Vibration-Based Thermal Health Monitoring for Face Layer Debonding Detection in Aerospace Sandwich Structures

This paper investigates the potential of a novel vibration-based thermal health monitoring method for continuous and on-board damage detection in fiber reinforced polymer sandwich structures, as typically used in aerospace applications. This novel structural health monitoring method uses the same pr...

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Main Authors: Thomas Bergmayr, Christoph Kralovec, Martin Schagerl
Format: Article
Language:English
Published: MDPI AG 2021-12-01
Series:Applied Sciences
Subjects:
Online Access:https://www.mdpi.com/2076-3417/11/1/211
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spelling doaj-887f1d57de9d454183f6a7780f97382e2020-12-29T00:02:44ZengMDPI AGApplied Sciences2076-34172021-12-011121121110.3390/app11010211Vibration-Based Thermal Health Monitoring for Face Layer Debonding Detection in Aerospace Sandwich StructuresThomas Bergmayr0Christoph Kralovec1Martin Schagerl2Institute of Structural Lightweight Design, Johannes Kepler University Linz, 4040 Linz, AustriaInstitute of Structural Lightweight Design, Johannes Kepler University Linz, 4040 Linz, AustriaInstitute of Structural Lightweight Design, Johannes Kepler University Linz, 4040 Linz, AustriaThis paper investigates the potential of a novel vibration-based thermal health monitoring method for continuous and on-board damage detection in fiber reinforced polymer sandwich structures, as typically used in aerospace applications. This novel structural health monitoring method uses the same principles, which are used for vibration-based thermography in combination with the concept of the local defect resonance, as a well known non-destructive testing method (NDT). The use of heavy shakers for applying strong excitation and infrared cameras for observing thermal responses are key hindrances for the application of vibration-based thermography in real-life structures. However, the present study circumvents these limitations by using piezoelectric wafer active sensors as excitation source, which can be permanently bonded on mechanical structures. Additionally, infrared cameras are replaced by surface temperature sensors for observing the thermal responses due to vibrations and damage. This makes continuous and on-board thermal health monitoring possible. The new method is experimentally validated in laboratory experiments by a sandwich structure with face layer debonding as damage scenario. The debonding is realized by introduction of an insert during the manufacturing process of the specimen. The surface temperature sensor results successfully show the temperature increase in the area of the debonding caused by a sinusoidal excitation of the sandwich structure with the PWAS at the first resonance frequency of the damage. This is validated by conventional infrared thermography. These findings demonstrate the potential of the proposed novel thermal health monitoring method for detecting, localizing and estimating sizes of face layer debonding in sandwich structures.https://www.mdpi.com/2076-3417/11/1/211vibration-based thermographyfiber reinforced polymerthermal health monitoringsandwich structureface layer debondingaerospace structures
collection DOAJ
language English
format Article
sources DOAJ
author Thomas Bergmayr
Christoph Kralovec
Martin Schagerl
spellingShingle Thomas Bergmayr
Christoph Kralovec
Martin Schagerl
Vibration-Based Thermal Health Monitoring for Face Layer Debonding Detection in Aerospace Sandwich Structures
Applied Sciences
vibration-based thermography
fiber reinforced polymer
thermal health monitoring
sandwich structure
face layer debonding
aerospace structures
author_facet Thomas Bergmayr
Christoph Kralovec
Martin Schagerl
author_sort Thomas Bergmayr
title Vibration-Based Thermal Health Monitoring for Face Layer Debonding Detection in Aerospace Sandwich Structures
title_short Vibration-Based Thermal Health Monitoring for Face Layer Debonding Detection in Aerospace Sandwich Structures
title_full Vibration-Based Thermal Health Monitoring for Face Layer Debonding Detection in Aerospace Sandwich Structures
title_fullStr Vibration-Based Thermal Health Monitoring for Face Layer Debonding Detection in Aerospace Sandwich Structures
title_full_unstemmed Vibration-Based Thermal Health Monitoring for Face Layer Debonding Detection in Aerospace Sandwich Structures
title_sort vibration-based thermal health monitoring for face layer debonding detection in aerospace sandwich structures
publisher MDPI AG
series Applied Sciences
issn 2076-3417
publishDate 2021-12-01
description This paper investigates the potential of a novel vibration-based thermal health monitoring method for continuous and on-board damage detection in fiber reinforced polymer sandwich structures, as typically used in aerospace applications. This novel structural health monitoring method uses the same principles, which are used for vibration-based thermography in combination with the concept of the local defect resonance, as a well known non-destructive testing method (NDT). The use of heavy shakers for applying strong excitation and infrared cameras for observing thermal responses are key hindrances for the application of vibration-based thermography in real-life structures. However, the present study circumvents these limitations by using piezoelectric wafer active sensors as excitation source, which can be permanently bonded on mechanical structures. Additionally, infrared cameras are replaced by surface temperature sensors for observing the thermal responses due to vibrations and damage. This makes continuous and on-board thermal health monitoring possible. The new method is experimentally validated in laboratory experiments by a sandwich structure with face layer debonding as damage scenario. The debonding is realized by introduction of an insert during the manufacturing process of the specimen. The surface temperature sensor results successfully show the temperature increase in the area of the debonding caused by a sinusoidal excitation of the sandwich structure with the PWAS at the first resonance frequency of the damage. This is validated by conventional infrared thermography. These findings demonstrate the potential of the proposed novel thermal health monitoring method for detecting, localizing and estimating sizes of face layer debonding in sandwich structures.
topic vibration-based thermography
fiber reinforced polymer
thermal health monitoring
sandwich structure
face layer debonding
aerospace structures
url https://www.mdpi.com/2076-3417/11/1/211
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AT christophkralovec vibrationbasedthermalhealthmonitoringforfacelayerdebondingdetectioninaerospacesandwichstructures
AT martinschagerl vibrationbasedthermalhealthmonitoringforfacelayerdebondingdetectioninaerospacesandwichstructures
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