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复合材料蜂窝夹芯结构低速冲击位置识别研究
引用本文:赵林虎,周丽. 复合材料蜂窝夹芯结构低速冲击位置识别研究[J]. 振动与冲击, 2012, 31(2): 67-71,108. DOI:  
作者姓名:赵林虎  周丽
作者单位:南京航空航天大学,飞行器结构力学与控制教育部重点实验室,结构强度研究所,南京 210016
基金项目:国家自然科学基金(10572058);航空基金(2008ZA52012);博士学科点专项科研基金(20050287016)
摘    要:
进行了碳纤维增强复合材料蜂窝夹芯结构的低速冲击实验,采用一种基于应力波和免疫遗传算法的冲击载荷定位方法对蜂窝夹芯结构上的低速冲击载荷进行分析和定位。首先,通过一组事先确定冲击位置的低速冲击载荷产生的冲击应力波实验数据,使用小波变换方法对其在时频域进行分析,获得多个频率上冲击应力波在蜂窝夹芯结构中的传播速度;然后在此基础上,考虑蜂窝夹芯结构中应力波的各向异性特性,采用免疫遗传算法对未知的低速冲击载荷进行位置识别。实验研究结果表明了该方法的可行性和有效性

关 键 词:复合材料蜂窝夹芯结构  低速冲击定位  应力波  免疫遗传算法  

Localization of low-velocity impact on a composite honeycomb sandwich structure
ZHAO Lin-hu,ZHOU Li. Localization of low-velocity impact on a composite honeycomb sandwich structure[J]. Journal of Vibration and Shock, 2012, 31(2): 67-71,108. DOI:  
Authors:ZHAO Lin-hu  ZHOU Li
Affiliation:MOE Key Lab of Structure Mechanics and Control for Aircraft; Institute of Structures & Strength; Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:
Low-velocity impact tests were performed on a carbon fiber reinforced composite honeycomb sandwich structure,and a localization method using stress wave and immune genetic algorithm(IGA) was used to analyze and locate the low-velocity impact on this composite structure.Firstly,after obtaining a set of impact-induced stress wave signals from location pre-determined impact tests,wavelet transformation was used to analyze these stress wave signals in time-frequency domain to obtain the propagation velocity of the impact-induced stress waves in the composite structure.Then,considering the anisotropic properties of stress wave propagation in composite honeycomb structure,IGA was employed to identify the location of unknown low-velocity impact.Experimental results demonstrated the applicability and effectiveness of the proposed impact localization method.
Keywords:composite honeycomb sandwich structure  localization of low-velocity impact  stress wave  immune genetic algorithm(IGA)
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