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WO1997038140A1 - Refractory liner and lining method for a vertical shaft metallurgical vessel - Google Patents

Refractory liner and lining method for a vertical shaft metallurgical vessel Download PDF

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Publication number
WO1997038140A1
WO1997038140A1 PCT/US1997/005529 US9705529W WO9738140A1 WO 1997038140 A1 WO1997038140 A1 WO 1997038140A1 US 9705529 W US9705529 W US 9705529W WO 9738140 A1 WO9738140 A1 WO 9738140A1
Authority
WO
WIPO (PCT)
Prior art keywords
lining
shell
refractory
working lining
working
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/US1997/005529
Other languages
French (fr)
Inventor
Ronald G. Brenneman
Douglas K. Doza
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Allied Mineral Products LLC
Original Assignee
Allied Mineral Products LLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Allied Mineral Products LLC filed Critical Allied Mineral Products LLC
Priority to DE19780414T priority Critical patent/DE19780414T1/en
Publication of WO1997038140A1 publication Critical patent/WO1997038140A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21BMANUFACTURE OF IRON OR STEEL
    • C21B7/00Blast furnaces
    • C21B7/04Blast furnaces with special refractories
    • C21B7/06Linings for furnaces
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27BFURNACES, KILNS, OVENS OR RETORTS IN GENERAL; OPEN SINTERING OR LIKE APPARATUS
    • F27B1/00Shaft or like vertical or substantially vertical furnaces
    • F27B1/10Details, accessories or equipment specially adapted for furnaces of these types
    • F27B1/12Shells or casings; Supports therefor
    • F27B1/14Arrangements of linings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27DDETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D1/00Casings; Linings; Walls; Roofs
    • F27D1/16Making or repairing linings ; Increasing the durability of linings; Breaking away linings
    • CCHEMISTRY; METALLURGY
    • C21METALLURGY OF IRON
    • C21CPROCESSING OF PIG-IRON, e.g. REFINING, MANUFACTURE OF WROUGHT-IRON OR STEEL; TREATMENT IN MOLTEN STATE OF FERROUS ALLOYS
    • C21C1/00Refining of pig-iron; Cast iron
    • C21C1/10Making spheroidal graphite cast-iron
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27DDETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D1/00Casings; Linings; Walls; Roofs
    • F27D1/16Making or repairing linings ; Increasing the durability of linings; Breaking away linings
    • F27D1/1621Making linings by using shaped elements, e.g. bricks
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27FURNACES; KILNS; OVENS; RETORTS
    • F27DDETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D1/00Casings; Linings; Walls; Roofs
    • F27D1/16Making or repairing linings ; Increasing the durability of linings; Breaking away linings
    • F27D1/1626Making linings by compacting a refractory mass in the space defined by a backing mould or pattern and the furnace wall

Definitions

  • a hot blast cupola is a type of vertical cylindrical shaft furnace that normally is used
  • the primary source of energy for melting the scrap charge is
  • the liquid iron and slag at a temperature of about 2500 °F. to 2700 °F., flow out of the furnace through a tap hole.
  • Cupolas typically have a tap
  • lining layer preferably will surround as much of the working lining as is practical in all areas
  • the secondary liner also may be installed adjacent to only a portion
  • a sealing layer 46 (shown in FIG. 3) may be provided on the top of the dry-vibratable layer 42 on the bottom 34 of the shell to protect
  • the liner therefore may
  • the lining extends continuously from the hearth 32 through the transition area 40
  • a retainer 44 may be provided between a wall portion 54 of the
  • dry-vibratable layer 42 and the shell 38 to cover any surface venting perforations in the shell.
