Loading…

Anisotropic Thermal Diffusivities of Plasma-Sprayed Thermal Barrier Coatings

Thermal barrier coatings (TBCs) are used to shield the blades of gas turbines from heat and wear. There is a pressing need to evaluate the thermal conductivity of TBCs in the thermal design of advanced gas turbines with high energy efficiency. These TBCs consist of a ceramic-based top coat and a bon...

Full description

Saved in:
Bibliographic Details
Published in:International journal of thermophysics 2017-09, Vol.38 (9), Article 134
Main Authors: Akoshima, Megumi, Takahashi, Satoru
Format: Article
Language:English
Subjects:
Citations: Items that this one cites
Items that cite this one
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by cdi_FETCH-LOGICAL-c382t-daef5711e35f52c8cf1ae12063b2895ffb61d415cf267feb99c5b0bfd6fbac153
cites cdi_FETCH-LOGICAL-c382t-daef5711e35f52c8cf1ae12063b2895ffb61d415cf267feb99c5b0bfd6fbac153
container_end_page
container_issue 9
container_start_page
container_title International journal of thermophysics
container_volume 38
creator Akoshima, Megumi
Takahashi, Satoru
description Thermal barrier coatings (TBCs) are used to shield the blades of gas turbines from heat and wear. There is a pressing need to evaluate the thermal conductivity of TBCs in the thermal design of advanced gas turbines with high energy efficiency. These TBCs consist of a ceramic-based top coat and a bond coat on a superalloy substrate. Usually, the focus is on the thermal conductivity in the thickness direction of the TBC because heat tends to diffuse from the surface of the top coat to the substrate. However, the in-plane thermal conductivity is also important in the thermal design of gas turbines because the temperature distribution within the turbine cannot be ignored. Accordingly, a method is developed in this study for measuring the in-plane thermal diffusivity of the top coat. Yttria-stabilized zirconia top coats are prepared by thermal spraying under different conditions. The in-plane and cross-plane thermal diffusivities of the top coats are measured by the flash method to investigate the anisotropy of thermal conduction in a TBC. It is found that the in-plane thermal diffusivity is higher than the cross-plane one for each top coat and that the top coats have significantly anisotropic thermal diffusivity. The cross-sectional and in-plane microstructures of the top coats are observed, from which their porosities are evaluated. The thermal diffusivity and its anisotropy are discussed in detail in relation to microstructure and porosity.
doi_str_mv 10.1007/s10765-017-2267-x
format article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_1919261887</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>1919261887</sourcerecordid><originalsourceid>FETCH-LOGICAL-c382t-daef5711e35f52c8cf1ae12063b2895ffb61d415cf267feb99c5b0bfd6fbac153</originalsourceid><addsrcrecordid>eNp1kE1LAzEURYMoWKs_wN2A62hexiSTZa2fUFCwgruQyeTVlHZmTKbS_nunjIgbV29z7r28Q8g5sEtgTF0lYEoKykBRzqWi2wMyAqE41UKqQzJioAXVvHg_JicpLRljWul8RGaTOqSmi00bXDb_8HFtV9ltQNyk8BW64FPWYPaysmlt6Wsb7c5Xv9yNjTH4mE0b24V6kU7JEdpV8mc_d0ze7u_m00c6e354mk5m1OUF72hlPQoF4HOBgrvCIVgPnMm85IUWiKWE6hqEw_4T9KXWTpSsxEpiaR2IfEwuht42Np8bnzqzbDax7icNaNBcQlGonoKBcrFJKXo0bQxrG3cGmNlLM4M000sze2lm22f4kEk9Wy98_NP8b-gbexpxKw</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1919261887</pqid></control><display><type>article</type><title>Anisotropic Thermal Diffusivities of Plasma-Sprayed Thermal Barrier Coatings</title><source>Springer Link</source><creator>Akoshima, Megumi ; Takahashi, Satoru</creator><creatorcontrib>Akoshima, Megumi ; Takahashi, Satoru</creatorcontrib><description>Thermal barrier coatings (TBCs) are used to shield the blades of gas turbines from heat and wear. There is a pressing need to evaluate the thermal conductivity of TBCs in the