Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines
Abstract Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system an...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Kuznetsov, V. P. [verfasserIn] |
|---|
| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2007 |
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| Schlagwörter: |
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| Anmerkung: |
© Springer Science+Business Media, Inc. 2007 |
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| Übergeordnetes Werk: |
Enthalten in: Metal science and heat treatment - Springer US, 1959, 49(2007), 5-6 vom: Mai, Seite 253-259 |
|---|---|
| Übergeordnetes Werk: |
volume:49 ; year:2007 ; number:5-6 ; month:05 ; pages:253-259 |
| Links: |
|---|
| DOI / URN: |
10.1007/s11041-007-0045-2 |
|---|
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OLC2048070108 |
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| 520 | |a Abstract Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a $ ZrO_{2} $: $ Y_{2} $$ O_{3} $ ceramics are presented. A complex gradient coating possessing unique protective properties at t = 1100–1200°C for single-crystal blades from alloy ZhS36VI for advanced gas turbine engines with gas temperature of 1550°C at the inlet to the turbine is described. | ||
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| 700 | 1 | |a Muboyadzhyan, S. A. |4 aut | |
| 700 | 1 | |a Repina, O. V. |4 aut | |
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10.1007/s11041-007-0045-2 doi (DE-627)OLC2048070108 (DE-He213)s11041-007-0045-2-p DE-627 ger DE-627 rakwb eng 670 620 660 VZ Kuznetsov, V. P. verfasserin aut Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines 2007 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media, Inc. 2007 Abstract Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a $ ZrO_{2} $: $ Y_{2} $$ O_{3} $ ceramics are presented. A complex gradient coating possessing unique protective properties at t = 1100–1200°C for single-crystal blades from alloy ZhS36VI for advanced gas turbine engines with gas temperature of 1550°C at the inlet to the turbine is described. Turbine Blade Diffusion Zone Aluminide Coating External Zone Complex Coating Lesnikov, V. P. aut Muboyadzhyan, S. A. aut Repina, O. V. aut Enthalten in Metal science and heat treatment Springer US, 1959 49(2007), 5-6 vom: Mai, Seite 253-259 (DE-627)129596981 (DE-600)240858-2 (DE-576)015090159 0026-0673 nnns volume:49 year:2007 number:5-6 month:05 pages:253-259 https://doi.org/10.1007/s11041-007-0045-2 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_70 GBV_ILN_4319 AR 49 2007 5-6 05 253-259 |
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10.1007/s11041-007-0045-2 doi (DE-627)OLC2048070108 (DE-He213)s11041-007-0045-2-p DE-627 ger DE-627 rakwb eng 670 620 660 VZ Kuznetsov, V. P. verfasserin aut Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines 2007 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media, Inc. 2007 Abstract Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a $ ZrO_{2} $: $ Y_{2} $$ O_{3} $ ceramics are presented. A complex gradient coating possessing unique protective properties at t = 1100–1200°C for single-crystal blades from alloy ZhS36VI for advanced gas turbine engines with gas temperature of 1550°C at the inlet to the turbine is described. Turbine Blade Diffusion Zone Aluminide Coating External Zone Complex Coating Lesnikov, V. P. aut Muboyadzhyan, S. A. aut Repina, O. V. aut Enthalten in Metal science and heat treatment Springer US, 1959 49(2007), 5-6 vom: Mai, Seite 253-259 (DE-627)129596981 (DE-600)240858-2 (DE-576)015090159 0026-0673 nnns volume:49 year:2007 number:5-6 month:05 pages:253-259 https://doi.org/10.1007/s11041-007-0045-2 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_70 GBV_ILN_4319 AR 49 2007 5-6 05 253-259 |
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10.1007/s11041-007-0045-2 doi (DE-627)OLC2048070108 (DE-He213)s11041-007-0045-2-p DE-627 ger DE-627 rakwb eng 670 620 660 VZ Kuznetsov, V. P. verfasserin aut Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines 2007 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media, Inc. 2007 Abstract Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a $ ZrO_{2} $: $ Y_{2} $$ O_{3} $ ceramics are presented. A complex gradient coating possessing unique protective properties at t = 1100–1200°C for single-crystal blades from alloy ZhS36VI for advanced gas turbine engines with gas temperature of 1550°C at the inlet to the turbine is described. Turbine Blade Diffusion Zone Aluminide Coating External Zone Complex Coating Lesnikov, V. P. aut Muboyadzhyan, S. A. aut Repina, O. V. aut Enthalten in Metal science and heat treatment Springer US, 1959 49(2007), 5-6 vom: Mai, Seite 253-259 (DE-627)129596981 (DE-600)240858-2 (DE-576)015090159 0026-0673 nnns volume:49 year:2007 number:5-6 month:05 pages:253-259 https://doi.org/10.1007/s11041-007-0045-2 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_70 GBV_ILN_4319 AR 49 2007 5-6 05 253-259 |
