Novel Lanthanum Zirconate Thermal Barrier Coatings for Gas Turbines

dc.contributor.authorZhang, Jing
dc.contributor.authorGuo, Xingye
dc.contributor.authorJung, Yeon-Gil
dc.contributor.authorLi, Li
dc.contributor.authorKnapp, James
dc.date.accessioned2016-05-03T18:36:43Z
dc.date.available2016-05-03T18:36:43Z
dc.date.issued2015-04-17
dc.descriptionposter abstracten_US
dc.description.abstractPyrochlore lanthanum zirconate (La2Zr2O7) is a very promising candidate material for thermal barrier coating (TBC) applications. Layered microstructure was designed and prepared using air plasma spray to improve the thermal durability. The physical, mechanical and thermal properties of the coatings were measured. La2Zr2O7 shows outstanding phase stability in high temperatures and lower thermal conductivity than commercial 8YSZ TBCs material. Coating lifetime performance was also estimated through the JETS (Jet Engine Thermal Simulation) and TGMF (Thermal Gradient Mechanical Fatigue) tests.en_US
dc.identifier.citationJing Zhang, Xingye Guo, Yeon-Gil Jung,Li Li, and James Knapp. 2015 April 17.Novel Lanthanum Zirconate Thermal Barrier Coatings for Gas Turbines. Poster session presented at IUPUI Research Day 2015, Indianapolis, Indiana.en_US
dc.identifier.urihttps://hdl.handle.net/1805/9508
dc.language.isoen_USen_US
dc.publisherOffice of the Vice Chancellor for Researchen_US
dc.subjectPyrochlore lanthanum zirconate (La2Zr2O7)en_US
dc.subjectthermal barrier coating (TBC)en_US
dc.subjectGas Turbinesen_US
dc.titleNovel Lanthanum Zirconate Thermal Barrier Coatings for Gas Turbinesen_US
dc.typePosteren_US
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