WO2013180219A1 - Lining structure for molten-metal container - Google Patents
Lining structure for molten-metal container Download PDFInfo
- Publication number
- WO2013180219A1 WO2013180219A1 PCT/JP2013/065045 JP2013065045W WO2013180219A1 WO 2013180219 A1 WO2013180219 A1 WO 2013180219A1 JP 2013065045 W JP2013065045 W JP 2013065045W WO 2013180219 A1 WO2013180219 A1 WO 2013180219A1
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- WIPO (PCT)
- Prior art keywords
- heat insulating
- gap
- insulating material
- refractory
- iron skin
- Prior art date
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D41/00—Casting melt-holding vessels, e.g. ladles, tundishes, cups or the like
- B22D41/02—Linings
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21C—PROCESSING OF PIG-IRON, e.g. REFINING, MANUFACTURE OF WROUGHT-IRON OR STEEL; TREATMENT IN MOLTEN STATE OF FERROUS ALLOYS
- C21C7/00—Treating molten ferrous alloys, e.g. steel, not covered by groups C21C1/00 - C21C5/00
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
- F27D1/00—Casings; Linings; Walls; Roofs
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
- F27D1/00—Casings; Linings; Walls; Roofs
- F27D1/0003—Linings or walls
- F27D1/0006—Linings or walls formed from bricks or layers with a particular composition or specific characteristics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
- F27D3/00—Charging; Discharging; Manipulation of charge
- F27D3/12—Travelling or movable supports or containers for the charge
- F27D3/123—Furnace cars
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
- F27D3/00—Charging; Discharging; Manipulation of charge
- F27D3/14—Charging or discharging liquid or molten material
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- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21C—PROCESSING OF PIG-IRON, e.g. REFINING, MANUFACTURE OF WROUGHT-IRON OR STEEL; TREATMENT IN MOLTEN STATE OF FERROUS ALLOYS
- C21C5/00—Manufacture of carbon-steel, e.g. plain mild steel, medium carbon steel or cast steel or stainless steel
- C21C5/28—Manufacture of steel in the converter
- C21C5/42—Constructional features of converters
- C21C5/44—Refractory linings
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02W—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO WASTEWATER TREATMENT OR WASTE MANAGEMENT
- Y02W30/00—Technologies for solid waste management
- Y02W30/50—Reuse, recycling or recovery technologies
- Y02W30/91—Use of waste materials as fillers for mortars or concrete
Definitions
- the present invention relates to a lining structure of a molten metal container.
- the lining structure of a molten metal container (hereinafter also simply referred to as “container”) that contains molten metal such as hot metal or molten steel has a structure in which an iron skin as an outermost layer supports a refractory.
- Refractories used for molten metal containers include regular refractories and irregular refractories.
- the amorphous refractory is also called a castable and is often used as a refractory constituting a work refractory layer in contact with molten metal because of its ease of construction.
- the amorphous refractory is generally formed into a lining shape by adding water to a mixture of powder and particles of a high melting point material such as alumina and fluidizing the mixture into a container.
- Patent Document 1 uses silica fine particles as a main material.
- a heat insulating material which is a microporous molded body is disclosed.
- the amorphous refractory When molten steel or the like is charged in the molten metal container, if moisture remains in the amorphous refractory constituting the workpiece refractory layer, the water vapor pressure rises to, for example, 10 atm or more at 200 ° C., The amorphous refractory may explode and be damaged. Therefore, when the molten metal container is used, the amorphous refractory is previously dried by heating (hereinafter also referred to as “pre-drying”). The pre-drying is performed over a long period of time at a relatively low temperature in order to prevent the irregular refractory from being damaged by water vapor pressure.
- the temperature at the beginning of pre-drying is as low as 100 ° C. or less at the outer surface side of the irregular refractory, and steam is emitted from the inside of the irregular refractory. Part of the water condenses into liquid water. Thereafter, the portion on the outer surface side of the irregular refractory gradually becomes 100 ° C. or higher, and the moisture becomes steam.
- a through-hole is formed in the iron skin, which is the outermost layer of the container, and the vapor emitted from the amorphous refractory by pre-drying is exhausted to the outside through this through-hole.
- the present invention has been made in view of the above points, and an object of the present invention is to improve air permeability during pre-drying of an amorphous refractory in a lining structure of a molten metal container provided with a heat insulating material.
- the present inventors have intensively studied to achieve the above object. As a result, it has been found that by making the heat insulating material, which is a sheet-like polygonal member, a specific arrangement, the vapor permeability can be improved during the preliminary drying of the irregular refractory, and the present invention has been completed. That is, the present invention provides the following (1) to (3).
- a lining structure of a molten metal container for containing a molten metal which constitutes the outermost layer of the molten metal container, and has an iron skin having a plurality of through holes penetrating an outer surface and an inner surface;
- One or two permanent refractory layers provided on the inner side of the iron skin, and provided on the inner side of the permanent refractory layer, forming an operating surface in contact with the molten metal, at least a part of which is an amorphous refractory
- a workpiece refractory layer composed of a sheet-like polygonal member, which is constructed between the iron skin and the permanent refractory layer, or between the two layers of the permanent refractory layer,
- a plurality of heat insulating materials arranged adjacent to each other along the inner surface of the iron skin, and one heat insulating material and at least one of the other heat insulating materials arranged adjacent to the heat insulating material.
