Abstract

At present, most of the research on low velocity impact of composite laminates focuses on load location and damage assessment. To provide further early warnings about structural impact damage, impact energy can be monitored and identified. For high strength composite laminates with variable thickness, in order to further accurately evaluate the impact energy, it is necessary to adopt more suitable dynamic load signal analysis and impact energy identification methods. Therefore, a new low velocity impact monitoring and identification method for composite plates with variable thickness is proposed. All impact sample signals collected by optical fiber sensor network are decomposed by whitening Empirical Mode Decomposition (EMD); the energy feature set is established according to the impact energy eigenvalue of sample signal; according to the first order component of signal decomposition, the thickness coefficient is determined and the energy feature set is modified to evaluate the actual impact energy. Meanwhile, combined with optical fiber sensing and signal processing technology, an impact energy monitoring system has been established, and the low velocity impact monitoring and identification experiments of composite laminates with variable thickness were carried out. The proposed energy identification method successfully identified 1–3 J impact energy with an average error of 4.82%, and the average error of large thickness area with low sensitivity was significantly reduced from 13.25% to 5.67%. The results show that the thickness coefficient correction method based on whitening EMD can evaluate the low velocity impact energy more accurately, and the thickness coefficient correction step significantly improves the recognition performance.

Highlights

  • In recent years, composite materials used in aerospace, mechanical, marine, medical, construction, transportation, and other fields have increased significantly due to their superior mechanical properties over metal materials

  • The effect of external low velocity impact load on the structure can cause the center wavelength of fiber Bragg grating sensor shift, Fiber Bragg Grating (FBG) sensor can be used in the research of low velocity impact monitoring of variable thickness composite laminates

  • The results show that the recognition results with the thickness coefficient correction has better performance than the uncorrected result

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Summary

Introduction

Composite materials used in aerospace, mechanical, marine, medical, construction, transportation, and other fields have increased significantly due to their superior mechanical properties over metal materials. The composite laminate may suffer substantial internal damage without any visible damage, especially internal cracks or delamination caused by external low velocity impact These forms of damage, most of which are hidden in the composite structure, can result in significant degradation of the mechanical properties of the composite structure [4]. The real-time monitoring of composite board with variable thickness of impact signal can early warning the structural low velocity impact damage [7]. The key algorithm of whitening Empirical Mode Decomposition (EMD) is used to extract the eigenvalues of the impact signal of variable thickness plate with serious aliasing, and the low velocity impact energy level is identified, which ensures the effectiveness of impact location early warning

Fiber Bragg Grating Strain Sensing Technology
Low Velocity Impact Feature Extraction Algorithm
Low Velocity Impact Energy Recognition Steps
Low Velocity Impact Experiment
Build a Sample Low Velocity Impact Signal Database
Analysis of Low Velocity Impact Experimental Results
Analysis of Low Velocity Impact Energy Recognition
Findings
Conclusions
Full Text
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