Recent Developments in the Field of Thermal Barrier Coatings

Abstract Conventional thermal barrier coating (TBC) systems consist of a duplex structure with a metallic bondcoat and a ceramic, heat-isolative topcoat. Several recent research activities are concentrating on developing improved bondcoat or topcoat materials; for the topcoat especially, those with...
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Gespeichert in:

Autor*in:	Vassen, Robert [verfasserIn] Stuke, Alexandra Stöver, Detlev

Format:	Artikel
Sprache:	Englisch

Erschienen:	2009

Schlagwörter:	ceramic top coats gas turbines multifunctional coatings plasma spraying thermal barrier coating

Anmerkung:	© ASM International 2009

Übergeordnetes Werk:	Enthalten in: Journal of thermal spray technology - Springer US, 1992, 18(2009), 2 vom: 26. März, Seite 181-186
Übergeordnetes Werk:	volume:18 ; year:2009 ; number:2 ; day:26 ; month:03 ; pages:181-186

Links:	Volltext

DOI / URN:	10.1007/s11666-009-9312-7

Katalog-ID:	OLC2060557127

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allfields	10.1007/s11666-009-9312-7 doi (DE-627)OLC2060557127 (DE-He213)s11666-009-9312-7-p DE-627 ger DE-627 rakwb eng 670 VZ Vassen, Robert verfasserin aut Recent Developments in the Field of Thermal Barrier Coatings 2009 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © ASM International 2009 Abstract Conventional thermal barrier coating (TBC) systems consist of a duplex structure with a metallic bondcoat and a ceramic, heat-isolative topcoat. Several recent research activities are concentrating on developing improved bondcoat or topcoat materials; for the topcoat especially, those with reduced thermal conductivity are investigated. Using advanced topcoat materials, the ceramic coating can be further divided into layers with different functions. One example is the double-layer system in which conventional yttria-stabilized zirconia (YSZ) is used as bottom and new materials such as pyrochlores or perovskites are used as topcoat layers. These systems demonstrated an improved temperature capability compared to standard YSZ. In addition, new functions are introduced within the TBCs. These can be sensorial properties that can be used for an improved temperature control or even for monitoring remaining lifetime. Further increased application temperatures will also lead to efforts for a further improvement of the reflectivity of the coatings to reduce the radiative heat transfer through the TBC. ceramic top coats gas turbines multifunctional coatings plasma spraying thermal barrier coating Stuke, Alexandra aut Stöver, Detlev aut Enthalten in Journal of thermal spray technology Springer US, 1992 18(2009), 2 vom: 26. März, Seite 181-186 (DE-627)131101544 (DE-600)1118266-0 (DE-576)038867699 1059-9630 nnns volume:18 year:2009 number:2 day:26 month:03 pages:181-186 https://doi.org/10.1007/s11666-009-9312-7 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_60 GBV_ILN_70 AR 18 2009 2 26 03 181-186
spelling	10.1007/s11666-009-9312-7 doi (DE-627)OLC2060557127 (DE-He213)s11666-009-9312-7-p DE-627 ger DE-627 rakwb eng 670 VZ Vassen, Robert verfasserin aut Recent Developments in the Field of Thermal Barrier Coatings 2009 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © ASM International 2009 Abstract Conventional thermal barrier coating (TBC) systems consist of a duplex structure with a metallic bondcoat and a ceramic, heat-isolative topcoat. Several recent research activities are concentrating on developing improved bondcoat or topcoat materials; for the topcoat especially, those with reduced thermal conductivity are investigated. Using advanced topcoat materials, the ceramic coating can be further divided into layers with different functions. One example is the double-layer system in which conventional yttria-stabilized zirconia (YSZ) is used as bottom and new materials such as pyrochlores or perovskites are used as topcoat layers. These systems demonstrated an improved temperature capability compared to standard YSZ. In addition, new functions are introduced within the TBCs. These can be sensorial properties that can be used for an improved temperature control or even for monitoring remaining lifetime. Further increased application temperatures will also lead to efforts for a further improvement of the reflectivity of the coatings to reduce the radiative heat transfer through the TBC. ceramic top coats gas turbines multifunctional coatings plasma spraying thermal barrier coating Stuke, Alexandra aut Stöver, Detlev aut Enthalten in Journal of thermal spray technology Springer US, 1992 18(2009), 2 vom: 26. März, Seite 181-186 (DE-627)131101544 (DE-600)1118266-0 (DE-576)038867699 1059-9630 nnns volume:18 year:2009 number:2 day:26 month:03 pages:181-186 https://doi.org/10.1007/s11666-009-9312-7 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_60 GBV_ILN_70 AR 18 2009 2 26 03 181-186
