Yan Yin , Yibo Shang , Weifeng He , Chen Wang , Liucheng Zhou
{"title":"激光冲击强化和喷丸强化提高Ti-6Al-4V燕尾接头的微动疲劳性能","authors":"Yan Yin , Yibo Shang , Weifeng He , Chen Wang , Liucheng Zhou","doi":"10.1016/j.ijfatigue.2025.108996","DOIUrl":null,"url":null,"abstract":"<div><div>Ti-6Al-4V is widely used in aero-engine compressor blades, but its low fretting fatigue resistance makes integrity challenging. Compound treatment has been recognized as a future technology with enhanced mechanical properties. However, these attempts were limited to low-cycle fatigue. The beneficial fretting fatigue performance enhancements through compound strengthening are still prominent. This study investigates the effect of laser shock peening (LSP) and shock peening (SP) compound treatment on fretting fatigue. The experiment results show a large residual stress near the contact surface. Larger depths of surface grain refinement have also been found. Hence, the LSP + SP had the better-strengthened effect (4.57 times) on fretting fatigue life as compared with single LSP (3.94 times) or SP (2.87 times) treatment. The results reveal that LSP + SP can affect the location and number of crack initiation sites, thereby increasing the initiation life. The large depth distribution of residual stresses and the multiaxial stresses induced by fretting fatigue can mitigate stress concentration. The retardation of crack propagation by LSP + SP was also revealed by statistical analysis of fatigue striation spacing. This work provides valuable insights into the development of a strengthening process for compressor blades against fretting fatigue.</div></div>","PeriodicalId":14112,"journal":{"name":"International Journal of Fatigue","volume":"198 ","pages":"Article 108996"},"PeriodicalIF":5.7000,"publicationDate":"2025-04-12","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Improving the fretting fatigue properties of Ti-6Al-4V dovetail joint treated by laser shock peening and shot peening\",\"authors\":\"Yan Yin , Yibo Shang , Weifeng He , Chen Wang , Liucheng Zhou\",\"doi\":\"10.1016/j.ijfatigue.2025.108996\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Ti-6Al-4V is widely used in aero-engine compressor blades, but its low fretting fatigue resistance makes integrity challenging. Compound treatment has been recognized as a future technology with enhanced mechanical properties. However, these attempts were limited to low-cycle fatigue. The beneficial fretting fatigue performance enhancements through compound strengthening are still prominent. This study investigates the effect of laser shock peening (LSP) and shock peening (SP) compound treatment on fretting fatigue. The experiment results show a large residual stress near the contact surface. Larger depths of surface grain refinement have also been found. Hence, the LSP + SP had the better-strengthened effect (4.57 times) on fretting fatigue life as compared with single LSP (3.94 times) or SP (2.87 times) treatment. The results reveal that LSP + SP can affect the location and number of crack initiation sites, thereby increasing the initiation life. The large depth distribution of residual stresses and the multiaxial stresses induced by fretting fatigue can mitigate stress concentration. The retardation of crack propagation by LSP + SP was also revealed by statistical analysis of fatigue striation spacing. This work provides valuable insights into the development of a strengthening process for compressor blades against fretting fatigue.</div></div>\",\"PeriodicalId\":14112,\"journal\":{\"name\":\"International Journal of Fatigue\",\"volume\":\"198 \",\"pages\":\"Article 108996\"},\"PeriodicalIF\":5.7000,\"publicationDate\":\"2025-04-12\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"International Journal of Fatigue\",\"FirstCategoryId\":\"88\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0142112325001938\",\"RegionNum\":2,\"RegionCategory\":\"材料科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, MECHANICAL\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"International Journal of Fatigue","FirstCategoryId":"88","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0142112325001938","RegionNum":2,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
Improving the fretting fatigue properties of Ti-6Al-4V dovetail joint treated by laser shock peening and shot peening
Ti-6Al-4V is widely used in aero-engine compressor blades, but its low fretting fatigue resistance makes integrity challenging. Compound treatment has been recognized as a future technology with enhanced mechanical properties. However, these attempts were limited to low-cycle fatigue. The beneficial fretting fatigue performance enhancements through compound strengthening are still prominent. This study investigates the effect of laser shock peening (LSP) and shock peening (SP) compound treatment on fretting fatigue. The experiment results show a large residual stress near the contact surface. Larger depths of surface grain refinement have also been found. Hence, the LSP + SP had the better-strengthened effect (4.57 times) on fretting fatigue life as compared with single LSP (3.94 times) or SP (2.87 times) treatment. The results reveal that LSP + SP can affect the location and number of crack initiation sites, thereby increasing the initiation life. The large depth distribution of residual stresses and the multiaxial stresses induced by fretting fatigue can mitigate stress concentration. The retardation of crack propagation by LSP + SP was also revealed by statistical analysis of fatigue striation spacing. This work provides valuable insights into the development of a strengthening process for compressor blades against fretting fatigue.
期刊介绍:
Typical subjects discussed in International Journal of Fatigue address:
Novel fatigue testing and characterization methods (new kinds of fatigue tests, critical evaluation of existing methods, in situ measurement of fatigue degradation, non-contact field measurements)
Multiaxial fatigue and complex loading effects of materials and structures, exploring state-of-the-art concepts in degradation under cyclic loading
Fatigue in the very high cycle regime, including failure mode transitions from surface to subsurface, effects of surface treatment, processing, and loading conditions
Modeling (including degradation processes and related driving forces, multiscale/multi-resolution methods, computational hierarchical and concurrent methods for coupled component and material responses, novel methods for notch root analysis, fracture mechanics, damage mechanics, crack growth kinetics, life prediction and durability, and prediction of stochastic fatigue behavior reflecting microstructure and service conditions)
Models for early stages of fatigue crack formation and growth that explicitly consider microstructure and relevant materials science aspects
Understanding the influence or manufacturing and processing route on fatigue degradation, and embedding this understanding in more predictive schemes for mitigation and design against fatigue
Prognosis and damage state awareness (including sensors, monitoring, methodology, interactive control, accelerated methods, data interpretation)
Applications of technologies associated with fatigue and their implications for structural integrity and reliability. This includes issues related to design, operation and maintenance, i.e., life cycle engineering
Smart materials and structures that can sense and mitigate fatigue degradation
Fatigue of devices and structures at small scales, including effects of process route and surfaces/interfaces.