  • dry-vibratable secondary liner of the present invention may be used effectively in conjunction with other conventional and
  • the rammed lining may be installed over the

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Furnace Housings, Linings, Walls, And Ceilings (AREA)

Abstract

A liner (32) and lining method for a vertical shaft metallurgical vessel (30). The liner (32) includes a working lining (50) within the shell of the vessel (38) and a secondary lining (42) exhibiting fluid properties, such as a dry-vibratable refractory lining, between the shell (38) and a portion of the working lining (50). The lining method includes the steps of providing a working lining (50) within the shell (38) of the vessel (30) and providing a secondary fluid refractory lining (42) such as a dry-vibratable refractory lining between the shell (38) and a portion of the working lining (50). The secondary lining (42) provides as a barrier to any molten metal and slag that may penetrate through the working lining (50) and may assist in prolonging the operating life of the working lining (50).

Description

REFRACTORY LINER AND LINING METHOD FOR A VERTICAL SHAFT METALLURGICAL VESSEL
BACKGROUND AND SUMMARY OF THE INVENTION
This invention relates to a refractory liner and lining method for a vertical shaft metallurgical vessel, such as a hot blast cupola. The liner and lining method is advantageous
for many types of vertical shaft vessels, but offers special advantages for "dry-bottom"
cupolas and for the hearths (wells) of so-called "liningless" cupolas.
A hot blast cupola is a type of vertical cylindrical shaft furnace that normally is used
for the production of molten iron. The molten iron typically is used for making iron castings
in foundries; however, it also can be used in the production of steel. A cupola produces iron
by melting iron and steel scrap. The primary source of energy for melting the scrap charge is
supplied by the combustion of carbon (in the form of coke) with oxygen (from preheated pressurized air introduced into the furnace).
A cupola is a "counterflow" shaft furnace. The metallic scrap iron and coke fuel
normally are introduced from the top of the shaft and descend to the bottom. Meanwhile, the
preheated air ("hot blast") is introduced in the lower part of the shaft through a number of
nozzles (called "tuyeres") arranged around the periphery of the shaft. The combustion of the
hot blast with coke produces heat and gases that flow up the shaft, transferring heat to the
coke and metallic scrap. As the descending scrap approaches the combustion zone (at the melt and become liquid slag. The liquid iron and slag accumulate at the bottom of the shaft in
an area called the hearth or well. From here, the liquid iron and slag, at a temperature of about 2500 °F. to 2700 °F., flow out of the furnace through a tap hole. Cupolas typically have a tap
hole located in a side wall of the hearth for discharging the iron and slag from the hearth.
The iron and slag, in their liquid states, can be separated by flotation because of the
difference in their specific gravities. This separation takes place in a separator, siphon box or
other device constructed for this purpose. The separator may be connected to the cupola or
located apart from the cupola. After the iron has been separated from the slag, it is
transported to its end use through refractory-lined channels (called "launders") and transport
vessels (called "ladles"). The slag is cooled and disposed of or recycled for various uses.
To contain the heat, gases and molten metal and slag in a cupola and its associated
separators and to protect the structures of these units, specialized refractory materials in the
form of bricks, blocks, ramming masses, refractory plastics and refractory castables typically
are used, either alone or in combination with air and water cooling of the cupola structures.
The cupola hearth (i.e., the portion of the cupola below the tuyere level) typically has a
structural steel shell. (Unless otherwise specified, the term "hearth" includes any associated
slag separators, whether or not the separators are integral with the cupola, and the transition
areas between the hearth and the slag separators.) The shell is lined with a refractory to
maintain the steel shell below its maximum operating temperature limits and to contain the
molten metal and slag produced during the operation of the cupola. The refractory liner of the shell is a consumable material that is eroded or otherwise
damaged by exposure to the conditions within the cupola. When a certain amount of
consumption or damage to the liner has occurred, the operation of the cupola must be halted —
sometimes for an extended time ~ in order to repair or replace the refractory liner. The
frequency of these interruptions is determined by the consumption rate of the refractory liner
by the process. The duration of these interruptions is dependent on the consumption rate and
whether it is possible to repair localized damage to the liner without removing the undamaged
portions and replacing the entire liner.