allfields_unstemmed	10.1007/s11666-009-9312-7 doi (DE-627)OLC2060557127 (DE-He213)s11666-009-9312-7-p DE-627 ger DE-627 rakwb eng 670 VZ Vassen, Robert verfasserin aut Recent Developments in the Field of Thermal Barrier Coatings 2009 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © ASM International 2009 Abstract Conventional thermal barrier coating (TBC) systems consist of a duplex structure with a metallic bondcoat and a ceramic, heat-isolative topcoat. Several recent research activities are concentrating on developing improved bondcoat or topcoat materials; for the topcoat especially, those with reduced thermal conductivity are investigated. Using advanced topcoat materials, the ceramic coating can be further divided into layers with different functions. One example is the double-layer system in which conventional yttria-stabilized zirconia (YSZ) is used as bottom and new materials such as pyrochlores or perovskites are used as topcoat layers. These systems demonstrated an improved temperature capability compared to standard YSZ. In addition, new functions are introduced within the TBCs. These can be sensorial properties that can be used for an improved temperature control or even for monitoring remaining lifetime. Further increased application temperatures will also lead to efforts for a further improvement of the reflectivity of the coatings to reduce the radiative heat transfer through the TBC. ceramic top coats gas turbines multifunctional coatings plasma spraying thermal barrier coating Stuke, Alexandra aut Stöver, Detlev aut Enthalten in Journal of thermal spray technology Springer US, 1992 18(2009), 2 vom: 26. März, Seite 181-186 (DE-627)131101544 (DE-600)1118266-0 (DE-576)038867699 1059-9630 nnns volume:18 year:2009 number:2 day:26 month:03 pages:181-186 https://doi.org/10.1007/s11666-009-9312-7 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_60 GBV_ILN_70 AR 18 2009 2 26 03 181-186
allfieldsGer	10.1007/s11666-009-9312-7 doi (DE-627)OLC2060557127 (DE-He213)s11666-009-9312-7-p DE-627 ger DE-627 rakwb eng 670 VZ Vassen, Robert verfasserin aut Recent Developments in the Field of Thermal Barrier Coatings 2009 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © ASM International 2009 Abstract Conventional thermal barrier coating (TBC) systems consist of a duplex structure with a metallic bondcoat and a ceramic, heat-isolative topcoat. Several recent research activities are concentrating on developing improved bondcoat or topcoat materials; for the topcoat especially, those with reduced thermal conductivity are investigated. Using advanced topcoat materials, the ceramic coating can be further divided into layers with different functions. One example is the double-layer system in which conventional yttria-stabilized zirconia (YSZ) is used as bottom and new materials such as pyrochlores or perovskites are used as topcoat layers. These systems demonstrated an improved temperature capability compared to standard YSZ. In addition, new functions are introduced within the TBCs. These can be sensorial properties that can be used for an improved temperature control or even for monitoring remaining lifetime. Further increased application temperatures will also lead to efforts for a further improvement of the reflectivity of the coatings to reduce the radiative heat transfer through the TBC. ceramic top coats gas turbines multifunctional coatings plasma spraying thermal barrier coating Stuke, Alexandra aut Stöver, Detlev aut Enthalten in Journal of thermal spray technology Springer US, 1992 18(2009), 2 vom: 26. März, Seite 181-186 (DE-627)131101544 (DE-600)1118266-0 (DE-576)038867699 1059-9630 nnns volume:18 year:2009 number:2 day:26 month:03 pages:181-186 https://doi.org/10.1007/s11666-009-9312-7 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_60 GBV_ILN_70 AR 18 2009 2 26 03 181-186
allfieldsSound	10.1007/s11666-009-9312-7 doi (DE-627)OLC2060557127 (DE-He213)s11666-009-9312-7-p DE-627 ger DE-627 rakwb eng 670 VZ Vassen, Robert verfasserin aut Recent Developments in the Field of Thermal Barrier Coatings 2009 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © ASM International 2009 Abstract Conventional thermal barrier coating (TBC) systems consist of a duplex structure with a metallic bondcoat and a ceramic, heat-isolative topcoat. Several recent research activities are concentrating on developing improved bondcoat or topcoat materials; for the topcoat especially, those with reduced thermal conductivity are investigated. Using advanced topcoat materials, the ceramic coating can be further divided into layers with different functions. One example is the double-layer