2019
DOI: 10.1111/ijac.13388
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Microstructure, properties, and application of low carbon Al2O3‐C refractories used as submerged entry nozzles

Abstract: With the aim to achieve the application of low carbon Al2O3‐C refractory as submerged entry nozzle (SEN) materials, a comprehensive study on the microstructure, thermo‐mechanical properties, as well as application performance during use in the continuous casting was carried out by comparing with the traditional one. Both hot and cold modulus of ruptures of the low carbon Al2O3‐C refractory were superior to the traditional one, and its thermal shock resistance still kept in an acceptable level. The increase in … Show more

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Cited by 10 publications
(4 citation statements)
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“…The formed SiO gas reacts with carbon or carbon monoxide in the system to form SiC 2,19,24,28,29,34,38 according to Equations () and (): SiOnormalgbadbreak+2Cnormalsbadbreak>1200normalCSiCnormalsgoodbreak+normalCOnormalg\begin{equation}{\rm{Si}}{{\rm{O}}_{\left( {\rm{g}} \right)}} + {\rm{\;}}2{{\rm{C}}_{\left( {\rm{s}} \right)}}\mathop \to \limits^{ > 1200^\circ {\rm{C}}} {\rm{\;Si}}{{\rm{C}}_{\left( {\rm{s}} \right)}} + {\rm{C}}{{\rm{O}}_{\left( {\rm{g}} \right)}}\end{equation} SiOnormalgbadbreak+COnormalgbadbreak>1200normalCSiCnormalsgoodbreak+O2()g\begin{equation}{\rm{Si}}{{\rm{O}}_{\left( {\rm{g}} \right)}} + {\rm{\;C}}{{\rm{O}}_{\left( {\rm{g}} \right)}}\mathop \to \limits^{ > 1200^\circ {\rm{C}}} {\rm{\;Si}}{{\rm{C}}_{\left( {\rm{s}} \right)}} + {\rm{\;}}{{\rm{O}}_{2{\rm{\;}}\left( {\rm{g}} \right)}}\end{equation}…”
Section: Resultsmentioning
confidence: 99%
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“…The formed SiO gas reacts with carbon or carbon monoxide in the system to form SiC 2,19,24,28,29,34,38 according to Equations () and (): SiOnormalgbadbreak+2Cnormalsbadbreak>1200normalCSiCnormalsgoodbreak+normalCOnormalg\begin{equation}{\rm{Si}}{{\rm{O}}_{\left( {\rm{g}} \right)}} + {\rm{\;}}2{{\rm{C}}_{\left( {\rm{s}} \right)}}\mathop \to \limits^{ > 1200^\circ {\rm{C}}} {\rm{\;Si}}{{\rm{C}}_{\left( {\rm{s}} \right)}} + {\rm{C}}{{\rm{O}}_{\left( {\rm{g}} \right)}}\end{equation} SiOnormalgbadbreak+COnormalgbadbreak>1200normalCSiCnormalsgoodbreak+O2()g\begin{equation}{\rm{Si}}{{\rm{O}}_{\left( {\rm{g}} \right)}} + {\rm{\;C}}{{\rm{O}}_{\left( {\rm{g}} \right)}}\mathop \to \limits^{ > 1200^\circ {\rm{C}}} {\rm{\;Si}}{{\rm{C}}_{\left( {\rm{s}} \right)}} + {\rm{\;}}{{\rm{O}}_{2{\rm{\;}}\left( {\rm{g}} \right)}}\end{equation}…”
Section: Resultsmentioning
confidence: 99%
“…The formed SiO gas reacts with carbon or carbon monoxide in the system to form SiC 2,19,24,28,29,34,38 according to Equations (10) and (11):…”
Section: Phase Analysismentioning
confidence: 99%
“…[4,5] During continuous casting, the lower part of the nozzle is inserted into the mold, and the refractory material outside the nozzle can be continuously corroded by the mold flux inside the mold. [6][7][8] Although ZrO 2 -C materials with good corrosion resistance have been used on the outside of nozzle as slag-line materials, the corrosion problem still exists. [6,7,9,10] This phenomenon not only limits the production efficiency of continuous casting but also brings hidden dangers to production safety.…”
Section: Introductionmentioning
confidence: 99%
“…Thermal Protection System (TPS) is critical in hypersonic vehicles subjected to severe aerodynamic heating. 1,2 Low-density carbon/phenolic (C/Ph) composites have been extensively applied in the heatshield of hypersonic vehicles because of their excellent ablation resistance. 3 The thermal protection mechanism is that C/Ph composites absorb heat mainly through phenolic pyrolysis and the thermal blocking effect generated by pyrolysis gas to prevent heat transfer to the back face.…”
Section: Introductionmentioning
confidence: 99%