elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Datenschutz | Kontakt | English
Schriftgröße: [-] Text [+]

Elastic and inelastic mechanical behaviour of free standing EB-PVD thermal barrier coatings

Bartsch, Marion und Fuchs, Uwe und Xu, Jianmin (2009) Elastic and inelastic mechanical behaviour of free standing EB-PVD thermal barrier coatings. In: Seminar on Material Science - Department of Intelligent Mechanical Engineering. Seminar on Materials Science - Department of Intelligent Mechanical Engineering, 2009-06-02, Fukuoka, Japan.

Dieses Archiv kann nicht den Volltext zur Verfügung stellen.

Kurzfassung

Thermal barrier coatings (TBC) processed by electron beam physical vapor deposition (EB-PVD) show complex deformation behavior due to their columnar microstructure and multi-scale porosity. The existing data for the elastic properties of EB-PVD coatings varies in a wide range, depending on the measurement method. In most cases, the fragile EB-PVD coatings are tested on the substrate, onto which they were deposited. Since the ceramic coatings are deposited onto metallic substrates, having about 1000°C, compressive residual stresses develop in the coating after cooling down. Since the deformation behavior of EB-PVD coatings is known to be stress dependent, the residual stresses cannot be calculated without knowledge of the stress-strain response, and without knowledge of the residual stress the elastic properties cannot be measured correctly. To overcome this dilemma, tubular free standing EB-PVD coating samples with a thickness of 250μm have been processed and tested in compression at room temperature. For introducing the mechanical load safely into the gauge length a soft clamping has been developed, and the strain was measured using a contact-free laser extensometer. Several subsequent loading and unloading cycles were performed on specimens with different thermal pre heat treatments. Specimens in as coated condition displayed non-linear stress-strain behavior, showing increasing stiffness with increasing compressive stress. Long term thermally aged specimens showed higher stiffness than as processed specimens and linear stress-strain behaviour. The data measured on the free standing tubular specimens are compared to the data obtained from the same coating system but using different testing methods.

elib-URL des Eintrags:https://elib.dlr.de/61355/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Elastic and inelastic mechanical behaviour of free standing EB-PVD thermal barrier coatings
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Bartsch, Marionmarion.bartsch (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Fuchs, Uweuwe.fuchs (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Xu, JianminRoll Royce DeutschlandNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:2 Juni 2009
Erschienen in:Seminar on Material Science - Department of Intelligent Mechanical Engineering
Referierte Publikation:Nein
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Thermal Barrier Coating System, EB-PVD, elastic deformation, creep
Veranstaltungstitel:Seminar on Materials Science - Department of Intelligent Mechanical Engineering
Veranstaltungsort:Fukuoka, Japan
Veranstaltungsart:Andere
Veranstaltungsdatum:2 Juni 2009
Veranstalter :Prof. Shijie Zhu, Department of Intelligent Mechanical Engineering, Fukuoka Institute of Technology
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:L VU - Luftverkehr und Umwelt (alt)
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L VU - Luftverkehr und Umwelt
DLR - Teilgebiet (Projekt, Vorhaben):L - Schadstoffarmer Luftverkehr (alt)
Standort: Köln-Porz
Institute & Einrichtungen:Institut für Werkstoff-Forschung > Experimentelle und numerische Methoden
Hinterlegt von: Bartsch, Dr.-Ing. Marion
Hinterlegt am:03 Dez 2009 15:23
Letzte Änderung:24 Apr 2024 19:26

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
electronic library verwendet EPrints 3.3.12
Gestaltung Webseite und Datenbank: Copyright © Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.