Impact Damage Ascertainment in Composite Plates Using In-Situ Acoustic Emission Signal Signature Identification

Barely visible impact damage (BVID) due to low velocity impact events in composite aircraft structures are becoming prevalent. BVID can have an adverse effect on the strength and safety of the structure. During aircraft inspections it can be extremely difficult to visually detect BVID. Moreover, it...

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Main Authors: Robin James, Roshan Prakash Joseph, Victor Giurgiutiu
Format: Article
Language:English
Published: MDPI AG 2021-03-01
Series:Journal of Composites Science
Subjects:
Online Access:https://www.mdpi.com/2504-477X/5/3/79
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spelling doaj-dcc3f22cdd3d4f9fa9a627405cd4ca392021-03-13T00:01:35ZengMDPI AGJournal of Composites Science2504-477X2021-03-015797910.3390/jcs5030079Impact Damage Ascertainment in Composite Plates Using In-Situ Acoustic Emission Signal Signature IdentificationRobin James0Roshan Prakash Joseph1Victor Giurgiutiu2Department of Mechanical Engineering, University of South Carolina, Columbia, SC 29208, USADepartment of Mechanical Engineering, University of South Carolina, Columbia, SC 29208, USADepartment of Mechanical Engineering, University of South Carolina, Columbia, SC 29208, USABarely visible impact damage (BVID) due to low velocity impact events in composite aircraft structures are becoming prevalent. BVID can have an adverse effect on the strength and safety of the structure. During aircraft inspections it can be extremely difficult to visually detect BVID. Moreover, it is also a challenge to ascertain if the BVID has in-fact caused internal damage to the structure or not. This paper describes a method to ascertain whether or not internal damage happened during the impact event by analyzing the high-frequency information contained in the recorded acoustic emission signal signature. Multiple 2 mm quasi-isotropic carbon fiber reinforced polymer (CFRP) composite coupons were impacted using the ASTM D7136 standard in a drop weight impact testing machine to determine the mass, height and energy parameters to obtain approximately 1” impact damage size in the coupons iteratively. For subsequent impact tests, four piezoelectric wafer active sensors (PWAS) were bonded at specific locations on each coupon to record the acoustic emission (AE) signals during the impact event using the MISTRAS micro-II digital AE system. Impact tests were conducted on these instrumented 2 mm coupons using previously calculated energies that would create either no damage or 1” impact damage in the coupons. The obtained AE waveforms and their frequency spectrums were analyzed to distinguish between different AE signatures. From the analysis of the recorded AE signals, it was verified if the structure had indeed been damaged due to the impact event or not. Using our proposed structural health monitoring technique, it could be possible to rapidly identify impact events that cause damage to the structure in real-time and distinguish them from impact events that do not cause damage to the structure. An invention disclosure describing our acoustic emission structural health monitoring technique has been filed and is in the process of becoming a provisional patent.https://www.mdpi.com/2504-477X/5/3/79barely visible impact damage (BVID)composite structuresdamage detectioncarbon fiber reinforced polymer (CFRP)acoustic emissionstructural health monitoring
collection DOAJ
language English
format Article
sources DOAJ
author Robin James
Roshan Prakash Joseph
Victor Giurgiutiu
spellingShingle Robin James
Roshan Prakash Joseph
Victor Giurgiutiu
Impact Damage Ascertainment in Composite Plates Using In-Situ Acoustic Emission Signal Signature Identification
Journal of Composites Science
barely visible impact damage (BVID)
composite structures
damage detection
carbon fiber reinforced polymer (CFRP)
acoustic emission
structural health monitoring
author_facet Robin James
Roshan Prakash Joseph
Victor Giurgiutiu
author_sort Robin James
title Impact Damage Ascertainment in Composite Plates Using In-Situ Acoustic Emission Signal Signature Identification
title_short Impact Damage Ascertainment in Composite Plates Using In-Situ Acoustic Emission Signal Signature Identification
title_full Impact Damage Ascertainment in Composite Plates Using In-Situ Acoustic Emission Signal Signature Identification
title_fullStr Impact Damage Ascertainment in Composite Plates Using In-Situ Acoustic Emission Signal Signature Identification
title_full_unstemmed Impact Damage Ascertainment in Composite Plates Using In-Situ Acoustic Emission Signal Signature Identification
title_sort impact damage ascertainment in composite plates using in-situ acoustic emission signal signature identification
publisher MDPI AG
series Journal of Composites Science
issn 2504-477X
publishDate 2021-03-01
description Barely visible impact damage (BVID) due to low velocity impact events in composite aircraft structures are becoming prevalent. BVID can have an adverse effect on the strength and safety of the structure. During aircraft inspections it can be extremely difficult to visually detect BVID. Moreover, it is also a challenge to ascertain if the BVID has in-fact caused internal damage to the structure or not. This paper describes a method to ascertain whether or not internal damage happened during the impact event by analyzing the high-frequency information contained in the recorded acoustic emission signal signature. Multiple 2 mm quasi-isotropic carbon fiber reinforced polymer (CFRP) composite coupons were impacted using the ASTM D7136 standard in a drop weight impact testing machine to determine the mass, height and energy parameters to obtain approximately 1” impact damage size in the coupons iteratively. For subsequent impact tests, four piezoelectric wafer active sensors (PWAS) were bonded at specific locations on each coupon to record the acoustic emission (AE) signals during the impact event using the MISTRAS micro-II digital AE system. Impact tests were conducted on these instrumented 2 mm coupons using previously calculated energies that would create either no damage or 1” impact damage in the coupons. The obtained AE waveforms and their frequency spectrums were analyzed to distinguish between different AE signatures. From the analysis of the recorded AE signals, it was verified if the structure had indeed been damaged due to the impact event or not. Using our proposed structural health monitoring technique, it could be possible to rapidly identify impact events that cause damage to the structure in real-time and distinguish them from impact events that do not cause damage to the structure. An invention disclosure describing our acoustic emission structural health monitoring technique has been filed and is in the process of becoming a provisional patent.
topic barely visible impact damage (BVID)
composite structures
damage detection
carbon fiber reinforced polymer (CFRP)
acoustic emission
structural health monitoring
url https://www.mdpi.com/2504-477X/5/3/79
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