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Claims  |
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We claim:
1. A method of manufacturing a refractory liner, comprising the steps of:
forming a pumpable casting composition including about 36-92% by weight
silicon carbide, about 8-20% by weight aqueous colloidal silica having an
average particle diameter of 4-100 millimicrons, zero to about 10% by
weight free carbon, and zero to about 50% by weight of an alumina
component;
transporting the casting composition to a mold assembly using a pump; and
molding the casting composition to form a refractory liner.
2. The method of claim 1, wherein the silicon carbide has an average
particle diameter of about 30 micrometers to about 3.5 millimeters.
3. The method of claim 1 wherein the silicon carbide is present at about
40-85% by weight of the casting composition.
4. The method of claim 1, wherein the silicon carbide is present at about
45-80% by weight of the casting composition.
5. The method of claim 1, wherein the alumina component is present at about
10-40% by weight of the casting composition.
6. The method of claim 1, wherein the alumina component comprises a
material selected from the group consisting of brown fused alumina, white
fused alumina, tabular alumina, and mixtures thereof.
7. The method of claim 1, wherein the free carbon is present at about 2-6%
by weight of the casting composition.
8. The method of claim 7, wherein the free carbon is present in the form of
graphite or pitch.
9. A refractory liner formed according to the method of claim 1.
10. A method of manufacturing a refractory liner, comprising the steps of:
forming a casting composition including about 36-92 % by weight silicon
carbide, about 8-20% by weight aqueous colloidal silica having an average
particle diameter of 4-100 millimicrons, zero to about 10% by weight free
carbon, and zero to about 50% by weight of an alumina component;
transporting the casting composition to a molten metal containment device
using a pump; and
forming a refractory liner from the casting composition in situ in the
metal containment device.
11. The method of claim 10, wherein the casting composition further
comprises about 1-10% by weight microsilica.
12. The method of claim 10, wherein the casting composition further
comprises about 5-20% by weight calcined alumina.
13. The method of claim 10, wherein the casting composition further
comprises about 0.02-1.0% by weight of a setting agent.
14. A refractory liner formed according to the method of claim 10.
15. A method of forming a refractory liner, comprising the steps of:
forming a lower refractory layer using a casting composition which includes
about 55-90% by weight of a granular base material selected from the group
consisting of calcined clay, mullite, brown fused alumina, tabular alumina
and mixtures thereof, a colloidal silica binder having an average particle
diameter of 4-100 millimicrons, and up to about 35 % by weight silicon
carbide;
hardening the lower refractory layer;
forming an upper refractory layer above the lower refractory layer using a
casting composition which includes about 36-92 % by weight silicon
carbide, a colloidal silica binder having an average particle diameter of
4-100 millimicrons, zero to about 10% by weight graphite, and zero to
about 50% by weight of an alumina component;
hardening the upper refractory layer; and
heating the upper and lower refractory layers at above 250.degree. F.
16. A refractory liner formed according to the method of claim 15. |
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Claims  |
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Description  |
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FIELD OF THE INVENTION
The present invention is a pumpable refractory composition especially
adapted for the regions of molten metal containment devices which have the
greatest exposure to slag, and a method of use.
BACKGROUND OF THE INVENTION
U.S. Pat. No. 5,147,830, issued to Banerjee and Connors, Jr., discloses a
pumpable refractory casting composition used for forming new liners, and
repairing existing liners, in molten metal containment devices. The
pumpable refractory composition replaced earlier refractory compositions
which were not pumpable and had to be transported using buckets and
cranes. The uses for the pumpable refractory composition include, but are
not limited to, tundishes, ladles, troughs, runners, blast furnaces, and
other molten metal containment devices.
The compositions disclosed in U.S. Pat. No. 5,147,830 include, as a primary
ingredient, 55-90% by weight of a refractory base material which can be
calcined clay, mullite, brown fused alumina, tabular alumina or
combinations thereof. All of these base materials include significant
amounts of alumina. Calcined clay includes about 43-48% by weight alumina.
