基于电阻法的碳纤维断裂损伤识别研究#br#

摘要/Abstract

摘要： 利用电阻法识别拉伸状态下碳纤维增强树脂基复合材料内部纤维的断裂情况，为实现飞机复合材料结构的在线健康监控进行初步的理论探索。针对T800 型碳纤维单向铺层的复合材料层合板试件[0]8 进行通电状态下的拉伸试验和有限元仿真模拟。结果表明，电阻法可较好地反映纤维断裂情况，同时给出电阻法识别T800 型纤维断裂的判断依据：在电阻变化率ΔR/R0 达到0.25 前，纤维仅发生弹性变形；在ΔR/R0 达到0.25 时，纤维出现断裂；在ΔR/R0 达到3.5 时，纤维损伤严重。

关键词: 碳纤维, 复合材料, 电阻法, 有限元分析

Abstract: Electrical resistance method is used to identify the internal fiber fracture of CFRP under tension. A preliminary theoretical exploration is carried out to realize on-line health monitoring on aircraft composite structure. Energized tension test and finite element simulation are conducted aiming at the unidirectional laminate [0]8 of T800 carbon fiber. It is proven that the electrical resistance method can soundly reflect fiber fracture. The judging standard of T800 fiber fracture by electrical resistance method is given: before resistance changing rate ΔR/R0 reaches 0.25, only fiber elastically deformation occurs; when ΔR/R0 reaches 0.25, fiber breaks; when ΔR/R0 reaches 3.5, the serious fiber damage occurs.

Key words: carbon fiber, composite, electrical method, finite element analysis

中图分类号:

卢翔, 赵振耀, 蔺越国, 贾宝惠. 基于电阻法的碳纤维断裂损伤识别研究#br#[J]. 中国民航大学学报, 2019, 37(3): 60-64.

LU Xiang, ZHAO Zhenyao, LIN Yueguo, JIA Baohui. Carbon fiber fracture recognition based on electrical resistance method#br#[J]. Journal of Civil Aviation University of China, 2019, 37(3): 60-64.

参考文献 12

[1]	沈观林,胡更开,刘彬.复合材料力学[M]. 2 版. 北京: 清华大学出版社, 2013.
[2]	PARK J B, OKABE T, TAKEDA N. New concept for modeling the electromechanical behavior of unidirectional carbon-fiber-reinforced plastic under tensile loading[J]. Smart Materials and Structures，2003, 12(1): 105-114.
[3]	GIGLIOTTI M, LAFARIE-FRENOT M C, LIN YUEGUO, et al. Electro-mechanical fatigue of CFRP laminates for aircraft applications [J].Composite Structures, 2015, 127(1): 436-449.
[4]	GIGLIOTTI M. Development of experimental and modelling tools for the characterisation of the thermo-electro-mechanical behaviour of composite materials for, aircraft applications[J]. Mécanique & Industries,2011, 12(2): 87-101.
[5]	VAVOULIOTIS A, PAIPETIS A, KOSTOPOULOS V. On the fatigue life prediction of CFRP laminates using the electrical resistance change method[J]. Composites Science & Technology, 2011, 71(5): 630-642.
[6]	B魻HRK H, LESCHINSKI P, REIMER T. Electrical resistivity measurement of carbon-fiber-reinforced ceramic matrix composite under thermomechanical load[J]. Composites Science & Technology, 2013, 76(4): 1-7.
[7]	SUJIDKUL T, XIA ZHENHAI. Coupled thermal-mechanical modeling of carbon fibers reinforced polymer composites for damage detection[J].Composites Part B: Engineering, 2012, 43(3): 1631-1636.
[8]	TODOROKI A, TANAKA M, SHIMAMURA Y. Measurement of orthotropic electric conductance of CFRP laminates and analysis of the effect on delamination monitoring with an electric resistance change method[J]. Composites Science & Technology, 2002, 62(5): 619-628.
[9]	PARK J B, OKABE T, TAKEDA N, et al. Electromechanical modeling of unidirectional CFRP composites under tensile loading congdition[J].Composites Part A: Applied Science and Manufacturing, 2002, 33 (2):
26	7-275.
[10]	XIA ZHENHAI， OKABE T, PARK J B, et al. Quantitative damage detection in CFRP composites: Coupled mechanical and electrical models
[J]	Composites Science and Technology, 2003, 63(10): 1411-1422.
[11]	SWAIT T J, JONES F R, HAYES S A. A practical structural health monitoring system for carbon fibre reinforced composite based on electrical esistance[J]. Composites Science & Technology, 2012, 72(13):
15	15-1523.
[12]	姚武, 王瑞卿. 基于隧道效应的CFRC 材料的导电模型[J]. 复合材料学报, 2006, 23(5): 121-125.

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