Ceramic thermal barrier coatings for commercial gas turbine engines
Abstract Thermal barrier coatings have been used for over 20 years to extend the durability of aircraft gas turbine engine combustors. Improvements to the chemical composition of the ceramic and to the composition and microstructure of the underlying bond coat have allowed the application of thermal...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Meier, Susan Manning [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
1991 |
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| Schlagwörter: |
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| Anmerkung: |
© TMS 1991 |
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| Übergeordnetes Werk: |
Enthalten in: JOM - Springer-Verlag, 1989, 43(1991), 3 vom: März, Seite 50-53 |
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| Übergeordnetes Werk: |
volume:43 ; year:1991 ; number:3 ; month:03 ; pages:50-53 |
| Links: |
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| DOI / URN: |
10.1007/BF03220164 |
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| Katalog-ID: |
OLC2059867738 |
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| 520 | |a Abstract Thermal barrier coatings have been used for over 20 years to extend the durability of aircraft gas turbine engine combustors. Improvements to the chemical composition of the ceramic and to the composition and microstructure of the underlying bond coat have allowed the application of thermal barrier coating technology to turbine components, with similar benefits. Recent ceramic process improvements have led to the incorporation of very durable electron beam-physical vapor deposited coatings on the most demanding of stationary and rotating turbine components. | ||
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| 700 | 1 | |a Gupta, Dinesh K. |4 aut | |
| 700 | 1 | |a Sheffler, Keith D. |4 aut | |
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10.1007/BF03220164 doi (DE-627)OLC2059867738 (DE-He213)BF03220164-p DE-627 ger DE-627 rakwb eng 670 VZ 19,1 ssgn Meier, Susan Manning verfasserin aut Ceramic thermal barrier coatings for commercial gas turbine engines 1991 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © TMS 1991 Abstract Thermal barrier coatings have been used for over 20 years to extend the durability of aircraft gas turbine engine combustors. Improvements to the chemical composition of the ceramic and to the composition and microstructure of the underlying bond coat have allowed the application of thermal barrier coating technology to turbine components, with similar benefits. Recent ceramic process improvements have led to the incorporation of very durable electron beam-physical vapor deposited coatings on the most demanding of stationary and rotating turbine components. Bond Coat Thermal Barrier Coating Thermal Barrier Coat 7YSZ Coating Thermal Barrier Coating System Gupta, Dinesh K. aut Sheffler, Keith D. aut Enthalten in JOM Springer-Verlag, 1989 43(1991), 3 vom: März, Seite 50-53 (DE-627)130823368 (DE-600)1015034-1 (DE-576)023064358 0148-6608 nnns volume:43 year:1991 number:3 month:03 pages:50-53 https://doi.org/10.1007/BF03220164 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_21 GBV_ILN_23 GBV_ILN_30 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_70 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2027 GBV_ILN_4029 GBV_ILN_4036 GBV_ILN_4046 GBV_ILN_4307 GBV_ILN_4317 GBV_ILN_4319 GBV_ILN_4700 AR 43 1991 3 03 50-53 |
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10.1007/BF03220164 doi (DE-627)OLC2059867738 (DE-He213)BF03220164-p DE-627 ger DE-627 rakwb eng 670 VZ 19,1 ssgn Meier, Susan Manning verfasserin aut Ceramic thermal barrier coatings for commercial gas turbine engines 1991 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © TMS 1991 Abstract Thermal barrier coatings have been used for over 20 years to extend the durability of aircraft gas turbine engine combustors. Improvements to the chemical composition of the ceramic and to the composition and microstructure of the underlying bond coat have allowed the application of thermal barrier coating technology to turbine components, with similar benefits. Recent ceramic process improvements have led to the incorporation of very durable electron beam-physical vapor deposited coatings on the most demanding of stationary and rotating turbine components. Bond Coat Thermal Barrier Coating Thermal Barrier Coat 7YSZ Coating Thermal Barrier Coating System Gupta, Dinesh K. aut Sheffler, Keith D. aut Enthalten in JOM Springer-Verlag, 1989 43(1991), 3 vom: März, Seite 50-53 (DE-627)130823368 (DE-600)1015034-1 (DE-576)023064358 0148-6608 nnns volume:43 year:1991 number:3 month:03 pages:50-53 https://doi.org/10.1007/BF03220164 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_21 GBV_ILN_23 GBV_ILN_30 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_70 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2027 GBV_ILN_4029 GBV_ILN_4036 GBV_ILN_4046 GBV_ILN_4307 GBV_ILN_4317 GBV_ILN_4319 GBV_ILN_4700 AR 43 1991 3 03 50-53 |
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10.1007/BF03220164 doi (DE-627)OLC2059867738 (DE-He213)BF03220164-p DE-627 ger DE-627 rakwb eng 670 VZ 19,1 ssgn Meier, Susan Manning verfasserin aut Ceramic thermal barrier coatings for commercial gas turbine engines 1991 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © TMS 1991 Abstract Thermal barrier coatings have been used for over 20 years to extend the durability of aircraft gas turbine engine combustors. Improvements to the chemical composition of the ceramic and to the composition and microstructure of the underlying bond coat have allowed the application of thermal barrier coating technology to turbine components, with similar benefits. Recent ceramic process improvements have led to the incorporation of very durable electron beam-physical vapor deposited coatings on the most demanding of stationary and rotating turbine components. Bond Coat Thermal Barrier Coating Thermal Barrier Coat 7YSZ Coating Thermal Barrier Coating System Gupta, Dinesh K. aut Sheffler, Keith D. aut Enthalten in JOM Springer-Verlag, 1989 43(1991), 3 vom: März, Seite 50-53 (DE-627)130823368 (DE-600)1015034-1 (DE-576)023064358 0148-6608 nnns volume:43 year:1991 number:3 month:03 pages:50-53 https://doi.org/10.1007/BF03220164 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_21 GBV_ILN_23 GBV_ILN_30 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_70 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2027 GBV_ILN_4029 GBV_ILN_4036 GBV_ILN_4046 GBV_ILN_4307 GBV_ILN_4317 GBV_ILN_4319 GBV_ILN_4700 AR 43 1991 3 03 50-53 |
