Tensile Creep Behavior and Thermal Stability of Orthogonal Three-Dimensional Woven TyrannoTM ZMI Fiber/Silicon-Titanium-Carbon-Oxygen Matrix Composites
This article presents experimental results for tensile creep behavior of orthogonal three-dimensional woven Tyranno™ ZMI fiber/Si-Ti-C-O ceramic matrix composites at 1300°–1450°C in air. The composite contained Tyranno ZMI (56% silicon, 1% zirconium, 34% carbon, and 9% oxygen) fibers with a BN coati...
Ausführliche Beschreibung
Autor*in: |
Ogasawara, Toshio [verfasserIn] Ishikawa, Takashi [verfasserIn] Ohsawa, Yutaka [verfasserIn] |
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E-Artikel |
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Erschienen: |
Westerville, Ohio: American Ceramics Society ; 2002 |
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Online-Ressource |
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Reproduktion: |
2004 ; Blackwell Publishing Journal Backfiles 1879-2005 |
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Übergeordnetes Werk: |
In: Journal of the American Ceramic Society - American Ceramic Society ; GKD-ID: 6113X, Oxford [u.a.] : Wiley-Blackwell, 1918, 85(2002), 2, Seite 0 |
Übergeordnetes Werk: |
volume:85 ; year:2002 ; number:2 ; pages:0 |
Links: |
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DOI / URN: |
10.1111/j.1151-2916.2002.tb00102.x |
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10.1111/j.1151-2916.2002.tb00102.x doi (DE-627)NLEJ243462247 DE-627 ger DE-627 rakwb Ogasawara, Toshio verfasserin aut Tensile Creep Behavior and Thermal Stability of Orthogonal Three-Dimensional Woven TyrannoTM ZMI Fiber/Silicon-Titanium-Carbon-Oxygen Matrix Composites Westerville, Ohio American Ceramics Society 2002 Online-Ressource nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier This article presents experimental results for tensile creep behavior of orthogonal three-dimensional woven Tyranno™ ZMI fiber/Si-Ti-C-O ceramic matrix composites at 1300°–1450°C in air. The composite contained Tyranno ZMI (56% silicon, 1% zirconium, 34% carbon, and 9% oxygen) fibers with a BN coating layer to improve interface properties, and it exhibited excellent tensile properties at elevated temperature in air. For creep stresses between 60 and 140 MPa, the creep rate decreased continuously with time, with no apparent steady-state regime observed at 1300°–1450°C. Under the test conditions, the microstructure of the Tyranno ZMI fiber and Si-Ti-C-O matrix was unstable, resulting in weight loss and SiC grain growth. As a result, the viscosity of the fiber and matrix increased, because increased viscosity caused a creep rate that continuously decreased, which made steady-state creep impossible under these conditions. 2004 Blackwell Publishing Journal Backfiles 1879-2005 |2004|||||||||| ceramic matrix composites Ishikawa, Takashi verfasserin aut Ohsawa, Yutaka verfasserin aut Ochi, Yasuo oth Zhu, Shijie oth In American Ceramic Society ; GKD-ID: 6113X Journal of the American Ceramic Society Oxford [u.a.] : Wiley-Blackwell, 1918 85(2002), 2, Seite 0 Online-Ressource (DE-627)NLEJ243927835 (DE-600)2008170-4 1551-2916 nnns volume:85 year:2002 number:2 pages:0 http://dx.doi.org/10.1111/j.1151-2916.2002.tb00102.x text/html Verlag Deutschlandweit zugänglich Volltext GBV_USEFLAG_U ZDB-1-DJB GBV_NL_ARTICLE AR 85 2002 2 0 |
