Abstract

Through the use of the wave reflection from any damage in a structure, a Hilbert spectral analysis-based rapid multi-damage identification (HSA-RMDI) technique with piezoelectric wafer sensor arrays (PWSA) is developed to monitor and identify the presence, location and severity of damage in carbon fiber composite structures. The capability of the rapid multi-damage identification technique to extract and estimate hidden significant information from the collected data and to provide a high-resolution energy-time spectrum can be employed to successfully interpret the Lamb waves interactions with single/multiple damage. Nevertheless, to accomplish the precise positioning and effective quantification of multiple damage in a composite structure, two functional metrics from the RMDI technique are proposed and used in damage identification, which are the energy density metric and the energy time-phase shift metric. In the designed damage experimental tests, invisible damage to the naked eyes, especially delaminations, were detected in the leftward propagating waves as well as in the selected sensor responses, where the time-phase shift spectra could locate the multiple damage whereas the energy density spectra were used to quantify the multiple damage. The increasing damage was shown to follow a linear trend calculated by the RMDI technique. All damage cases considered showed completely the developed RMDI technique potential as an effective online damage inspection and assessment tool.

Highlights

  • A reliable, effective and autonomous damage assessment technique for composite structures will be a very important factor in smart aerospace system design in the future

  • From the measurement of a specific physical property of wave propagation in a structure, the energy density of wave propagation in a structure, the energy density metric will give the necessary information to quantify the severities of various damage through the metric will give the necessary information to quantify the severities of various damage through the relevant energy density spectra

  • The energy time-phase shift metric is known as the key tool to infer the locations and sizes of multiple damage through the relevant energy-time spectra

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Summary

Introduction

A reliable, effective and autonomous damage assessment technique for composite structures will be a very important factor in smart aerospace system design in the future. Developed a computational model based on a spectral finite element method to simulate Lamb wave propagation with the hole and crack damage types, and verified the significant advantages of the proposed SFE method, which included the fact that the computational time for modeling Lamb wave propagation is faster than that of the FEM, and the optimization of sensor shape, size, locations and probing waveform could be implemented. The rapid multi-damage identification technique based on the multi-functional multi-metrics index algorithm was applied successfully to indicate the Lamb waves interactions with a variety of damage, and this technique is developed for the modern real-time engineering inspection which is to determine the presence, location and severity of damage in carbon fiber composite structures

Method of Approach
Determination of the Group Velocity of Propagating Waves
Rapid Multi-Damage Index Algorithm Based on Multi-Functional Multi-Metrics
Experimental Setup
Results and Discussion
Determination
Multi-Damage Quantification and Track by Energy Density Metric
Multi-Damage
Full Text
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