thermal design of advanced gas turbines with high energy efficiency. These TBCs consist of a ceramic-based top coat and a bond coat on a superalloy substrate. Usually, the focus is on the thermal conductivity in the thickness direction of the TBC because heat tends to diffuse from the surface of the top coat to the substrate. However, the in-plane thermal conductivity is also important in the thermal design of gas turbines because the temperature distribution within the turbine cannot be ignored. Accordingly, a method is developed in this study for measuring the in-plane thermal diffusivity of the top coat. Yttria-stabilized zirconia top coats are prepared by thermal spraying under different conditions. The in-plane and cross-plane thermal diffusivities of the top coats are measured by the flash method to investigate the anisotropy of thermal conduction in a TBC. It is found that the in-plane thermal diffusivity is higher than the cross-plane one for each top coat and that the top coats have significantly anisotropic thermal diffusivity. The cross-sectional and in-plane microstructures of the top coats are observed, from which their porosities are evaluated. The thermal diffusivity and its anisotropy are discussed in detail in relation to microstructure and porosity.</description><identifier>ISSN: 0195-928X</identifier><identifier>EISSN: 1572-9567</identifier><identifier>DOI: 10.1007/s10765-017-2267-x</identifier><language>eng</language><publisher>New York: Springer US</publisher><subject>Anisotropy ; Asian Thermophysical Properties Conference ; ATPC 2016: Selected Papers of the 11th Asian Thermophysical Properties Conference ; Classical Mechanics ; Coatings ; Condensed Matter Physics ; Diffusivity ; Evaluation ; Gas turbines ; Geophysics ; Heat conductivity ; Heat transfer ; Industrial Chemistry/Chemical Engineering ; Microstructure ; Physical Chemistry ; Physics ; Spraying ; Substrates ; Superalloys ; Temperature distribution ; Thermal barrier coatings ; Thermal conductivity ; Thermal design ; Thermal diffusivity ; Thermal energy ; Thermodynamics ; Turbine blades ; Yttria-stabilized zirconia ; Yttrium oxide</subject><ispartof>International journal of thermophysics, 2017-09, Vol.38 (9), Article 134</ispartof><rights>Springer Science+Business Media, LLC 2017</rights><rights>Springer Science+Business Media, LLC 2017.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c382t-daef5711e35f52c8cf1ae12063b2895ffb61d415cf267feb99c5b0bfd6fbac153</citedby><cites>FETCH-LOGICAL-c382t-daef5711e35f52c8cf1ae12063b2895ffb61d415cf267feb99c5b0bfd6fbac153</cites><orcidid>0000-0003-1092-7339</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Akoshima, Megumi</creatorcontrib><creatorcontrib>Takahashi, Satoru</creatorcontrib><title>Anisotropic Thermal Diffusivities of Plasma-Sprayed Thermal Barrier Coatings</title><title>International journal of thermophysics</title><addtitle>Int J Thermophys</addtitle><description>Thermal barrier coatings (TBCs) are used to shield the blades of gas turbines from heat and wear. There is a pressing need to evaluate the thermal conductivity of TBCs in the thermal design of advanced gas turbines with high energy efficiency. These TBCs consist of a ceramic-based top coat and a bond coat on a superalloy substrate. Usually, the focus is on the thermal conductivity in the thickness direction of the TBC because heat tends to diffuse from the surface of the top coat to the substrate. However, the in-plane thermal conductivity is also important in the thermal design of gas turbines because the temperature distribution within the turbine cannot be ignored. Accordingly, a method is developed in this study for measuring the in-plane thermal diffusivity of the top coat. Yttria-stabilized zirconia top coats are prepared by thermal spraying under different conditions. The in-plane and cross-plane thermal diffusivities of the top coats are measured by the flash method to investigate the anisotropy of thermal conduction in a TBC. It is found that the in-plane thermal diffusivity is higher than the cross-plane one for each top coat and that the top coats have significantly anisotropic thermal diffusivity. The cross-sectional and in-plane microstructures of the top coats are observed, from which their porosities are evaluated. The thermal diffusivity and its anisotropy are discussed in detail in relation to microstructure and porosity.