- a gap is formed between them, and the gap is positioned on the through
- the air permeability during the pre-drying of the irregular refractory can be improved.
- FIG. 6 is a graph showing the relationship between the ratio of the width of the gap G to the thickness of the heat insulating material 5 and the temperature of the gap G on the iron skin 2 side.
- (A) is an infrared thermal image showing the molten steel pan 1 in which the thickness of the iron skin 2 is 30 mm and the width of the gap G of the heat insulating material 5 is 40 to 50 mm
- (b) is the infrared thermal image of (a).
- (A) is an infrared thermal image showing the molten steel pan 1 in which the thickness of the iron skin 2 is 30 mm and the width G of the heat insulating material 5 is 20 to 30 mm
- (b) is the infrared thermal image of (a). It is a graph which shows the temperature distribution of the lines A and B in an image.
- Embodiment described below is an application example to the molten steel pan 1 which accommodates the molten steel 61 as a molten metal.
- FIG. 1 is a side view showing the molten steel pan 1 with a part cut away.
- the molten steel ladle 1 shown in FIG. 1 accommodates and holds a molten steel 61 converted from molten iron in a converter.
- a slag (not shown) floats on the surface of the molten steel 61.
- a secondary refining process is performed in which impurities are removed from the molten steel 61 and additional elements are added.
- the molten steel 61 that has undergone secondary refining is transported by the molten steel pan 1 and subjected to a continuous casting process.
- the lining structure of the molten steel pan 1 basically has an iron skin 2, a permanent refractory layer 3, and a workpiece refractory layer 4 in order from the outside. Furthermore, the heat insulating material 5 which exhibits a heat insulation function is constructed in the side surface part etc. of the molten steel pan 1. Below, based on FIG. 1, the permanent refractory layer 3 and the workpiece
- the permanent refractory layer 3 is provided inside the iron skin 2.
- the permanent refractory layer 3 is a brick layer that is constructed in order to ensure safety so that the molten steel 61 does not leak even when (a part of) the workpiece refractory layer 4 described later is damaged and falls off.
- the permanent refractory layer 3 may be a single layer or two layers as shown in FIG.
- the thickness of the permanent refractory layer 3 is preferably 40 mm or more from the reason that the molten steel 61 does not leak immediately even if the workpiece refractory peels off for some reason, and for the reason of preventing the molten steel 61 from flowing out through the joint. Two-layer construction is more preferable.
- the workpiece refractory layer 4 is provided inside the permanent refractory layer 3.
- the workpiece refractory layer 4 is a layer that forms an operating surface that contacts the molten steel 61.
- FIG. 1 shows an example in which an amorphous refractory is used as the refractory (also referred to as “work refractory”) 41 constituting the work refractory layer 4.
- amorphous refractory 41 a mixture of powder and particles of a high melting point material such as alumina (Al 2 O 3 ) or magnesia (MgO) added to fluidize the permanent refractory layer 3. Pour between molds (not shown) to form a lining.
- the water vapor pressure inside the amorphous refractory 41 rises to 10 atm or more at 200 ° C., for example.
- the unshaped refractory 41 may explode and be damaged. Therefore, in order to prevent such breakage, preliminary drying is performed at a relatively low temperature for a long time.
- the pre-drying is generally performed from the inside of the molten steel pan 1 (that is, the working surface side of the workpiece refractory layer 4) using a burner or the like.
- the temperature of the part on the outer surface side of the irregular refractory 41 (that is, the iron skin 2 side of the workpiece refractory layer 4) is as low as 100 ° C. or less in the early stage of pre-drying, and comes out of the irregular refractory 41. A part of the vapor condenses into liquid water. Thereafter, in the middle stage to the final stage of pre-drying, the portion on the outer surface side of the irregular refractory 41 becomes 100 ° C. or higher, and the moisture becomes vapor and is exhausted from a through hole H described later formed in the iron skin 2.
- the thickness of the workpiece refractory layer 4 is advantageous to increase the thickness in order to reduce the repair frequency and increase the operation rate.
- the thickness of the workpiece refractory layer 4 is preferably 100 to 250 mm, and the vicinity of the boundary with the laying part (bottom part) is exposed to the molten steel flow or residual slag, so that it is thick.
- the other parts are thin, and it is more preferable to change the thickness for each part.
- the iron skin 2 is a steel structure that supports a refractory (refractory 31, refractory 41) as the outermost layer of the molten steel pan 1.
- a refractory refractory 31, refractory 41
- the thickness of the iron skin 2 (the length indicated by T2 in FIG. 1), the lower limit is determined from the strength calculation. The thicker it is, the harder it is to be deformed and the longer the life is. There are many examples to do.
- a plurality of through holes H penetrating the outer surface and the inner surface of the iron skin 2 are formed in the iron skin 2.
- the through-hole H allows the vapor emitted from the amorphous refractory 41 to pass through the above-described preliminary drying.
- the hole diameter of the through-hole H is not specifically limited, It is preferable that it is 6 mm or more from a viewpoint of prevention of clogging with a refractory piece. On the other hand, as long as it can prevent clogging, sufficient air permeability can be ensured, so it is often 30 mm or less.