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10.1111/j.1151-2916.2002.tb00102.x doi (DE-627)NLEJ243462247 DE-627 ger DE-627 rakwb Ogasawara, Toshio verfasserin aut Tensile Creep Behavior and Thermal Stability of Orthogonal Three-Dimensional Woven TyrannoTM ZMI Fiber/Silicon-Titanium-Carbon-Oxygen Matrix Composites Westerville, Ohio American Ceramics Society 2002 Online-Ressource nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier This article presents experimental results for tensile creep behavior of orthogonal three-dimensional woven Tyranno™ ZMI fiber/Si-Ti-C-O ceramic matrix composites at 1300°–1450°C in air. The composite contained Tyranno ZMI (56% silicon, 1% zirconium, 34% carbon, and 9% oxygen) fibers with a BN coating layer to improve interface properties, and it exhibited excellent tensile properties at elevated temperature in air. For creep stresses between 60 and 140 MPa, the creep rate decreased continuously with time, with no apparent steady-state regime observed at 1300°–1450°C. Under the test conditions, the microstructure of the Tyranno ZMI fiber and Si-Ti-C-O matrix was unstable, resulting in weight loss and SiC grain growth. As a result, the viscosity of the fiber and matrix increased, because increased viscosity caused a creep rate that continuously decreased, which made steady-state creep impossible under these conditions. 2004 Blackwell Publishing Journal Backfiles 1879-2005 |2004|||||||||| ceramic matrix composites Ishikawa, Takashi verfasserin aut Ohsawa, Yutaka verfasserin aut Ochi, Yasuo oth Zhu, Shijie oth In American Ceramic Society ; GKD-ID: 6113X Journal of the American Ceramic Society Oxford [u.a.] : Wiley-Blackwell, 1918 85(2002), 2, Seite 0 Online-Ressource (DE-627)NLEJ243927835 (DE-600)2008170-4 1551-2916 nnns volume:85 year:2002 number:2 pages:0 http://dx.doi.org/10.1111/j.1151-2916.2002.tb00102.x text/html Verlag Deutschlandweit zugänglich Volltext GBV_USEFLAG_U ZDB-1-DJB GBV_NL_ARTICLE AR 85 2002 2 0 |
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10.1111/j.1151-2916.2002.tb00102.x doi (DE-627)NLEJ243462247 DE-627 ger DE-627 rakwb Ogasawara, Toshio verfasserin aut Tensile Creep Behavior and Thermal Stability of Orthogonal Three-Dimensional Woven TyrannoTM ZMI Fiber/Silicon-Titanium-Carbon-Oxygen Matrix Composites Westerville, Ohio American Ceramics Society 2002 Online-Ressource nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier This article presents experimental results for tensile creep behavior of orthogonal three-dimensional woven Tyranno™ ZMI fiber/Si-Ti-C-O ceramic matrix composites at 1300°–1450°C in air. The composite contained Tyranno ZMI (56% silicon, 1% zirconium, 34% carbon, and 9% oxygen) fibers with a BN coating layer to improve interface properties, and it exhibited excellent tensile properties at elevated temperature in air. For creep stresses between 60 and 140 MPa, the creep rate decreased continuously with time, with no apparent steady-state regime observed at 1300°–1450°C. Under the test conditions, the microstructure of the Tyranno ZMI fiber and Si-Ti-C-O matrix was unstable, resulting in weight loss and SiC grain growth. As a result, the viscosity of the fiber and matrix increased, because increased viscosity caused a creep rate that continuously decreased, which made steady-state creep impossible under these conditions. 2004 Blackwell Publishing Journal Backfiles 1879-2005 |2004|||||||||| ceramic matrix composites Ishikawa, Takashi verfasserin aut Ohsawa, Yutaka verfasserin aut Ochi, Yasuo oth Zhu, Shijie oth In American Ceramic Society ; GKD-ID: 6113X Journal of the American Ceramic Society Oxford [u.a.] : Wiley-Blackwell, 1918 85(2002), 2, Seite 0 Online-Ressource (DE-627)NLEJ243927835 (DE-600)2008170-4 1551-2916 nnns volume:85 year:2002 number:2 pages:0 http://dx.doi.org/10.1111/j.1151-2916.2002.tb00102.x text/html Verlag Deutschlandweit zugänglich Volltext GBV_USEFLAG_U ZDB-1-DJB GBV_NL_ARTICLE AR 85 2002 2 0 |