Conventional refractory liners for cupola hearths typically consist of various
combinations of refractory bricks, blocks, and refractory specialty materials, such as
refractory plastics and refractory ramming mixes. These materials may have a relatively short
life (high consumption rate) and may require removal and replacement of the entire liner when
only a portion of the liner is eroded or damaged. This increases the cost of repair and greatly
increases downtime.
These materials also are prone to crack formation. Some cracks that form can extend
completely through the liner from the hot face (molten metal side) to the cold face (steel shell
side). When cracks of this nature occur during the operation of a cupola, the possibility of
molten metal and/or slag penetrating via these cracks to the cupola steel shell exists. When
this occurs, the molten materials can burn through the shell, resulting in the danger of
extensive damage to equipment and/or injury to personnel. A burn-through of this type can cause long, unscheduled delays in the operation to make repairs to the liner, steel shell and
structure, and any surrounding equipment.
Advances in refractory technology have produced new and improved refractory
materials that potentially offer advantages of longer life (lower consumption rate) and lower
operating and maintenance costs when compared to the prior liner designs. Foremost in these
technological advancements have been developments in refractory castable products. These
include low-moisture, low-cement, ultra-low cement, and no-cement castables. These
materials offer the potential for longer life and easier, faster, less expensive installations and
maintenance when compared to lining materials typically applied. For example, damaged
portions of castable liners generally can be repaired without removal and replacement of the
entire liner.
Unfortunately, castable refractories, like conventional lining materials, generally are
prone to crack formation. Some cracks that form in castable refractories can extend
completely through the cast body from the hot face to the cold face, resulting in the risk of
burn-through of the steel shell. Such lining failure may result in considerable damage and
production delays during repair of the damage. The tendency of castable refractories to form
cracks has been a major factor preventing widespread adaptation of technically advanced
castable refractories in cupola liners.
In view of the disadvantage of the prior art, a need exists for a cupola liner and lining
method that offers the advantages of a castable liner, has excellent resistance to crack
propagation and is easy to repair. This invention employs the unique characteristics of a refractory that exhibits fluid
properties, such as a dry-vibratable refractory. The fluid refractory is installed as a layer
surrounding all or part of a working lining of a cupola hearth, a slag separator, and/or the
transition area between them. This secondary lining layer reduces the risk of molten materials
contacting the shell of any of these units.
Dry-vibratable refractory is a preferred fluid refractory because it has excellent
resistance to crack propagation and is easy to repair. The characteristics of dry-vibratable
refractory enable it to form a barrier to any molten metal and slag that penetrates through the
working lining. As described further below, the characteristics of dry-vibratable material also
may contribute to extending the operating life of the working lining.
Dry-vibratable refractory exists in situ as an unbonded monolithic material. In this
unbonded state, it lacks the brittle behavior characteristic of formed refractories, and
therefore, tends not to form cracks or voids when subjected to external stresses under normal
operating conditions. The unbonded dry-vibratable material is able to absorb and distribute
local stresses without formation of cracks, as is typical with brittle refractories.
The chemical and mineralogical composition of dry-vibratable refractories can be
chosen to be resistant to the specific types and temperatures of metals and slags inherent to
each process, and can be designed to form strong ceramic bonds in predetermined temperature
ranges and at controlled rates of formation. When ceramic bonding of properly selected
dry-vibratable refractories occurs in this manner, the bonded portion of the material becomes 6 dense and hard. The bonded dry-vibratable material is chemically and physically resistant to
penetration of both molten metal and slag.
Meanwhile, the portion of the dry-vibratable layer that remains below the critical
temperature for the formation of ceramic bonding remains as an unbonded monolithic and
does not exhibit brittle behavior or cracking tendencies. In this manner, the bond formation is
progressive in nature and is influenced by time, temperature, and atmosphere.
