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Fatigue Limit of Custom 465 with Surface Strengthening Treatment

In order to study the effect of nitriding or shot peening on the surface modification and fatigue properties of martensitic stainless-steel Custom 465, the residual stress and micro-hardness of the strengthened layer are determined by X-ray and micro-hardness tester, respectively. The up-and-down me...

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Autores principales: An, Gang, Liu, Ren-jing, Yin, Guang-qiang
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2020
Materias:
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6981755/
https://www.ncbi.nlm.nih.gov/pubmed/31935829
http://dx.doi.org/10.3390/ma13010238
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author An, Gang
Liu, Ren-jing
Yin, Guang-qiang
author_facet An, Gang
Liu, Ren-jing
Yin, Guang-qiang
author_sort An, Gang
collection PubMed
description In order to study the effect of nitriding or shot peening on the surface modification and fatigue properties of martensitic stainless-steel Custom 465, the residual stress and micro-hardness of the strengthened layer are determined by X-ray and micro-hardness tester, respectively. The up-and-down method is used to measure the rotational bending fatigue strength at 1 × 10(7) cycles, and the fatigue fracture characteristic is observed by scanning electron microscopy. The relationship between surface residual stress and internal fatigue limit of surface strengthening treatment is discussed. Results show that nitriding or shot peening surface strengthening layer forms a certain depth of compressive residual stress, where in the surface compressive residual stress of the nitrided specimens is greater than the shot peened specimens. The micro-hardness of the nitrided or shot peened surface strengthening layer is significantly improved, where in the surface micro-hardness of nitriding specimens are higher than shot peening specimens. The nitriding or shot peening surface strengthening can significantly improve the fatigue limit of Custom 465, wherein the fatigue limits of nitrided and shot peened surface strengthened specimens are 50.09% and 50.66% higher than that of the un-surface strengthened specimens, respectively. That is, the effect of the two strengthening methods on fatigue limit is not very different. The fracture characteristics show that the fatigue crack of the un-surface strengthened specimens originates from the surface, while the fatigue crack of surface strengthened specimens originates from the subsurface layer under the strengthened layer. The relationship between the internal fatigue limit and the surface residual stress of the surface strengthened specimen can be used as a method for predicting the fatigue limit of the surface strengthened specimens.
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spelling pubmed-69817552020-02-07 Fatigue Limit of Custom 465 with Surface Strengthening Treatment An, Gang Liu, Ren-jing Yin, Guang-qiang Materials (Basel) Article In order to study the effect of nitriding or shot peening on the surface modification and fatigue properties of martensitic stainless-steel Custom 465, the residual stress and micro-hardness of the strengthened layer are determined by X-ray and micro-hardness tester, respectively. The up-and-down method is used to measure the rotational bending fatigue strength at 1 × 10(7) cycles, and the fatigue fracture characteristic is observed by scanning electron microscopy. The relationship between surface residual stress and internal fatigue limit of surface strengthening treatment is discussed. Results show that nitriding or shot peening surface strengthening layer forms a certain depth of compressive residual stress, where in the surface compressive residual stress of the nitrided specimens is greater than the shot peened specimens. The micro-hardness of the nitrided or shot peened surface strengthening layer is significantly improved, where in the surface micro-hardness of nitriding specimens are higher than shot peening specimens. The nitriding or shot peening surface strengthening can significantly improve the fatigue limit of Custom 465, wherein the fatigue limits of nitrided and shot peened surface strengthened specimens are 50.09% and 50.66% higher than that of the un-surface strengthened specimens, respectively. That is, the effect of the two strengthening methods on fatigue limit is not very different. The fracture characteristics show that the fatigue crack of the un-surface strengthened specimens originates from the surface, while the fatigue crack of surface strengthened specimens originates from the subsurface layer under the strengthened layer. The relationship between the internal fatigue limit and the surface residual stress of the surface strengthened specimen can be used as a method for predicting the fatigue limit of the surface strengthened specimens. MDPI 2020-01-06 /pmc/articles/PMC6981755/ /pubmed/31935829 http://dx.doi.org/10.3390/ma13010238 Text en © 2020 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).
spellingShingle Article
An, Gang
Liu, Ren-jing
Yin, Guang-qiang
Fatigue Limit of Custom 465 with Surface Strengthening Treatment
title Fatigue Limit of Custom 465 with Surface Strengthening Treatment
title_full Fatigue Limit of Custom 465 with Surface Strengthening Treatment
title_fullStr Fatigue Limit of Custom 465 with Surface Strengthening Treatment
title_full_unstemmed Fatigue Limit of Custom 465 with Surface Strengthening Treatment
title_short Fatigue Limit of Custom 465 with Surface Strengthening Treatment
title_sort fatigue limit of custom 465 with surface strengthening treatment
topic Article
url https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6981755/
https://www.ncbi.nlm.nih.gov/pubmed/31935829
http://dx.doi.org/10.3390/ma13010238
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