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Delamination-Indicating Thermal Barrier CoatingsThe risk of premature failure of thermal barrier coatings (TBCs), typically composed of yttria-stabilized zirconia (YSZ), compromises the reliability of TBCs used to provide thermal protection for turbine engine components. Unfortunately, TBC delamination proceeds well beneath the TBC surface and cannot be monitored by visible inspection. Nondestructive diagnostic tools that could reliably probe the subsurface damage state of TBCs would alleviate the risk of TBC premature failure by indicating when the TBC needs to be replaced before the level of TBC damage threatens engine performance or safety. To meet this need, a new coating design for thermal barrier coatings (TBCs) that are self-indicating for delamination has been successfully implemented by incorporating a europium-doped luminescent sublayer at the base of a TBC composed of YSZ. The luminescent sublayer has the same YSZ composition as the rest of the TBC except for the addition of low-level europium doping and therefore does not alter TBC performance.
Document ID
20100010925
Acquisition Source
Glenn Research Center
Document Type
Other - NASA Tech Brief
Authors
Eldridge, Jeffrey I.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
September 1, 2007
Publication Information
Publication: NASA Tech Briefs, September 2007
Subject Category
Man/System Technology And Life Support
Report/Patent Number
LEW-17929-1/30-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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