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Analysis of Maximum Crack Opening Displacement of Turbine Disk Cracks Under Low Cycle Fatigue Load

  • Xi'an Jiaotong University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Fatigue crack initiation and growth of turbine disks often cause catastrophic damage to the aircraft, it is essential to study the failure mechanism and feature extraction of the crack for turbine disks. This paper presents a methodology to calculate the maximum crack opening displacement (MCOD) of turbine discs subjected to low cycle fatigue. Initially, the variations of the MCOD with rotational speed during cyclic loading were studied. Subsequently, the finite element method was employed to verify the results and establish the correlation between the MCOD and rotational speed. A functional correlation between the variation of the MCOD and the rotational speed change under cyclic loading was developed.

源语言英语
主期刊名ICSMD 2024 - 5th International Conference on Sensing, Measurement and Data Analytics in the Era of Artificial Intelligence
出版商Institute of Electrical and Electronics Engineers Inc.
ISBN(电子版)9798331529192
DOI
出版状态已出版 - 2024
活动5th International Conference on Sensing, Measurement and Data Analytics in the Era of Artificial Intelligence, ICSMD 2024 - Huangshan, 中国
期限: 31 10月 20243 11月 2024

丛书

姓名ICSMD 2024 - 5th International Conference on Sensing, Measurement and Data Analytics in the Era of Artificial Intelligence

会议

会议5th International Conference on Sensing, Measurement and Data Analytics in the Era of Artificial Intelligence, ICSMD 2024
国家/地区中国
Huangshan
时期31/10/243/11/24

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