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10.1007/BF03220164 doi (DE-627)OLC2059867738 (DE-He213)BF03220164-p DE-627 ger DE-627 rakwb eng 670 VZ 19,1 ssgn Meier, Susan Manning verfasserin aut Ceramic thermal barrier coatings for commercial gas turbine engines 1991 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © TMS 1991 Abstract Thermal barrier coatings have been used for over 20 years to extend the durability of aircraft gas turbine engine combustors. Improvements to the chemical composition of the ceramic and to the composition and microstructure of the underlying bond coat have allowed the application of thermal barrier coating technology to turbine components, with similar benefits. Recent ceramic process improvements have led to the incorporation of very durable electron beam-physical vapor deposited coatings on the most demanding of stationary and rotating turbine components. Bond Coat Thermal Barrier Coating Thermal Barrier Coat 7YSZ Coating Thermal Barrier Coating System Gupta, Dinesh K. aut Sheffler, Keith D. aut Enthalten in JOM Springer-Verlag, 1989 43(1991), 3 vom: März, Seite 50-53 (DE-627)130823368 (DE-600)1015034-1 (DE-576)023064358 0148-6608 nnns volume:43 year:1991 number:3 month:03 pages:50-53 https://doi.org/10.1007/BF03220164 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_21 GBV_ILN_23 GBV_ILN_30 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_70 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2027 GBV_ILN_4029 GBV_ILN_4036 GBV_ILN_4046 GBV_ILN_4307 GBV_ILN_4317 GBV_ILN_4319 GBV_ILN_4700 AR 43 1991 3 03 50-53 |
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10.1007/BF03220164 doi (DE-627)OLC2059867738 (DE-He213)BF03220164-p DE-627 ger DE-627 rakwb eng 670 VZ 19,1 ssgn Meier, Susan Manning verfasserin aut Ceramic thermal barrier coatings for commercial gas turbine engines 1991 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © TMS 1991 Abstract Thermal barrier coatings have been used for over 20 years to extend the durability of aircraft gas turbine engine combustors. Improvements to the chemical composition of the ceramic and to the composition and microstructure of the underlying bond coat have allowed the application of thermal barrier coating technology to turbine components, with similar benefits. Recent ceramic process improvements have led to the incorporation of very durable electron beam-physical vapor deposited coatings on the most demanding of stationary and rotating turbine components. Bond Coat Thermal Barrier Coating Thermal Barrier Coat 7YSZ Coating Thermal Barrier Coating System Gupta, Dinesh K. aut Sheffler, Keith D. aut Enthalten in JOM Springer-Verlag, 1989 43(1991), 3 vom: März, Seite 50-53 (DE-627)130823368 (DE-600)1015034-1 (DE-576)023064358 0148-6608 nnns volume:43 year:1991 number:3 month:03 pages:50-53 https://doi.org/10.1007/BF03220164 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_11 GBV_ILN_20 GBV_ILN_21 GBV_ILN_23 GBV_ILN_30 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_70 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2027 GBV_ILN_4029 GBV_ILN_4036 GBV_ILN_4046 GBV_ILN_4307 GBV_ILN_4317 GBV_ILN_4319 GBV_ILN_4700 AR 43 1991 3 03 50-53 |
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ceramic thermal barrier coatings for commercial gas turbine engines |
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Ceramic thermal barrier coatings for commercial gas turbine engines |
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Abstract Thermal barrier coatings have been used for over 20 years to extend the durability of aircraft gas turbine engine combustors. Improvements to the chemical composition of the ceramic and to the composition and microstructure of the underlying bond coat have allowed the application of thermal barrier coating technology to turbine components, with similar benefits. Recent ceramic process improvements have led to the incorporation of very durable electron beam-physical vapor deposited coatings on the most demanding of stationary and rotating turbine components. © TMS 1991 |
| abstractGer |
Abstract Thermal barrier coatings have been used for over 20 years to extend the durability of aircraft gas turbine engine combustors. Improvements to the chemical composition of the ceramic and to the composition and microstructure of the underlying bond coat have allowed the application of thermal barrier coating technology to turbine components, with similar benefits. Recent ceramic process improvements have led to the incorporation of very durable electron beam-physical vapor deposited coatings on the most demanding of stationary and rotating turbine components. © TMS 1991 |
| abstract_unstemmed |
Abstract Thermal barrier coatings have been used for over 20 years to extend the durability of aircraft gas turbine engine combustors. Improvements to the chemical composition of the ceramic and to the composition and microstructure of the underlying bond coat have allowed the application of thermal barrier coating technology to turbine components, with similar benefits. Recent ceramic process improvements have led to the incorporation of very durable electron beam-physical vapor deposited coatings on the most demanding of stationary and rotating turbine components. © TMS 1991 |
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Ceramic thermal barrier coatings for commercial gas turbine engines |
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