsurface simultaneously. The fatigue striation in the fracture treated with LSP was narrower than that in the untreated specimens. Moreover, dimples with tear ridges were found in the fatigued zones of the LSP treated specimens, which would be caused by severe plastic deformation. Low-cycle fatigue behavior of Ni-based superalloy GH586 with laser shock processing(LSP) was investigated. The residual stress of the specimens treated with LSP was assessed by X-ray diffraction method. The microstructure and fracture morphology were characterized by using an optical microscope(OM), a scanning electron microscope(SEM), and a transmission electron microscope(TEM). The results indicated that the maximum residual compressive stress was at about 1 mm from the shocking spot center, where the residual compressive stress was slightly lower. High density tangling dislocations, dislocation walls, and dislocation cells in the microstructure of the specimens treated with LSP effectively prevented fatigue cracks propagation. The fatigue life was roughly twice as long as that of the specimens without LSP. The fatigue crack initiation(FCI) in specimens treated with LSP was observed in the lateral section and the subsurface simultaneously. The fatigue striation in the fracture treated with LSP was narrower than that in the untreated specimens. Moreover, dimples with tear ridges were found in the fatigued zones of the LSP treated specimens, which would be caused by severe plastic deformation.
出处 《Journal of Wuhan University of Technology(Materials Science)》 SCIE EI CAS 2017年第5期1186-1192,共7页 武汉理工大学学报(材料科学英文版)
基金 Funded by the Key Program Project of National Natural Science Foundation of China(NSFC)(No.51641102) Natural Science Foundation of Jiangsu Province(No.16KJB430035) Qing Lan Project of Jiangsu Province in China National Key Laboratory of Science and Technology on Power Beam Processes of Beijing Aeronautical Manufacturing Technology Research Institute
关键词 laser shock processing Ni-based superalloy fatigue fracture microstructure laser shock processing Ni-based superalloy fatigue fracture microstructure
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