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10.1007/s11041-007-0045-2 doi (DE-627)OLC2048070108 (DE-He213)s11041-007-0045-2-p DE-627 ger DE-627 rakwb eng 670 620 660 VZ Kuznetsov, V. P. verfasserin aut Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines 2007 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media, Inc. 2007 Abstract Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a $ ZrO_{2} $: $ Y_{2} $$ O_{3} $ ceramics are presented. A complex gradient coating possessing unique protective properties at t = 1100–1200°C for single-crystal blades from alloy ZhS36VI for advanced gas turbine engines with gas temperature of 1550°C at the inlet to the turbine is described. Turbine Blade Diffusion Zone Aluminide Coating External Zone Complex Coating Lesnikov, V. P. aut Muboyadzhyan, S. A. aut Repina, O. V. aut Enthalten in Metal science and heat treatment Springer US, 1959 49(2007), 5-6 vom: Mai, Seite 253-259 (DE-627)129596981 (DE-600)240858-2 (DE-576)015090159 0026-0673 nnns volume:49 year:2007 number:5-6 month:05 pages:253-259 https://doi.org/10.1007/s11041-007-0045-2 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_70 GBV_ILN_4319 AR 49 2007 5-6 05 253-259 |
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10.1007/s11041-007-0045-2 doi (DE-627)OLC2048070108 (DE-He213)s11041-007-0045-2-p DE-627 ger DE-627 rakwb eng 670 620 660 VZ Kuznetsov, V. P. verfasserin aut Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines 2007 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media, Inc. 2007 Abstract Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a $ ZrO_{2} $: $ Y_{2} $$ O_{3} $ ceramics are presented. A complex gradient coating possessing unique protective properties at t = 1100–1200°C for single-crystal blades from alloy ZhS36VI for advanced gas turbine engines with gas temperature of 1550°C at the inlet to the turbine is described. Turbine Blade Diffusion Zone Aluminide Coating External Zone Complex Coating Lesnikov, V. P. aut Muboyadzhyan, S. A. aut Repina, O. V. aut Enthalten in Metal science and heat treatment Springer US, 1959 49(2007), 5-6 vom: Mai, Seite 253-259 (DE-627)129596981 (DE-600)240858-2 (DE-576)015090159 0026-0673 nnns volume:49 year:2007 number:5-6 month:05 pages:253-259 https://doi.org/10.1007/s11041-007-0045-2 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC GBV_ILN_70 GBV_ILN_4319 AR 49 2007 5-6 05 253-259 |
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Abstract Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a $ ZrO_{2} $: $ Y_{2} $$ O_{3} $ ceramics are presented. A complex gradient coating possessing unique protective properties at t = 1100–1200°C for single-crystal blades from alloy ZhS36VI for advanced gas turbine engines with gas temperature of 1550°C at the inlet to the turbine is described. © Springer Science+Business Media, Inc. 2007 |
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Abstract Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a $ ZrO_{2} $: $ Y_{2} $$ O_{3} $ ceramics are presented. A complex gradient coating possessing unique protective properties at t = 1100–1200°C for single-crystal blades from alloy ZhS36VI for advanced gas turbine engines with gas temperature of 1550°C at the inlet to the turbine is described. © Springer Science+Business Media, Inc. 2007 |
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Abstract Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a $ ZrO_{2} $: $ Y_{2} $$ O_{3} $ ceramics are presented. A complex gradient coating possessing unique protective properties at t = 1100–1200°C for single-crystal blades from alloy ZhS36VI for advanced gas turbine engines with gas temperature of 1550°C at the inlet to the turbine is described. © Springer Science+Business Media, Inc. 2007 |
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<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">OLC2048070108</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20230503192210.0</controlfield><controlfield tag="007">tu</controlfield><controlfield tag="008">200819s2007 xx ||||| 00| ||eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/s11041-007-0045-2</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)OLC2048070108</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-He213)s11041-007-0045-2-p</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">670</subfield><subfield code="a">620</subfield><subfield code="a">660</subfield><subfield code="q">VZ</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Kuznetsov, V. P.</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2007</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">ohne Hilfsmittel zu benutzen</subfield><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Band</subfield><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© Springer Science+Business Media, Inc. 2007</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a $ ZrO_{2} $: $ Y_{2} $$ O_{3} $ ceramics are presented. 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