</description><subject>Anisotropy</subject><subject>Asian Thermophysical Properties Conference</subject><subject>ATPC 2016: Selected Papers of the 11th Asian Thermophysical Properties Conference</subject><subject>Classical Mechanics</subject><subject>Coatings</subject><subject>Condensed Matter Physics</subject><subject>Diffusivity</subject><subject>Evaluation</subject><subject>Gas turbines</subject><subject>Geophysics</subject><subject>Heat conductivity</subject><subject>Heat transfer</subject><subject>Industrial Chemistry/Chemical Engineering</subject><subject>Microstructure</subject><subject>Physical Chemistry</subject><subject>Physics</subject><subject>Spraying</subject><subject>Substrates</subject><subject>Superalloys</subject><subject>Temperature distribution</subject><subject>Thermal barrier coatings</subject><subject>Thermal conductivity</subject><subject>Thermal design</subject><subject>Thermal diffusivity</subject><subject>Thermal energy</subject><subject>Thermodynamics</subject><subject>Turbine blades</subject><subject>Yttria-stabilized zirconia</subject><subject>Yttrium oxide</subject><issn>0195-928X</issn><issn>1572-9567</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNp1kE1LAzEURYMoWKs_wN2A62hexiSTZa2fUFCwgruQyeTVlHZmTKbS_nunjIgbV29z7r28Q8g5sEtgTF0lYEoKykBRzqWi2wMyAqE41UKqQzJioAXVvHg_JicpLRljWul8RGaTOqSmi00bXDb_8HFtV9ltQNyk8BW64FPWYPaysmlt6Wsb7c5Xv9yNjTH4mE0b24V6kU7JEdpV8mc_d0ze7u_m00c6e354mk5m1OUF72hlPQoF4HOBgrvCIVgPnMm85IUWiKWE6hqEw_4T9KXWTpSsxEpiaR2IfEwuht42Np8bnzqzbDax7icNaNBcQlGonoKBcrFJKXo0bQxrG3cGmNlLM4M000sze2lm22f4kEk9Wy98_NP8b-gbexpxKw</recordid><startdate>20170901</startdate><enddate>20170901</enddate><creator>Akoshima, Megumi</creator><creator>Takahashi, Satoru</creator><general>Springer US</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><orcidid>https://orcid.org/0000-0003-1092-7339</orcidid></search><sort><creationdate>20170901</creationdate><title>Anisotropic Thermal Diffusivities of Plasma-Sprayed Thermal Barrier Coatings</title><author>Akoshima, Megumi ; Takahashi, Satoru</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c382t-daef5711e35f52c8cf1ae12063b2895ffb61d415cf267feb99c5b0bfd6fbac153</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Anisotropy</topic><topic>Asian Thermophysical Properties Conference</topic><topic>ATPC 2016: Selected Papers of the 11th Asian Thermophysical Properties Conference</topic><topic>Classical Mechanics</topic><topic>Coatings</topic><topic>Condensed Matter Physics</topic><topic>Diffusivity</topic><topic>Evaluation</topic><topic>Gas turbines</topic><topic>Geophysics</topic><topic>Heat conductivity</topic><topic>Heat transfer</topic><topic>Industrial Chemistry/Chemical Engineering</topic><topic>Microstructure</topic><topic>Physical Chemistry</topic><topic>Physics</topic><topic>Spraying</topic><topic>Substrates</topic><topic>Superalloys</topic><topic>Temperature distribution</topic><topic>Thermal barrier coatings</topic><topic>Thermal conductivity</topic><topic>Thermal design</topic><topic>Thermal diffusivity</topic><topic>Thermal energy</topic><topic>Thermodynamics</topic><topic>Turbine blades</topic><topic>Yttria-stabilized zirconia</topic><topic>Yttrium