journal article·2018-05

Surface characteristics and fatigue behavior of shot peened Inconel 718

T. Klotz, D. Delbergue, P. Bocher, M. Lévesque, M. Brochu

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Abstract

Abstract Shot peening is commonly used in the aerospace industry to improve mechanical components fatigue life. It introduces compressive residual stresses and cold work at the surface which tend to close short fatigue cracks and delay their propagation, respectively. However, shot peening also creates surface irregularities that can be detrimental to fatigue. The effect of different shot peening conditions on Inconel 718 tested in low and high cycle fatigue is presented in this study. An analysis of the fatigue life, crack initiation mechanisms, residual stress relaxation, process induced strain hardening and surface roughness showed that, in high cycle fatigue, shot peening can increase Inconel 718 fatigue life from 2 to 20 times, depending on the shot peening conditions. This observation suggests that careful selection of peening parameters is crucial. In low cycle fatigue the roughness resulting from shot peening is to be considered while in high cycle fatigue, it is the presence of significant residual stresses.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Surface Treatment and Residual Stress · Erosion and Abrasive Machining · Energetic Materials and Combustion

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

References (35)

Show source-provided references
1. Fatigue crack initiation and propagation on shot-peened surfaces in A316 stainless steel10.1016/0142-1123(95)00044-T ↗
2. An analysis of stress concentrations caused by shot peening and its application in predicting fatigue strength10.1111/j.1460-2695.1992.tb01262.x ↗
3. The effect of machined topography and integrity on fatigue life10.1016/j.ijmachtools.2003.10.018 ↗
4. Mechanical surface treatments on titanium, aluminum and magnesium alloys10.1016/S0921-5093(98)01168-X ↗
5. Prevéy P. The effect of cold work on the thermal stability of residual compression in surface enhanced IN718. Tech Rep, DTIC Document; 2000.
6. Nakamura H, Takanashi M, Itabashi Y, Kuroki H, Ueda Y. Shot peening effect on low cycle fatigue properties of Ti-6Al-4V and Inconel 718. In: ASME 2011 Turbo Expo: turbine technical conference and exposition, American Society of Mechanical Engineers; 2011. p. 791–7.10.1115/GT2011-46847 ↗
7. Cammett JT, Prevéy PS, Jayaraman N. The effect of shot peening coverage on residual stress, cold work, and fatigue in a nickel-base superalloy. Tech Rep, DTIC Document; 2005.
8. The influence of microstructure and operating temperature on the fatigue endurance of hot forged Inconel® 718 components10.1016/j.msea.2013.07.053 ↗
9. High-cycle fatigue properties at cryogenic temperatures in INCONEL 718 nickel-based superalloy10.2320/matertrans.45.342 ↗
10. Modelling the optimum grain size on the low cycle fatigue life of a Ni based superalloy in the presence of two possible crack initiation sites10.1016/j.scriptamat.2003.09.043 ↗
11. An investigation of surface damage in the high speed turning of Inconel 718 with use of whisker reinforced ceramic tools10.1016/j.jmatprotec.2011.09.022 ↗
12. Low cycle fatigue behavior of Inconel 718 at 298 K and 823 K10.1007/BF02667395 ↗
13. 1D cyclic yield model independent of load spectrum characteristics and its application to Inconel 71810.1016/j.mechmat.2017.03.011 ↗
14. Crystallographic fatigue crack initiation in nickel-based superalloy rené 88DT at elevated temperature10.1016/j.actamat.2009.08.022 ↗
15. High resolution mapping of strain localization near twin boundaries in a nickel-based superalloy10.1016/j.actamat.2015.07.016 ↗
16. Microstructural extremes and the transition from fatigue crack initiation to small crack growth in a polycrystalline nickel-base superalloy10.1016/j.actamat.2012.01.049 ↗
17. A combined grain scale elastic–plastic criterion for identification of fatigue crack initiation sites in a twin containing polycrystalline nickel-base superalloy10.1016/j.actamat.2015.09.050 ↗
18. ASTM Standard E8M-13a. Standard test methods for tension testing of metallic materials; 2013.
19. SAE AMS5663M. Nickel alloy, corrosion and heat-resistant, bars, forgings, and rings 52.5Ni–19Cr–3.0Mo–5.1Cb (Nb)–0.90Ti–0.5Al–18Fe consumable electrode or vacuum induction melted 1775 °F (968 °C) solution and precipitation heat treated; 2009.
20. Cyclic deformation mechanisms of precipitation-hardened Inconel 718 superalloy10.1016/j.msea.2006.10.181 ↗
21. ASTM Standard E466-07. Standard practice for conducting force controlled constant amplitude axial fatigue tests of metallic materials; 2007.
22. SAE AMS2430T. Shot peening, automatic; 2015.
23. ASTM Standard E384-11. Standard test method for Knoop and vickers hardness of materials; 2011.
24. Noyan · 2013
25. Influence of image processing conditions of debye Scherrer ring images in x-ray stress measurement using an imaging plate
26. Comparison of two X-ray residual stress measurement methods: Sin2 ψ and cos α, through the determination of a martensitic steel X-ray elastic constant
27. Moore MG, Evans WP. Mathematical correction for stress in removed layers in X-ray diffraction residual stress analysis. Tech Rep, SAE technical paper; 1958.10.4271/580035 ↗
28. Warren B. X-ray diffraction; courier corporation: 1969.
29. The measurement of subsurface residual stress and cold work distributions in nickel base alloys
30. An analysis of residual stress fields caused by shot peening10.1007/s11661-002-0186-2 ↗
31. Bianchetti C, Lévesque M, Brochu M. Probabilistic analysis of the effect of shot peening on the high and low cycle fatigue behaviors of AA 7050-T7451. Sub Int J Fatigue. November 2017.10.1016/j.ijfatigue.2018.02.029 ↗
32. Abramovich · 2013
33. Depth profiles of macro residual stresses in thin shot peened steel plates determined by X-ray and neutron diffraction10.1016/S1359-6462(01)01063-6 ↗
34. Effects of plastic straining on residual stresses induced by shot-peening.(retroactive coverage)
35. Materials science perspective of metal fatigue resistance10.1179/mst.1993.9.6.453 ↗