Mullite includes about 57-73% by weight alumina. Brown fused alumina
includes about 93-98% by weight alumina, and tabular alumina includes
about 98.5-99.9% by weight alumina.
The compositions disclosed in U.S. Pat. No. 5,147,830 also include a
colloidal silica binder, and may include other refractory ingredients
(e.g. silicon carbide, graphite, microsilica) and a setting agent. The
colloidal silica, in addition to serving as a binder, contributes
excellent flow properties which facilitate the pumping of the casting
composition during its application.
Many metal containment devices, for example, blast furnace runners and
troughs, contain molten metal which includes some impurities. These
impurities tend to float to the top of the molten metal, forming what is
called a "slag" layer. The slag layer typically includes non-metallic
impurities, many of which are oxidized or oxidizable, and reactive gases
such as entrained oxygen or air.
Impurities in the slag layer react with the alumina and any carbon in the
refractory liner, causing oxidation of carbon and general weakening of the
liner. As a result, the portion of the refractory liner which is adjacent
to the slag layer wears out faster than the remaining refractory liner,
accelerating the time at which the refractory liner must be repaired or
replaced. Therefore, there is a need or desire in the iron and steel
industry for a refractory material which is especially resistant to attack
from slag, and which can be used in refractory liners in regions exposed
to slag.
SUMMARY OF THE INVENTION
The present invention is directed to a pumpable casting composition which
is especially resistant to attack from slag, and a method of use thereof.
The pumpable casting composition includes, as an essential ingredients
about 36-92% by weight silicon carbide preferably having an average
particle diameter of about 30 micrometers to about 3.5 millimeters. The
silicon carbide is especially resistant to corrosion and other chemical
reactions in the presence of slag. When silicon carbide is used in these
high quantities in the casting composition, the entire composition becomes
more resistant to attack from the slag layers in blast furnaces, troughs,
runners, and other molten metal containment devices.
The pumpable casting composition also includes, as an essential ingredient,
about 8-20% by weight of a binder which includes about 15-70% by weight
colloidal silica in water. The aqueous colloidal silica serves two
important functions. First, the aqueous colloidal silica provides the
casting composition with ideal flow properties that permit the casting
composition to be transported efficiently using a concrete pump or another
similar pump, from a source to the location of the refractory lining being
formed. Second, after the liner has been formed and dried, the colloidal
silica serves as an excellent binder for the casting composition,
providing strength and resistance to erosion during use.
The pumpable casting composition may include other refractory ingredients
as needed for the particular end use application. These other refractory
ingredients include, but are not limited to, about 0-10% by weight free
carbon, about 0-10% by weight pitch (which is a mixture of carbon and
organic volatiles), and about 0-50% by weight alumina.
An important characteristic of the casting composition is the ability to
transport the composition to a mold assembly using a standard concrete
pump or other similar pump. The casting composition of the invention may
either be used alone (i.e. to form an entire refractory liner) or may be
used in conjunction with a known casting composition. For example, a known
pumpable casting composition described in U.S. Pat. No. 5,147,830, the
disclosure of which is incorporated herein by reference, may be used to
line the lower portion of a molten metal containment device that is not
directly exposed to slag. Then, the casting composition of the invention
may be layered on top of the conventional casting composition, to line the
upper portion of the molten metal containment device which is directly
exposed to slag. Variations of this procedure may be employed depending on
the type of molten metal containment device being lined, and its size,
shape and contents.
With the foregoing in mind, it is a feature and advantage of the invention
to provide a pumpable casting composition that forms a refractory liner
which is especially resistant to attack from slag.
It is also a feature and advantage of the invention to provide a pumpable
casting composition which can be used alone or in addition to a
conventional casting composition when forming a refractory liner.
It is also a feature and advantage of the invention to provide a method of
forming a refractory liner that is especially resistant to attack from
slag.
