{"title":"船用Ti-6Al-4V薄板焊接结构冲击损伤及破坏机理研究","authors":"Xiaoyu Wang , Shuangxi Xu , Jian Yu , Gaopeng Chen , Wei Dong , Wei Shen","doi":"10.1016/j.engfailanal.2025.110114","DOIUrl":null,"url":null,"abstract":"<div><div>With the development of lightweight, titanium alloy materials have been gradually applied to high-speed ships or superstructure, but the research on impact resistance of titanium alloy hull structure under low-speed collision has not been effectively carried out. Taking the butt welded structure of Ti-6Al-4V thin plate prepared by GTAW as the research object, the low-speed impact test was carried out on the weld position of the welded structure by using the horizontal impact test platform, and the constitutive model and failure criterion of Ti-6Al-4V weld under low-speed impact were verified. In order to ensure the reliability of the sample, high-purity argon gas is used in the sample preparation process (the front and rear gas flows are 20 and 15 L min, respectively, and oxygen is less than 50 ppm). The optimized welding parameters are voltage 20.4 V, current 140A and speed 5 mm/s. After welding, the surface reagent penetrant testing and ultrasonic nondestructive testing are carried out. SEM microscopic analysis of Ti-6Al-4V weld after low-speed impact shows that the fracture mode of Ti-6Al-4V weld after impact is a mixed fracture of brittleness and toughness. Through the thermal–mechanical coupling simulation calculation of double ellipsoid heat source and blind hole method, the distribution law of welding residual stress in welded joint is obtained and verified. Furthermore, the welding residual stress is introduced into the impact simulation model to quantify the influence of residual stress on the impact resistance of titanium alloy welded structure. The results show that the welding residual stress reduces the impact contact stiffness of the structure, accelerates the crack propagation and reduces the impact resistance by about 10 %. The residual stress after welding significantly reduces the impact resistance of the structure.</div></div>","PeriodicalId":11677,"journal":{"name":"Engineering Failure Analysis","volume":"182 ","pages":"Article 110114"},"PeriodicalIF":5.7000,"publicationDate":"2025-09-12","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Study on impact damage and failure mechanism of marine Ti-6Al-4V thin plate welded structure\",\"authors\":\"Xiaoyu Wang , Shuangxi Xu , Jian Yu , Gaopeng Chen , Wei Dong , Wei Shen\",\"doi\":\"10.1016/j.engfailanal.2025.110114\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>With the development of lightweight, titanium alloy materials have been gradually applied to high-speed ships or superstructure, but the research on impact resistance of titanium alloy hull structure under low-speed collision has not been effectively carried out. Taking the butt welded structure of Ti-6Al-4V thin plate prepared by GTAW as the research object, the low-speed impact test was carried out on the weld position of the welded structure by using the horizontal impact test platform, and the constitutive model and failure criterion of Ti-6Al-4V weld under low-speed impact were verified. In order to ensure the reliability of the sample, high-purity argon gas is used in the sample preparation process (the front and rear gas flows are 20 and 15 L min, respectively, and oxygen is less than 50 ppm). The optimized welding parameters are voltage 20.4 V, current 140A and speed 5 mm/s. After welding, the surface reagent penetrant testing and ultrasonic nondestructive testing are carried out. SEM microscopic analysis of Ti-6Al-4V weld after low-speed impact shows that the fracture mode of Ti-6Al-4V weld after impact is a mixed fracture of brittleness and toughness. Through the thermal–mechanical coupling simulation calculation of double ellipsoid heat source and blind hole method, the distribution law of welding residual stress in welded joint is obtained and verified. Furthermore, the welding residual stress is introduced into the impact simulation model to quantify the influence of residual stress on the impact resistance of titanium alloy welded structure. The results show that the welding residual stress reduces the impact contact stiffness of the structure, accelerates the crack propagation and reduces the impact resistance by about 10 %. The residual stress after welding significantly reduces the impact resistance of the structure.</div></div>\",\"PeriodicalId\":11677,\"journal\":{\"name\":\"Engineering Failure Analysis\",\"volume\":\"182 \",\"pages\":\"Article 110114\"},\"PeriodicalIF\":5.7000,\"publicationDate\":\"2025-09-12\",\"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/S1350630725008556\",\"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/S1350630725008556","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}
Study on impact damage and failure mechanism of marine Ti-6Al-4V thin plate welded structure
With the development of lightweight, titanium alloy materials have been gradually applied to high-speed ships or superstructure, but the research on impact resistance of titanium alloy hull structure under low-speed collision has not been effectively carried out. Taking the butt welded structure of Ti-6Al-4V thin plate prepared by GTAW as the research object, the low-speed impact test was carried out on the weld position of the welded structure by using the horizontal impact test platform, and the constitutive model and failure criterion of Ti-6Al-4V weld under low-speed impact were verified. In order to ensure the reliability of the sample, high-purity argon gas is used in the sample preparation process (the front and rear gas flows are 20 and 15 L min, respectively, and oxygen is less than 50 ppm). The optimized welding parameters are voltage 20.4 V, current 140A and speed 5 mm/s. After welding, the surface reagent penetrant testing and ultrasonic nondestructive testing are carried out. SEM microscopic analysis of Ti-6Al-4V weld after low-speed impact shows that the fracture mode of Ti-6Al-4V weld after impact is a mixed fracture of brittleness and toughness. Through the thermal–mechanical coupling simulation calculation of double ellipsoid heat source and blind hole method, the distribution law of welding residual stress in welded joint is obtained and verified. Furthermore, the welding residual stress is introduced into the impact simulation model to quantify the influence of residual stress on the impact resistance of titanium alloy welded structure. The results show that the welding residual stress reduces the impact contact stiffness of the structure, accelerates the crack propagation and reduces the impact resistance by about 10 %. The residual stress after welding significantly reduces the impact resistance of the structure.
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.