Hypervelocity impact induced shock acoustic emission waves for quantitative damage evaluation using in situ miniaturized piezoelectric sensor network

Hypervelocity impact induced shock acoustic emission waves for quantitative damage evaluation using in situ miniaturized piezoelectric sensor network

论文摘要

Manmade debris and natural meteoroids, travelling in the Low Earth Orbit at a speed of several kilometers per second, pose a severe safety concern to the spacecraft in service through the HyperVelocity Impact(HVI). To address this issue, an investigation of shock Acoustic Emission(AE) waves induced by HVI to a downscaled two-layer Whipple shielding structure is performed,to realize a quantitative damage evaluation. Firstly a hybrid numerical model integrating smoothparticle hydrodynamics and finite element is built to obtain the wave response. The projectiles, with various impact velocities and directions, are modelled to impact the shielding structure with different thicknesses. Then experimental validation is carried out with built-in miniaturized piezoelectric sensors to in situ sense the HVI-induced AE waves. A quantitative agreement is obtained between numerical and experimental results, demonstrating the correctness of the hybrid model and facilitating the explanation of obtained AE signals in experiment. Based on the understanding of HVI-induced wave components, assessment of the damage severity, i.e., whether the outer shielding layer is perforated or not, is performed using the energy ratio between the regions of ‘‘high frequency" and ‘‘low frequency" in the acquired AE signals. Lastly, the direct-arrival fundamentalsymmetric wave mode is isolated from each sensing signal to be input into an enhanced delay-andsum algorithm, which visualizes HVI spots accurately and instantaneously with different sensor network configuration. All these works demonstrate the potential of quantitative, in situ, and real time HVI monitoring using miniaturized piezoelectric sensor network.

论文目录

文章来源

类型: 期刊论文

作者: Menglong LIU,Qiang WANG,Qingming ZHANG,Renrong LONG,Fangsen CUI,Zhongqing SU

来源: Chinese Journal of Aeronautics 2019年05期

年度: 2019

分类: 工程科技Ⅱ辑,工程科技Ⅰ辑

专业: 安全科学与灾害防治,航空航天科学与工程

单位: Institute of High Performance Computing A*STAR (Agency for Science, Technology and Research),School of Automation, Nanjing University of Posts and Telecommunications,State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology,Institute of High Performance Computing (A*STAR Agency for Science, Technology and Research),Department of Mechanical Engineering, The Hong Kong Polytechnic University

基金: the Hong Kong Research Grants Council via a General Research Fund(Nos.15201416 and 15212417),the National Natural Science Foundation of China(No.51635008)

分类号: V528;V467

页码: 1059-1070

总页数: 12

文件大小: 1558K

下载量: 11

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Hypervelocity impact induced shock acoustic emission waves for quantitative damage evaluation using in situ miniaturized piezoelectric sensor network
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