• 文献检索
  • 文档翻译
  • 深度研究
  • 学术资讯
  • Suppr Zotero 插件Zotero 插件
  • 邀请有礼
  • 套餐&价格
  • 历史记录
应用&插件
Suppr Zotero 插件Zotero 插件浏览器插件Mac 客户端Windows 客户端微信小程序
定价
高级版会员购买积分包购买API积分包
服务
文献检索文档翻译深度研究API 文档MCP 服务
关于我们
关于 Suppr公司介绍联系我们用户协议隐私条款
关注我们

Suppr 超能文献

核心技术专利:CN118964589B侵权必究
粤ICP备2023148730 号-1Suppr @ 2026

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验

预测表面波纹度对电弧增材制造Ti-6Al-4V合金疲劳寿命的影响

Predicting the Effect of Surface Waviness on Fatigue Life of a Wire + Arc Additive Manufactured Ti-6Al-4V Alloy.

作者信息

Shamir Muhammad, Zhang Xiang, Syed Abdul Khadar, Sadler Wayne

机构信息

Centre for Manufacturing and Materials, Coventry University, Coventry CV1 5FB, UK.

出版信息

Materials (Basel). 2023 Jul 30;16(15):5355. doi: 10.3390/ma16155355.

DOI:10.3390/ma16155355
PMID:37570059
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC10419546/
Abstract

This paper reports the effect of as-deposited surface conditions on the fatigue strength of an additively manufactured titanium alloy, Ti-6Al-4V (WAAM Ti64). First, the local stress concentration caused by the surface waviness was quantified using a metrology technique and computer modelling. Fatigue tests were conducted under bending loads at a cyclic load ratio of 0.1. The applicability of two predictive methods was the focus of this study. The traditional notch stress method was unable to predict the correct S-N curve trend slope, which could be attributed to the early crack initiation from the troughs on the as-built surface, with crack propagation being the dominant failure mechanism. By treating the troughs as small cracks, the fracture mechanics approach delivered good predictions at every applied stress level. Surface machining and polishing may not always be practical or required; it depends on the applications and service load levels. This research demonstrated that the fracture mechanics approach can be used for predicting the fatigue life of WAAM titanium alloys in as-built conditions and, hence, can be a tool for decision making on the level of surface machining.

摘要

本文报道了增材制造钛合金Ti-6Al-4V(WAAM Ti64)沉积态表面条件对疲劳强度的影响。首先,使用计量技术和计算机建模对由表面波纹引起的局部应力集中进行了量化。在循环载荷比为0.1的弯曲载荷下进行了疲劳试验。本研究的重点是两种预测方法的适用性。传统的缺口应力方法无法预测正确的S-N曲线趋势斜率,这可能归因于在增材制造表面的波谷处早期裂纹萌生,裂纹扩展是主要的失效机制。通过将波谷视为小裂纹,断裂力学方法在每个施加应力水平下都给出了良好的预测。表面加工和抛光可能并不总是可行或必要的;这取决于应用和服役载荷水平。本研究表明,断裂力学方法可用于预测增材制造条件下WAAM钛合金的疲劳寿命,因此可作为决定表面加工水平的工具。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/5b0b356d9f28/materials-16-05355-g013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/898b70ebb4b6/materials-16-05355-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/6cbc5d70249c/materials-16-05355-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/ebe59f9785ee/materials-16-05355-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/b5237251b69b/materials-16-05355-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/ae8900d47346/materials-16-05355-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/0a975ef835dc/materials-16-05355-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/4bad74190fa9/materials-16-05355-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/211e45e5edb0/materials-16-05355-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/cbf75875b18a/materials-16-05355-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/7a7f204a456e/materials-16-05355-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/f0646f32c15f/materials-16-05355-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/3496ddbf10d1/materials-16-05355-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/5b0b356d9f28/materials-16-05355-g013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/898b70ebb4b6/materials-16-05355-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/6cbc5d70249c/materials-16-05355-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/ebe59f9785ee/materials-16-05355-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/b5237251b69b/materials-16-05355-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/ae8900d47346/materials-16-05355-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/0a975ef835dc/materials-16-05355-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/4bad74190fa9/materials-16-05355-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/211e45e5edb0/materials-16-05355-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/cbf75875b18a/materials-16-05355-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/7a7f204a456e/materials-16-05355-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/f0646f32c15f/materials-16-05355-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/3496ddbf10d1/materials-16-05355-g012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/1347/10419546/5b0b356d9f28/materials-16-05355-g013.jpg