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10.1111/j.1151-2916.2002.tb00102.x doi (DE-627)NLEJ243462247 DE-627 ger DE-627 rakwb Ogasawara, Toshio verfasserin aut Tensile Creep Behavior and Thermal Stability of Orthogonal Three-Dimensional Woven TyrannoTM ZMI Fiber/Silicon-Titanium-Carbon-Oxygen Matrix Composites Westerville, Ohio American Ceramics Society 2002 Online-Ressource nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier This article presents experimental results for tensile creep behavior of orthogonal three-dimensional woven Tyranno™ ZMI fiber/Si-Ti-C-O ceramic matrix composites at 1300°–1450°C in air. The composite contained Tyranno ZMI (56% silicon, 1% zirconium, 34% carbon, and 9% oxygen) fibers with a BN coating layer to improve interface properties, and it exhibited excellent tensile properties at elevated temperature in air. For creep stresses between 60 and 140 MPa, the creep rate decreased continuously with time, with no apparent steady-state regime observed at 1300°–1450°C. Under the test conditions, the microstructure of the Tyranno ZMI fiber and Si-Ti-C-O matrix was unstable, resulting in weight loss and SiC grain growth. As a result, the viscosity of the fiber and matrix increased, because increased viscosity caused a creep rate that continuously decreased, which made steady-state creep impossible under these conditions. 2004 Blackwell Publishing Journal Backfiles 1879-2005 |2004|||||||||| ceramic matrix composites Ishikawa, Takashi verfasserin aut Ohsawa, Yutaka verfasserin aut Ochi, Yasuo oth Zhu, Shijie oth In American Ceramic Society ; GKD-ID: 6113X Journal of the American Ceramic Society Oxford [u.a.] : Wiley-Blackwell, 1918 85(2002), 2, Seite 0 Online-Ressource (DE-627)NLEJ243927835 (DE-600)2008170-4 1551-2916 nnns volume:85 year:2002 number:2 pages:0 http://dx.doi.org/10.1111/j.1151-2916.2002.tb00102.x text/html Verlag Deutschlandweit zugänglich Volltext GBV_USEFLAG_U ZDB-1-DJB GBV_NL_ARTICLE AR 85 2002 2 0 |
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10.1111/j.1151-2916.2002.tb00102.x doi (DE-627)NLEJ243462247 DE-627 ger DE-627 rakwb Ogasawara, Toshio verfasserin aut Tensile Creep Behavior and Thermal Stability of Orthogonal Three-Dimensional Woven TyrannoTM ZMI Fiber/Silicon-Titanium-Carbon-Oxygen Matrix Composites Westerville, Ohio American Ceramics Society 2002 Online-Ressource nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier This article presents experimental results for tensile creep behavior of orthogonal three-dimensional woven Tyranno™ ZMI fiber/Si-Ti-C-O ceramic matrix composites at 1300°–1450°C in air. The composite contained Tyranno ZMI (56% silicon, 1% zirconium, 34% carbon, and 9% oxygen) fibers with a BN coating layer to improve interface properties, and it exhibited excellent tensile properties at elevated temperature in air. For creep stresses between 60 and 140 MPa, the creep rate decreased continuously with time, with no apparent steady-state regime observed at 1300°–1450°C. Under the test conditions, the microstructure of the Tyranno ZMI fiber and Si-Ti-C-O matrix was unstable, resulting in weight loss and SiC grain growth. As a result, the viscosity of the fiber and matrix increased, because increased viscosity caused a creep rate that continuously decreased, which made steady-state creep impossible under these conditions. 2004 Blackwell Publishing Journal Backfiles 1879-2005 |2004|||||||||| ceramic matrix composites Ishikawa, Takashi verfasserin aut Ohsawa, Yutaka verfasserin aut Ochi, Yasuo oth Zhu, Shijie oth In American Ceramic Society ; GKD-ID: 6113X Journal of the American Ceramic Society Oxford [u.a.] : Wiley-Blackwell, 1918 85(2002), 2, Seite 0 Online-Ressource (DE-627)NLEJ243927835 (DE-600)2008170-4 1551-2916 nnns volume:85 year:2002 number:2 pages:0 http://dx.doi.org/10.1111/j.1151-2916.2002.tb00102.x text/html Verlag Deutschlandweit zugänglich Volltext GBV_USEFLAG_U ZDB-1-DJB GBV_NL_ARTICLE AR 85 2002 2 0 |
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Tensile Creep Behavior and Thermal Stability of Orthogonal Three-Dimensional Woven TyrannoTM ZMI Fiber/Silicon-Titanium-Carbon-Oxygen Matrix Composites |
abstract |