- the heat insulating material 5 is constructed at least on the side surface portion of the molten steel pan 1, it may also be constructed on the laying portion (bottom surface portion). As a construction position of the heat insulating material 5, when two permanent refractory layers 3 are provided, it may be between these two layers. However, for the reason that the temperature of the heat insulating material 5 can be operated low and the heat insulating performance can be exhibited for a long time (for example, 2 years or more), the space between the iron skin 2 and the permanent refractory layer 3 is preferable as shown in FIG. . Below, although the case where the heat insulating material 5 is constructed between the iron skin 2 and the permanent refractory layer 3 is demonstrated to an example, this invention is not limited to this.
- the heat insulating material 5 is a sheet-like member, and is composed of, for example, a microporous molded body mainly composed of fine particles such as silica (SiO 2 ) and alumina (Al 2 O 3 ).
- a microporous molded body mainly composed of fine particles such as silica (SiO 2 ) and alumina (Al 2 O 3 ).
- the microporous material formed by molding fine particles such as silica is fluidized when it comes into contact with moisture of the liquid and loses heat insulation. Therefore, when the amorphous refractory 41 constructed by adding moisture is used, the heat insulating property of the heat insulating material 5 may be lowered. Therefore, it is preferable that the heat insulating material 5 is housed in a waterproof covering material 51 to prevent deterioration due to moisture.
- the material of the covering material 51 is not particularly limited as long as it is waterproof, and examples thereof include a resin film. Specifically, for example, a resin such as polypropylene or polyethylene is suitable. In addition, a material obtained by laminating an aluminum foil with these resins in order to improve the moisture barrier property is also used.
- the thickness of the heat insulating material 5 (the length indicated by T5 in FIG. 1) is not particularly limited. However, even when the molten steel 61 contacts the heat insulating material 5 for some reason, the molten steel 61 causes the heat insulating material 5 to melt. For the purpose of preventing extension over a wide range, it is preferably 15 mm or less, more preferably 3 to 10 mm. Note that the thickness of the heat insulating material 5 includes the covering material 51.
- FIG. 2 is a schematic view of a plurality of heat insulating materials 5 arranged along the inner surface of the iron skin 2 as viewed from the inside of the molten steel pan 1.
- configurations other than the iron skin 2 and the heat insulating material 5 are omitted.
- FIG. 2 shows a rectangular shape as the sheet-like heat insulating material 5.
- the shape of the heat insulating material 5 is not particularly limited as long as it is a polygonal shape, and examples thereof include a shape such as a trapezoid and a triangle in addition to a rectangle.
- the shape of the heat insulating material 5 can be a trapezoid.
- a plurality of heat insulating materials 5 are arranged adjacent to each other along the inner surface of the iron skin 2.
- the heat insulating material 5 is fixed to the inner surface of the iron skin 2 with, for example, an adhesive tape made of the same material as the covering material 51 (see FIG. 1).
- a gap G is formed between one heat insulating material 5 and at least one of the other heat insulating materials 5 adjacent thereto.
- other heat insulating materials 5b to 5e are arranged adjacent to each other around the heat insulating material 5a.
- interval G is formed in the position between the heat insulating material 5a and the heat insulating material 5b, and between the heat insulating material 5a and the heat insulating material 5d, respectively. Therefore, in FIG. 2 in which the permanent refractory layer 3 and the workpiece refractory layer 4 are omitted, the iron skin 2 is exposed from the gap G.
- the heat insulating material 5 is arranged so that the gap G to be formed is positioned on the through hole H.
- the gap G is positioned on the through hole H means that the heat insulating material 5 that forms the gap G shields a part of the through hole H, and the heat insulating material 5 that forms the gap G is the through hole H.
- the concept includes the case of exposing without shielding.
- the arrangement of the through holes H is not limited to this.
- variety (length shown by W in FIG. 2) of the clearance gap G of the heat insulating material 5 shall be more than the thickness (length shown by T5 in FIG. 1) mentioned above. .
- Such a lower limit value of the width of the gap G is set from the viewpoint of ensuring air permeability.
- the present inventors When the present inventors initially arranged the heat insulating material 5 having a thickness of 6 mm so that the width of the gap G was 1 to 3 mm, the time required for the pre-drying was greatly extended. As a result of the dismantling investigation after use, this is because the mortar 32 used when constructing the permanent refractory layer 3 entered the gap G of the heat insulating material 5 and the air permeability of the gap G was impaired. found. Therefore, the present inventors arranged the heat insulating material 5 so that the width of the gap G has various dimensions, and observed the generation of steam from the through hole H and the temperature increase of the iron skin 2 during the pre-drying. .
- the thickness of the heat insulating material 5 is 6 mm, the time required for pre-drying is extended when the width of the gap G is less than 6 mm, and if the thickness of the heat insulating material 5 is 3 mm, the width of the gap G The time required for pre-drying was extended when the thickness was less than 3 mm.
- the temperature during pre-drying of the mortar 32 that entered the gap G of the heat insulating material 5 was estimated by heat transfer calculation.
- FIG. 3 is a graph showing the relationship between the ratio of the width of the gap G to the thickness of the heat insulating material 5 and the temperature of the gap G on the iron skin 2 side.
- the horizontal axis indicates the ratio (unit:%) of the width of the gap G to the thickness of the heat insulating material 5.