The unbonded dry-vibratable material exhibits fluid properties. Thus, the dry-
vibratable material may protect the structural elements of the cupola from expansion of the
rigid refractory when it is heated and assist in isolating the rigid lining from mechanical
stresses. Dry-vibratable material also is relatively insulating compared to rigid refractories of the same mineralogical makeup. A dry-vibratable secondary lining insulates the working
lining, reducing the thermal gradient across the working lining. These properties of the dry-
vibratable lining may reduce stresses in the rigid, brittle working lining that may lead to
cracking or surface spalling. The reduction of these stresses may extend the operating life of
the working lining.
These and further objects of the invention will become apparent from the following
detailed description.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a cut-away partial side view of a dry-bottom, water-cooled cupola.
FIG. 2 is a sectional view of a slag separator of a dry-bottom cupola.
FIG. 3 is a side sectional view of the liner of the present invention installed in portions
of the hearth and slag separators of a dry-bottom cupola.
FIG. 4 is a top sectional view of the liner of FIG. 3.
FIG. 5 is a detail view of a portion of the liner of FIG. 4
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
The liner of the present invention is used in the shell of a vertical shaft metallurgical
vessel to contain the molten metal and slag produced during the operation of the vessel. The
liner includes a working lining within the shell of the vessel and a secondary fluid refractory
lining between the shell and the working lining. The secondary lining provides an additional
barrier to the passage of any molten metal and slag that penetrates through the working lining.
Preferably, the fluid refractory lining is a dry-vibratable refractory. However, the invention
also contemplates the use of other fluid refractory linings.
The invention will be described with particular reference to a hot blast cupola vertical
shaft furnace used for melting iron; however, it also may be used to advantage in other types
of vertical shaft vessels. FIG. 1 shows a dry-bottom, water-cooled cupola 10. The cupola
includes a vertical shaft 12 with a water-cooling system 14. Scrap iron and steel and coke fuel
are introduced into the top of the shaft through charge door 16. Preheated air ("hot blast") is introduced in the lower part of the shaft through tuyeres 18. In some cupolas, oxygen may
also be injected through the tuyeres. Plasma torches may be used to further increase cupola
operating capacities.
The cupola includes a hearth 20 at the bottom of the shaft 12, below the level of the
tuyeres 18. The hearth 20 has a refractory lining 22. The cupola of FIG. 1 may be referred to
as a "liningless" cupola because the refractory lining 22 does not extend above the tuyere
level. The molten iron and slag accumulate in the hearth 20 before flowing out of the furnace
through a tap hole 24, shown in FIG. 2. FIG. 2 shows a slag separator 26 attached to a dry-
bottom cupola. A transition area 28 separates the tap hole 24 from the separator 26.
The secondary liner may be provided in a new cupola (whether or not the cupola has been designed to accommodate a fluid secondary lining) or during the replacement or repair of
the working liner of an existing cupola. It may be installed as a layer between the shell and all
or part of the working lining of the hearth, the slag separator, and/or the transition area
between them. To maximize the benefit of this invention, the secondary (dry-vibratable)
lining layer preferably will surround as much of the working lining as is practical in all areas
below the maximum molten metal and slag pooling level, during all phases of operation. In
the case of a dry-bottom cupola, this includes the bottom and sides of the hearth (well), the
attached or adjacent separator(s), and the transition between the cupola hearth and the body of
the separators). However, the secondary liner also may be installed adjacent to only a portion
of the working liner of one or more of these units to protect the shell in an area where consumption of the working lining historically has been high or where such consumption is
predicted to be high.
FIG. 3 shows the liner of the present invention installed in a dry bottom, hot blast
cupola 30. The cupola 30 includes a hearth 32 having a bottom 34 and sides 36 defined by a
shell 38. Two slag separators 39 are attached to the hearth 32. A transition area 40 extends
between the hearth 32 and each of the slag separators. The dry-vibratable material 42 may be
installed in a portion of the bottom 34 of the hearth, a portion of the walls 36 of the furnace, or, as shown in FIG. 3, a portion of both the bottom 34 and the walls 36. The dry-vibratable
material is installed in the hearth bottom 34 using conventional techniques, such as those
recommended by the manufacturer of the dry-vibratable refractory.
