首页> 外文会议>AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference >Composite Wind Turbine Blade Effects of Defects: Part B-Progressive Damage Modeling of Fiberglass/Epoxy Laminates with Manufacturing Induced Flaws
【24h】

Composite Wind Turbine Blade Effects of Defects: Part B-Progressive Damage Modeling of Fiberglass/Epoxy Laminates with Manufacturing Induced Flaws

机译:复合风力涡轮机叶片的缺陷效应:B部分-具有制造缺陷的玻璃纤维/环氧层压板的渐进式损伤建模

获取原文

摘要

The Effects of Defects is important for the reliability of modern composite wind turbine blades. The DOE has sponsored a comprehensive study to characterize common manufacturing defects and establish damage growth and validation tools to contribute to a wind turbine blade reliability infrastructure. To support this development of a reliability infrastructure, progressive damage modeling of blade representative coupons has been performed. Initial modeling efforts have been established and correlated to existing experimental results. Two types of analytical models have been investigated and developed with larger scale testing and analytical correlation in mind. A progressive damage routine utilizing combined maximum stress/maximum strain failure criteria was implemented allowing for different types of damage to be estimated. The material properties for damaged elements were then degraded for the appropriate damage mode and type. Two-dimensional (2D), four-layer coupon level models were utilized in increasing complexity from Controls to a flawed specimen containing an In-Plane Wave. Initial models were used to develop convergence in compression and tension before developing a model for an In-Plane Wave group. The results indicate that reasonable correlation was achieved between all groups and their respective experimental data. While some minor discrepancies exist, it appears that they will be an initial point for modeling of larger scale coupons or subsections.
机译:缺陷的影响对于现代复合材料风力涡轮机叶片的可靠性至关重要。 DOE赞助了一项全面研究,以表征常见的制造缺陷,并建立损伤增长和验证工具,从而为风力涡轮机叶片可靠性基础设施做出贡献。为了支持可靠性基础结构的这种发展,已经对叶片代表试样进行了渐进式损坏建模。初步的建模工作已经建立,并与现有的实验结果相关。已经研究和开发了两种类型的分析模型,其中考虑了大规模测试和分析相关性。利用组合的最大应力/最大应变破坏准则进行了渐进式破坏程序,可以估算出不同类型的破坏。然后,针对适当的损坏模式和类型,损坏元素的材料特性会降低。二维(2D),四层试片级别模型被用于增加从控件到包含平面波的有缺陷样本的复杂性。在为平面波组开发模型之前,使用初始模型来建立压缩和拉伸的收敛性。结果表明,所有组及其各自的实验数据之间均实现了合理的相关性。尽管存在一些细微的差异,但它们似乎将是对较大规模的优惠券或小节进行建模的起点。

著录项

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