- the vertical axis represents the iron skin of the gap G into which the mortar 32 has entered in the pre-drying middle plate where the outer surface temperature of the amorphous refractory 41 constituting the workpiece refractory layer 4 is 120 ° C. and the vapor pressure is 2 atm. This is a value (unit: ° C) calculated from the temperature on the second side.
- the width of the gap G of the heat insulating material 5 is set to be equal to or larger than the thickness of the heat insulating material 5.
- the width of the gap G of the heat insulating material 5 is less than the thickness of the iron skin 2 (the length indicated by T2 in FIG. 1) from the viewpoint of minimizing the decrease in the heat insulating effect due to the formation of the gap G. Preferably there is.
- the upper limit value of the width of the gap G will be described.
- FIG. 4A shows an infrared ray showing a molten steel pan 1 (diameter: 4.0 m, height: 4.5 m) in which the thickness of the iron skin 2 is 30 mm and the width of the gap G of the heat insulating material 5 is 40 to 50 mm.
- FIG. 4 (b) is a graph showing the temperature distribution of lines A and B in the infrared thermal image of FIG. 4 (a). More specifically, the infrared thermal image of FIG. 4 (a) is a view of the molten steel pan 1 in a state in which the molten steel 61 lifted by a crane is accommodated from a slightly lower side, and is bright (color is light). It shows that the part is hotter. Further, the graph of FIG.
- 4B is a temperature distribution in a range (lines A and B) that starts at the point x and ends at the other end in the infrared thermal image of FIG.
- the lengths of lines A and B are 1.05 m and 1.08 m, respectively.
- the horizontal axis indicates the number of pixels in lines A and B with the x point as the left end, and the vertical axis indicates the temperature (unit: ° C.).
- the temperature at the point x is about 240 ° C.
- the part located in the gap G (hereinafter, also referred to as “iron gap part 2a”) of the iron skin 2 is slightly brighter in FIG. 4A, and is a mountain in the graph of FIG. There are two places other than the x point.
- the iron crevice gap 2a is about 20-30 ° C. higher than other parts, and a temperature rise is observed.
- the radiation heat radiation to the outside is proportional to the fourth power of the outer surface temperature of the iron skin 2, and the radiation heat radiation to the outside is increased by 20% in the iron skin gap 2a.
- the width of the gap G of the heat insulating material 5 is preferably as small as possible.
- the lower limit value of the width of the gap G described above that is, the thickness of the heat insulating material 5 is generally about 1 to 20 mm, it is difficult to accurately construct the gap G in accordance with the lower limit value. It is.
- FIG. 5 is a graph showing the relationship between the ratio of the width of the gap G to the thickness of the iron skin 2 and the amount of radiant heat released from the iron skin gap 2a.
- the horizontal axis indicates the ratio (unit:%) of the width of the gap G to the thickness of the iron skin 2.
- the vertical axis is a value obtained by calculating the radiation heat radiation to the outside of the core gap 2a in a state where the molten steel 61 is accommodated in the molten steel pan 1, and the horizontal axis is an index with the calculation result of 100% being 100%. It is. From the graph of FIG. 5, it is suggested that when the width of the gap G is larger than the thickness of the iron shell 2, the radiation heat dissipation increases rapidly.
- FIG. 6A is an infrared thermal image showing the molten steel pan 1 in which the thickness of the iron skin 2 is 30 mm and the width of the gap G of the heat insulating material 5 is 20 to 30 mm.
- FIG. It is a graph which shows the temperature distribution of the lines A and B in the infrared thermal image of (a). 6 (a) and 6 (b) are the same as FIGS. 4 (a) and 4 (b), respectively, and the description thereof is omitted. However, the lengths of the lines A and B are each 0. .58 m and 1.10 m. 6 (a) and 6 (b), it can be seen that the temperature increase in the iron-skin gap 2a, which was recognized in FIGS.
- the width of the gap G of the heat insulating material 5 is equal to or less than the thickness of the iron shell 2 because a significant decrease in the heat insulating effect can be suppressed.
- stacked aluminum foil in order to improve moisture-proof property) is provided between the iron skin 2 and the permanent refractory layer 3 except a floor part.
- a heat insulating material 5 (thickness: 5 mm) was applied.
- the heat insulating material 5 was composed of a microporous molded body mainly composed of silica and alumina fine particles, and the shape thereof was rectangular (500 to 1000 mm ⁇ 350 to 500 mm).
- a plurality of the heat insulating materials 5 were fixed to the inner surface of the iron skin 2 with an adhesive tape made of the same material as the covering material 51 and arranged adjacent to each other.
- the through-hole H hole diameter: 12 mm
- the gap G positioned on the through-hole H is formed on the upper and lower sides of the heat insulating material 5 as shown in FIG. Formed.
- the construction of the heat insulating material 5 was performed manually. At the time of construction, a pencil with a diameter of 8 mm was carried, and attention was paid so that the width of the gap G would be a dimension from the diameter of this pencil to twice the diameter. That is, the width of the gap G was set to 8 to 16 mm. As a result of such construction, some of the through holes H in which the gap G is positioned are shielded by the heat insulating material 5 in about a quarter.
