Thermal cycling behavior of (Gd0.9Yb0.1)2Zr2O7/8YSZ gradient thermal barrier coatings deposited on Hf-doped NiAl bond coat by EB-PVD
Authors:
- Hailin ZhangHZHailin Zhang
- Lei GuoLGLei Guo
- Yue MaYMYue Ma
- Hui PengHPHui Peng
- Hongbo GuoHGHongbo Guo
- Shengkai GongSGShengkai Gong
- 1 November 2014
- journal article
- Published by Elsevier in Surface and Coatings Technology
- Vol. 258, 950-955
Abstract
No abstract availableFunding Information
- National Key Research and Development Program of China (2012CB625100, 2012AA03A512)
- National Natural Science Foundation of China (51201005, 51231001, 51271011)
This publication has 33 references indexed in Scilit:
- Influence of partial substitution of Sc2O3 with Gd2O3 on the phase stability and thermal conductivity of Sc2O3-doped ZrO2Ceramics International, 2013
- Properties of plasma sprayed La2Zr2O7 coating fabricated from powder synthesized by a single-step solution combustion methodSurface and Coatings Technology, 2013
- Characterization of microstructure and thermal properties of Gd2Zr2O7-type thermal barrier coatingJournal of the European Ceramic Society, 2012
- Jet Engine Coatings for Resisting Volcanic Ash DamageAdvanced Materials, 2011
- Effects of deposition conditions on composition and thermal cycling life of lanthanum zirconate coatingsSurface and Coatings Technology, 2008
- The influence of oxides on the performance of advanced gas turbinesJournal of the European Ceramic Society, 2008
- Thermal barrier coating materialsMaterials Today, 2005
- EB-PVD processing of pyrochlore-structured La2Zr2O7-based TBCsSurface and Coatings Technology, 2004
- Low thermal conductivity and high temperature stability of ZrO2–Y2O3–La2O3 coatings produced by electron beam PVDScripta Materialia, 2004
- Thermal Barrier Coatings for Gas-Turbine Engine ApplicationsScience, 2002