The present invention relates to taper plate assemblies for use in steel production ladles, and more particularly relates to taper plate assemblies that protect and provide compression for refractory linings of the ladles.
There are presently various methods of restraining refractory linings in steel ladles by keeping the linings in compression. These include using metal plates and/or metal anchors covered in a refractory castable material and providing metal extension rings at the top of the ladles. However, conventional extension rings deform during use and lose the ability to provide adequate compression to refractory linings over time. As a result, the unconstrained refractory linings can result in loss of refractory bricks during slag dumping or cleaning of ladles, and may allow steel infiltration between joints that can lead to premature removal of ladle from service. The conventional extension rings also require routine maintenance or replacement to address their deformation.
The present invention provides taper plate assemblies that may be installed on the top of steel casting ladles to restrain and maintain refractory lining materials in compression during casting operations. The taper plate assemblies include a generally conical taper plate supported by a ring-shaped support flange and a support collar. The taper plate is located at least partially above a refractory top ring that may comprise a castable refractory material, and is designed to maintain the refractory top ring in compression during multiple casting operations.
An aspect of the present invention is to provide a taper plate assembly for a steel casting ladle, the assembly comprising: an annular support flange attached to the support collar and extending radially outward from the support collar; and a generally conical taper plate extending upward and radially inward from the support flange at a taper plate angle AT of greater than 30° measured from a vertical direction.
Another aspect of the present invention is to provide a steel casting ladle comprising: a ladle shell; and a taper plate assembly attached to an upper edge of the ladle shell. The taper plate assembly comprises: an annular support flange attached to the support collar and extending radially outward from the support collar; and a generally conical taper plate extending upward and radially inward from the support flange at a taper plate angle AT of greater than 30° measured from a vertical direction.
These and other aspects of the present invention will be more apparent from the following description.
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The radially inwardly extending coverage distance DT of the taper plate 40 may be sufficient to cover at least a portion of the refractory working lining 16, i.e., at least a portion of the radial thickness of the refractory working lining 16 is located vertically below the taper plate 40. For example, the coverage distance DT of the taper plate 40 is sufficient to cover at least 10 percent of the radial thickness of the underlying refractory working lining 16 as measured at the upper edge of the working lining, or at least 15 percent, or at least 20 percent, or at least 25 percent. The coverage distance DT may be sufficient to cover from 20 to 100 percent of the radial thickness of the refractory working lining 16, or from 20 to 75 percent, or from 20 to 50 percent, or from 25 to 75 percent.
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The taper plate thickness TT is typically greater than the support collar wall thickness TC. For example, the ratio of TT:TC is typically greater than 1.2:1, or greater than 1.4:1, or greater than 1.5:1. The ratio of TT:TC may typically range from 1.3:1 to 5:1, or from 1.4:1 to 4:1, or from 1.5:1 to 3:1. In certain embodiments, the ratio of TT:TC may be about 1.75:1, or about 2:1, or about 2.25:1.
The support flange 24 has a thickness TR typically greater than 2 inches, for example, greater than 2.5 inches. The support flange thickness TR may typically be from 2 to 5 inches, for example, from 2.25 to 4 inches, or from 2.5 to 3.5 inches, or about 3 inches. The support flange 24 has a width WR typically greater than 4 inches, for example, greater than 6 inches, or greater than 7 inches, or greater than 8 inches. The support flange ring width WR may typically be from 5 to 12 inches, for example, from 6 to 10 inches, or from 7 to 9 inches.
The support flange thickness TR is typically greater than the support collar wall thickness TC. For example, the ratio of TR:TC is typically greater than 1.2:1, or greater than 1.4:1, or greater than 1.5:1. The ratio of TR:TC may typically range from 1.3:1 to 5:1, or from 1.4:1 to 4:1, or from 1.5:1 to 3:1. In certain embodiments, the ratio of TR:TC may be about 1.75:1, or about 2:1, or about 2.25:1.
The taper plate thickness Ti may be the same or different than the support flange thickness TR. For example, the ratio of TT:TR may range from 0.5:1 to 2:1, or from 0.7:1 to 1.5:1, or from 0.8:1 to 1.3:1, or may be about 1:1.
