Gas injection nozzle refractory and gas injection nozzle
US-11821691-B2 · Nov 21, 2023 · US
US11976340B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11976340-B2 |
| Application number | US-202017601681-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 24, 2020 |
| Priority date | Apr 5, 2019 |
| Publication date | May 7, 2024 |
| Grant date | May 7, 2024 |
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A refining vessel for high-temperature melt includes a refractory for gas blowing nozzle that includes a central refractory embedded with metal tubules, and an outer refractory circumferentially surrounding the central refractory. The refractory for gas blowing nozzle has a horizontal projection on which a minimum radius of an imaginary circle encompassing all the metal tubules embedded in the central refractory is R (mm), wherein the central refractory has an outline that falls between one circle that is concentric with the imaginary circle and has a radius of R+10 mm, and another circle that is concentric with the imaginary circle and has a radius of R+150 mm. The central refractory is formed of a MgO—C refractory having a carbon content of 30 to 80 mass %, and the outer refractory is formed of a MgO—C refractory having a carbon content of 10 to 25 mass %.
Opening claim text (preview).
The invention claimed is: 1. A refining vessel for high-temperature melt comprising a gas blowing nozzle configured from a refractory for gas blowing nozzle with one or more gas-blowing metal tubules embedded in a carbon-containing refractory, the refractory for gas blowing nozzle including a central refractory embedded with the one or more gas-blowing metal tubules, and an outer refractory circumferentially surrounding the central refractory, the refractory for gas blowing nozzle having an operating plane in which a minimum radius of an imaginary circle encompassing all the gas-blowing metal tubules embedded in the central refractory is R (mm), wherein the central refractory has an outline that falls between one circle that is concentric with the imaginary circle and has a radius of R+10 mm, and another circle that is concentric with the imaginary circle and has a radius of R+150 mm, the central refractory is formed of a MgO—C refractory having a carbon content of 30 to 80 mass %, and the outer refractory is formed of a MgO—C refractory having a carbon content of 10 to 25 mass %, wherein the outer refractory has an outline that falls between one circle concentric with the imaginary circle and having a radius of R×2, and another circle concentric with the imaginary circle and having a radius of R×8. 2. The refining vessel according to claim 1 , wherein the central refractory has an outline that falls between one circle concentric with the imaginary circle and having a radius of R+40 mm, and another circle concentric with the imaginary circle and having a radius of R+70 mm. 3. The refining vessel according to claim 1 , wherein the central refractory has a circular outline concentric with the imaginary circle. 4. The refining vessel according to claim 1 , wherein the central refractory is formed of a MgO—C refractory having a carbon content of 50 to 70 mass %, and the outer refractory is formed of a MgO—C refractory having a carbon content of 15 to 25 mass %. 5. The refining vessel according to claim 1 , wherein the refining vessel comprises the gas blowing nozzle at a furnace bottom portion. 6. The refining vessel according to claim 2 , wherein the central refractory has a circular outline concentric with the imaginary circle. 7. The refining vessel according to claim 2 , wherein the central refractory is formed of a MgO—C refractory having a carbon content of 50 to 70 mass %, and the outer refractory is formed of a MgO—C refractory having a carbon content of 15 to 25 mass %. 8. The refining vessel according to claim 3 , wherein the central refractory is formed of a MgO—C refractory having a carbon content of 50 to 70 mass %, and the outer refractory is formed of a MgO—C refractory having a carbon content of 15 to 25 mass %. 9. The refining vessel according to claim 2 , wherein the refining vessel comprises the gas blowing nozzle at a furnace bottom portion. 10. The refining vessel according to claim 3 , wherein the refining vessel comprises the gas blowing nozzle at a furnace bottom portion. 11. The refining vessel according to claim 6 , wherein the refining vessel comprises the gas blowing nozzle at a furnace bottom portion. 12. The refining vessel according to claim 7 , wherein the refining vessel comprises the gas blowing nozzle at a furnace bottom portion. 13. The refining vessel according to claim 1 , wherein the central refractory contains less than 3.0 mass % of at least one of metal aluminum, metal silicon, Al—Mg, SiC, and B 4 C.
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Oxygen · CPC title
the fluid being a fuel · CPC title
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