Complete recovery of high temperature oxidation resistance in carbon fiber reinforced SiC composites by a recoating repair methodology
The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepare...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Mei, Hui [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2015transfer abstract |
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| Umfang: |
5 |
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| Übergeordnetes Werk: |
Enthalten in: Generation of 3X FLAG-tagged human embryonic stem cell (hESC) line to study WNT-induced β-catenin DNA interactions (HVRDe009-A-2) - Cutts, Joshua ELSEVIER, 2021, Amsterdam |
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| Übergeordnetes Werk: |
volume:631 ; year:2015 ; day:17 ; month:04 ; pages:33-37 ; extent:5 |
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| DOI / URN: |
10.1016/j.msea.2015.02.036 |
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ELV018647510 |
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| 245 | 1 | 0 | |a Complete recovery of high temperature oxidation resistance in carbon fiber reinforced SiC composites by a recoating repair methodology |
| 264 | 1 | |c 2015transfer abstract | |
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| 520 | |a The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. | ||
| 520 | |a The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. | ||
| 650 | 7 | |a Heat treatment |2 Elsevier | |
| 650 | 7 | |a Oxidation resistance |2 Elsevier | |
| 650 | 7 | |a Coating repair |2 Elsevier | |
| 650 | 7 | |a C/SiC composite |2 Elsevier | |
| 700 | 1 | |a Ji, Tianming |4 oth | |
| 700 | 1 | |a Chen, Xi |4 oth | |
| 700 | 1 | |a Bai, Qianglai |4 oth | |
| 700 | 1 | |a Cheng, Laifei |4 oth | |
| 773 | 0 | 8 | |i Enthalten in |n Elsevier |a Cutts, Joshua ELSEVIER |t Generation of 3X FLAG-tagged human embryonic stem cell (hESC) line to study WNT-induced β-catenin DNA interactions (HVRDe009-A-2) |d 2021 |g Amsterdam |w (DE-627)ELV007117167 |
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10.1016/j.msea.2015.02.036 doi GBVA2015015000025.pica (DE-627)ELV018647510 (ELSEVIER)S0921-5093(15)00153-7 DE-627 ger DE-627 rakwb eng 600 670 530 600 DE-600 670 DE-600 530 DE-600 570 VZ Mei, Hui verfasserin aut Complete recovery of high temperature oxidation resistance in carbon fiber reinforced SiC composites by a recoating repair methodology 2015transfer abstract 5 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. Heat treatment Elsevier Oxidation resistance Elsevier Coating repair Elsevier C/SiC composite Elsevier Ji, Tianming oth Chen, Xi oth Bai, Qianglai oth Cheng, Laifei oth Enthalten in Elsevier Cutts, Joshua ELSEVIER Generation of 3X FLAG-tagged human embryonic stem cell (hESC) line to study WNT-induced β-catenin DNA interactions (HVRDe009-A-2) 2021 Amsterdam (DE-627)ELV007117167 volume:631 year:2015 day:17 month:04 pages:33-37 extent:5 https://doi.org/10.1016/j.msea.2015.02.036 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U SSG-OLC-PHA AR 631 2015 17 0417 33-37 5 045F 600 |
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10.1016/j.msea.2015.02.036 doi GBVA2015015000025.pica (DE-627)ELV018647510 (ELSEVIER)S0921-5093(15)00153-7 DE-627 ger DE-627 rakwb eng 600 670 530 600 DE-600 670 DE-600 530 DE-600 570 VZ Mei, Hui verfasserin aut Complete recovery of high temperature oxidation resistance in carbon fiber reinforced SiC composites by a recoating repair methodology 2015transfer abstract 5 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. Heat treatment Elsevier Oxidation resistance Elsevier Coating repair Elsevier C/SiC composite Elsevier Ji, Tianming oth Chen, Xi oth Bai, Qianglai oth Cheng, Laifei oth Enthalten in Elsevier Cutts, Joshua ELSEVIER Generation of 3X FLAG-tagged human embryonic stem cell (hESC) line to study WNT-induced β-catenin DNA interactions (HVRDe009-A-2) 2021 Amsterdam (DE-627)ELV007117167 volume:631 year:2015 day:17 month:04 pages:33-37 extent:5 https://doi.org/10.1016/j.msea.2015.02.036 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U SSG-OLC-PHA AR 631 2015 17 0417 33-37 5 045F 600 |
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10.1016/j.msea.2015.02.036 doi GBVA2015015000025.pica (DE-627)ELV018647510 (ELSEVIER)S0921-5093(15)00153-7 DE-627 ger DE-627 rakwb eng 600 670 530 600 DE-600 670 DE-600 530 DE-600 570 VZ Mei, Hui verfasserin aut Complete recovery of high temperature oxidation resistance in carbon fiber reinforced SiC composites by a recoating repair methodology 2015transfer abstract 5 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. Heat treatment Elsevier Oxidation resistance Elsevier Coating repair Elsevier C/SiC composite Elsevier Ji, Tianming oth Chen, Xi oth Bai, Qianglai oth Cheng, Laifei oth Enthalten in Elsevier Cutts, Joshua ELSEVIER Generation of 3X FLAG-tagged human embryonic stem cell (hESC) line to study WNT-induced β-catenin DNA interactions (HVRDe009-A-2) 2021 Amsterdam (DE-627)ELV007117167 volume:631 year:2015 day:17 month:04 pages:33-37 extent:5 https://doi.org/10.1016/j.msea.2015.02.036 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U SSG-OLC-PHA AR 631 2015 17 0417 33-37 5 045F 600 |