Table 1 lists various angles and height of tapers and their corresponding coverage over the refractory lining. The taper plate angles AT range from 30° to 45°, and different taper plate heights and inward radial coverage distances or projection lengths are shown, in inches. The taper plates with 35° and 45° taper angles provide significantly improved compression to the underlying refractory top ring 18 and refractory linings 14 and 16 during extended use, and are significantly more durable than the taper plates with 30° taper angles having smaller vertical heights and horizontal projections.
By extending the taper plate height HT to, e.g., 10 or 11 inches and providing a taper angle AT of about 35° or 45°, the stress originating not only from the refractory safety lining 14 but also at least a portion of the stress and vertical expansion of the refractory working lining 16 will be covered. Compressive stress is increased in the refractory top ring 18 installed above the brick lining 14 and 16. The compressive strength of refractory top ring 18 is high enough that the increased stress will not have a negative impact on the performance of the refractory top ring 18.
At 11 inches and a 35-degree angle, the horizontal coverage is 7.77 inches, thus covering the entire safety lining 14 (e.g., 5.5 inches) and 2.2 inches of the working lining 16 (e.g., out of an 8 inch thick working lining). Changing the taper plate angle AT from 30° to 35° and increasing the vertical length of the taper plate from 8.6 inches to 11 inches thus significantly improves performance of the taper plate assembly. The combined effect of changing the vertical height HT of the taper plate 40 and the taper plate angle AT is such that the horizontal coverage distance DT is at least 20 percent of the working lining 16 thickness for effective compression.
The taper plate assemblies of the present invention provide improved compression for refractory linings, which help achieve longer campaign life and thus reduce cost. Additionally, the present taper plate assemblies address the common issue in the steel mill of losing compression in the lining due to deformation of the top over time. The present taper plate assemblies last significantly longer, and may not need any repairs of the top section of ladle. In contrast, conventional ladle designs require replacement of the top sections of ladles after a certain number of years to maintain the same level of compression. The taper plate assemblies address the issue of lip ring-related failures and repair common in the steel mills. The assemblies can help lower costs of steel ladle refractories by improving performance, keeping linings in compression and reducing costs for steel ladle shell repair work.
As used herein, “including,” “containing” and like terms are understood in the context of this application to be synonymous with “comprising” and are therefore open-ended and do not exclude the presence of additional undescribed or unrecited elements, materials, phases or method steps. As used herein, “consisting of” is understood in the context of this application to exclude the presence of any unspecified element, material, phase or method step. As used herein, “consisting essentially of” is understood in the context of this application to include the specified elements, materials, phases, or method steps, where applicable, and to also include any unspecified elements, materials, phases, or method steps that do not materially affect the basic or novel characteristics of the invention.
Notwithstanding that the numerical ranges and parameters setting forth the broad scope of the invention are approximations, the numerical values set forth in the specific examples are reported as precisely as possible. Any numerical value, however, inherently contains certain errors necessarily resulting from the standard variation found in their respective testing measurements.
Also, it should be understood that any numerical range recited herein is intended to include all sub-ranges subsumed therein. For example, a range of “1 to 10” is intended to include all sub-ranges between (and including) the recited minimum value of 1 and the recited maximum value of 10, that is, having a minimum value equal to or greater than 1 and a maximum value of equal to or less than 10.
In this application, the use of the singular includes the plural and plural encompasses singular, unless specifically stated otherwise. In addition, in this application, the use of “or” means “and/or” unless specifically stated otherwise, even though “and/or” may be explicitly used in certain instances. In this application and the appended claims, the articles “a,” “an,” and “the” include plural referents unless expressly and unequivocally limited to one referent.
Whereas particular embodiments of this invention have been described above for purposes of illustration, it will be evident to those skilled in the art that numerous variations of the details of the present invention may be made without departing from the invention as defined in the appended claims.
This application claims the benefit of U.S. Provisional Patent Application No. 62/979,901 filed Feb. 21, 2020, which is incorporated herein by reference.
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20210260648 | Dhaka | Aug 2021 | A1 |
Number | Date | Country | |
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20210260648 A1 | Aug 2021 | US |
Number | Date | Country | |
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62979901 | Feb 2020 | US |