复合材料科学与工程 ›› 2025, Vol. 0 ›› Issue (11): 48-54.DOI: 10.19936/j.cnki.2096-8000.20251128.006

• 基础与力学性能研究 • 上一篇    下一篇

大厚度蜂窝固化受压过程的精细结构仿真研究

舒沈云浩, 卢红龙, 轩立新   

  1. 航空工业济南特种结构研究所 高性能电磁窗航空科技重点实验室,济南 250023
  • 收稿日期:2024-08-15 出版日期:2025-11-28 发布日期:2025-12-24
  • 作者简介:舒沈云浩(1997—),男,硕士研究生,工程师,研究方向为民用飞机复合材料结构强度设计,shusyh@avic.com。

Investigations on large thickness honeycomb with curing pressure through a fine-structure numerical approach

SHU-SHEN Yunhao, LU Honglong, XUAN Lixin   

  1. Aviation Key Lab of Science and Technology on High Performance Electromagnetic Windows, Research Institute for Special Structure of Aeronautical Composite, AVIC, Jinan 250023, China
  • Received:2024-08-15 Online:2025-11-28 Published:2025-12-24

摘要: 为探究大厚度Nomex蜂窝在成型固化过程中出现的侧向变形滑移的问题,采用有限元分析方法对蜂窝精细结构进行建模和计算,并将计算结果与工艺试验结果对比。本文先对蜂窝平面压缩测试试验件进行精细结构建模,计算得到的蜂窝芯体的加载响应与试验结果相符且误差较小,可以证明使用2D壳单元对蜂窝格孔进行建模计算的可靠性与准确性。在此基础上建立蜂窝成型工艺试验件有限元模型,计算得到蜂窝芯体在成型固化过程中的局部力学响应,模拟出了蜂窝从格孔壁失稳屈曲到试验件边缘滑移的变化过程;与成型工艺试验结果对比,两者蜂窝变形趋势基本相符,证明该仿真模型可以为工艺试验及蜂窝芯稳定化选择提供参考。

关键词: 蜂窝夹芯结构, 芳纶纸蜂窝, 有限元分析, 固化过程, 蜂窝边缘塌陷, 复合材料

Abstract: To investigate the issue of lateral deformation and sliding of large thickness Nomex honeycomb in curing process, a fine-structure honeycomb finite element model was established and calculated, and the calculation results were compared with technological test results. The flatwise compression specimens of honeycomb were modeled first, and the calculation results indicated that the loading response is consistent with the experiment with a small error. It can prove the great accuracy of using 2D shell element to model the honeycomb cells. On this basis, a finite element model of the honeycomb forming technological specimens was established. After calculation, the local mechanical response of the honeycomb core in curing process was obtained and the transition from buckling of cells to sliding of specimens’ edges can be simulated. Compared with the technological test results, the deformation trend of honeycomb is basically consistent. Therefore, the fine-structure simulation model can provide a reference for technological test and the selection of honeycomb stabilization methods.

Key words: honeycomb sandwich, Nomex honeycomb, finite element analysis (FEA), curing process, honeycomb edge depression, composites

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