- the heat insulating material 5 was applied in the same manner as in Invention Example 1 except that the width of the gap G was 20 to 40 mm. At the time of construction, a round bar having a diameter of 20 mm was carried, and attention was paid so that the width of the gap G would be a dimension from the diameter of this round bar to twice the diameter. By increasing the allowable range of the interval, a larger heat insulating material can be used, and the workability is improved.
- Invention Examples 1 and 2 required a shorter time for pre-drying than Comparative Example 1, and had good air permeability during pre-drying. Further, in Comparative Example 1, peeling wear during use was observed, and there was a possibility that the drying was insufficient despite the long pre-drying time. In addition, it was found that Invention Example 1 had a smaller temperature difference between the iron skin gap 2a and the other part of the iron skin 2 than the Invention Example 2, and the temperature increase of the iron skin gap 2a was suppressed. In Invention Example 1, the temperature rise of the iron gap portion 2a was 10 ° C. or less, and the increase in radiation heat dissipation was in a negligible range.
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- Organic Chemistry (AREA)
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Abstract
Description
溶融金属容器に使用される耐火物としては、定形耐火物と不定形耐火物とがある。とりわけ、不定形耐火物は、キャスタブルとも呼ばれ、その施工の容易さから、溶融金属に接するワーク耐火物層を構成する耐火物として、多く使用されている。
不定形耐火物は、一般に、アルミナ等の高融点物質の粉や粒の混合物に、水を加えて流動化させて容器に流し込み、内張り形状とされる。 The lining structure of a molten metal container (hereinafter also simply referred to as “container”) that contains molten metal such as hot metal or molten steel has a structure in which an iron skin as an outermost layer supports a refractory.
Refractories used for molten metal containers include regular refractories and irregular refractories. In particular, the amorphous refractory is also called a castable and is often used as a refractory constituting a work refractory layer in contact with molten metal because of its ease of construction.
The amorphous refractory is generally formed into a lining shape by adding water to a mixture of powder and particles of a high melting point material such as alumina and fluidizing the mixture into a container.
従来、溶融金属容器に断熱性を付与する方法としては、ワーク耐火物層の背面側に断熱材を挿入する方法が提案されており、例えば、特許文献1には、シリカ微粒子を主材とした微孔性成形体である断熱材が開示されている。 By the way, since many metals such as iron have a melting point as high as several hundred to several hundreds of degrees Celsius, molten metal containers are required to have heat resistance as well as fire resistance.
Conventionally, as a method of imparting heat insulation to a molten metal container, a method of inserting a heat insulating material on the back side of the workpiece refractory layer has been proposed. For example,
そのため、溶融金属容器が使用されるにあたっては、不定形耐火物に対して、事前に加熱による乾燥(以下、「事前乾燥」ともいう。)が施される。事前乾燥は、水蒸気圧による不定形耐火物の破損を防ぐために、比較的低温で長時間をかけて行なわれる。 When molten steel or the like is charged in the molten metal container, if moisture remains in the amorphous refractory constituting the workpiece refractory layer, the water vapor pressure rises to, for example, 10 atm or more at 200 ° C., The amorphous refractory may explode and be damaged.
Therefore, when the molten metal container is used, the amorphous refractory is previously dried by heating (hereinafter also referred to as “pre-drying”). The pre-drying is performed over a long period of time at a relatively low temperature in order to prevent the irregular refractory from being damaged by water vapor pressure.
容器の最外層である鉄皮には貫通孔が形成されており、事前乾燥によって不定形耐火物から出る蒸気は、この貫通孔から外部に排気される。 Since pre-drying is performed from the inside of the container using a burner or the like, the temperature at the beginning of pre-drying is as low as 100 ° C. or less at the outer surface side of the irregular refractory, and steam is emitted from the inside of the irregular refractory. Part of the water condenses into liquid water. Thereafter, the portion on the outer surface side of the irregular refractory gradually becomes 100 ° C. or higher, and the moisture becomes steam.
A through-hole is formed in the iron skin, which is the outermost layer of the container, and the vapor emitted from the amorphous refractory by pre-drying is exhausted to the outside through this through-hole.
そのため、不定形耐火物の内部に水分が残存しているにもかかわらず、事前乾燥が終了したと誤認して、容器に溶融金属を装入してしまい、不定形耐火物の爆裂破損を招くおそれがある。 However, when a heat insulating material is inserted on the back side of the workpiece refractory layer, exhaust from the through hole is obstructed. Moreover, since the inner surface side of the amorphous refractory is already solidified and partially sintered by pre-drying, the steam that has not been exhausted from the through-hole is not easily exhausted from the inner surface side, and remains inside.
Therefore, even though moisture remains inside the amorphous refractory, it is misunderstood that the pre-drying has been completed, and the molten metal is charged into the container, resulting in explosion breakage of the amorphous refractory. There is a fear.
すなわち、本発明は、以下の(1)~(3)を提供する。 The present inventors have intensively studied to achieve the above object. As a result, it has been found that by making the heat insulating material, which is a sheet-like polygonal member, a specific arrangement, the vapor permeability can be improved during the preliminary drying of the irregular refractory, and the present invention has been completed.
That is, the present invention provides the following (1) to (3).
