Gradient residual stress evolution and its influence on fatigue life under combined carburising heat treatment and ultrasonic surface rolling process
•Carburizing heat treatment (CHT) combined with ultrasonic surface rolling process (USRP) were introduced to improve the rotary-bending fatigue behavior.•Rotary-bending fatigue life and surface integrity were improved after combined treatment (CHT + USRP).•The mechanism of gradient compressive resid...
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| Veröffentlicht in: | Engineering fracture mechanics Jg. 308; S. 110315 |
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| Hauptverfasser: | , , , , , |
| Format: | Journal Article |
| Sprache: | Englisch |
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20.09.2024
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| ISSN: | 0013-7944 |
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| Abstract | •Carburizing heat treatment (CHT) combined with ultrasonic surface rolling process (USRP) were introduced to improve the rotary-bending fatigue behavior.•Rotary-bending fatigue life and surface integrity were improved after combined treatment (CHT + USRP).•The mechanism of gradient compressive residual stress (CRS) evolution affecting fatigue was revealed.•Two stages of gradient CRS relaxation were identified by the Kodama model.
This study combined carburising heat treatment (CHT) with the ultrasonic surface rolling process (USRP) to improve the rotary bending fatigue properties of 18CrNiMo7-6 alloy steel. Based on the experimentally obtained fatigue limit (σ-1), the evolution of gradient compressive residual stress (CRS) of CHT- and CHT + USRP-treated specimens was analysed below the fatigue limit stress level. Subsequently, the evolution mechanism of gradient CRS of the two reinforced specimens was discussed and analysed from the opposing effects of austenite transformation and dislocation density change on the evolution of CRS. The results demonstrated that the selective bending fatigue performance of the alloy was evidently improved after the introduction of CRS; however, the change in fatigue limit was not evident. The durability under other loads (such as cyclic tension/compression and torsion loads) needs further study. The gradient CRS evolution of CHT specimens was mainly caused by the large residual austenite transformation and small dislocation density change. Therefore, the volume expansion caused by residual austenite transformation gradually increased the gradient compression residual stress of CHT specimens with an increased number of cycles. Contrarily, the degree residual stress evolution of CHT + USRP specimens was more affected by the dislocation density, and the gradient compression residual stress gradually decreased with an increased number of cycles. Finally, the residual stress evolution rate of the two reinforced specimens was divided into two stages: fast and slow. |
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| AbstractList | •Carburizing heat treatment (CHT) combined with ultrasonic surface rolling process (USRP) were introduced to improve the rotary-bending fatigue behavior.•Rotary-bending fatigue life and surface integrity were improved after combined treatment (CHT + USRP).•The mechanism of gradient compressive residual stress (CRS) evolution affecting fatigue was revealed.•Two stages of gradient CRS relaxation were identified by the Kodama model.
This study combined carburising heat treatment (CHT) with the ultrasonic surface rolling process (USRP) to improve the rotary bending fatigue properties of 18CrNiMo7-6 alloy steel. Based on the experimentally obtained fatigue limit (σ-1), the evolution of gradient compressive residual stress (CRS) of CHT- and CHT + USRP-treated specimens was analysed below the fatigue limit stress level. Subsequently, the evolution mechanism of gradient CRS of the two reinforced specimens was discussed and analysed from the opposing effects of austenite transformation and dislocation density change on the evolution of CRS. The results demonstrated that the selective bending fatigue performance of the alloy was evidently improved after the introduction of CRS; however, the change in fatigue limit was not evident. The durability under other loads (such as cyclic tension/compression and torsion loads) needs further study. The gradient CRS evolution of CHT specimens was mainly caused by the large residual austenite transformation and small dislocation density change. Therefore, the volume expansion caused by residual austenite transformation gradually increased the gradient compression residual stress of CHT specimens with an increased number of cycles. Contrarily, the degree residual stress evolution of CHT + USRP specimens was more affected by the dislocation density, and the gradient compression residual stress gradually decreased with an increased number of cycles. Finally, the residual stress evolution rate of the two reinforced specimens was divided into two stages: fast and slow. |
| ArticleNumber | 110315 |
| Author | Xu, Guangtao Wang, Gang Zhang, Yue Peng, Zhenlong Zhao, Minghao Hou, Xiaofan |
| Author_xml | – sequence: 1 givenname: Gang surname: Wang fullname: Wang, Gang organization: School of Mechanical and Power Engineering, Zhengzhou University, Zhengzhou, Henan 450001, China – sequence: 2 givenname: Xiaofan surname: Hou fullname: Hou, Xiaofan organization: School of Mechanical and Power Engineering, Zhengzhou University, Zhengzhou, Henan 450001, China – sequence: 3 givenname: Yue surname: Zhang fullname: Zhang, Yue organization: School of Mechanical and Power Engineering, Zhengzhou University, Zhengzhou, Henan 450001, China – sequence: 4 givenname: Zhenlong surname: Peng fullname: Peng, Zhenlong email: pengzl@zzu.edu.cn organization: School of Mechanical and Power Engineering, Zhengzhou University, Zhengzhou, Henan 450001, China – sequence: 5 givenname: Guangtao surname: Xu fullname: Xu, Guangtao organization: School of Mechanical and Power Engineering, Zhengzhou University, Zhengzhou, Henan 450001, China – sequence: 6 givenname: Minghao surname: Zhao fullname: Zhao, Minghao organization: School of Mechanical and Power Engineering, Zhengzhou University, Zhengzhou, Henan 450001, China |
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| CitedBy_id | crossref_primary_10_1007_s00170_024_14608_2 crossref_primary_10_1016_j_msea_2025_148992 crossref_primary_10_1021_acsami_4c22686 crossref_primary_10_1002_adem_202402045 crossref_primary_10_1007_s11665_025_11955_3 crossref_primary_10_1016_j_ijfatigue_2025_109269 crossref_primary_10_1111_ffe_14685 crossref_primary_10_1557_s43578_025_01638_z crossref_primary_10_1016_j_ijfatigue_2025_108993 crossref_primary_10_1016_j_rineng_2025_105938 |
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| Keywords | Fatigue Ultrasonic surface rolling process Evolution mechanism Carburising heat treatment Gradient residual stress evolution |
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