Conventional installation techniques for dry-vibratable materials are not readily
adaptable to installation of the wall portions 42A of the dry-vibratable liner 42 in a hot blast
cupola of an existing design. Thus, a new installation method was required to install the dry-
vibratable secondary lining in the walls 36 of the hot blast cupola 30. This new method
includes the use of retainer 44 (best shown in FIGS. 4 and 5) to hold the dry-vibratable
material 42 in position adjacent to the shell wall 36 during installation of the dry-vibratable material. The retainers 44 are installed around the periphery of the steel shell 38 at a
predetermined distance from the shell wall 36 (including any liner components attached to the
shell). In a normally cylindrical cupola, such as the cupola 30 of FIG. 4, the retainers may
define an annular ring (or an arc thereof) within the cupola shell 38. The retainers 44 and the shell wall 36 define a void of the desired thickness of the dry-vibratable layer to be installed along the wall of the shell.
The retainers 44 may take the form of shapes, such as thin (typically about 1 lΛ -3
inches thick) flat or curved plates made from refractory castable. Retainers of other designs or
compositions, such as refractory bricks or blocks, also could be used, provided that they
perform the function of holding the dry-vibratable material in a desired position during
installation and their composition is compatible with the cupola lining. When precast shapes
are used, they are placed over the layer of dry-vibratable material or other liner material
installed over the bottom of the shell. A spacer or clip may be provided between the top of
the precast shape and the corresponding portion of the shell wall to assist in maintaining the
shape in a desired position relative to the shell wall.
After the retainers 44 are placed in position, a sealing layer 46 (shown in FIG. 3) may be provided on the top of the dry-vibratable layer 42 on the bottom 34 of the shell to protect
the dry-vibratable layer from mechanical damage and contamination during forming and
casting. The sealing layer 46 may be provided over the entire dry-vibratable bottom layer 42
or over selected portions of this layer. Preferably, the sealing layer is formed from a layer of
ramming or plastic refractory material. However, the sealing layer also may be formed by
other suitable methods, including, but not limited to, providing a layer of castable refractory
material, applying heat to the upper surface of the dry-vibratable layer, or spraying a sealing
liquid, such as sodium silicate, over the dry-vibratable layer. Typically, a sealing layer of
ramming material in a full-size cupola will in the range of about 1 -2 inches thick; however, 11 the thickness may vary with the cupola size and conditions and the material used to form the
sealing layer. Use of a layer of ramming refractory or similar material as the sealing layer is
preferred when retainer shapes are used because this material provides the further benefit of
assisting in securing the retainers in their proper positions during installation of the dry-
vibratable material along the shell wall.
When the retainers 44 have been installed and any sealing layer 46 has been provided,
the space formed between the retainers 44 and the shell wall 36 is filled with dry-vibratable refractory 42A using conventional installation methods for such spaces. When the installation
of the dry-vibratable material in this space is complete, the top of the dry-vibratable wall
material 42A may be covered with a layer of a compatible refractory material 48, such as
ramming material, to seal the dry-vibratable layer and protect it from damage during
installation of the remainder of the liner.
The steel shell 38 of the cupola may include perforations (not shown in the drawings)
spaced at intervals over the bottom and walls to allow water and gases in the lining materials
to escape when these materials are dried and heated. These perforations typically are large
enough to allow dry-vibratable refractory to pass through them. The liner therefore may
include a heat-resistant, moisture permeable web 49 (shown in FIG. 5) between the shell, or at
least the perforated portions of the shell, and the dry-vibratable layer. The web 49 confines
the dry-vibratable refractory within the shell while allowing moisture to escape through the
perforations when the lining materials are heated. The web preferably is a woven high-
temperature fabric made from a spun refractory fabric, although other materials with similar properties also may be used.
When the secondary liner 42 has been installed, the installation of the remainder of the
cupola liner (referred to as the "working lining") may proceed. In the liner of the present
invention, the working lining 50 is spaced at a distance from the shell 38, and extends over the
bottom 34 and at least a portion of the walls 36 of the shell 38. Preferably, the working lining
50 is a castable refractory. However, other materials, such a carbon block or ramming
refractory, also could be used to form all or part of the working lining.