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10.1016/j.msea.2015.02.036 doi GBVA2015015000025.pica (DE-627)ELV018647510 (ELSEVIER)S0921-5093(15)00153-7 DE-627 ger DE-627 rakwb eng 600 670 530 600 DE-600 670 DE-600 530 DE-600 570 VZ Mei, Hui verfasserin aut Complete recovery of high temperature oxidation resistance in carbon fiber reinforced SiC composites by a recoating repair methodology 2015transfer abstract 5 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. Heat treatment Elsevier Oxidation resistance Elsevier Coating repair Elsevier C/SiC composite Elsevier Ji, Tianming oth Chen, Xi oth Bai, Qianglai oth Cheng, Laifei oth Enthalten in Elsevier Cutts, Joshua ELSEVIER Generation of 3X FLAG-tagged human embryonic stem cell (hESC) line to study WNT-induced β-catenin DNA interactions (HVRDe009-A-2) 2021 Amsterdam (DE-627)ELV007117167 volume:631 year:2015 day:17 month:04 pages:33-37 extent:5 https://doi.org/10.1016/j.msea.2015.02.036 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U SSG-OLC-PHA AR 631 2015 17 0417 33-37 5 045F 600 |
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10.1016/j.msea.2015.02.036 doi GBVA2015015000025.pica (DE-627)ELV018647510 (ELSEVIER)S0921-5093(15)00153-7 DE-627 ger DE-627 rakwb eng 600 670 530 600 DE-600 670 DE-600 530 DE-600 570 VZ Mei, Hui verfasserin aut Complete recovery of high temperature oxidation resistance in carbon fiber reinforced SiC composites by a recoating repair methodology 2015transfer abstract 5 nicht spezifiziert zzz rdacontent nicht spezifiziert z rdamedia nicht spezifiziert zu rdacarrier The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. Heat treatment Elsevier Oxidation resistance Elsevier Coating repair Elsevier C/SiC composite Elsevier Ji, Tianming oth Chen, Xi oth Bai, Qianglai oth Cheng, Laifei oth Enthalten in Elsevier Cutts, Joshua ELSEVIER Generation of 3X FLAG-tagged human embryonic stem cell (hESC) line to study WNT-induced β-catenin DNA interactions (HVRDe009-A-2) 2021 Amsterdam (DE-627)ELV007117167 volume:631 year:2015 day:17 month:04 pages:33-37 extent:5 https://doi.org/10.1016/j.msea.2015.02.036 Volltext GBV_USEFLAG_U GBV_ELV SYSFLAG_U SSG-OLC-PHA AR 631 2015 17 0417 33-37 5 045F 600 |
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Enthalten in Generation of 3X FLAG-tagged human embryonic stem cell (hESC) line to study WNT-induced β-catenin DNA interactions (HVRDe009-A-2) Amsterdam volume:631 year:2015 day:17 month:04 pages:33-37 extent:5 |
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Enthalten in Generation of 3X FLAG-tagged human embryonic stem cell (hESC) line to study WNT-induced β-catenin DNA interactions (HVRDe009-A-2) Amsterdam volume:631 year:2015 day:17 month:04 pages:33-37 extent:5 |
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As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. 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Complete recovery of high temperature oxidation resistance in carbon fiber reinforced SiC composites by a recoating repair methodology |
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The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. |
| abstractGer |
The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. |
| abstract_unstemmed |
The current work reports on the oxidation behavior and residual flexural strength of carbon fiber–reinforced silicon carbide composites (C/SiC) after induction of thermal crack damage by heat treatment (HT) at 1900°C and the effect, therein, of a repair process involving recoating by SiC. As-prepared, heat-treated and heat-treated/recoated specimens, were subjected to static oxidation tests in air at a temperature range of 500–1500°C for 10h and then tested in three-point bending. It was found that composite weight of heat-treated samples decreased dramatically with increasing oxidation temperature with weight loss values of ~30% being systematically observed for oxidation temperatures above 800°C. On the other hand, as-prepared and heat-treated/SiC-recoated specimens reached almost their original weight after oxidation. The residual flexural strength of C/SiC composites with thermally-induced crack damage decreased significantly compared to as-prepared specimens, while SiC recoating was found to efficiently enable strength enhancement. Microstructural analysis showed that HT was associated with increased population and dimensions of micro-cracks on the C/SiC surface while SiC recoating enabled repair of HT-induced thermal crack damage hence leading to oxidation resistance recovery of the material. |
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