Raddatz, Florian und Heinze, Christoph und Dienel, Christoph und Lingenauber, Martin (2013) Non-destructive Testing and Damage Assessment of Composite Aerospace Structures Using Lamb Waves. In: Proceedings of the 4th International Workshop on Aircraft Systems Technologies, Seiten 425-436. Shaker Verlag. 4th International Workshop on Aircraft System Technologies, 2013-04-23 - 2013-04-24, Hamburg. ISBN 978-3-8440-1850-9. ISSN 0945-2214.
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Kurzfassung
This paper shows the special requirements and challenges of non-destructive testing (NDT) methods that arise from the increasing use of composite materials in aerospace structures. Current NDT methods often fail due to the large size of the structures or the material properties of composites. Manual testing methods are very time consuming for large structures and therefore increase the grounding time of the aircraft. They are also subject to human errors and do not provide the documentation quality of automated systems. To solve these problems a method based on the propagation of Lamb waves is presented that can be used for testing and monitoring the structure for defects. An optical measurement platform for the detection of Lamb waves, that is currently being developed at the DLR, is presented and it is shown, how damages can be localized in complex parts. Based on wave propagation simulation and damage assessment techniques the speci?c impact of the damage on the integrity of the structure and suitable repair concepts can be derived.
elib-URL des Eintrags: | https://elib.dlr.de/82314/ | ||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag, Paper) | ||||||||||||||||||||
Titel: | Non-destructive Testing and Damage Assessment of Composite Aerospace Structures Using Lamb Waves | ||||||||||||||||||||
Autoren: |
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Datum: | 23 April 2013 | ||||||||||||||||||||
Erschienen in: | Proceedings of the 4th International Workshop on Aircraft Systems Technologies | ||||||||||||||||||||
Referierte Publikation: | Nein | ||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||
Seitenbereich: | Seiten 425-436 | ||||||||||||||||||||
Verlag: | Shaker Verlag | ||||||||||||||||||||
ISSN: | 0945-2214 | ||||||||||||||||||||
ISBN: | 978-3-8440-1850-9 | ||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||
Stichwörter: | structural health monitoring, lamb waves, vibrometry | ||||||||||||||||||||
Veranstaltungstitel: | 4th International Workshop on Aircraft System Technologies | ||||||||||||||||||||
Veranstaltungsort: | Hamburg | ||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||
Veranstaltungsbeginn: | 23 April 2013 | ||||||||||||||||||||
Veranstaltungsende: | 24 April 2013 | ||||||||||||||||||||
Veranstalter : | Technische Universität Hamburg-Harburg | ||||||||||||||||||||
HGF - Forschungsbereich: | keine Zuordnung | ||||||||||||||||||||
HGF - Programm: | keine Zuordnung | ||||||||||||||||||||
HGF - Programmthema: | keine Zuordnung | ||||||||||||||||||||
DLR - Schwerpunkt: | keine Zuordnung | ||||||||||||||||||||
DLR - Forschungsgebiet: | keine Zuordnung | ||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | keine Zuordnung | ||||||||||||||||||||
Standort: | Braunschweig | ||||||||||||||||||||
Institute & Einrichtungen: | Institut für Faserverbundleichtbau und Adaptronik > Multifunktionswerkstoffe | ||||||||||||||||||||
Hinterlegt von: | Raddatz, Dr.-Ing. Florian | ||||||||||||||||||||
Hinterlegt am: | 13 Aug 2013 09:39 | ||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 19:48 |
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