Similarly, the liner of the present invention may be installed in a bottom or wall portion of a slag separator 39, or the bottom or wall portion of the transition area 40.
Preferably, the lining extends continuously from the hearth 32 through the transition area 40
to the slag separator 39. However, the lining also may be installed separately in any one or
more of these units.
The method of lining the cupola shell 38 includes the steps of:
A. Providing a working lining 50 within the shell 38 that extends over the bottom 34 and
at least a portion of the walls 36 of the shell; and
B. Providing a secondary lining 42 between the shell 38 and a portion of the working
lining 50.
As noted above, the working lining 50 preferably is a castable refractory, although other
lining materials also may be used. The secondary lining 42 is a refractory exhibiting fluid
properties, and preferably a dry-vibratable refractory. The lining method also may include one or more additional steps. A sealing layer 46,
formed from a layer of ramming material or by another suitable method, may be provided
between the bottom portion 52 of the working lining 50 and the corresponding portion 42B of
the secondary lining to prevent damage to the dry-vibratable refractory during installation of
the working lining 50. A retainer 44 may be provided between a wall portion 54 of the
working lining 50 and the corresponding portion 42A of the secondary lining. A sealing layer
46 comprising a ramming refractory may assist in maintaining the retainers 44 in position.
In addition, a heat-resistant, moisture-permeable web 49 may be provided between the
dry-vibratable layer 42 and the shell 38 to cover any surface venting perforations in the shell.
The surface venting holes may be plugged after the liner is completely dried.
When castable refractory concrete is installed in a hot blast cupola or separator as the
working lining by casting, a forming system must be employed in order to establish the final
configuration of the inside of the cupola or separator lining and to confine the castable
material to its finished shape during the curing period or until it becomes sufficiently strong to
be self-supporting. The forming system must be of sufficient strength to resist the pressure
and buoyant force of the refractory concrete mass in a fluid state and must be constructed so
as to be removable without disturbing the structural integrity of the solidified monolithic
refractory mass. If the secondary lining is installed before the working lining, it may assist in shaping the exterior of the cast lining. The installation procedure for a castable refractory concrete lining consists of: (1)
forming, (2) casting (pouring), (3) curing, (4) form removal, and (5) drying and heating to
operating temperature. Each of these steps is discussed in more detail below.
Forming of the inside cavity of the cupola hearth and the separators can be done as described above using rigid materials such as steel, wood, or plastic or metal mesh.
Casting includes mixing the castable in a mechanical mixer with water or other liquids
and other ingredients to fluidize the material for installation purposes and activate the bonding
mechanism. When the castable refractory has been mixed for the prescribed amount of time or has reached the preferred consistency, it is poured, or pumped or otherwise transported to
the cupola and installed into the formed cavities. Many castable refractories tend to be
thixotropic, therefore, they may require vibration during installation in order to flow properly
or to consolidate into a monolithic mass of the highest possible density.
After the material has been cast into the formed cavity, a curing period normally is
required. During this period, the castable refractory mixture solidifies into a solid, monolithic
mass as the result of chemical reactions between the mixed ingredients. During the time
required for curing, the castable normally must be left undisturbed and maintained within a
prescribed temperature range. During the curing period, the castable refractory increases in
strength as a result of the desired chemical bonding reactions. The curing period is complete
when these reactions have proceed to completion or the castable has acquired sufficient strength to be self-supporting (referred to as "green strength"). When the curing period has been completed, the forms may be removed. In some
cases, forms or parts of forms of specific designs may be left in place to become a part of the
lining structure or to be consumed in due course during the operation of the cupola.