system in which conventional yttria-stabilized zirconia (YSZ) is used as bottom and new materials such as pyrochlores or perovskites are used as topcoat layers. These systems demonstrated an improved temperature capability compared to standard YSZ. In addition, new functions are introduced within the TBCs. These can be sensorial properties that can be used for an improved temperature control or even for monitoring remaining lifetime. Further increased application temperatures will also lead to efforts for a further improvement of the reflectivity of the coatings to reduce the radiative heat transfer through the TBC. ceramic top coats gas turbines multifunctional coatings plasma spraying thermal barrier coating Stuke, Alexandra aut Stöver, Detlev aut Enthalten in Journal of thermal spray technology Springer US, 1992 18(2009), 2 vom: 26. März, Seite 181-186 (DE-627)131101544 (DE-600)1118266-0 (DE-576)038867699 1059-9630 nnns volume:18 year:2009 number:2 day:26 month:03 pages:181-186 https://doi.org/10.1007/s11666-009-9312-7 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_60 GBV_ILN_70 AR 18 2009 2 26 03 181-186
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abstract	Abstract Conventional thermal barrier coating (TBC) systems consist of a duplex structure with a metallic bondcoat and a ceramic, heat-isolative topcoat. Several recent research activities are concentrating on developing improved bondcoat or topcoat materials; for the topcoat especially, those with reduced thermal conductivity are investigated. Using advanced topcoat materials, the ceramic coating can be further divided into layers with different functions. One example is the double-layer system in which conventional yttria-stabilized zirconia (YSZ) is used as bottom and new materials such as pyrochlores or perovskites are used as topcoat layers. These systems demonstrated an improved temperature capability compared to standard YSZ. In addition, new functions are introduced within the TBCs. These can be sensorial properties that can be used for an improved temperature control or even for monitoring remaining lifetime. Further increased application temperatures will also lead to efforts for a further improvement of the reflectivity of the coatings to reduce the radiative heat transfer through the TBC. © ASM International 2009
abstractGer	Abstract Conventional thermal barrier coating (TBC) systems consist of a duplex structure with a metallic bondcoat and a ceramic, heat-isolative topcoat. Several recent research activities are concentrating on developing improved bondcoat or topcoat materials; for the topcoat especially, those with reduced thermal conductivity are investigated. Using advanced topcoat materials, the ceramic coating can be further divided into layers with different functions. One example is the double-layer system in which conventional yttria-stabilized zirconia (YSZ) is used as bottom and new materials such as pyrochlores or perovskites are used as topcoat layers. These systems demonstrated an improved temperature capability compared to standard YSZ. In addition, new functions are introduced within the TBCs. These can be sensorial properties that can be used for an improved temperature control or even for monitoring remaining lifetime. Further increased application temperatures will also lead to efforts for a further improvement of the reflectivity of the coatings to reduce the radiative heat transfer through the TBC. © ASM International 2009
abstract_unstemmed	Abstract Conventional thermal barrier coating (TBC) systems consist of a duplex structure with a metallic bondcoat and a ceramic, heat-isolative topcoat. Several recent research activities are concentrating on developing improved bondcoat or topcoat materials; for the topcoat especially, those with reduced thermal conductivity are investigated. Using advanced topcoat materials, the ceramic coating can be further divided into layers with different functions. One example is the double-layer system in which conventional yttria-stabilized zirconia (YSZ) is used as bottom and new materials such as pyrochlores or perovskites are used as topcoat layers. These systems demonstrated an improved temperature capability compared to standard YSZ. In addition, new functions are introduced within the TBCs. These can be sensorial properties that can be used for an improved temperature control or even for monitoring remaining lifetime. Further increased application temperatures will also lead to efforts for a further improvement of the reflectivity of the coatings to reduce the radiative heat transfer through the TBC. © ASM International 2009
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up_date	2024-07-04T01:38:16.585Z
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