相似文献

1
Predicting the Effect of Surface Waviness on Fatigue Life of a Wire + Arc Additive Manufactured Ti-6Al-4V Alloy.预测表面波纹度对电弧增材制造Ti-6Al-4V合金疲劳寿命的影响
Materials (Basel). 2023 Jul 30;16(15):5355. doi: 10.3390/ma16155355.
2
Low-Cycle Fatigue Behavior of Wire and Arc Additively Manufactured Ti-6Al-4V Material.电弧增材制造Ti-6Al-4V材料的低周疲劳行为
Materials (Basel). 2023 Sep 5;16(18):6083. doi: 10.3390/ma16186083.
3
Surface roughness and fatigue performance of commercially pure titanium and Ti-6Al-4V alloy after different polishing protocols.不同抛光工艺后工业纯钛和Ti-6Al-4V合金的表面粗糙度及疲劳性能
J Prosthet Dent. 2005 Apr;93(4):378-85. doi: 10.1016/j.prosdent.2005.01.010.
4
Effect of Oxygen Variation on High Cycle Fatigue Behavior of Ti-6Al-4V Titanium Alloy.氧含量变化对Ti-6Al-4V钛合金高周疲劳行为的影响
Materials (Basel). 2020 Sep 1;13(17):3858. doi: 10.3390/ma13173858.
5
Formation of Structure and Properties of Two-Phase Ti-6Al-4V Alloy during Cold Metal Transfer Additive Deposition with Interpass Forging.带层间锻造的冷金属过渡增材沉积过程中两相Ti-6Al-4V合金的组织与性能形成
Materials (Basel). 2021 Aug 6;14(16):4415. doi: 10.3390/ma14164415.
6
An Investigation of the Anisotropic Fatigue Properties of Laser Additively Manufactured Ti-6Al-4V under Vibration Loading.振动载荷下激光增材制造Ti-6Al-4V的各向异性疲劳性能研究
Materials (Basel). 2023 Jul 19;16(14):5099. doi: 10.3390/ma16145099.
7
Analysis of the Effect of Machining of the Surfaces of WAAM 18Ni 250 Maraging Steel Specimens on Their Durability.搅拌摩擦增材制造18Ni 250马氏体时效钢试样表面加工对其耐久性影响的分析
Materials (Basel). 2022 Dec 13;15(24):8890. doi: 10.3390/ma15248890.
8
Fatigue strength reduction of Ti-6Al-4V titanium alloy after contact with high-frequency cauterising instruments.高频电刀接触后 Ti-6Al-4V 钛合金疲劳强度降低。
Med Eng Phys. 2020 Jul;81:58-67. doi: 10.1016/j.medengphy.2020.05.016. Epub 2020 May 18.
9
The State of the Art in Machining Additively Manufactured Titanium Alloy Ti-6Al-4V.增材制造钛合金Ti-6Al-4V的加工技术现状
Materials (Basel). 2023 Mar 24;16(7):2583. doi: 10.3390/ma16072583.
10
Fatigue crack propagation in additively manufactured porous biomaterials.增材制造多孔生物材料中的疲劳裂纹扩展
Mater Sci Eng C Mater Biol Appl. 2017 Jul 1;76:457-463. doi: 10.1016/j.msec.2017.03.091. Epub 2017 Mar 16.

引用本文的文献

1
USAF Characteristic Approach: A Robust Tool for Predicting Fatigue Crack Growth under Various Underload Spectra.美国空军特征法:一种预测各种欠载谱下疲劳裂纹扩展的强大工具。
Materials (Basel). 2024 Jul 4;17(13):3303. doi: 10.3390/ma17133303.

本文引用的文献

1
Modelling the Variability and the Anisotropic Behaviour of Crack Growth in SLM Ti-6Al-4V.模拟选择性激光熔化Ti-6Al-4V中裂纹扩展的变异性和各向异性行为。
Materials (Basel). 2021 Mar 13;14(6):1400. doi: 10.3390/ma14061400.
2
Further Studies into Crack Growth in Additively Manufactured Materials.增材制造材料中裂纹扩展的进一步研究。
Materials (Basel). 2020 May 12;13(10):2223. doi: 10.3390/ma13102223.