首页> 外文OA文献 >Different failure modes assessment to improve the sandwich composite panel stiffness with honeycomb core for marine structures application
【2h】

Different failure modes assessment to improve the sandwich composite panel stiffness with honeycomb core for marine structures application

机译:评估不同的破坏模式,以改善蜂窝结构夹芯复合板的刚度,以用于海洋结构

摘要

This research paper focuses on the prediction of different failure modes to improve the sandwich composite panel with honeycomb core for application in marine structures. Marine, automotive and aerospace industries are continually trying to optimize material performance in terms of strength and weight. Success has been achieved through the growth of high performance materials, including fibrous composites such as ceramics, new alloys, and carbon fiber composites and through the use of structural concepts such as sandwich composite panel construction. Sandwich composite panel construction with honeycomb core consists of three components: two facing sheets, the core that fill the space between the facing sheet and the core-to-facing bonding adhesives. The facing sheets of a sandwich panel can be compared to the flanges of an I-beam element, as they carry the bending stresses to which the beam is subjected. With one facing sheet in compression, the other is in tension. Similarly the honeycomb core corresponds to the web of the I-beam that resists the shear loads and vertical compressive load to the face sheet. This paper presents a model for prediction of different failure mode of face sheet and core material. The obtained results of this model were compared with experimental results and presents that it is a simple and good model.
机译:本文的研究重点是对不同破坏模式的预测,以改进蜂窝结构夹芯复合板在海洋结构中的应用。船舶,汽车和航空航天工业一直在努力在强度和重量方面优化材料性能。通过包括纤维复合材料(例如陶瓷,新合金和碳纤维复合材料)在内的高性能材料的发展以及通过使用结构概念(例如夹心复合材料面板结构),已经取得了成功。具有蜂窝状芯的夹心复合板结构由三个组件组成:两个饰面板,填充饰面板之间空间的芯和芯对面粘合胶。可以将夹心板的面板与工字梁元件的法兰进行比较,因为它们承受梁承受的弯曲应力。当一个饰面板处于压缩状态时,另一个处于张紧状态。类似地,蜂窝芯对应于工字梁的腹板,该腹板抵抗剪切载荷和面板的垂直压缩载荷。本文提出了一种预测面板和芯材不同失效模式的模型。将该模型获得的结果与实验结果进行比较,表明它是一个简单而良好的模型。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利

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