首页> 外文期刊>航空太空及民航學刊, B >Structural Optimization of the Fiber-Reinforced Composite Sandwich Plate with a Honeycombed Core
【24h】

Structural Optimization of the Fiber-Reinforced Composite Sandwich Plate with a Honeycombed Core

机译:蜂窝芯纤维增强复合材料夹芯板的结构优化

获取原文
获取原文并翻译 | 示例
获取外文期刊封面目录资料

摘要

Recently, the design concepts of sandwich structures have been changed because of the improvements of materials and their manufacturing technology. Fiber-reinforced composites are adopted to make the bilateral faceplates of the sandwich structure instead of using conventional materials, while the honeycombed structures are widely used as the core layer instead of applying solid or other forms of structures. This study concerns with the optimal design of the fiber-reinforced sandwich plate with a honeycombed core with regard to the constraints of the structural buckling strength and the failure strength of the composite sandwich plate under axial compression. The objective is to determine the optimal configuration parameters of the fiber-reinforced sandwich plate with a honeycombed core. The configuration parameters include the thickness of the faceplates, the angle that the laminated fiber is arranged within the faceplate, and the geometric characteristics of the honeycombed core structure, which are including the thickness of the cell wall and the diameter of the cell. Besides, the evaluation will be done with regard to the influence of the parameter design on the fiber-reinforced composite sandwich plate with a honeycombed core.
机译:近来,由于材料及其制造技术的改进,三明治结构的设计概念已经改变。纤维增强复合材料被用来代替传统材料来制造夹层结构的两侧面板,而蜂窝结构被广泛用作芯层,而不是应用固体或其他形式的结构。这项研究涉及到蜂窝增强纤维夹芯板的优化设计,该结构考虑了复合夹芯板在轴向压缩下的结构屈曲强度和破坏强度。目的是确定具有蜂窝状芯的纤维增强夹芯板的最佳配置参数。构造参数包括面板的厚度,层压纤维在面板内的排列角度以及蜂窝状芯结构的几何特性,其中包括孔壁的厚度和孔的直径。此外,将评估参数设计对蜂窝芯纤维增强复合材料夹心板的影响。

著录项

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