...
首页> 外文期刊>Renewable energy >Assessing progressive failure in long wind turbine blades under quasi-static and cyclic loads
【24h】

Assessing progressive failure in long wind turbine blades under quasi-static and cyclic loads

机译:评估长风力涡轮机叶片在准静态和周期性载荷下的渐进式故障

获取原文
获取原文并翻译 | 示例
           

摘要

Predicting progressive failure and consequential loss in the load-bearing capability of large-scale composite wind blades is vital for accurately assessing their service life and maintenance. A physics-based multi-scale damage model describing progressive ply cracking and joint adhesive debonding in blades under both quasi-static and cyclic loading is presented. The complete structure of the blade was considered including the shell-spar adhesive joint and shell-root adhesive joint. For quasi-static loading, the geometrical transition region of the blade was observed as the critical ply crack damage region, which was in agreement with previous experimental results. The matrix micro-cracking damage was mainly caused by high gale wind speeds, and adhesive debonding ultimately initiated at the shell-spar joint. The blade tip deflection increased nonlinearly with increasing wind speeds, reaching 29.0% of the blade length at 19 mis. For cyclic loading, sub-critical damage grew along the length of the blade with increasing cycles, gradually increasing the normal and shear stresses in the joint adhesive layer as the crack density increased, eventually leading to local shell-spar adhesive debonding. The simulation methodology presented here will be useful for assessing the durability and increasing the safety and accuracy of service life prediction of large-scale blade structures. (C) 2017 Elsevier Ltd. All rights reserved.
机译:预测大型复合材料风叶片的渐进式故障和相应的承载能力损失对于准确评估其使用寿命和维护至关重要。提出了一种基于物理的多尺度损伤模型,该模型描述了叶片在准静态和循环载荷下的渐进式层裂和接头胶粘剂的脱粘现象。考虑到叶片的完整结构,包括壳梁翼梁粘结接头和壳根粘结接头。对于准静态载荷,叶片的几何过渡区域被视为临界层裂纹损坏区域,这与先前的实验结果一致。基体的微裂纹损坏主要是由于高风速引起的,并且粘合剂脱粘最终在壳梁连接处开始。叶片尖端挠度随风速的增加而非线性增加,在19 mis时达到叶片长度的29.0%。对于循环载荷,随着裂纹周期的增加,亚临界损伤沿着叶片的长度增加,随着裂纹密度的增加,接合粘合剂层的法向应力和剪切应力逐渐增加,最终导致局部壳梁胶粘剂剥离。此处介绍的模拟方法将有助于评估大型叶片结构的耐用性并提高使用寿命预测的安全性和准确性。 (C)2017 Elsevier Ltd.保留所有权利。

著录项

  • 来源
    《Renewable energy》 |2018年第4期|754-766|共13页
  • 作者单位

    Northwestern Polytech Univ, Dept Mech Engn, 127 Youyi Ave West, Xian 710072, Shaanxi, Peoples R China;

    Univ Waterloo, Mech & Mechatron Engn, 200 Univ Ave West, Waterloo, ON N2L 3G1, Canada;

    Univ Toronto, Dept Mat Sci & Engn, 184 Coll St,Suite 140, Toronto, ON M5S 3E4, Canada;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Wind turbine blade; Multi-scale model; CZM; Fatigue progressive failure;

    机译:风力发电机叶片;多尺度模型;CZM;疲劳渐进破坏;

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号