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基于碳纤维增强聚合物的雷电损伤因素有限元分析

Finite Element Analysis of Lightning Damage Factors Based on Carbon Fiber Reinforced Polymer.

作者信息

Zhu Yansong, Ming Yueke, Wang Ben, Duan Yugang, Xiao Hong, Zhang Chenping, Sun Jinru, Tian Xiangyu

机构信息

State Key Laboratory for Manufacturing Systems Engineering, Xi'an Jiaotong University, Xi'an 710049, China.

State Key Laboratory of Electrical Insulation and Power Equipment, Xi'an Jiaotong University, Xi'an 710049, China.

出版信息

Materials (Basel). 2021 Sep 10;14(18):5210. doi: 10.3390/ma14185210.

Abstract

While carbon-fiber-reinforced polymers (CFRPs) are widely used in the aerospace industry, they are not able to disperse current from lightning strikes because their conductivity is relatively low compared to metallic materials. As such, the undispersed current can cause the vaporization or delamination of the composites, threatening aircraft safety. In this paper, finite element models of lightning damage to CFRPs were established using commercial finite element analysis software, Abaqus, with the user-defined subroutines USDFLD and HEAVEL. The influences of factors such as the structural geometry, laminate sequence, and intrinsic properties of CFRPs on the degree of damage to the composites are further discussed. The results showed that when a current from lightning is applied to the CFRP surface, it mainly disperses along the fiber direction in the outermost layer. As the length of the CFRP increases, the injected current has a longer residence time in the material due to the increased current exporting distance. Consequently, larger amounts of current accumulate on the surface, eventually leading to more severe damage to the CFRP. This damage can be alleviated by increasing the thickness of the CFRP, as the greater overall resistance makes the CFRP a better insulator against the imposed current. This study also found that the damaged area increased as the angle between the first two layers increased, whereas the depth of the damage decreased due to the current dispersion between the first two layers. The analysis of the electrical conductivity of the composite suggested that damage in the fiber direction will be markedly reduced if the conductivity in the vertical fiber direction increases approximately up to the conductivity of the fiber direction. Moreover, increasing the thermal conductivity along the fiber direction will accelerate the heat dissipation process after the lightning strike, but the influence of the improved thermal conductivity on the extent of the lightning damage is less significant than that of the electrical conductivity.

摘要

虽然碳纤维增强聚合物(CFRP)在航空航天工业中广泛应用,但由于其导电性与金属材料相比相对较低,无法分散雷击产生的电流。因此,未分散的电流会导致复合材料汽化或分层,威胁飞机安全。本文利用商业有限元分析软件Abaqus以及用户自定义子程序USDFLD和HEAVEL建立了CFRP雷击损伤的有限元模型。进一步讨论了结构几何形状、层合顺序和CFRP固有特性等因素对复合材料损伤程度的影响。结果表明,当雷击电流施加到CFRP表面时,它主要在最外层沿纤维方向分散。随着CFRP长度的增加,由于电流输出距离增加,注入的电流在材料中的停留时间更长。因此,更多的电流积聚在表面,最终导致CFRP受到更严重的损伤。通过增加CFRP的厚度可以减轻这种损伤,因为更大的总电阻使CFRP成为更好的抗施加电流的绝缘体。本研究还发现,随着前两层之间夹角的增加,损伤面积增大,而损伤深度由于前两层之间的电流分散而减小。对复合材料电导率的分析表明,如果垂直于纤维方向的电导率增加到接近纤维方向的电导率,纤维方向的损伤将显著减少。此外,沿纤维方向增加热导率将加速雷击后的散热过程,但热导率改善对雷击损伤程度的影响不如电导率显著。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/5b4a/8467610/1168bb11afa4/materials-14-05210-g001.jpg

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