Effect of initial surface treatment on shot peening residual stress field: Analytical approach with experimental verification

2018 ◽  
Vol 137 ◽  
pp. 171-181 ◽  
Author(s):  
Khalil Sherafatnia ◽  
Gholam Hossein Farrahi ◽  
Amir Hossein Mahmoudi
Keyword(s):  
Residual Stress ◽  
Stress Field ◽  
Surface Treatment ◽  
Experimental Verification ◽  
Shot Peening ◽  
Analytical Approach ◽  
Initial Surface ◽  
Residual Stress Field

3D Computational Simulation of Multi-Impact Shot Peening

2012 ◽  
Vol 1485 ◽  
pp. 35-40
Author(s):  
Juan Solórzano-López ◽  
Francisco Alfredo García-Pastor
Keyword(s):  
Residual Stress ◽  
Fatigue Life ◽  
Stress Field ◽  
Surface Treatment ◽  
Shot Peening ◽  
Compressive Residual Stress ◽  
Fatigue Testing ◽  
Computational Simulation ◽  
Target Material ◽  
Residual Stress Field

ABSTRACTShot peening is a widely applied surface treatment in a number of manufacturing processes in several industries including automotive, mechanical and aeronautical. This surface treatment is used with the aim of increasing surface toughness and extending fatigue life. The increased performance during fatigue testing of the peened components is mainly the result of the sub-surface compressive residual stress field resulting from the plastic deformation of the surface layers of the target material, caused by the high-velocity impact of the shot. This compressive residual stress field hinders the propagation and coalescence of cracks during the second stage of fatigue testing, effectively increasing the fatigue life well beyond the expected life of a non-peened component.This paper describes a 3D computational model of spherical projectiles impacting simultaneously upon a flat surface. The multi-impact model was developed in ABAQUS/Explicit using finite element method (FEM) and taking into account controlling parameters such as the velocity of the projectiles, their incidence angle and different impact locations in the target surface. Additionally, a parametric study of the physical properties of the target material was carried out in order to assess the effect of temperature on the residual stress field.The simulation has been able to successfully represent a multi-impact processing scenario, showing the indentation caused by each individual shot, as well as the residual stress field for each impact and the interaction between each one of them. It has been found that there is a beneficial effect on the residual stress field magnitude when shot peening is carried out at a relatively high temperature. The results are discussed in terms of the current shot-peening practice in the local industry and the leading edge developments of new peening technologies. Finally, an improved and affordable processing route to increase the fatigue life of automotive components is suggested.

Assessment of the Crack Compliance Method and the Introduction of Residual Stresses by Shot Peening Using the Finite Element Method

2009 ◽  
Vol 15 ◽  
pp. 109-114 ◽  
Author(s):  
G. Urriolagoitia-Sosa ◽  
E. Zaldivar-González ◽  
J.M. Sandoval Pineda ◽  
J. García-Lira
Keyword(s):  
Numerical Simulation ◽  
Residual Stress ◽  
Stress Field ◽  
Residual Stresses ◽  
Shot Peening ◽  
Working Life ◽  
The Finite Element Method ◽  
Residual Stress Field ◽  
Main Effect

The interest on the application of the shot peening process to arrest and/or delay crack growth is rising. The main effect of the shot peening technique is to introduce a residual stress field that increases the working life of mechanical components. In this paper, it is presented the numerical simulation (FEM) of the shot peening process and the effect of introducing a residual stress field. Besides, the consequence of changing the sizes of the impacting ball is analyzed. This work also used the Crack Compliance Method (CCM) for the determination of residual stresses in beams subjected to a numerical simulation of a shot peening process. The numerical results obtained provide a quantitative demonstration of the effect of shot peening on the introduction of residual stresses by using different sizes of impacting balls and assess the efficiency of the CCM.

Kugelstrahlsimulation mit neuartiger Elementarzelle – Bauteilauslegung bis Strahlparameter/Shot Peening Simulation with a Novel Unit Cell – Component Design to Peening Parameters – Part 1: Simulation Model and Residual Stress Field

Konstruktion ◽  
2019 ◽  
Vol 71 (07-08) ◽  
pp. 82-89
Author(s):  
Christoph Hermann Richter ◽  
Patrick Gerken ◽  
Michaela Zeißig ◽  
Gerd Telljohann
Keyword(s):  
Residual Stress ◽  
Stress Field ◽  
Simulation Model ◽  
Shot Peening ◽  
Unit Cell ◽  
Wird Eine ◽  
Residual Stress Field ◽  
Cell Component ◽  
Component Design

