scispace - formally typeset
Search or ask a question
Topic

Shot peening

About: Shot peening is a research topic. Over the lifetime, 5548 publications have been published within this topic receiving 71101 citations.


Papers
More filters
Journal ArticleDOI
TL;DR: In this paper, the effect of DR on the low-cycle fatigue (LCF) and high cycle fatigue (HCF) behavior of a Ti-6Al-4V alloy is examined, with particular emphasis on the thermal and mechanical stability of the residual stress states and the near-surface microstructures.
Abstract: It is well known that mechanical surface treatments, such as deep rolling, shot peening and laser shock peening, can significantly improve the fatigue behavior of highly-stressed metallic components. Deep rolling (DR) is particularly attractive since it is possible to generate, near the surface, deep compressive residual stresses and work hardened layers while retaining a relatively smooth surface finish. In the present investigation, the effect of DR on the low-cycle fatigue (LCF) and high-cycle fatigue (HCF) behavior of a Ti–6Al–4V alloy is examined, with particular emphasis on the thermal and mechanical stability of the residual stress states and the near-surface microstructures. Preliminary results on laser shock peened Ti–6Al–4V are also presented for comparison. Particular emphasis is devoted to the question of whether such surface treatments are effective for improving the fatigue properties at elevated temperatures up to ∼450 °C, i.e. at a homologous temperature of ∼0.4 T/T m (where T m is the melting temperature). Based on cyclic deformation and stress/life ( S / N ) fatigue behavior, together with the X-ray diffraction and in situ transmission electron microscopy (TEM) observations of the microstructure, it was found that deep rolling can be quite effective in retarding the initiation and initial propagation of fatigue cracks in Ti–6Al–4V at such higher temperatures, despite the almost complete relaxation of the near-surface residual stresses. In the absence of such stresses, it is shown that the near-surface microstructures, which in Ti–6Al–4V consist of a layer of work hardened nanoscale grains, play a critical role in the enhancement of fatigue life by mechanical surface treatment.

466 citations

Journal ArticleDOI
TL;DR: In this paper, the authors investigated the UFG microstructures in the surface layer of an aluminum alloy 7075 heavily worked by ultrasonic shot peening and found that the grain subdivision into the subgrains was the main mechanism responsible for grain refinement.

418 citations

Journal ArticleDOI
TL;DR: In this paper, a non-destructive method for measuring residual stresses in structural engineering components is described. But the method is not suitable for the analysis of the residual stress distributions introduced by welding and the beneficial stresses produced by autofrettage, cold hole expansion and shot peening.

385 citations

Journal ArticleDOI
TL;DR: In this article, an ultrasonic shot peening (USSP) technique was used to construct a nanocrystalline surface layer on a pure Fe plate by using an X-ray diffraction (XRD) and transmission electron microscope (TEM).

374 citations

Journal ArticleDOI
TL;DR: In this article, the effect of machining surface roughness on fatigue performance was investigated for a variety of workpiece materials and post-machining surface treatments, such as shot peening.
Abstract: The paper reviews published data which address the effect of machining (conventional and non-conventional processes) and the resulting workpiece surface topography/integrity on fatigue performance, for a variety of workpiece materials. The effect of post-machining surface treatments, such as shot peening, are also detailed. The influence of amplitude height parameters (Ra, Rt), amplitude distribution (Rsk) and shape (Rku) parameters, as well as spatial (Std, Sal) and hybrid (Ssc) measures, are considered. There is some disagreement in the literature about the correlation between workpiece surface roughness and fatigue life. In most cases, it has been reported that lower roughness results in longer fatigue life, but that for roughness values in the range 2.5–5 μm Ra it is primarily dependent on workpiece residual stress and surface microstructure, rather than roughness. In the absence of residual stress, machined surface roughness in excess of 0.1 μm Ra has a strong influence on fatigue life. Temperatures above 400 °C reduce the effects of both residual stress and surface roughness on fatigue, due to stress relieving and the change in crack initiation from the surfaces to internal sites. The presence of inclusions an order of magnitude larger than the machined surface roughness generally overrides the effect of surface topography.

371 citations


Network Information
Related Topics (5)
Alloy
171.8K papers, 1.7M citations
86% related
Microstructure
148.6K papers, 2.2M citations
84% related
Fracture mechanics
58.3K papers, 1.3M citations
83% related
Coating
379.8K papers, 3.1M citations
82% related
Ultimate tensile strength
129.2K papers, 2.1M citations
81% related
Performance
Metrics
No. of papers in the topic in previous years
YearPapers
2023169
2022379
2021208
2020224
2019232
2018241