Improving Fatigue Properties of 316L Stainless Steel Welded Joints by Surface Spinning Strengthening

被引:0
|
作者
Wang, Dongqiqiong [1 ,2 ,3 ]
Wang, Qiang [4 ]
Li, Xiaowu [1 ,2 ]
Zhang, Zhefeng [1 ,2 ,3 ]
机构
[1] Northeastern Univ, Sch Mat Sci & Engn, Dept Mat Phys & Chem, Shenyang 110819, Peoples R China
[2] Northeastern Univ, Key Lab Anisotropy & Texture Mat, Minist Educ, Shenyang 110819, Peoples R China
[3] Chinese Acad Sci, Inst Met Res, Shi Changxu Innovat Ctr Adv Mat, Shenyang 110016, Peoples R China
[4] Liaoning Univ, Coll Light Ind, Shenyang 110036, Peoples R China
基金
中国国家自然科学基金;
关键词
316L stainless steel; Welded joint; Surface spinning strengthening; Nanotwin; Fatigue life; LOW-CYCLE FATIGUE; 50CRMNMOVNB SPRING STEEL; TUNGSTEN INERT-GAS; MICROSTRUCTURAL EVOLUTION; MAXIMUM MICROHARDNESS; MECHANICAL-PROPERTIES; GRADIENT LAYER; GRAIN-SIZE; BEHAVIOR; LASER;
D O I
10.1007/s40195-024-01668-2
中图分类号
TF [冶金工业];
学科分类号
0806 ;
摘要
The surface spinning strengthening (3S) mechanism and fatigue life extension mechanism of 316L stainless steel welded joint were systematically elucidated by microstructural analyses and mechanical tests. Results indicate that surface gradient hardening layer of approximately 1 mm is formed in the base material through grain fragmentation and deformation twin strengthening, as well as in the welding zone composed of deformed delta-phases and nanotwins. The fatigue strength of welded joint after 3S significantly rises by 32% (from 190 to 250 MPa), which is attributed to the effective elimination of surface geometric defects, discrete refinement of delta-Fe phases and the appropriate improvement in the surface strength, collectively mitigating strain localization and surface fatigue damage within the gradient strengthening layer. The redistributed fine delta-Fe phases benefited by strong stress transfer of 3S reduce the risk of surface weak phase cracking, causing the fatigue fracture to transition from microstructure defects to crystal defects dominated by slip, further suppressing the initiation and early propagation of fatigue cracks.
引用
收藏
页码:840 / 854
页数:15
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