Effects of lightning strike on damage of aeronautical carbon fiber reinforced plastic

被引：0

作者：

Zhang B. ^{[1
,2
]}

Chen X.-N. ^{[2
]}

Huang L.-Y. ^{[2
]}

Gu C.-C. ^{[2
]}

机构：

[1] Armored Equipment Department, Armored Force Academy of Chinese People's Liberation Army, Bengbu, 233000, Anhui

[2] Power and Intelligent Research Center, Chinese People's Liberation Army University of Science and Technology, Nanjing

来源：

Cailiao Gongcheng/Journal of Materials Engineering | 2016年 / 44卷 / 12期

关键词：

Action integral; CFRP; Coupled thermal-electric analysis; Injury; Lightning strike;

D O I：

10.11868/j.issn.1001-4381.2016.12.015

中图分类号：

学科分类号：

摘要：

The thermal-electric finite element simulation model of carbon fiber reinforced plastic(CFRP) damage caused by lightning strike was established. The superimposed temperature was treated as the internal injury. The accuracy and effectiveness of coupled thermal-electric simulation method were verified by comparing with the experimental results. The regression analysis was taken into consideration to give a quantitative analysis of lightning parameters and CFRP lightning damage, and the relevant curves were drawn. The results show that action integral is a key factor in determining the injury status of CFRP laminates. Fiber damage area and delamination area have a linear relationship with the action integral. And resin damage area and damage thickness have a logarithmic relation with the action integral. © 2016, Journal of Materials Engineering. All right reserved.

引用

页码：92 / 99

页数：7

共 17 条

[1]

Yan M.G., Wu X.R., Zhu Z.S., Et al., Recent progress and prospects for aeronautical material technologies, Aeronautical Manufacturing Technology, 12, pp. 19-25, (2003)

[2]

Uman M.A., Rakov V.A., The interaction of lightning with airborne vehicles, Progress in Aerospace Sciences, 39, 1, pp. 61-81, (2003)

[3]

Yang N.B., Liang W., Introduction of the Design of Large Aircraft Composite Structures, pp. 11-16, (2009)

[4]

Horvath T., Understanding Lightning and Lightning Protection:A Multimedia Teaching Guide, (2006)

[5]

Welch J.M., Repair design, test, and process considerations for lightning strikes, 3rd F-AA/EASA/Boeing/Airbus Joint Workshop on and Certification, (2007)

[6]

Yamanakay J., Japan airlines perspective on application and field experiences for composite structure, 4th FAA/EASA/Boeing/Airbus Joint Workshop on and Certification, (2009)

[7]

Nakayama N., Field experience:lightning strike damage of ANA B767, 4th FAA/EASA/Boeing/Airbus Joint Workshop on and Certification, (2009)

[8]

Hirano Y., Katsumata S., Iwahori Y., Et al., Articial lightning testing on graphite/epoxy composite laminate, Composites:Part A, 41, 10, pp. 1461-1470, (2010)

[9]

Feraboli P., Miller M., Damage resistance and tolerance of carbon/epoxy composite coupons subjected to simulated lighting strike, Composite Part A:Applied Science and Manufacturing, 40, 6-7, pp. 954-967, (2009)

[10]

Ding N., Zhao B., Liu Z.Q., Et al., Simulation of ablation damage of composite laminates subjected to lightning strike, Acta Aeronautica et Astronautica Sinica, 34, 2, pp. 301-308, (2013)

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