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Guided Wave-based Structural Health Monitoring for a Composite Aircraft Fuselage under Mechanical Load

Moix-Bonet, Maria und Schmidt, Daniel und Wierach, Peter (2023) Guided Wave-based Structural Health Monitoring for a Composite Aircraft Fuselage under Mechanical Load. European Conference on Non-Destructive Testing 2023, 2023-07-03 - 2023-07-07, Lissabon, Portugal.

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Kurzfassung

The introduction of composite materials in aeronautics has brought numerous advantages, along with unique damage and failure modes. The structure health is currently ensured with an increase in non-destructive inspection activities and a damage-tolerant design. Among other techniques, Guided Wave-based Structural Health Monitoring (GW-SHM) has gained interest as a cost and time effective alternative to traditional non-destructive techniques. One of the main challenges for GW-SHM is the influence of environmental and operational conditions. Aircraft structures undergo a broad range of mechanical load conditions, affecting the GW-SHM system. A full-scale CFRP door surrounding structure was instrumented with a GW-SHM system and tested under mechanical load. The test object has a dimension of 4100 x 5700 mm and covers 9 frames, 17 stringers, 4 windows and the door surround structure. A hydraulic test rig was used to apply three load cases in quasi-static conditions on the structure: tension, lateral bending and vertical bending. A network of robust piezocomposite transducers to monitor the structure has been designed and manufactured during the project. The network is organized in arrays, which include the transducers, cabling and a connecting base plate for optimized sensor installation. A multiplexing module is directly connected to the base plate enabling a fast and reliable sensor connection, a drastic cable weight reduction, and a modular design. The load influence on the GW-SHM system has been analysed: on the transducer network as well as on the damage identification performance. The transducers were monitored using electromechanical impedance throughout the test campaign in order to check for debonding from the structure and piezoceramic breakage. Finally, a data-driven approach to damage identification has allowed the detection and localization of barely visible impact damage introduced during the test campaign.

elib-URL des Eintrags:https://elib.dlr.de/199521/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Guided Wave-based Structural Health Monitoring for a Composite Aircraft Fuselage under Mechanical Load
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Moix-Bonet, MariaMaria.Moix-Bonet (at) dlr.dehttps://orcid.org/0000-0002-1327-0080NICHT SPEZIFIZIERT
Schmidt, DanielDaniel.Schmidt (at) dlr.dehttps://orcid.org/0009-0004-5722-2891NICHT SPEZIFIZIERT
Wierach, PeterPeter.Wierach (at) dlr.dehttps://orcid.org/0000-0003-0852-9112NICHT SPEZIFIZIERT
Datum:4 Juli 2023
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:akzeptierter Beitrag
Stichwörter:Guided Waves, SHM, Environmental and Operational Conditions, Composite Structures
Veranstaltungstitel:European Conference on Non-Destructive Testing 2023
Veranstaltungsort:Lissabon, Portugal
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:3 Juli 2023
Veranstaltungsende:7 Juli 2023
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Komponenten und Systeme
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L CS - Komponenten und Systeme
DLR - Teilgebiet (Projekt, Vorhaben):L - Strukturwerkstoffe und Bauweisen, L - Wartung und Kabine
Standort: Braunschweig
Institute & Einrichtungen:Institut für Systemleichtbau > Multifunktionswerkstoffe
Hinterlegt von: Moix-Bonet, Maria
Hinterlegt am:27 Nov 2023 08:27
Letzte Änderung:24 Apr 2024 21:00

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