以下では、まず、図1に基づいて、永久耐火物層3およびワーク耐火物層4について説明する。 The lining structure of the
Below, based on FIG. 1, the permanent
永久耐火物層3を構成する耐火物(「永久耐火物」ともいう。)31としては、例えば、ろう石煉瓦などの定形耐火物(成形煉瓦)が用いられる。耐火物31は、図1に示すように、モルタル32を目地材として用いて、煉瓦積み施工される。 The permanent
As the refractory material (also referred to as “permanent refractory material”) 31 constituting the permanent
図1では、ワーク耐火物層4を構成する耐火物(「ワーク耐火物」ともいう。)41としては、不定形耐火物を用いた例を示す。不定形耐火物41を用いる場合、アルミナ(Al2O3)やマグネシア(MgO)等の高融点物質の粉や粒の混合物に水を加えて流動化させたものを、永久耐火物層3と型枠(図示せず)との間に流し込み、内張り形状とする。 The workpiece
FIG. 1 shows an example in which an amorphous refractory is used as the refractory (also referred to as “work refractory”) 41 constituting the work
事前乾燥は、一般的に、バーナ等を用いて、溶鋼鍋1の内側(すなわち、ワーク耐火物層4の稼働面側)から行なわれる。そのため、不定形耐火物41の外面側(すなわち、ワーク耐火物層4の鉄皮2側)の部位は、事前乾燥の序盤では温度が100℃以下と低く、不定形耐火物41の内部から出る蒸気の一部が、凝縮して液体の水となる。その後、事前乾燥の中盤~終盤では、不定形耐火物41の外面側の部位も100℃以上となり、水分が蒸気となって、鉄皮2に形成された後述する貫通孔Hから排気される。 By the way, if moisture remains in the
The pre-drying is generally performed from the inside of the molten steel pan 1 (that is, the working surface side of the workpiece refractory layer 4) using a burner or the like. Therefore, the temperature of the part on the outer surface side of the irregular refractory 41 (that is, the
鉄皮2の厚さ(図1中、T2で示す長さ)としては、下限は強度計算から定められ、厚いほど変形し難く長寿命であるが、費用と重量制約とから30~90mmを採用する例が多い。 Next, the
As for the thickness of the iron skin 2 (the length indicated by T2 in FIG. 1), the lower limit is determined from the strength calculation. The thicker it is, the harder it is to be deformed and the longer the life is. There are many examples to do.
貫通孔Hの孔径は、特に限定されないが、耐火物片などによる詰まり防止の観点から6mm以上であるのが好ましい。一方、詰まりさえ防げれば通気性は十分確保できるので30mm以下とすることが多い。 A plurality of through holes H penetrating the outer surface and the inner surface of the
Although the hole diameter of the through-hole H is not specifically limited, It is preferable that it is 6 mm or more from a viewpoint of prevention of clogging with a refractory piece. On the other hand, as long as it can prevent clogging, sufficient air permeability can be ensured, so it is often 30 mm or less.
断熱材5の施工位置としては、永久耐火物層3が2層設けられる場合は、この2層の間でもよい。しかし、断熱材5の温度を低く運用でき、長期間(例えば2年以上)断熱性能を発揮できるという理由から、図1に示すように、鉄皮2と永久耐火物層3との間が好ましい。
以下では、鉄皮2と永久耐火物層3との間に断熱材5が施工される場合を例に説明するが、本発明はこれに限定されるものではない。 Next, the
As a construction position of the
Below, although the case where the
ところで、シリカ等の微粒子を成形した微孔性材質は、液体の水分に接すると流動化して断熱性が失われる。そのため、水分を加えて施工される不定形耐火物41が用いられる場合には、断熱材5の断熱性が低下するおそれがある。
そこで、断熱材5は、防水性の被覆材51に収納され、水分による劣化が防止されるのが好ましい。被覆材51の材質としては、防水性であれば特に限定されないが、例えば、樹脂フィルム等が挙げられ、具体的には、例えば、ポリプロピレンやポリエチレンなどの樹脂が適する。また、遮湿性を高めるためにこれらの樹脂でアルミ箔をラミネートした材質も用いられる。 The
By the way, the microporous material formed by molding fine particles such as silica is fluidized when it comes into contact with moisture of the liquid and loses heat insulation. Therefore, when the amorphous refractory 41 constructed by adding moisture is used, the heat insulating property of the
Therefore, it is preferable that the
このとき、1つの断熱材5と、これに隣接する他の断熱材5のうちの少なくとも1つの断熱材5との間に、間隙Gが形成される。
例えば、図2中、断熱材5aの周囲には、他の断熱材5b~5eが隣接配置される。このうち、断熱材5aと断熱材5bとの間、および、断熱材5aと断熱材5dとの間の位置に、それぞれ、間隙Gが形成される。そのため、永久耐火物層3およびワーク耐火物層4を省略した図2においては、間隙Gから鉄皮2が露出している。 As shown in FIG. 2, a plurality of
At this time, a gap G is formed between one
For example, in FIG. 2, other
そこで、本発明者らは、断熱材5を、間隙Gの幅が様々な寸法となるように配置し、事前乾燥中における貫通孔Hからの蒸気発生と鉄皮2の温度上昇とを観察した。その結果、断熱材5の厚さが6mmであると、間隙Gの幅が6mm未満の場合に事前乾燥の所要時間が延長し、断熱材5の厚さが3mmであると、間隙Gの幅が3mm未満の場合に事前乾燥の所要時間が延長した。
この現象を検証すべく、断熱材5の間隙Gに侵入したモルタル32の事前乾燥中の温度を伝熱計算により推定した。 When the present inventors initially arranged the
Therefore, the present inventors arranged the
In order to verify this phenomenon, the temperature during pre-drying of the
より詳細には、図4(a)の赤外線熱画像は、クレーンで吊り上げた溶鋼61が収容された状態の溶鋼鍋1を側面のやや下側から見た図であり、明るい(色が薄い)部位ほど高温であることを示す。
また、図4(b)のグラフは、図4(a)の赤外線熱画像中の×点で始まり他端で終わる範囲(ラインAおよびB)の温度分布である。ラインAおよびBの長さは、それぞれ1.05mおよび1.08mである。図4(b)のグラフにおいて、横軸は×点を左端としたラインAおよびBのピクセル数を示し、縦軸は温度(単位:℃)を示す。 FIG. 4A shows an infrared ray showing a molten steel pan 1 (diameter: 4.0 m, height: 4.5 m) in which the thickness of the
More specifically, the infrared thermal image of FIG. 4 (a) is a view of the
Further, the graph of FIG. 4B is a temperature distribution in a range (lines A and B) that starts at the point x and ends at the other end in the infrared thermal image of FIG. The lengths of lines A and B are 1.05 m and 1.08 m, respectively. In the graph of FIG. 4B, the horizontal axis indicates the number of pixels in lines A and B with the x point as the left end, and the vertical axis indicates the temperature (unit: ° C.).