oxide</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Akoshima, Megumi</creatorcontrib><creatorcontrib>Takahashi, Satoru</creatorcontrib><collection>CrossRef</collection><jtitle>International journal of thermophysics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Akoshima, Megumi</au><au>Takahashi, Satoru</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Anisotropic Thermal Diffusivities of Plasma-Sprayed Thermal Barrier Coatings</atitle><jtitle>International journal of thermophysics</jtitle><stitle>Int J Thermophys</stitle><date>2017-09-01</date><risdate>2017</risdate><volume>38</volume><issue>9</issue><artnum>134</artnum><issn>0195-928X</issn><eissn>1572-9567</eissn><abstract>Thermal barrier coatings (TBCs) are used to shield the blades of gas turbines from heat and wear. There is a pressing need to evaluate the thermal conductivity of TBCs in the thermal design of advanced gas turbines with high energy efficiency. These TBCs consist of a ceramic-based top coat and a bond coat on a superalloy substrate. Usually, the focus is on the thermal conductivity in the thickness direction of the TBC because heat tends to diffuse from the surface of the top coat to the substrate. However, the in-plane thermal conductivity is also important in the thermal design of gas turbines because the temperature distribution within the turbine cannot be ignored. Accordingly, a method is developed in this study for measuring the in-plane thermal diffusivity of the top coat. Yttria-stabilized zirconia top coats are prepared by thermal spraying under different conditions. The in-plane and cross-plane thermal diffusivities of the top coats are measured by the flash method to investigate the anisotropy of thermal conduction in a TBC. It is found that the in-plane thermal diffusivity is higher than the cross-plane one for each top coat and that the top coats have significantly anisotropic thermal diffusivity. The cross-sectional and in-plane microstructures of the top coats are observed, from which their porosities are evaluated. The thermal diffusivity and its anisotropy are discussed in detail in relation to microstructure and porosity.</abstract><cop>New York</cop><pub>Springer US</pub><doi>10.1007/s10765-017-2267-x</doi><orcidid>https://orcid.org/0000-0003-1092-7339</orcidid></addata></record>
fulltext fulltext
identifier ISSN: 0195-928X
ispartof International journal of thermophysics, 2017-09, Vol.38 (9), Article 134
issn 0195-928X
1572-9567
language eng
recordid cdi_proquest_journals_1919261887
source Springer Link
subjects Anisotropy
Asian Thermophysical Properties Conference
ATPC 2016: Selected Papers of the 11th Asian Thermophysical Properties Conference
Classical Mechanics
Coatings
Condensed Matter Physics
Diffusivity
Evaluation
Gas turbines
Geophysics
Heat conductivity
Heat transfer
Industrial Chemistry/Chemical Engineering
Microstructure
Physical Chemistry
Physics
Spraying
Substrates
Superalloys
Temperature distribution
Thermal barrier coatings
Thermal conductivity
Thermal design
Thermal diffusivity
Thermal energy
Thermodynamics
Turbine blades
Yttria-stabilized zirconia
Yttrium oxide
title Anisotropic Thermal Diffusivities of Plasma-Sprayed Thermal Barrier Coatings
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-06T10%3A12%3A22IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Anisotropic%20Thermal%20Diffusivities%20of%20Plasma-Sprayed%20Thermal%20Barrier%20Coatings&rft.jtitle=International%20journal%20of%20thermophysics&rft.au=Akoshima,%20Megumi&rft.date=2017-09-01&rft.volume=38&rft.issue=9&rft.artnum=134&rft.issn=0195-928X&rft.eissn=1572-9567&rft_id=info:doi/10.1007/s10765-017-2267-x&rft_dat=%3Cproquest_cross%3E1919261887%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c382t-daef5711e35f52c8cf1ae12063b2895ffb61d415cf267feb99c5b0bfd6fbac153%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=1919261887&rft_id=info:pmid/&rfr_iscdi=true