Knipe, Kevin and Sofronsky, Stephen and Almer, Jonathan and Meid, Carla and Bartsch, Marion and Manero, Albert and Okasinski, John and Wischek, Janine and Karlsson, Anette M. and Raghavan, Seetha (2014) SYNCHROTRON XRD MEASUREMENTS MAPPING INTERNAL STRAINS OF THERMAL BARRIER COATINGS DURING THERMAL GRADIENT MECHANICAL FATIGUE LOADING. In: ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, Vol. 6, V006T02A011. ASME Publishing, New York. ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, 2014-06-16 - 2014-06-20, Düsseldorf. doi: 10.1115/GT2014-26919. ISBN 978-0-7918-4575-2. ISSN GT2014-26919.
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Abstract
An understanding of the high temperature mechanics experienced in Thermal Barrier Coatings (TBC) during cycling conditions would be highly beneficial to extending the lifespan of the coatings. This study will present results obtained using synchrotron x-rays to measure depth resolved strains in the various layers of TBCs under thermal mechanical loading and a superposed thermal gradient. Tubular specimens, coated with Yttria Stabilized Zirconia (YSZ) and an aluminum containing nickel alloy as a bond coat both through Electron Beam - Physical Vapor Deposition (EBPVD), were subjected to external heating and controlled internal cooling generating a thermal gradient across the specimen’s wall. Temperatures at the external surface were in excess of 1000 °C. Throughout high temperature testing, 2-D high-resolution XRD strain measurements are taken at various locations through the entire depth of the coating layers. Across the YSZ a strain gradient was observed showing higher compressive strain at the interface to the bond coat than towards the surface. This behavior can be attributed to the specific microstructure of the EB-PVD-coating, which reveals higher porosity at the outer surface than at the interface to the bond coat, resulting in a lower in plane modulus near the surface. This location at the interface displays the most significant variation due to applied load at room temperature with this effect diminishing at elevated uniform temperatures. During thermal cycling with a thermal gradient and mechanical loading, the bond coat strain moves from a highly tensile state at room temperature to an initially compressive state at high temperature before relaxing to zero during the high temperature hold. The results of these experiments give insight into previously unseen material behavior at high temperature which can be used to develop an increased understanding of various failure modes and their causes.
Item URL in elib: | https://elib.dlr.de/91664/ | ||||||||||||||||||||||||||||||||||||||||||||
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Document Type: | Conference or Workshop Item (Speech) | ||||||||||||||||||||||||||||||||||||||||||||
Title: | SYNCHROTRON XRD MEASUREMENTS MAPPING INTERNAL STRAINS OF THERMAL BARRIER COATINGS DURING THERMAL GRADIENT MECHANICAL FATIGUE LOADING | ||||||||||||||||||||||||||||||||||||||||||||
Authors: |
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Date: | 19 June 2014 | ||||||||||||||||||||||||||||||||||||||||||||
Journal or Publication Title: | ASME Turbo Expo 2014: Turbine Technical Conference and Exposition | ||||||||||||||||||||||||||||||||||||||||||||
Refereed publication: | Yes | ||||||||||||||||||||||||||||||||||||||||||||
Open Access: | No | ||||||||||||||||||||||||||||||||||||||||||||
Gold Open Access: | No | ||||||||||||||||||||||||||||||||||||||||||||
In SCOPUS: | No | ||||||||||||||||||||||||||||||||||||||||||||
In ISI Web of Science: | No | ||||||||||||||||||||||||||||||||||||||||||||
Volume: | Vol. 6 | ||||||||||||||||||||||||||||||||||||||||||||
DOI: | 10.1115/GT2014-26919 | ||||||||||||||||||||||||||||||||||||||||||||
Page Range: | V006T02A011 | ||||||||||||||||||||||||||||||||||||||||||||
Publisher: | ASME Publishing, New York | ||||||||||||||||||||||||||||||||||||||||||||
Series Name: | ASME Turbo Expo 2014: Turbine Technical Conference and Exposition | ||||||||||||||||||||||||||||||||||||||||||||
ISSN: | GT2014-26919 | ||||||||||||||||||||||||||||||||||||||||||||
ISBN: | 978-0-7918-4575-2 | ||||||||||||||||||||||||||||||||||||||||||||
Status: | Published | ||||||||||||||||||||||||||||||||||||||||||||
Keywords: | Fatigue , Thermal barrier coatings , Temperature gradient | ||||||||||||||||||||||||||||||||||||||||||||
Event Title: | ASME Turbo Expo 2014: Turbine Technical Conference and Exposition | ||||||||||||||||||||||||||||||||||||||||||||
Event Location: | Düsseldorf | ||||||||||||||||||||||||||||||||||||||||||||
Event Type: | international Conference | ||||||||||||||||||||||||||||||||||||||||||||
Event Start Date: | 16 June 2014 | ||||||||||||||||||||||||||||||||||||||||||||
Event End Date: | 20 June 2014 | ||||||||||||||||||||||||||||||||||||||||||||
Organizer: | ASME - American Society of Mechanical Engineers | ||||||||||||||||||||||||||||||||||||||||||||
HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||||||||||||||||||||||||||||||||
HGF - Program: | Aeronautics | ||||||||||||||||||||||||||||||||||||||||||||
HGF - Program Themes: | propulsion systems | ||||||||||||||||||||||||||||||||||||||||||||
DLR - Research area: | Aeronautics | ||||||||||||||||||||||||||||||||||||||||||||
DLR - Program: | L ER - Engine Research | ||||||||||||||||||||||||||||||||||||||||||||
DLR - Research theme (Project): | L - Virtual Engine and Validation methods (old) | ||||||||||||||||||||||||||||||||||||||||||||
Location: | Köln-Porz | ||||||||||||||||||||||||||||||||||||||||||||
Institutes and Institutions: | Institute of Materials Research > Experimental and Numerical Methods | ||||||||||||||||||||||||||||||||||||||||||||
Deposited By: | Bartsch, Dr.-Ing. Marion | ||||||||||||||||||||||||||||||||||||||||||||
Deposited On: | 11 Nov 2014 14:51 | ||||||||||||||||||||||||||||||||||||||||||||
Last Modified: | 24 Apr 2024 19:57 |
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