journal article·2017-10

An engineering high cycle fatigue strength prediction model for low plasticity burnished samples

Xilin Yuan, Chunyan Li

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Abstract

Abstract High cycle fatigue performance is significantly affected by the surface conditions of mechanical components. Traditionally, one major effect of low plasticity burnishing process in promotion fatigue resistance has been ascribed to the generation of compressive residual stresses and the formation of gradient structure in the top-treated surface layer. However, the prediction model of fatigue performance considering the effects of roughness, microhardness and residual stress has not been well established. Thus, the aim of this work is to develop a model predicting the fatigue strength of high cycle fatigue for burnished metallic components. First, the main parameters affecting the fatigue performance of burnished components are investigated by dimension analysis method. Then, by introducing the influence factors of stress gradient and microhardness gradient, a fatigue strength prediction model is proposed to correlate the fatigue strength of untreated and treated samples. This model considers the effects of residual stress, microhardness, roughness, gradient and size. In order to verify the validity of the model, double faces low plasticity burnishing and tension-tension fatigue tests are carried out on TA2 alloy samples with center hole. In addition, to investigate the effect of low plasticity burnishing on the fatigue performance when the direction of crack propagation is perpendicular to the burnished surface, one face burnishing and three-point bending fatigue tests are also performed. The tension-tension fatigue strength and bending fatigue strength after low plasticity burnishing are 144 MPa and 329 MPa, respectively. The predicted tension-tension fatigue strength and bending fatigue strength after low plasticity burnishing are 133 MPa and 313 MPa, respectively. The error between the measured value and the predicted value is less than 15%. At last, fatigue comparison tests using new burnishing process parameters are carried out. The fatigue strength after treatment is 309 MPa. The predicted fatigue strength after treatment is 322 MPa. The prediction error is less than 10%. This demonstrates that the proposed model is effective in the high cycle fatigue strength prediction model for low plasticity burnished samples.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Surface Treatment and Residual Stress · Erosion and Abrasive Machining · High-Velocity Impact and Material Behavior

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (37)

Show source-provided references
1. Studies on fatigue life enhancement of pre-fatigued spring steel specimens using laser shock peening10.1016/j.matdes.2013.08.104 ↗
2. An investigation into the surface characteristics of burnished cast Al-Cu alloys10.1016/S0890-6955(96)00058-2 ↗
3. Austenite-martensite phase transformation of biomedical Nitinol by ball burnishing10.1016/j.jmatprotec.2014.07.019 ↗
4. Experimental parameter sensitivity analysis of residual stresses induced by deep rolling on 7075–T6 aluminium alloy10.1016/j.surfcoat.2014.06.008 ↗
5. Finite element analysis of ball burnishing process: comparisons between numerical results and experiments10.1007/s00170-012-4599-9 ↗
6. Multipass low-plasticity burnishing induced residual stresses: three-dimensional elastic-plastic finite element modelling10.1243/095440604774202303 ↗
7. Experimental investigation of the effect of burnishing force on service properties of AISI 1010 steel plates10.1007/s11665-014-1349-1 ↗
8. On the effect of deep-rolling and laser-peening on the stress-controlled low-and high-cycle fatigue behavior of Ti-6Al-4V at elevated temperatures up to 550°C10.1016/j.ijfatigue.2012.03.008 ↗
9. Deep surface rolling for fatigue life enhancement of laser clad aircraft aluminum alloy10.1016/j.apsusc.2014.09.139 ↗
10. Grain refined and basal textured surface produced by burnishing for improved corrosion performance of AZ31B Mg alloy10.1016/j.corsci.2011.12.018 ↗
11. Fatigue behavior of a rolled AZ31 magnesium alloy after surface treatment by EP and BB conditions10.1016/j.aej.2011.01.004 ↗
12. Influence of low-plasticity ball burnishing on the high-cycle fatigue strength of medium carbon AISI 1045 steel10.1016/j.ijfatigue.2013.06.024 ↗
13. Effect of size and stress gradient on fatigue behaviour10.1016/0308-0161(94)90024-8 ↗
14. Estimation of the fatigue strength distribution in high-cycle multiaxial fatigue taking into account the stress-strain gradient effect10.1016/j.ijfatigue.2005.06.048 ↗
15. Advanced volumetric method for fatigue life prediction using stress gradient effects at notch roots10.1016/j.commatsci.2006.08.017 ↗
16. Study of component structural equivalent fatigue based on a combined stress gradient approach and the theory of critical distance10.1016/j.engfailanal.2015.11.053 ↗
17. Predicting the effects of material properties gradient and residual stresses on the bending fatigue strength of induction hardened aeronautical gears10.1016/j.ijfatigue.2015.12.004 ↗
18. The description for fatigue behaviors of metals by stress field intensity approach
19. General relationship between strength and hardness10.1016/j.msea.2011.08.061 ↗
20. Hardness-strength relationships in the aluminum alloy 701010.1016/j.msea.2015.02.049 ↗
21. Hardness− strength relationships in fine and ultra-fine grained metals processed through constrained groove pressing10.1016/j.msea.2015.03.122 ↗
22. Some contributions on the effect of residual stress on fatigue behavior
23. A life prediction method for size effects on notched fatigue
24. Estimating the fatigue stress concentration factor of machined surfaces10.1016/S0142-1123(02)00012-9 ↗
25. Giga-fatigue life prediction of FV520B-I with surface roughness10.1016/j.matdes.2015.10.104 ↗
26. Application of different fatigue strength criteria to shot peened notched components. Part 1: fracture mechanics based approaches10.1016/j.apsusc.2013.10.131 ↗
27. Another mechanism for fatigue strength improvement of metallic parts by shot peening10.1361/105994903100277148 ↗
28. Meso-scopical effects during fatigue crack initiation
29. Effect of roller burnishing process parameters on the surface roughness and microhardness for TA2 alloy10.1007/s00170-015-8031-0 ↗
30. Influence of ball burnishing on residual stress profile of a 15–5PH stainless steel10.1016/j.cirpj.2015.12.003 ↗
31. Effect of burnishing parameters on surface roughness and hardness10.3139/120.110963 ↗
32. Experimental investigation into the effect of low plasticity burnishing parameters on the surface integrity of TA2
33. Finite element analysis and design optimization of low plasticity burnishing process10.1007/s00170-013-5406-y ↗
34. Effects on structure and mechanical properties of TC11 titanium alloy by laser shock peening
35. Influence of surface integrity on the fatigue behaviour of a hot-forged and shot-peened C70 steel component10.1016/j.msea.2017.01.041 ↗
36. Surface modifications induced by shot peening and their effect on the plane bending fatigue strength of a Cr-Mo steel produced by powder metallurgy10.1016/j.msea.2010.12.072 ↗
37. Influence of different surface modification treatments on surface integrity and fatigue performance of TC4 titanium alloy