Effect of Stress Ratio(R) and Stress Concentration Factor (Kt) on Fatigue Properties of WSTi6211 Titanium Alloy

In this paper, the author studied the effects of different stress ratios(R) and stress concentration factors(Kt) on the fatigue properties of WSTi6211 titanium alloy.Through S-N curve, the author obtained the fatigue ultimate strength of the material under different conditions and analyzed character...

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Main Authors: Fang Hao, Yong Feng, Yuxuan Du, Yue Wang, Enen Xu, Kaixuan Wang, Yanwen Tian
Format: Article
Language:English
Published: EDP Sciences 2020-01-01
Series:MATEC Web of Conferences
Subjects:
Online Access:https://www.matec-conferences.org/articles/matecconf/pdf/2020/17/matecconf_ti2019_11065.pdf
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spelling doaj-782c7cfdbaa44f81a473742021ac40eb2021-08-11T12:58:32ZengEDP SciencesMATEC Web of Conferences2261-236X2020-01-013211106510.1051/matecconf/202032111065matecconf_ti2019_11065Effect of Stress Ratio(R) and Stress Concentration Factor (Kt) on Fatigue Properties of WSTi6211 Titanium AlloyFang HaoYong FengYuxuan Du0Yue Wang1Enen Xu2Kaixuan Wang3Yanwen Tian4State Key Laboratory of Solidification Processing,Northwest Polytechnical UniversityXi’an University of Architecture and Technology,Xi’anWestern Superconducting Technologies Co., Ltd.Western Superconducting Technologies Co., Ltd.Western Superconducting Technologies Co., Ltd.In this paper, the author studied the effects of different stress ratios(R) and stress concentration factors(Kt) on the fatigue properties of WSTi6211 titanium alloy.Through S-N curve, the author obtained the fatigue ultimate strength of the material under different conditions and analyzed characteristics of fatigue fractures, including the crack source sourse, the crack growth region and the final rupture region. The results show that when Kt=1, R=0.5, the fatigue ultimate strength σD is 626MPa; when Kt = 1, R=0.06, the fatigue ultimate strength σD is 527.5MPa; when Kt=3, R=0.06, the ultimate fatigue strength σD is 267MPa. Fatigue performance is very sensitive to R and Kt. The larger R is, the larger the fatigue ultimate strength is. The larger Kt is, the smaller the fatigue limit strength is. The fracture morphology shows typical fatigue fracture morphology. Most of the cracks originate on the surface of specimens and have typical fatigue bands. With the decrease of stress, the area of crack growth zone increases.https://www.matec-conferences.org/articles/matecconf/pdf/2020/17/matecconf_ti2019_11065.pdfwsti6211 titanium alloys-n curvestress ratiostress concentration factor
collection DOAJ
language English
format Article
sources DOAJ
author Fang Hao
Yong Feng
Yuxuan Du
Yue Wang
Enen Xu
Kaixuan Wang
Yanwen Tian
spellingShingle Fang Hao
Yong Feng
Yuxuan Du
Yue Wang
Enen Xu
Kaixuan Wang
Yanwen Tian
Effect of Stress Ratio(R) and Stress Concentration Factor (Kt) on Fatigue Properties of WSTi6211 Titanium Alloy
MATEC Web of Conferences
wsti6211 titanium alloy
s-n curve
stress ratio
stress concentration factor
author_facet Fang Hao
Yong Feng
Yuxuan Du
Yue Wang
Enen Xu
Kaixuan Wang
Yanwen Tian
author_sort Fang Hao
title Effect of Stress Ratio(R) and Stress Concentration Factor (Kt) on Fatigue Properties of WSTi6211 Titanium Alloy
title_short Effect of Stress Ratio(R) and Stress Concentration Factor (Kt) on Fatigue Properties of WSTi6211 Titanium Alloy
title_full Effect of Stress Ratio(R) and Stress Concentration Factor (Kt) on Fatigue Properties of WSTi6211 Titanium Alloy
title_fullStr Effect of Stress Ratio(R) and Stress Concentration Factor (Kt) on Fatigue Properties of WSTi6211 Titanium Alloy
title_full_unstemmed Effect of Stress Ratio(R) and Stress Concentration Factor (Kt) on Fatigue Properties of WSTi6211 Titanium Alloy
title_sort effect of stress ratio(r) and stress concentration factor (kt) on fatigue properties of wsti6211 titanium alloy
publisher EDP Sciences
series MATEC Web of Conferences
issn 2261-236X
publishDate 2020-01-01
description In this paper, the author studied the effects of different stress ratios(R) and stress concentration factors(Kt) on the fatigue properties of WSTi6211 titanium alloy.Through S-N curve, the author obtained the fatigue ultimate strength of the material under different conditions and analyzed characteristics of fatigue fractures, including the crack source sourse, the crack growth region and the final rupture region. The results show that when Kt=1, R=0.5, the fatigue ultimate strength σD is 626MPa; when Kt = 1, R=0.06, the fatigue ultimate strength σD is 527.5MPa; when Kt=3, R=0.06, the ultimate fatigue strength σD is 267MPa. Fatigue performance is very sensitive to R and Kt. The larger R is, the larger the fatigue ultimate strength is. The larger Kt is, the smaller the fatigue limit strength is. The fracture morphology shows typical fatigue fracture morphology. Most of the cracks originate on the surface of specimens and have typical fatigue bands. With the decrease of stress, the area of crack growth zone increases.
topic wsti6211 titanium alloy
s-n curve
stress ratio
stress concentration factor
url https://www.matec-conferences.org/articles/matecconf/pdf/2020/17/matecconf_ti2019_11065.pdf
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