Fatigue assessment of directionally solidified superalloy thin plates under bimodal random processes
•The fatigue performance of DZ125L alloy under bimodal random processes was studied.•The distribution of fatigue damage in bimodal random processes was analyzed.•The bimodal random vibration fatigue crack propagation mechanism was proposed.•The proposed new model is more suitable for the life predic...
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Published in | Thin-walled structures Vol. 205; p. 112411 |
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Main Authors | , , , , , |
Format | Journal Article |
Language | English |
Published |
Elsevier Ltd
01.12.2024
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Online Access | Get full text |
ISSN | 0263-8231 |
DOI | 10.1016/j.tws.2024.112411 |
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Abstract | •The fatigue performance of DZ125L alloy under bimodal random processes was studied.•The distribution of fatigue damage in bimodal random processes was analyzed.•The bimodal random vibration fatigue crack propagation mechanism was proposed.•The proposed new model is more suitable for the life prediction of bimodal processes.
During actual service, aviation aircraft often experience multiple complex alternating loads coupled with each other. If the frequency range of the excitation load spectrum covers the first two resonance frequencies of the structure, it can significantly impact the vibration fatigue life of the structure. In this study, bimodal random vibration fatigue tests were conducted on thin plates composed of DZ125L directionally solidified superalloy. The impact of low-frequency and high-frequency vibration signal intensities on the vibration fatigue behavior of DZ125L alloy thin plates was investigated separately during bimodal random processes. The crack propagation mechanism of bimodal random vibration fatigue was proposed based on the fracture morphology observed in DZ125L alloy thin plates that failed due to vibration fatigue. The study findings indicate that the number and location of crack initiation zones can influence the mechanism of fatigue crack propagation. Additionally, a new model was developed in this study to enhance the sensitivity of the frequency domain method to the intensity of low-frequency and high-frequency vibration signals in bimodal random processes. Compared to traditional frequency domain methods used for broadband and bimodal processes, the new model can effectively describe the variation characteristics of bimodal fatigue life with different component process intensities. Furthermore, it has broader applicability for predicting the vibration fatigue life of bimodal random processes with varying vibration signal intensities. |
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AbstractList | •The fatigue performance of DZ125L alloy under bimodal random processes was studied.•The distribution of fatigue damage in bimodal random processes was analyzed.•The bimodal random vibration fatigue crack propagation mechanism was proposed.•The proposed new model is more suitable for the life prediction of bimodal processes.
During actual service, aviation aircraft often experience multiple complex alternating loads coupled with each other. If the frequency range of the excitation load spectrum covers the first two resonance frequencies of the structure, it can significantly impact the vibration fatigue life of the structure. In this study, bimodal random vibration fatigue tests were conducted on thin plates composed of DZ125L directionally solidified superalloy. The impact of low-frequency and high-frequency vibration signal intensities on the vibration fatigue behavior of DZ125L alloy thin plates was investigated separately during bimodal random processes. The crack propagation mechanism of bimodal random vibration fatigue was proposed based on the fracture morphology observed in DZ125L alloy thin plates that failed due to vibration fatigue. The study findings indicate that the number and location of crack initiation zones can influence the mechanism of fatigue crack propagation. Additionally, a new model was developed in this study to enhance the sensitivity of the frequency domain method to the intensity of low-frequency and high-frequency vibration signals in bimodal random processes. Compared to traditional frequency domain methods used for broadband and bimodal processes, the new model can effectively describe the variation characteristics of bimodal fatigue life with different component process intensities. Furthermore, it has broader applicability for predicting the vibration fatigue life of bimodal random processes with varying vibration signal intensities. |
ArticleNumber | 112411 |
Author | Yue, Zhufeng Wang, Jundong Lu, Hao Wen, Zhixun Lian, Yeda Yang, Leike |
Author_xml | – sequence: 1 givenname: Hao orcidid: 0000-0001-8648-2693 surname: Lu fullname: Lu, Hao organization: School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, PR China – sequence: 2 givenname: Yeda surname: Lian fullname: Lian, Yeda email: lianyeda@nwpu.edu.cn organization: School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, PR China – sequence: 3 givenname: Jundong surname: Wang fullname: Wang, Jundong email: wangjundong@nwpu.edu.cn organization: School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, PR China – sequence: 4 givenname: Zhixun surname: Wen fullname: Wen, Zhixun organization: School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, PR China – sequence: 5 givenname: Leike surname: Yang fullname: Yang, Leike organization: School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, PR China – sequence: 6 givenname: Zhufeng surname: Yue fullname: Yue, Zhufeng organization: School of Mechanics, Civil Engineering and Architecture, Northwestern Polytechnical University, Xi'an 710072, PR China |
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Cites_doi | 10.1002/j.1538-7305.1944.tb00874.x 10.1016/j.oceaneng.2018.07.033 10.1016/S0142-1123(02)00032-4 10.1016/j.ymssp.2024.111519 10.1111/j.1460-2695.2012.01693.x 10.1016/0142-1123(92)90088-T 10.1016/j.oceaneng.2013.11.002 10.1016/j.ijfatigue.2023.107540 10.1016/j.ijfatigue.2019.02.031 10.1016/j.ijnaoe.2020.09.005 10.1016/j.ijfatigue.2004.10.007 10.1016/j.ijfatigue.2006.03.013 10.1108/RPJ-12-2011-0133 10.3901/JME.2021.22.052 10.1016/j.marstruc.2014.06.005 10.1016/j.ijfatigue.2016.12.017 10.1111/j.1460-2695.2004.00847.x 10.1016/j.probengmech.2012.12.002 10.1016/j.matdes.2018.04.032 10.1016/j.apor.2024.104039 10.1016/j.ijfatigue.2012.07.005 10.1016/j.ijfatigue.2020.105730 10.1016/j.ijfatigue.2023.107930 10.1016/j.oceaneng.2008.01.001 10.1016/j.tws.2023.111287 10.1016/j.ijfatigue.2017.02.005 10.1016/j.tws.2020.107218 10.1016/j.ijfatigue.2016.04.012 10.1016/0266-8920(90)90010-H 10.1016/j.engfracmech.2023.109184 10.1115/1.4009458 10.1016/j.tws.2024.111891 10.1061/JSDEAG.0005477 10.1016/j.ijfatigue.2023.107746 10.1016/j.ymssp.2023.110149 10.1016/j.ijfatigue.2016.10.006 10.1016/j.matdes.2014.04.059 10.1016/j.ceramint.2021.12.041 10.1016/S0142-1123(99)00113-9 10.1016/j.ijfatigue.2021.106152 10.1016/j.apor.2016.08.007 10.1007/s12540-018-0073-z 10.1016/j.ijfatigue.2004.09.004 10.1061/(ASCE)0733-9445(1990)116:4(1149) |
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Keywords | Life prediction Directionally solidified superalloy Frequency domain method Vibration fatigue Bimodal random process |
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SubjectTerms | Bimodal random process Directionally solidified superalloy Frequency domain method Life prediction Vibration fatigue |
Title | Fatigue assessment of directionally solidified superalloy thin plates under bimodal random processes |
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