Thermally-stabilized thermal barrier coating and process therefor
A thermal barrier coating (TBC 26 ) and method for forming the TBC ( 26 ) on a component ( 10 ) characterized by a stabilized microstructure that resists grain growth, sintering and pore coarsening or coalescence during high temperature excursions. The TBC ( 26 ) contains elemental carbon and/or a c...
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creator | Movchan, Boris Rudoy, Yuriy Nerodenko, Leonella Darolia, Ramgopal Spitsberg, Irene Thompson, Anthony Johnson, Curtis Wortman, David |
description | A thermal barrier coating (TBC
26
) and method for forming the TBC (
26
) on a component (
10
) characterized by a stabilized microstructure that resists grain growth, sintering and pore coarsening or coalescence during high temperature excursions. The TBC (
26
) contains elemental carbon and/or a carbon-containing gas that increase the amount of porosity (
32
) initially within the TBC (
26
) and form additional fine closed porosity (
32
) within the TBC (
26
) during subsequent exposures to high temperatures. A first method involves incorporating elemental carbon precipitates by evaporation into the TBC microstructure. A second method is to directly incorporate an insoluble gas, such as a carbon-containing gas, into an as-deposited TBC (
26
) and then partially sinter the TBC (
26
) to entrap the gas and produce fine stable porosity within the TBC (
26
). |
format | Patent |
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26
) and method for forming the TBC (
26
) on a component (
10
) characterized by a stabilized microstructure that resists grain growth, sintering and pore coarsening or coalescence during high temperature excursions. The TBC (
26
) contains elemental carbon and/or a carbon-containing gas that increase the amount of porosity (
32
) initially within the TBC (
26
) and form additional fine closed porosity (
32
) within the TBC (
26
) during subsequent exposures to high temperatures. A first method involves incorporating elemental carbon precipitates by evaporation into the TBC microstructure. A second method is to directly incorporate an insoluble gas, such as a carbon-containing gas, into an as-deposited TBC (
26
) and then partially sinter the TBC (
26
) to entrap the gas and produce fine stable porosity within the TBC (
26
).</description><language>eng</language><creationdate>2003</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20030129378$$EPDF$$P50$$Guspatents$$Hfree_for_read</linktopdf><link.rule.ids>230,308,776,869,881,64032</link.rule.ids><linktorsrc>$$Uhttps://patentcenter.uspto.gov/applications/10064791$$EView_record_in_USPTO$$FView_record_in_$$GUSPTO$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Movchan, Boris</creatorcontrib><creatorcontrib>Rudoy, Yuriy</creatorcontrib><creatorcontrib>Nerodenko, Leonella</creatorcontrib><creatorcontrib>Darolia, Ramgopal</creatorcontrib><creatorcontrib>Spitsberg, Irene</creatorcontrib><creatorcontrib>Thompson, Anthony</creatorcontrib><creatorcontrib>Johnson, Curtis</creatorcontrib><creatorcontrib>Wortman, David</creatorcontrib><title>Thermally-stabilized thermal barrier coating and process therefor</title><description>A thermal barrier coating (TBC
26
) and method for forming the TBC (
26
) on a component (
10
) characterized by a stabilized microstructure that resists grain growth, sintering and pore coarsening or coalescence during high temperature excursions. The TBC (
26
) contains elemental carbon and/or a carbon-containing gas that increase the amount of porosity (
32
) initially within the TBC (
26
) and form additional fine closed porosity (
32
) within the TBC (
26
) during subsequent exposures to high temperatures. A first method involves incorporating elemental carbon precipitates by evaporation into the TBC microstructure. A second method is to directly incorporate an insoluble gas, such as a carbon-containing gas, into an as-deposited TBC (
26
) and then partially sinter the TBC (
26
) to entrap the gas and produce fine stable porosity within the TBC (
26
).</description><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2003</creationdate><recordtype>patent</recordtype><sourceid>EFI</sourceid><recordid>eNrjZHAMyUgtyk3MyanULS5JTMrMyaxKTVEogQgqJCUWFWWmFikk5yeWZOalKyTmpSgUFOUnpxYXg9WkpuUX8TCwpiXmFKfyQmluBk031xBnD93S4oLEktS8kuL4xIKCnMxkoBH5ecXxRgYGxgaGRpbG5hbGpKgFABGmOVI</recordid><startdate>20030710</startdate><enddate>20030710</enddate><creator>Movchan, Boris</creator><creator>Rudoy, Yuriy</creator><creator>Nerodenko, Leonella</creator><creator>Darolia, Ramgopal</creator><creator>Spitsberg, Irene</creator><creator>Thompson, Anthony</creator><creator>Johnson, Curtis</creator><creator>Wortman, David</creator><scope>EFI</scope></search><sort><creationdate>20030710</creationdate><title>Thermally-stabilized thermal barrier coating and process therefor</title><author>Movchan, Boris ; Rudoy, Yuriy ; Nerodenko, Leonella ; Darolia, Ramgopal ; Spitsberg, Irene ; Thompson, Anthony ; Johnson, Curtis ; Wortman, David</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-uspatents_applications_200301293783</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2003</creationdate><toplevel>online_resources</toplevel><creatorcontrib>Movchan, Boris</creatorcontrib><creatorcontrib>Rudoy, Yuriy</creatorcontrib><creatorcontrib>Nerodenko, Leonella</creatorcontrib><creatorcontrib>Darolia, Ramgopal</creatorcontrib><creatorcontrib>Spitsberg, Irene</creatorcontrib><creatorcontrib>Thompson, Anthony</creatorcontrib><creatorcontrib>Johnson, Curtis</creatorcontrib><creatorcontrib>Wortman, David</creatorcontrib><collection>USPTO Published Applications</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Movchan, Boris</au><au>Rudoy, Yuriy</au><au>Nerodenko, Leonella</au><au>Darolia, Ramgopal</au><au>Spitsberg, Irene</au><au>Thompson, Anthony</au><au>Johnson, Curtis</au><au>Wortman, David</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Thermally-stabilized thermal barrier coating and process therefor</title><date>2003-07-10</date><risdate>2003</risdate><abstract>A thermal barrier coating (TBC
26
) and method for forming the TBC (
26
) on a component (
10
) characterized by a stabilized microstructure that resists grain growth, sintering and pore coarsening or coalescence during high temperature excursions. The TBC (
26
) contains elemental carbon and/or a carbon-containing gas that increase the amount of porosity (
32
) initially within the TBC (
26
) and form additional fine closed porosity (
32
) within the TBC (
26
) during subsequent exposures to high temperatures. A first method involves incorporating elemental carbon precipitates by evaporation into the TBC microstructure. A second method is to directly incorporate an insoluble gas, such as a carbon-containing gas, into an as-deposited TBC (
26
) and then partially sinter the TBC (
26
) to entrap the gas and produce fine stable porosity within the TBC (
26
).</abstract><oa>free_for_read</oa></addata></record> |
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recordid | cdi_uspatents_applications_20030129378 |
source | USPTO Published Applications |
title | Thermally-stabilized thermal barrier coating and process therefor |
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