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

FAILURE ANALYSIS OF PRE-OXIDIZED ReneN5/ β-(Ni,Pt)Al/7YSZ EB-PVD THERMAL BARRIER COATINGS

Mora-García, A.G. und Alvarado-Orozco, L.M. und Mondragón Rodríguez, G.C. und García-Herrera, J.E. und Cácerez-Díaz, L.A. und Konitzer, D.G. und Trágaga-Martínez, L.G. und Schulz, U. und Muñoz-Saldaña, J. (2013) FAILURE ANALYSIS OF PRE-OXIDIZED ReneN5/ β-(Ni,Pt)Al/7YSZ EB-PVD THERMAL BARRIER COATINGS. XXII International Materials Research Congress, 2013-08-11 - 2013-08-15, Cancún Mexiko.

Dieses Archiv kann nicht den Volltext zur Verfügung stellen.

Kurzfassung

Nowadays Pt-modified nickel aluminides, (Ni,Pt)Al, are highly used as alumina-forming alloys in the aerospace industry. These alloys have been studied to improve the lifetime of the thermal barrier coating systems (TBCs) when they are exposed to thermal-cyclic tests [1-3]. The use of (Ni,Pt)Al alloy as bond coat (BC) is to provide oxidation protection of the Ni-base superalloy (SA) used as a substrate of hot-section turbine blades. BCs act as an aluminum reservoir that leads to the formation of a thermally grown oxide (TGO). The TGO improves the adherence between the metal and a ceramic top coat (TC), which provides thermal insulation during the operation of these components. The aim of the present study is to evaluate the effect of the pre-oxidation treatments before TC deposition on the thermal-cyclic life of ReneN5/(Ni,Pt)Al/7YSZ TBCs. The effect of different oxygen partial pressures (pO2= 2.1x10-1, 1.05x10-1, 1x10-5 and 1x10-9 atm) pre-oxidation treatments were evaluated and compared to regular TBCs after EB-PVD TC deposition in “as-coated” conditions. A post-mortem analysis of the samples was also carried out after 1 h thermal-cyclic testing at 1100ºC to study the intrinsic mechanisms associated to the failure. Samples pre-oxidized with a combination of Argon-Gettered atmosphere (pO2=1x10-9 atm) showed the highest performance in average (1550 cycles to failure). For all the different pre-oxidation conditions, the failure occurred majority along the TC/TGO interface. Mapping of grain orientation determined by EBSD combined with nanoindentation tests were carried out to evaluate anisotropic effects and structural characterization with their mechanical properties after thermal-cyclic tests. Efforts are currently being done to link the failure of the samples to the microstructural characteristics. For instance a continuous layer of martensitic phase, L10, along the bond coat has been observed after failure for the thermal-cyclic tested samples. The reversible L10↔β phase transformation and the reaction β γ' are the main phenomena that take place during thermal cycling and results from the BC aluminum depletion due to TGO formation and its diffusion to the SA [4-6]. Moreover, cracks have been identified in the L10/γ' grains interface. Finally, it must be pointed out that the non-pre-oxidized TBCs have shown a mixed zone in the TGO, which consists on a region where zirconia particles are dispersed in the TGO matrix [7]. References [1] A.G. Evans, et.al., Progress in Materials Science 46 (2001) 505 - 553. [2] V.K. Tolpygo and D.R. Clarke, Surface & Coatings Technology 200 (2005) 1276 - 1281. [3] U. Schulz, et.al., Surface & Coatings Technology 203 (2008) 160 - 170. [4] M.W. Chen, et.al., Acta Materialia (2003), 4279 - 4294. [5] J.L. Smialek and R. Giballa; Metallurgical transactions A (1983), 2143 - 2161. [6] B. Gleeson, W. Wang, S. Hayashi, D.J. Sordelet; Mater Sci Forum 2004. [7] M.J. Stiger, et.al; Metallurgical and Materials Transitions A (2007) Vol.38A 848 - 857.

elib-URL des Eintrags:https://elib.dlr.de/84683/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:FAILURE ANALYSIS OF PRE-OXIDIZED ReneN5/ β-(Ni,Pt)Al/7YSZ EB-PVD THERMAL BARRIER COATINGS
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Mora-García, A.G.Cinvestav, Unidad Querétaro, MéxicoNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Alvarado-Orozco, L.M.University of PittsburghNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Mondragón Rodríguez, G.C.guillermo.mondragon-rodriguez (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
García-Herrera, J.E.Cinvestav, Unidad Querétaro, MéxicoNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Cácerez-Díaz, L.A.Cinvestav, Unidad Querétaro, MéxicoNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Konitzer, D.G.General Electric CincinnatiNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Trágaga-Martínez, L.G.Cinvestav, Unidad Querétaro, MéxicoNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Schulz, U.uwe.schulz (at) dlr.dehttps://orcid.org/0000-0003-0362-8103NICHT SPEZIFIZIERT
Muñoz-Saldaña, J.Cinvestav, Unidad Querétaro, MéxicoNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:13 August 2013
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:TBCs, pre-oxidation, thermal-cyclic testing, (Ni,Pt)Al BC, martensitic transformation, TGO.
Veranstaltungstitel:XXII International Materials Research Congress
Veranstaltungsort:Cancún Mexiko
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:11 August 2013
Veranstaltungsende:15 August 2013
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Antriebe (alt)
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L ER - Antriebsforschung
DLR - Teilgebiet (Projekt, Vorhaben):L - Turbinentechnologien (alt)
Standort: Köln-Porz
Institute & Einrichtungen:Institut für Werkstoff-Forschung > Hochtemperatur-und Funktionsschutzschichten
Hinterlegt von: Mondragon Rodriguez, Guillermo Cesar
Hinterlegt am:16 Okt 2013 09:51
Letzte Änderung:24 Apr 2024 19:50

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.