しかし、上述した間隙Gの幅の下限値、すなわち、断熱材5の厚さは、一般的に1~20mm程度であるため、間隙Gの幅を下限値に合わせて正確に施工することは困難である。 From the Stefan-Boltzmann law, the radiation heat radiation to the outside is proportional to the fourth power of the outer surface temperature of the
However, since the lower limit value of the width of the gap G described above, that is, the thickness of the
図5のグラフにおいて、横軸は、鉄皮2の厚さに対する間隙Gの幅の比率(単位:%)を示す。一方、縦軸は、溶鋼鍋1に溶鋼61が収容された状態における、鉄皮間隙部2aの外部への輻射放熱を計算した値であり、横軸が80%の計算結果を100とした指数である。
図5のグラフから、間隙Gの幅が鉄皮2の厚さよりも大きい場合は、輻射放熱が急激に増加することが示唆される。 FIG. 5 is a graph showing the relationship between the ratio of the width of the gap G to the thickness of the
In the graph of FIG. 5, the horizontal axis indicates the ratio (unit:%) of the width of the gap G to the thickness of the
From the graph of FIG. 5, it is suggested that when the width of the gap G is larger than the thickness of the
図6(a)および(b)からは、図4(a)および(b)では認められていた鉄皮間隙部2aでの温度上昇が、解消されていることが分かる。
したがって、断熱効果の大幅な低下が抑制できるという理由から、断熱材5の間隙Gの幅は、鉄皮2の厚さ以下とするのが好ましい。 FIG. 6A is an infrared thermal image showing the
6 (a) and 6 (b), it can be seen that the temperature increase in the iron-
Therefore, it is preferable that the width of the gap G of the
図1の溶鋼鍋1(直径:4.0m、高さ:4.5m)において、鉄皮2(厚さ:30mm)の内側に、ろう石煉瓦を耐火物31として使用し、モルタル32を目地材として永久耐火物層3(厚さ:50mm)を形成した。さらに、アルミナ-マグネシア質の不定形耐火物41を、6質量%の混練水分として、永久耐火物層3と型枠(図示せず)との間に流し込み、ワーク耐火物層4(厚さ:120mm)を形成した。 <Invention Example 1>
In the molten steel ladle 1 (diameter: 4.0 m, height: 4.5 m) in FIG. 1, a wax stone brick is used as the refractory 31 inside the iron skin 2 (thickness: 30 mm), and the
間隙Gの幅を、20~40mmとした以外は、発明例1と同様にして、断熱材5を施工した。施工に際しては、直径20mmの丸棒を携帯し、間隙Gの幅が、この丸棒の直径から直径の2倍までの寸法となるように留意した。間隔の許容範囲を大きくしたことにより、より大型の断熱材を用いることができ、施工性は向上した。 <Invention Example 2>
The
間隙Gの幅を、2~4mmとした以外は、発明例1と同様にして、断熱材5を施工した。施工に際しては、直径2mmの丸棒を携帯し、間隙Gの幅が、この丸棒の直径から直径の2倍までの寸法となるように留意した。 <Comparative Example 1>
A
各例において、不定形耐火物41を流し込みワーク耐火物層4を形成した後、バーナを用いて、ワーク耐火物層4の稼働面側から事前乾燥を、加熱温度等の各条件を同じにして行ない、事前乾燥の開始から所要時間を測定した。なお、事前乾燥は、鉄皮外面温度がアルミナセメントの脱水温度である150℃に到達することにより、終了したものと判断した。
各例の所要時間を、発明例1の所要時間を100とした指数で評価した。結果を下記第1表に示す。指数が小さいほど、事前乾燥が終了するまでの時間が短く、事前乾燥中の通気性が良好であるものとして評価できる。 <Evaluation>
In each example, after pouring the amorphous refractory 41 and forming the workpiece
The time required for each example was evaluated by an index with the time required for Example 1 as 100. The results are shown in Table 1 below. It can be evaluated that the smaller the index is, the shorter the time until the predrying is completed and the better the air permeability during the predrying.