This article presents experimental results for tensile creep behavior of orthogonal three-dimensional woven Tyranno™ ZMI fiber/Si-Ti-C-O ceramic matrix composites at 1300°–1450°C in air. The composite contained Tyranno ZMI (56% silicon, 1% zirconium, 34% carbon, and 9% oxygen) fibers with a BN coating layer to improve interface properties, and it exhibited excellent tensile properties at elevated temperature in air. For creep stresses between 60 and 140 MPa, the creep rate decreased continuously with time, with no apparent steady-state regime observed at 1300°–1450°C. Under the test conditions, the microstructure of the Tyranno ZMI fiber and Si-Ti-C-O matrix was unstable, resulting in weight loss and SiC grain growth. As a result, the viscosity of the fiber and matrix increased, because increased viscosity caused a creep rate that continuously decreased, which made steady-state creep impossible under these conditions. |
abstractGer |
This article presents experimental results for tensile creep behavior of orthogonal three-dimensional woven Tyranno™ ZMI fiber/Si-Ti-C-O ceramic matrix composites at 1300°–1450°C in air. The composite contained Tyranno ZMI (56% silicon, 1% zirconium, 34% carbon, and 9% oxygen) fibers with a BN coating layer to improve interface properties, and it exhibited excellent tensile properties at elevated temperature in air. For creep stresses between 60 and 140 MPa, the creep rate decreased continuously with time, with no apparent steady-state regime observed at 1300°–1450°C. Under the test conditions, the microstructure of the Tyranno ZMI fiber and Si-Ti-C-O matrix was unstable, resulting in weight loss and SiC grain growth. As a result, the viscosity of the fiber and matrix increased, because increased viscosity caused a creep rate that continuously decreased, which made steady-state creep impossible under these conditions. |
abstract_unstemmed |
This article presents experimental results for tensile creep behavior of orthogonal three-dimensional woven Tyranno™ ZMI fiber/Si-Ti-C-O ceramic matrix composites at 1300°–1450°C in air. The composite contained Tyranno ZMI (56% silicon, 1% zirconium, 34% carbon, and 9% oxygen) fibers with a BN coating layer to improve interface properties, and it exhibited excellent tensile properties at elevated temperature in air. For creep stresses between 60 and 140 MPa, the creep rate decreased continuously with time, with no apparent steady-state regime observed at 1300°–1450°C. Under the test conditions, the microstructure of the Tyranno ZMI fiber and Si-Ti-C-O matrix was unstable, resulting in weight loss and SiC grain growth. As a result, the viscosity of the fiber and matrix increased, because increased viscosity caused a creep rate that continuously decreased, which made steady-state creep impossible under these conditions. |
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Tensile Creep Behavior and Thermal Stability of Orthogonal Three-Dimensional Woven TyrannoTM ZMI Fiber/Silicon-Titanium-Carbon-Oxygen Matrix Composites |
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http://dx.doi.org/10.1111/j.1151-2916.2002.tb00102.x |
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author2 |
Ishikawa, Takashi Ohsawa, Yutaka Ochi, Yasuo Zhu, Shijie |
author2Str |
Ishikawa, Takashi Ohsawa, Yutaka Ochi, Yasuo Zhu, Shijie |
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NLEJ243927835 |
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doi_str |
10.1111/j.1151-2916.2002.tb00102.x |
up_date |
2024-07-06T05:32:01.801Z |
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1803806490552696832 |
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The composite contained Tyranno ZMI (56% silicon, 1% zirconium, 34% carbon, and 9% oxygen) fibers with a BN coating layer to improve interface properties, and it exhibited excellent tensile properties at elevated temperature in air. For creep stresses between 60 and 140 MPa, the creep rate decreased continuously with time, with no apparent steady-state regime observed at 1300°–1450°C. Under the test conditions, the microstructure of the Tyranno ZMI fiber and Si-Ti-C-O matrix was unstable, resulting in weight loss and SiC grain growth. 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