Development of next generation high temperature materials for high performance gas turbine

Thermal barrier coatings (TBCs) are advanced protective coating systems used to protect metallic substrates at high-temperature application. Currently, the state-of-the-art industrial TBC material is 6-8wt% Y2O3 stabilized ZrO2 (6-8YSZ), but it cannot be used over 1200oC for a long time due to sinte...

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Main Author: Zhang, P.
Other Authors: Choy, K. L.
Published: University College London (University of London) 2016
Subjects:
540
Online Access:https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.746069
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spelling ndltd-bl.uk-oai-ethos.bl.uk-7460692019-03-05T15:54:00ZDevelopment of next generation high temperature materials for high performance gas turbineZhang, P.Choy, K. L.2016Thermal barrier coatings (TBCs) are advanced protective coating systems used to protect metallic substrates at high-temperature application. Currently, the state-of-the-art industrial TBC material is 6-8wt% Y2O3 stabilized ZrO2 (6-8YSZ), but it cannot be used over 1200oC for a long time due to sintering behaviour and phase transformation. The purpose of this thesis was to explore new thermal barrier materials that can be used at high temperature for a long time to replace YSZ. Micron lanthanum titanium aluminum oxide (LaTi2Al9O19, LTA) has been proven as a very promising thermal barrier material due to low thermal conductivity, and excellent phase and thermochemical stability. The main drawback of LTA is the low fracture toughness. Therefore, this thesis studied nano-structured LTA, toughened LTA, and ion doped LTA synthesized by sol- gel method, and LTA and toughened LTA coatings on steel substrate prepared by air plasma spray (APS). The experimental results indicate that compared to micron LTA, the nano-structured LTA had higher coefficients of thermal expansion (CTEs) and comparable thermochemical stability. LTA toughened by 10vol% tetragonal zirconia (LTA-4YSZ) was synthesized by a hybrid sol-gel method. The ceramic composite LTA- 4YSZ had lower thermal conductivity of approximately 1.054 W/(m·K) at room temperature, stable CTEs, better sintering resistance, and mechanical properties. Single phase ion doped LTA by gadolinium was obtained with a Gd3+ content of less than 10mol%, La0.9Gd0.1Ti2Al9O19 (L9G1) had higher CTEs around 11.7×10-6 oC-1 at 950oC, lower thermal conductivity circa. 1.404 W/(m·K) at room temperature, and better sintering resistance than LTA. The APS produced LTA-4YSZ coatings were prepared with optimized granulated powders, which were typical APS coatings with five types of defects: cracks, gaps, cavities, voids, and interspace.540University College London (University of London)https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.746069http://discovery.ucl.ac.uk/1474017/Electronic Thesis or Dissertation
collection NDLTD
sources NDLTD
topic 540
spellingShingle 540
Zhang, P.
Development of next generation high temperature materials for high performance gas turbine
description Thermal barrier coatings (TBCs) are advanced protective coating systems used to protect metallic substrates at high-temperature application. Currently, the state-of-the-art industrial TBC material is 6-8wt% Y2O3 stabilized ZrO2 (6-8YSZ), but it cannot be used over 1200oC for a long time due to sintering behaviour and phase transformation. The purpose of this thesis was to explore new thermal barrier materials that can be used at high temperature for a long time to replace YSZ. Micron lanthanum titanium aluminum oxide (LaTi2Al9O19, LTA) has been proven as a very promising thermal barrier material due to low thermal conductivity, and excellent phase and thermochemical stability. The main drawback of LTA is the low fracture toughness. Therefore, this thesis studied nano-structured LTA, toughened LTA, and ion doped LTA synthesized by sol- gel method, and LTA and toughened LTA coatings on steel substrate prepared by air plasma spray (APS). The experimental results indicate that compared to micron LTA, the nano-structured LTA had higher coefficients of thermal expansion (CTEs) and comparable thermochemical stability. LTA toughened by 10vol% tetragonal zirconia (LTA-4YSZ) was synthesized by a hybrid sol-gel method. The ceramic composite LTA- 4YSZ had lower thermal conductivity of approximately 1.054 W/(m·K) at room temperature, stable CTEs, better sintering resistance, and mechanical properties. Single phase ion doped LTA by gadolinium was obtained with a Gd3+ content of less than 10mol%, La0.9Gd0.1Ti2Al9O19 (L9G1) had higher CTEs around 11.7×10-6 oC-1 at 950oC, lower thermal conductivity circa. 1.404 W/(m·K) at room temperature, and better sintering resistance than LTA. The APS produced LTA-4YSZ coatings were prepared with optimized granulated powders, which were typical APS coatings with five types of defects: cracks, gaps, cavities, voids, and interspace.
author2 Choy, K. L.
author_facet Choy, K. L.
Zhang, P.
author Zhang, P.
author_sort Zhang, P.
title Development of next generation high temperature materials for high performance gas turbine
title_short Development of next generation high temperature materials for high performance gas turbine
title_full Development of next generation high temperature materials for high performance gas turbine
title_fullStr Development of next generation high temperature materials for high performance gas turbine
title_full_unstemmed Development of next generation high temperature materials for high performance gas turbine
title_sort development of next generation high temperature materials for high performance gas turbine
publisher University College London (University of London)
publishDate 2016
url https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.746069
work_keys_str_mv AT zhangp developmentofnextgenerationhightemperaturematerialsforhighperformancegasturbine
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