Can Li , Dexin Zhang , Xiaoxing Li , Yingjian Guo , Yong Li
{"title":"扩散焊TC4钛合金室温和高温拉伸疲劳断裂行为","authors":"Can Li , Dexin Zhang , Xiaoxing Li , Yingjian Guo , Yong Li","doi":"10.1016/j.engfailanal.2025.110182","DOIUrl":null,"url":null,"abstract":"<div><div>The synergistic effects of matrix microstructure and bonding interface characteristics on the tensile and fatigue properties of the diffusion bonded (DB) TC4 titanium alloy at room temperature and 400℃ were studied. A double-stage heat treatment with various cooling conditions (750-850℃) was performed on the DB joints due to the precision manufacturing requirements of the fan blade. Matrix microstructure evolution caused significant tensile strength and fatigue life degradation of the DB joint at room temperature. At 400 °C, all tensile specimens exhibited ductile fracture morphology, with tensile strength showing negligible dependence on interface or matrix microstructure evolution. However, the influence of matrix microstructure and DB interface on fatigue performance at 400℃ was strongly related to the load conditions. During fatigue testing at 400℃ and 315 MPa (50 % of the tensile strength), the petal-like α + β colonies with a volume fraction of 10.5 % inhibited the crack propagation of the DB joint. Conversely, the preferentially oriented β grains with the < 111 > slip direction aligned parallel to the fatigue loading direction, along with lath α + β colonies exhibiting a 21.5 % volume fraction, facilitated crack initiation and propagation. Notably, when fatigue cracks extended into the weakly bonded region at the DB interface, crack propagation was impeded, accompanied by a shrinkage of the plastic zone at the crack tip. Under higher fatigue loads (70 % of the tensile strength), crack propagation was accelerated at the micro-pores of the DB interface, irrespective of testing temperature (room temperature or 400 °C). The fracture surfaces exhibited minimal plastic strain, resulting in negligible differences in fatigue life between the two heat-treated DB joints with distinct α + β colony microstructures.</div></div>","PeriodicalId":11677,"journal":{"name":"Engineering Failure Analysis","volume":"182 ","pages":"Article 110182"},"PeriodicalIF":5.7000,"publicationDate":"2025-10-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Fracture behavior in tensile and fatigue tests of diffusion bonded TC4 titanium alloy at room and high temperatures\",\"authors\":\"Can Li , Dexin Zhang , Xiaoxing Li , Yingjian Guo , Yong Li\",\"doi\":\"10.1016/j.engfailanal.2025.110182\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>The synergistic effects of matrix microstructure and bonding interface characteristics on the tensile and fatigue properties of the diffusion bonded (DB) TC4 titanium alloy at room temperature and 400℃ were studied. A double-stage heat treatment with various cooling conditions (750-850℃) was performed on the DB joints due to the precision manufacturing requirements of the fan blade. Matrix microstructure evolution caused significant tensile strength and fatigue life degradation of the DB joint at room temperature. At 400 °C, all tensile specimens exhibited ductile fracture morphology, with tensile strength showing negligible dependence on interface or matrix microstructure evolution. However, the influence of matrix microstructure and DB interface on fatigue performance at 400℃ was strongly related to the load conditions. During fatigue testing at 400℃ and 315 MPa (50 % of the tensile strength), the petal-like α + β colonies with a volume fraction of 10.5 % inhibited the crack propagation of the DB joint. Conversely, the preferentially oriented β grains with the < 111 > slip direction aligned parallel to the fatigue loading direction, along with lath α + β colonies exhibiting a 21.5 % volume fraction, facilitated crack initiation and propagation. Notably, when fatigue cracks extended into the weakly bonded region at the DB interface, crack propagation was impeded, accompanied by a shrinkage of the plastic zone at the crack tip. Under higher fatigue loads (70 % of the tensile strength), crack propagation was accelerated at the micro-pores of the DB interface, irrespective of testing temperature (room temperature or 400 °C). The fracture surfaces exhibited minimal plastic strain, resulting in negligible differences in fatigue life between the two heat-treated DB joints with distinct α + β colony microstructures.</div></div>\",\"PeriodicalId\":11677,\"journal\":{\"name\":\"Engineering Failure Analysis\",\"volume\":\"182 \",\"pages\":\"Article 110182\"},\"PeriodicalIF\":5.7000,\"publicationDate\":\"2025-10-01\",\"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/S1350630725009239\",\"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}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Engineering Failure Analysis","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1350630725009239","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}
Fracture behavior in tensile and fatigue tests of diffusion bonded TC4 titanium alloy at room and high temperatures
The synergistic effects of matrix microstructure and bonding interface characteristics on the tensile and fatigue properties of the diffusion bonded (DB) TC4 titanium alloy at room temperature and 400℃ were studied. A double-stage heat treatment with various cooling conditions (750-850℃) was performed on the DB joints due to the precision manufacturing requirements of the fan blade. Matrix microstructure evolution caused significant tensile strength and fatigue life degradation of the DB joint at room temperature. At 400 °C, all tensile specimens exhibited ductile fracture morphology, with tensile strength showing negligible dependence on interface or matrix microstructure evolution. However, the influence of matrix microstructure and DB interface on fatigue performance at 400℃ was strongly related to the load conditions. During fatigue testing at 400℃ and 315 MPa (50 % of the tensile strength), the petal-like α + β colonies with a volume fraction of 10.5 % inhibited the crack propagation of the DB joint. Conversely, the preferentially oriented β grains with the < 111 > slip direction aligned parallel to the fatigue loading direction, along with lath α + β colonies exhibiting a 21.5 % volume fraction, facilitated crack initiation and propagation. Notably, when fatigue cracks extended into the weakly bonded region at the DB interface, crack propagation was impeded, accompanied by a shrinkage of the plastic zone at the crack tip. Under higher fatigue loads (70 % of the tensile strength), crack propagation was accelerated at the micro-pores of the DB interface, irrespective of testing temperature (room temperature or 400 °C). The fracture surfaces exhibited minimal plastic strain, resulting in negligible differences in fatigue life between the two heat-treated DB joints with distinct α + β colony microstructures.
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.