また、発明例1は、発明例2よりも、鉄皮2における鉄皮間隙部2aと他部位との温度差が小さく、鉄皮間隙部2aの温度上昇が抑制されたことが分かった。なお、発明例1では、鉄皮間隙部2aの温度上昇が10℃以下であり、輻射放熱の増加は無視できる範囲であった。 From the results shown in Table 1, it was found that Invention Examples 1 and 2 required a shorter time for pre-drying than Comparative Example 1, and had good air permeability during pre-drying. Further, in Comparative Example 1, peeling wear during use was observed, and there was a possibility that the drying was insufficient despite the long pre-drying time.
In addition, it was found that Invention Example 1 had a smaller temperature difference between the
2 鉄皮
2a 鉄皮間隙部
3 永久耐火物層
31 耐火物(定形耐火物)
32 モルタル
4 ワーク耐火物層
41 耐火物(不定形耐火物)
5 断熱材
51 被覆材
61 溶鋼(溶融金属)
G 間隙
H 貫通孔
T2 鉄皮の厚さ
T5 断熱材の厚さ
W 間隙の幅 1 Molten steel pan (molten metal container)
2
32
5
G Gap H Through-hole T2 Iron skin thickness T5 Heat insulation thickness W Gap width
Claims (3)
- 溶融金属を収容する溶融金属容器のライニング構造であって、
前記溶融金属容器の最外層を構成し、外側面と内側面とを貫通する複数個の貫通孔を有する鉄皮と、
前記鉄皮の内側に設けられる、1層または2層の永久耐火物層と、
前記永久耐火物層の内側に設けられ、前記溶融金属と接する稼働面を形成し、少なくとも一部が不定形耐火物で構成されるワーク耐火物層と、
シート状の多角形部材であって、前記鉄皮と前記永久耐火物層との間、または、2層の前記永久耐火物層どうしの間に施工され、前記鉄皮の内側面に沿って隣接配置される複数枚の断熱材と、
を備え、
1つの前記断熱材と、当該断熱材に隣接配置される他の前記断熱材のうちの少なくとも1つとの間に、間隙が形成され、
前記間隙が、前記貫通孔上に位置付けられ、かつ、前記断熱材の厚さ以上の幅を有する、溶融金属容器のライニング構造。 A molten metal lining structure for containing molten metal,
The outermost layer of the molten metal container, the iron skin having a plurality of through holes penetrating the outer surface and the inner surface,
One or two permanent refractory layers provided inside the iron skin;
A workpiece refractory layer provided on the inside of the permanent refractory layer, forming a working surface in contact with the molten metal, at least a part of which is formed of an amorphous refractory;
A sheet-like polygonal member, which is constructed between the iron skin and the permanent refractory layer, or between the two layers of the permanent refractory layer, and is adjacent along the inner surface of the iron skin A plurality of thermal insulators arranged;
With
A gap is formed between one of the heat insulating materials and at least one of the other heat insulating materials arranged adjacent to the heat insulating material,
The molten metal container lining structure, wherein the gap is positioned on the through hole and has a width equal to or greater than a thickness of the heat insulating material. - 前記間隙の幅が、前記鉄皮の厚さ以下である、請求項1に記載の溶融金属容器のライニング構造。 The lining structure of a molten metal container according to claim 1, wherein a width of the gap is equal to or less than a thickness of the iron skin.
- 前記断熱材が、防水性の被覆材に収納されている、請求項1または2に記載の溶融金属容器のライニング構造。 The lining structure for a molten metal container according to claim 1 or 2, wherein the heat insulating material is housed in a waterproof covering material.
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Cited By (4)
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WO2018075680A1 (en) | 2016-10-18 | 2018-04-26 | Saint-Gobain Ceramics & Plastics, Inc. | Ceramic liner and method of forming |
CN109690218A (en) * | 2016-08-24 | 2019-04-26 | 维苏威美国公司 | Metallurgical tank liner with closed metal layer |
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JP2022065959A (en) * | 2020-10-16 | 2022-04-28 | Jfeスチール株式会社 | Steel shell structure of molten metal holding vessel and molten metal holding vessel |
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KR20230090630A (en) * | 2021-12-15 | 2023-06-22 | 재단법인 포항산업과학연구원 | Furnace wall having excellent heat loss reduction effect and corrosion reduction effect |
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CN109690218A (en) * | 2016-08-24 | 2019-04-26 | 维苏威美国公司 | Metallurgical tank liner with closed metal layer |
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EP3960329A1 (en) * | 2020-08-28 | 2022-03-02 | Oskar Frech GmbH + Co. KG | Casting component with anticorrosion layer structure |
JP2022065959A (en) * | 2020-10-16 | 2022-04-28 | Jfeスチール株式会社 | Steel shell structure of molten metal holding vessel and molten metal holding vessel |
JP7347393B2 (en) | 2020-10-16 | 2023-09-20 | Jfeスチール株式会社 | Shell structure of molten metal storage container and molten metal storage container |
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