Notch Fatigue Damage Evolution Mechanism of TC21 Alloy with Multilevel Lamellar Microstructures
This study aims to explore the effect of microstructural parameters on the notch fatigue damage behavior of the TC21 alloy. Different levels of lamellar microstructures were achieved through distinct aging temperatures of 550 °C, 600 °C, and 650 °C. The findings reveal that increasing aging temperat...
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2024-12-01
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| author | Xiaosong Zhou Xiang Li Chaowen Huang Quan Wu Fei Zhao |
| author_facet | Xiaosong Zhou Xiang Li Chaowen Huang Quan Wu Fei Zhao |
| author_sort | Xiaosong Zhou |
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| description | This study aims to explore the effect of microstructural parameters on the notch fatigue damage behavior of the TC21 alloy. Different levels of lamellar microstructures were achieved through distinct aging temperatures of 550 °C, 600 °C, and 650 °C. The findings reveal that increasing aging temperature primarily contributes to the augmentation of α colony (α<sub>c</sub>) thickness, grain boundaries α phase (GBα) thickness, and α fine (α<sub>fine</sub>) size alongside a reduction in α lath (α<sub>lath</sub>) thickness and α<sub>fine</sub> content. The notch alters stress distribution and relaxation effects at the root, enhancing notched tensile strength while weakening plasticity. Moreover, the increased thickness of GBα emerges as a critical factor leading to the increase area of intergranular cleavage fracture. It is noteworthy that more thickness α<sub>lath</sub> and smaller α<sub>fine</sub> facilitate deformation coordination and enhance dislocation accumulation at the interface, leading to a higher propensity for micro-voids and micro-cracks to propagate along the interface. Conversely, at elevated aging temperatures, thinner α<sub>lath</sub> and larger α<sub>fine</sub> are more susceptible to fracture, resulting in the liberation of dislocations at the interface. The reduction in α<sub>lath</sub> thickness is crucial for triggering the initiation of multi-system dislocations at the interface, which promotes the development of persistent slip bands (PSBs) and dislocation nets within α<sub>lath</sub>. This phenomenon induces inhomogeneous plastic deformation and localized hardening, fostering the formation of micro-voids and micro-cracks. |
| format | Article |
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| institution | Kabale University |
| issn | 2075-4701 |
| language | English |
| publishDate | 2024-12-01 |
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| spelling | doaj-art-906d282995be4f258338470dc6e43b312025-01-24T13:41:25ZengMDPI AGMetals2075-47012024-12-011511810.3390/met15010018Notch Fatigue Damage Evolution Mechanism of TC21 Alloy with Multilevel Lamellar MicrostructuresXiaosong Zhou0Xiang Li1Chaowen Huang2Quan Wu3Fei Zhao4School of Mechanical and Electrical Engineering, Guizhou Normal University, Guiyang 550025, ChinaCollege of Materials and Metallurgy, Guizhou University, Guiyang 550025, ChinaCollege of Materials and Metallurgy, Guizhou University, Guiyang 550025, ChinaSchool of Mechanical and Electrical Engineering, Guizhou Normal University, Guiyang 550025, ChinaCollege of Materials and Metallurgy, Guizhou University, Guiyang 550025, ChinaThis study aims to explore the effect of microstructural parameters on the notch fatigue damage behavior of the TC21 alloy. Different levels of lamellar microstructures were achieved through distinct aging temperatures of 550 °C, 600 °C, and 650 °C. The findings reveal that increasing aging temperature primarily contributes to the augmentation of α colony (α<sub>c</sub>) thickness, grain boundaries α phase (GBα) thickness, and α fine (α<sub>fine</sub>) size alongside a reduction in α lath (α<sub>lath</sub>) thickness and α<sub>fine</sub> content. The notch alters stress distribution and relaxation effects at the root, enhancing notched tensile strength while weakening plasticity. Moreover, the increased thickness of GBα emerges as a critical factor leading to the increase area of intergranular cleavage fracture. It is noteworthy that more thickness α<sub>lath</sub> and smaller α<sub>fine</sub> facilitate deformation coordination and enhance dislocation accumulation at the interface, leading to a higher propensity for micro-voids and micro-cracks to propagate along the interface. Conversely, at elevated aging temperatures, thinner α<sub>lath</sub> and larger α<sub>fine</sub> are more susceptible to fracture, resulting in the liberation of dislocations at the interface. The reduction in α<sub>lath</sub> thickness is crucial for triggering the initiation of multi-system dislocations at the interface, which promotes the development of persistent slip bands (PSBs) and dislocation nets within α<sub>lath</sub>. This phenomenon induces inhomogeneous plastic deformation and localized hardening, fostering the formation of micro-voids and micro-cracks.https://www.mdpi.com/2075-4701/15/1/18TC21 alloymultilevel lamellar microstructurenotch tensile and high cycle fatiguedamage evolution mechanism |
| spellingShingle | Xiaosong Zhou Xiang Li Chaowen Huang Quan Wu Fei Zhao Notch Fatigue Damage Evolution Mechanism of TC21 Alloy with Multilevel Lamellar Microstructures Metals TC21 alloy multilevel lamellar microstructure notch tensile and high cycle fatigue damage evolution mechanism |
| title | Notch Fatigue Damage Evolution Mechanism of TC21 Alloy with Multilevel Lamellar Microstructures |
| title_full | Notch Fatigue Damage Evolution Mechanism of TC21 Alloy with Multilevel Lamellar Microstructures |
| title_fullStr | Notch Fatigue Damage Evolution Mechanism of TC21 Alloy with Multilevel Lamellar Microstructures |
| title_full_unstemmed | Notch Fatigue Damage Evolution Mechanism of TC21 Alloy with Multilevel Lamellar Microstructures |
| title_short | Notch Fatigue Damage Evolution Mechanism of TC21 Alloy with Multilevel Lamellar Microstructures |
| title_sort | notch fatigue damage evolution mechanism of tc21 alloy with multilevel lamellar microstructures |
| topic | TC21 alloy multilevel lamellar microstructure notch tensile and high cycle fatigue damage evolution mechanism |
| url | https://www.mdpi.com/2075-4701/15/1/18 |
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