Inhalt: In diversen Branchen des Maschinenbaus wird Kugelstrahlen zur Steigerung der Bauteilfestigkeit eingesetzt. Die Auslegung der Verfestigung wird heute oft mit iterativen Versuchen vorgenommen. Im hier vorliegenden ersten Teil der Veröffentlichung, „Simulationsmodell und Eigenspannungsfeld“, wird eine wirtschaftliche Simulation auf Basis einer neuartigen Zellperiodizität vorgestellt. Diese erlaubt prozessrelevante Parameter vorherzusagen und resultierend auf die Eigenspannungsmessung zu verzichten. Ferner wird die in der Literatur nur selten behandelte Inhomogenität des Eigenspannungsfeldes näher untersucht. Im zweiten Teil der Veröffentlichung, „Anwendungen“, dienen im Schrifttum verfügbare Messdaten zu Almen-Proben der Validierung. Darüber hinaus wird der Nutzen des Kugelstrahlens am Beispiel der schwer zu beherrschenden Reibermüdung mit einer integrativen Simulation beleuchtet.

Residual Stress Field of a Single Edge Notch Specimen after Laser Shock Peening and Shot Peening Treatment

2018 ◽  
Vol 7 (4) ◽  
pp. 20170133
Author(s):  
Stefano Coratella ◽  
T. J. Spradlin ◽  
Kristina Langer ◽  
Michael A. Gharghouri ◽  
U. C. Heckenberger ◽  
...  
Keyword(s):  
Residual Stress ◽  
Stress Field ◽  
Shot Peening ◽  
Laser Shock Peening ◽  
Laser Shock ◽  
Single Edge ◽  
Residual Stress Field ◽  
Single Edge Notch ◽  
Edge Notch ◽  
Shock Peening

Investigation on shot-peening induced residual stress field

2010 ◽  
Vol 5 (4/5) ◽  
pp. 471 ◽  
Author(s):  
Georgios I. Mylonas ◽  
Ulrike Heckenberger ◽  
Georgios N. Lampeas
Keyword(s):  
Residual Stress ◽  
Stress Field ◽  
Shot Peening ◽  
Residual Stress Field

scholarly journals Effect of stress shot peening on the residual stress field and microstructure of nanostructured Mg-8Gd-3Y alloy

2021 ◽  
Vol 10 ◽  
pp. 74-83
Author(s):  
Huabing Liu ◽  
Xiaoxiao Wei ◽  
Shilong Xing ◽  
Lianbo Wang ◽  
Wenlong Zhu ◽  
...  
Keyword(s):  
Residual Stress ◽  
Stress Field ◽  
Shot Peening ◽  
Residual Stress Field

scholarly journals Small–Scale Experimental Investigation of Fatigue Performance Improvement of Ship Hatch Corner with Shot Peening Treatments by Considering Residual Stress Relaxation

2021 ◽  
Vol 9 (4) ◽  
pp. 419
Author(s):  
Jin Gan ◽  
Zi’ang Gao ◽  
Yiwen Wang ◽  
Zhou Wang ◽  
Weiguo Wu
Keyword(s):  
Residual Stress ◽  
Surface Roughness ◽  
Fatigue Life ◽  
Stress Relaxation ◽  
Stress Field ◽  
Shot Peening ◽  
Compressive Residual Stress ◽  
Fatigue Performance ◽  
Residual Stress Field ◽  
Residual Stress Relaxation

Ship hatch corner is a common structure in a ship and its fatigue problem has always been one of the focuses in ship engineering due to the long–term high–stress concentration state during the ship’s life. For investigating the fatigue life improvement of the ship hatch corner under different shot peening (SP) treatments, a series of fatigue tests, residual stress and surface topography measurements were conducted for SP specimens. Furthermore, the distributions of the surface residual stress are measured with varying numbers of cyclic loads, investigating the residual stress relaxation during cyclic loading. The results show that no matter which SP process parameters are used, the fatigue lives of the shot–peened ship hatch corner specimens are longer than those at unpeened specimens. The relaxation rate of the residual stress mainly depends on the maximum compressive residual stress (σRSmax) and the depth of the maximum compressive residual stress (δmax). The larger the values of σRSmax and δmax, the slower the relaxation rates of the residual stress field. The results imply that the effect of residual stress field and surface roughness should be considered comprehensively to improve the fatigue life of the ship hatch corner with SP treatment. The increase in peening intensity (PI) within a certain range can increase the depth of the compressive residual stress field (CRSF), so the fatigue performance of the ship hatch corner is improved. Once the PI exceeds a certain value, the surface damage caused by the increase in surface roughness will not be offset by the CRSF and the fatigue life cannot be improved optimally. This research provides an approach of fatigue performance enhancement for ship hatch corners in engineering application.

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