Thermal barrier coatings for turbine airfoils
Thermal barrier coatings (TBCs) for turbine airfoils in high performance engines represent an advanced materials technology that has both performance and durability benefits. Foremost of the benefits of TBCs is the reduction of heat transferred into air-cooled components. Other potential benefits in...
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Veröffentlicht in: | Thin solid films 1985-05, Vol.127 (1), p.93-106 |
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container_title | Thin solid films |
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creator | Strangman, Thomas E. |
description | Thermal barrier coatings (TBCs) for turbine airfoils in high performance engines represent an advanced materials technology that has both performance and durability benefits.
Foremost of the benefits of TBCs is the reduction of heat transferred into air-cooled components. Other potential benefits include increased resistance to hot corrosion, erosion and oxidation. To achieve these benefits, however, the TBC system must be reliable. Process-microstructure relationships are considered to be key factors in the achievement of TBC durability.
Microstructural requirements for strain tolerance for both plasma-sprayed and electron beam physically vapor-deposited TBC systems are discussed. The effect of processing on bond coating oxidation and durability is also reviewed. |
doi_str_mv | 10.1016/0040-6090(85)90215-9 |
format | Article |
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Foremost of the benefits of TBCs is the reduction of heat transferred into air-cooled components. Other potential benefits include increased resistance to hot corrosion, erosion and oxidation. To achieve these benefits, however, the TBC system must be reliable. Process-microstructure relationships are considered to be key factors in the achievement of TBC durability.
Microstructural requirements for strain tolerance for both plasma-sprayed and electron beam physically vapor-deposited TBC systems are discussed. The effect of processing on bond coating oxidation and durability is also reviewed.</description><identifier>ISSN: 0040-6090</identifier><identifier>EISSN: 1879-2731</identifier><identifier>DOI: 10.1016/0040-6090(85)90215-9</identifier><identifier>CODEN: THSFAP</identifier><language>eng</language><publisher>Lausanne: Elsevier B.V</publisher><subject>Applications ; Applied sciences ; Engineering techniques in metallurgy. Applications. Other aspects ; Exact sciences and technology ; Metals. Metallurgy</subject><ispartof>Thin solid films, 1985-05, Vol.127 (1), p.93-106</ispartof><rights>1985</rights><rights>1986 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c430t-23e05196930d339e5e6660c989e317c3bd0f9124cc682c0e4f52153f2760ae3</citedby><cites>FETCH-LOGICAL-c430t-23e05196930d339e5e6660c989e317c3bd0f9124cc682c0e4f52153f2760ae3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/0040-6090(85)90215-9$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,780,784,3550,27924,27925,45995</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=8721788$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Strangman, Thomas E.</creatorcontrib><title>Thermal barrier coatings for turbine airfoils</title><title>Thin solid films</title><description>Thermal barrier coatings (TBCs) for turbine airfoils in high performance engines represent an advanced materials technology that has both performance and durability benefits.
Foremost of the benefits of TBCs is the reduction of heat transferred into air-cooled components. Other potential benefits include increased resistance to hot corrosion, erosion and oxidation. To achieve these benefits, however, the TBC system must be reliable. Process-microstructure relationships are considered to be key factors in the achievement of TBC durability.
Microstructural requirements for strain tolerance for both plasma-sprayed and electron beam physically vapor-deposited TBC systems are discussed. The effect of processing on bond coating oxidation and durability is also reviewed.</description><subject>Applications</subject><subject>Applied sciences</subject><subject>Engineering techniques in metallurgy. Applications. Other aspects</subject><subject>Exact sciences and technology</subject><subject>Metals. Metallurgy</subject><issn>0040-6090</issn><issn>1879-2731</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1985</creationdate><recordtype>article</recordtype><recordid>eNp9kEtPwzAQhC0EEqXwDzjkgBAcAutHHPuChCpeUiUO9G65zhqM0rjYCRL_npRWPXLayzczO0PIOYUbClTeAggoJWi4UtW1BkarUh-QCVW1LlnN6SGZ7JFjcpLzJwBQxviElIsPTCvbFkubUsBUuGj70L3nwsdU9ENahg4LG5KPoc2n5MjbNuPZ7k7J2-PDYvZczl-fXmb389IJDn3JOEJFtdQcGs41ViilBKeVRk5rx5cNeE2ZcE4q5gCFr8afuWe1BIt8Si63rusUvwbMvVmF7LBtbYdxyIYJxXVNxQiKLehSzDmhN-sUVjb9GApms4zZ1Dab2kZV5m8Zo0fZxc7fZmdbn2znQt5rVc1ordSI3W0xHJt-j9uY7AJ2DpuQ0PWmieH_nF8dj3T9</recordid><startdate>19850510</startdate><enddate>19850510</enddate><creator>Strangman, Thomas E.</creator><general>Elsevier B.V</general><general>Elsevier Science</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>8BQ</scope><scope>8FD</scope><scope>JG9</scope></search><sort><creationdate>19850510</creationdate><title>Thermal barrier coatings for turbine airfoils</title><author>Strangman, Thomas E.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c430t-23e05196930d339e5e6660c989e317c3bd0f9124cc682c0e4f52153f2760ae3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1985</creationdate><topic>Applications</topic><topic>Applied sciences</topic><topic>Engineering techniques in metallurgy. Applications. Other aspects</topic><topic>Exact sciences and technology</topic><topic>Metals. Metallurgy</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Strangman, Thomas E.</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><jtitle>Thin solid films</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Strangman, Thomas E.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Thermal barrier coatings for turbine airfoils</atitle><jtitle>Thin solid films</jtitle><date>1985-05-10</date><risdate>1985</risdate><volume>127</volume><issue>1</issue><spage>93</spage><epage>106</epage><pages>93-106</pages><issn>0040-6090</issn><eissn>1879-2731</eissn><coden>THSFAP</coden><abstract>Thermal barrier coatings (TBCs) for turbine airfoils in high performance engines represent an advanced materials technology that has both performance and durability benefits.
Foremost of the benefits of TBCs is the reduction of heat transferred into air-cooled components. Other potential benefits include increased resistance to hot corrosion, erosion and oxidation. To achieve these benefits, however, the TBC system must be reliable. Process-microstructure relationships are considered to be key factors in the achievement of TBC durability.
Microstructural requirements for strain tolerance for both plasma-sprayed and electron beam physically vapor-deposited TBC systems are discussed. The effect of processing on bond coating oxidation and durability is also reviewed.</abstract><cop>Lausanne</cop><pub>Elsevier B.V</pub><doi>10.1016/0040-6090(85)90215-9</doi><tpages>14</tpages></addata></record> |
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subjects | Applications Applied sciences Engineering techniques in metallurgy. Applications. Other aspects Exact sciences and technology Metals. Metallurgy |
title | Thermal barrier coatings for turbine airfoils |
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