The foregoing and other features and advantages of the invention will
become further apparent from the following detailed description of the
presently preferred embodiments, read in conjunction with the accompanying
example and drawing. The detailed description, examples and drawing are
merely illustrative rather than limiting, the scope of the invention being
defined by the appended claims and equivalents thereof.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a side sectional view of a blast furnace trough filled with
molten metal.
DETAILED DESCRIPTION OF THE PRESENTLY PREFERRED EMBODIMENTS
Referring to FIG. 1, a molten metal containment device 10, which is a blast
furnace trough, includes an outer steel shell 14, a conventional back-up
refractory lining 16, and an inner refractory lining 12. The inner
refractory lining 12 includes a lower layer 13 of a conventional pumpable
casting material and an upper layer 15 of the slag resistant pumpable
casting composition of the invention. This invention is directed to the
upper layer 15, the combination of the upper layer 15 with the lower layer
13, and, particularly to a method of forming these layers.
During operation, the molten metal containment device 10 is mostly filled
with molten metal 25. The impurities in the molten metal, which tend to be
lighter than the molten metal, rise to the top. As a result, the metal 25
in the trough becomes separated into a lower region 27 of purified molten
metal and an upper region 29 which is the slag layer filled with
impurities.
The slag ingredients attack conventional refractory lining materials based
primarily on alumina, requiring periodic replacement of exposed inner
linings. As explained above, the inner refractory lining 12 includes a
lower layer 13 of a conventional pumpable casting material and an upper
layer 15 of the slag-resistant pumpable refractory composition of the
invention.
The lower refractory layer 13 is exposed primarily to the generally pure
molten metal layer 27 and is not significantly exposed to the slag 29.
Hence, the lower refractory layer 13 experiences only normal wear and
tear, and can be formed from any of the conventional refractory
compositions including, for example, the pumpable compositions disclosed
in U.S. Pat. No. 5,147,830, the contents of which are incorporated herein
by reference. Generally, these conventional pumpable compositions include
about 55-90% by weight of a granular base material selected from calcined
clay, mullite, brown fused alumina, tabular alumina and mixtures thereof;
about 8-14% by weight of a silica binder formed from a dispersion of about
15-70% by weight colloidal silica in water; optionally, about 5-20% by
weight calcined alumina and/or 1-35% by weight silicon carbide; and,
preferably, about 0.02-1.0% by weight of a setting agent such as calcium
aluminate cement or magnesium oxide, and about 1-10% by weight
microsilica.
The lower refractory layer may be installed using a concrete pump or
another pump as described in U.S. Pat. No. 5,147,830. In order to
facilitate installation of the refractory layers 13 and 15, a mold or form
may be constructed or installed in the vessel at a predetermined distance
from the back-up refractory lining 16, and the refractory casting material
can be injected into the space between the back-up lining 16 and the
installed mold or form. A detailed description of a refractory lining
installation, using a mold or form, is provided in U.S. patent application
Ser. No. 08/156,163, filed on Nov. 22, 1993, the contents of which are
incorporated herein by reference.
After the lower refractory layer 13 has been formed, the layer should be
permitted to harden and set before the upper refractory layer 15 is
formed. This setting and hardening can be accomplished at room temperature
in about 15 minutes to about 5 hours, depending on the thickness of the
refractory layer 13. After the lower refractory layer 13 has sufficiently
hardened, the upper refractory layer 15 can be formed from the casting
composition of the invention, using the same pumping equipment and
procedure. The upper layer 15 should be large enough to cover the entire
region of the tundish vessel 10 which is exposed to the slag layer 29 on a
continuous or frequent basis.
After the upper refractory layer 15 has hardened or set for about 15
minutes to about five hours, the entire inner refractory lining 12 can be
further dried, if necessary, for up to about four more hours at room
temperature or at an elevated temperature not exceeding about 250.degree.
F. Then, the refractory lining 12 can be baked at a higher temperature
(above 250.degree. F.) for about 5-30 hours.
