考虑过载迟滞的风电塔节点疲劳性能评估方法

唐骁; 熊川楠; 常颖; 罗宇骁; 王健泽; 戴靠山

doi:doi:10.19912/j.0254-0096.tynxb.2024-2088

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考虑过载迟滞的风电塔节点疲劳性能评估方法

更新时间：2026-07-22

- 考虑过载迟滞的风电塔节点疲劳性能评估方法
- 考虑过载迟滞的风电塔节点疲劳性能评估方法
- 太阳能学报 2026年47卷第4期页码：231-239
- 作者机构：
- 作者简介：
- 基金信息：
  
  国家自然科学基金（52308186;52278512）;四川省科技计划（2023ZHJY0012）;中国博士后科学基金（2023M742501）
- DOI：doi:10.19912/j.0254-0096.tynxb.2024-2088
  中图分类号： U467
- 网络首发：2026-05-08，
  
  纸质出版：2026
- 稿件说明：
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唐骁, 熊川楠, 常颖, 等. 考虑过载迟滞的风电塔节点疲劳性能评估方法[J]. 太阳能学报, 2026,47(4):231-239.

唐骁, 熊川楠, 常颖, et al. 考虑过载迟滞的风电塔节点疲劳性能评估方法[J]. 2026, 47(4): 231-239.
唐骁, 熊川楠, 常颖, 等. 考虑过载迟滞的风电塔节点疲劳性能评估方法[J]. 太阳能学报, 2026,47(4):231-239. DOI： doi:10.19912/j.0254-0096.tynxb.2024-2088.

唐骁, 熊川楠, 常颖, et al. 考虑过载迟滞的风电塔节点疲劳性能评估方法[J]. 2026, 47(4): 231-239. DOI： doi:10.19912/j.0254-0096.tynxb.2024-2088.

摘要

该文构建一个考虑迟滞效应的风电塔螺栓节点裂纹扩展迟滞模型

并结合有限元建模进行疲劳分析。首先

通过有限元分析

揭示了M20高强螺栓的第一啮合螺纹根部应力集中系数最高

达到4.80

相应的疲劳缺口系数为4.61。进一步利用裂纹迟滞模型分析表明

考虑迟滞效应的裂纹扩展速率显著降低

在30、55、80 MPa应力幅作用下

疲劳失效寿命的差异至少为27.8%。此外

关键参数分析结果表明

应力比增大、迟滞因子计算指数减小以及过载比降低均会加速疲劳失效进程。

Abstract

This study aims to develop a crack growth retardation model for wind turbine tower bolt joints

incorporating retardation effects

and to perform a fatigue analysis through finite element modeling. Firstly

through finite element analysis

the study reveals that the stress concentration factor at the first engagement thread root of M20 high-strength bolts is highest

reaching 4.80

with the corresponding fatigue notch factor being 4.61. Further analysis using the crack growth retardation model shows that the crack growth rate considering retardation effects is significantly reduced. Under stress ranges of 30

and 80 MPa

the difference in fatigue failure life is at least 27.8%. Additionally

the key parameter analysis results indicate that an increase in stress ratio

a decrease in retardation factor calculation exponent

and a reduction in overload ratio all accelerate the fatigue failure process.

关键词

Keywords

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