Miaodong Zhao , Dianyin Hu , Jianxing Mao , Jinchao Pan , Tinglian Zhang , Rongqiao Wang
{"title":"A novel TCD framework for fatigue lifetime prediction incorporating defect and stress concentration effects","authors":"Miaodong Zhao , Dianyin Hu , Jianxing Mao , Jinchao Pan , Tinglian Zhang , Rongqiao Wang","doi":"10.1016/j.engfailanal.2025.109900","DOIUrl":null,"url":null,"abstract":"<div><div>Defects in powder metallurgy (PM) superalloy tend to become a source of cracks under cyclic loading, reducing the fatigue lifetime of crack initiation and affecting the safety of aero-engines. The mechanism of crack initiation is affected by both the defect type and the gradient stress distribution, resulting in the large difference of fatigue lifetime. To study the relationship between the defect type at the crack source and the fatigue lifetime under the influence of stress concentrations, a series of fatigue experiments of notched round bar specimens were carried out. Then a modified theory of critical distance (TCD) on the basis of concern range of defect was proposed, which accommodates both surface defects and internal defects cracking mechanism. Compared to the experimental results, prediction results of fatigue lifetime fell within a scatter band of ±4. Finally, a concept of inclusion sensitive area (ISA) was proposed to quantify the area of stress concentration that was susceptible to cracking due to inclusion. It was validated by the fracture surface observation, where all inclusions on crack sources in the experiment were within the predicted region. This work will support lifetime prediction and defect detection strategies for aero-engine components.</div></div>","PeriodicalId":11677,"journal":{"name":"Engineering Failure Analysis","volume":"180 ","pages":"Article 109900"},"PeriodicalIF":4.4000,"publicationDate":"2025-07-15","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Engineering Failure Analysis","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1350630725006417","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
引用次数: 0
Abstract
Defects in powder metallurgy (PM) superalloy tend to become a source of cracks under cyclic loading, reducing the fatigue lifetime of crack initiation and affecting the safety of aero-engines. The mechanism of crack initiation is affected by both the defect type and the gradient stress distribution, resulting in the large difference of fatigue lifetime. To study the relationship between the defect type at the crack source and the fatigue lifetime under the influence of stress concentrations, a series of fatigue experiments of notched round bar specimens were carried out. Then a modified theory of critical distance (TCD) on the basis of concern range of defect was proposed, which accommodates both surface defects and internal defects cracking mechanism. Compared to the experimental results, prediction results of fatigue lifetime fell within a scatter band of ±4. Finally, a concept of inclusion sensitive area (ISA) was proposed to quantify the area of stress concentration that was susceptible to cracking due to inclusion. It was validated by the fracture surface observation, where all inclusions on crack sources in the experiment were within the predicted region. This work will support lifetime prediction and defect detection strategies for aero-engine components.
期刊介绍:
Engineering Failure Analysis publishes research papers describing the analysis of engineering failures and related studies.
Papers relating to the structure, properties and behaviour of engineering materials are encouraged, particularly those which also involve the detailed application of materials parameters to problems in engineering structures, components and design. In addition to the area of materials engineering, the interacting fields of mechanical, manufacturing, aeronautical, civil, chemical, corrosion and design engineering are considered relevant. Activity should be directed at analysing engineering failures and carrying out research to help reduce the incidences of failures and to extend the operating horizons of engineering materials.
Emphasis is placed on the mechanical properties of materials and their behaviour when influenced by structure, process and environment. Metallic, polymeric, ceramic and natural materials are all included and the application of these materials to real engineering situations should be emphasised. The use of a case-study based approach is also encouraged.
Engineering Failure Analysis provides essential reference material and critical feedback into the design process thereby contributing to the prevention of engineering failures in the future. All submissions will be subject to peer review from leading experts in the field.