As stated above, the refractory lining 12, including the layers 13 and 15,
can be formed in situ in the metal containment device 10 using the
techniques described in U.S. application Ser. No. 08/156,163, filed on
Nov. 22, 1993. The refractory lining 12 can alternatively be formed apart
from the metal containment device using known techniques, and later
inserted into the metal containment device. If the inner refractory lining
12 is only partially exposed to slag on a regular basis, as is the case
with the through described above, then it is only necessary to use the
refractory composition of the invention in the regions of the inner liner
12 which are frequently exposed to slag. On the other hand, if most or all
of the lining 12 is to be exposed to slag, as may be the case with a slag
runner, for instance, then it is desirable to construct the refractory
lining entirely using the casting composition of the invention.
The pumpable casting composition of the invention includes about 36-92% by
weight silicon carbide, which causes the composition to have excellent
resistance to slag. Preferably, the casting composition includes about
40-85% by weight silicon carbide, most preferably about 45-80% by weight
silicon carbide. Higher amounts of silicon carbide generally contribute to
increased slag resistance. The silicon carbide is itself chemically
resistant to attack from slag ingredients, and also helps protect other
ingredients of the composition which would otherwise be less resistant The
silicon carbide should have an average particle diameter between about 30
micrometers and about 3.5 millimeters, in order to promote flow of the
composition during pumping and strength of the resulting lining. A wide
distribution of particle sizes facilitates flow and castability of the
composition.
The pumpable casting composition of the invention also includes about 8-20%
by weight of an aqueous colloidal silica binder, and preferably includes
about 8-14% by weight of this binder. The binder should include about
15-70% by weight colloidal silica in water, preferably about 30-50% by
weight colloidal silica in water, most preferably about 40% by weight
colloidal silica in water. The colloidal silica should have an average
silica particle diameter of about 4-100 millimicrons, preferably about
6-50 millimicrons, most preferably about 8-20 millimicrons.
The colloidal silica binder serves two important purposes. During pumping
of the casting composition, the aqueous colloidal silica imparts excellent
flow properties which permit the casting composition to be easily
transported from a source to a destination using a concrete pump or
another suitable pump. After the refractory lining has been formed and
dried, the colloidal silica acts as an excellent binder, thereby
contributing strength and erosion resistance to the refractory lining.
The pumpable casting composition of the invention may include about 0-50%
by weight of an alumina component, preferably about 10-40% by weight of
the alumina component. The presence of alumina as a minor component
improves the strength of the refractory liner without significantly
increasing the susceptibility of the liner to attack from slag
ingredients. The alumina component preferably has an average particle
diameter of about 30 micrometers to about 7 millimeters, and is preferably
selected from brown fused alumina, white fused alumina, tabular alumina,
and mixtures thereof.
The casting composition of the invention may also include about 1-10% by
weight microsilica having an average particle diameter of about 0.1-1.0
microns, preferably about 0.15-0.25 microns. The microsilica, whose
diameter is larger than that of colloidal silica, further improves the
flow of the casting composition during pumping.
The casting composition of the invention may also include about 5-20% by
weight calcined alumina having an average particle diameter of about
0.2-70 microns. The calcined alumina is believed to react with the
colloidal silica binder to form a sediment phase which causes further
improved binding characteristics, especially at higher temperatures.
The casting composition of the invention may also include about 0-10% by
weight free carbon, preferably about 2-6% free carbon, having an average
particle diameter of about 40 microns to about 0.5 mm. The carbon serves
as a nonwetting agent which further inhibits any chemical reaction between
slag and the refractory liner. In essence, the carbon helps prevent
attachment to or penetration of the refractory lining by slag. Typically,
the carbon is in the form of graphite or pitch, which is a mixture of
carbon and volatile organic compounds.
The casting composition of the invention preferably includes about
0.02-1.0% by weight of a setting agent. Examples of suitable setting
agents include calcium aluminate cement, magnesium oxide, and mixtures
thereof.
One example of a concrete pump which is suitable for use with the casting
composition of the invention is the Thom-Kat TVS16-2065, available from
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