Before starting and operating the cupola, the lining normally is dried by applying heat
either directly or indirectly in a controlled manner to the refractory lining. The purpose of this
drying procedure is to remove water or other liquids that remain in the lining. The result of
not properly drying the materials can be the uncontrolled generation of a large volume of
steam or other gasses during either the heat-up to the operating temperature or operation of the
cupola. In extreme cases, the steam or gases generated can create sufficient pressure to cause
disruption of the lining (steam spalling) or explosion of gases that can accumulate as a result of various chemical reactions taking place in the lining.
After drying, the temperature of the lining may be increased gradually toward the
operating temperature. During the drying and heat-up period, many desirable and
consequential chemical and physical reactions may take place in the lining, and the increasing
temperature of the lining may accelerate these reactions. These reactions usually include the
expansion of the lining, which must be accommodated in the lining design. The result of not
properly allowing for expansion in the design can be catastrophic failure of the lining
components or the cupola structure. When drying and heat-up are completed, the lining is ready for the cupola start-up procedure to begin.
In some cases, the castable refractory may be installed using formless installation
techniques, such as gunite or shotcrete installation techniques. Such installation method avoid the need for interior forms during installation of the working lining walls, resulting in
significant time and cost savings. Use of formless installation techniques is particularly
advantageous during repairs to minimize downtime; however, they may be used in new installations as well. As with casting installation techniques, the secondary lining may be
used to assist in shaping the exterior of a castable lining installed using formless techniques.
In some instances, the use of a refractory castable working lining described above is
not possible or practical. In these instances, the dry-vibratable secondary liner of the present invention may be used effectively in conjunction with other conventional and
nonconventional working linings. Some of these alternatives are described below.
The working lining may be formed from cupola lining blocks or bricks. When these
materials are used, the dry-vibratable bottom layer is installed and compacted (vibrated) using
conventional methods. The cupola blocks or bricks are installed at a predetermined distance
from the cupola shell. Dry-vibratable refractory is then installed in the annular space behind
the blocks or bricks. Precast retainer shapes are not required to maintain the dry-vibratable
material in position along the sides of the shell.
The working lining also may be formed from ramming or plastic refractory material.
For these types of working linings, the dry-vibratable lining may be installed as described for
the castable working lining using precast retainer shapes to maintain the dry-vibratable
material in position along the sides of the shell. The rammed lining may be installed over the
dry-vibratable lining with or without the use of a ramming form. The design of the present invention, including selection of particular materials for the
working lining and the secondary lining and their respective thicknesses, is made using
conventional thermal analysis and liner design techniques. Among the factors considered in
designing a liner for a particular operating conditions are (1) the boundary conditions relating
to the dimensions of the shell and the desired capacity of the molten metal pool, (2) the
identity and physical properties of the metal, and (3) the expected operating environment of
the vessel, including its rated capacity and the presence of features such as oxygen injection,
plasma torches, and water or air cooling devices. A thermal profile of the vessel is developed
based upon these factors. Materials are selected based on this profile and desired operating
conditions (including, but not limited to, campaign time, ease of repair and material costs.)
Generally, materials are selected for the working lining and the secondary lining such that the
temperature at the interface of these structures is below the freezing temperature of the metal
to be process in the vessel, and the temperature at the interface of the secondary lining and the
shell is low enough to maintain the structural integrity of the shell.
In particular, the dry-vibratable material is selected based upon the thermal
environment of the furnace and the chemical and metallurgical reactions to be carried out in
the furnace. The dry-vibratable materials must be resistant to the temperatures and types of
metal(s) and slag(s) inherent to the metallurgical process. For example, the dry-vibratable
material in a hot blast cupola used for melting iron must be capable of withstanding
temperatures of about 2500 to 3000 °F. or more, under pressure, in a reducing atmosphere. The dry-vibratable material is selected with an appropriate sintering temperature range that will allow the formation of strong ceramic bonds in the region adjacent to the
working lining as a result of exposure to the operating conditions expected in this region.
The bonded dry-vibratable material will be dense and hard. It also will be chemically and
physically resistant to penetration of both molten metal and slag. The dry-vibratable material
outside this region, which generally is exposed to less severe operating conditions, will
remain in its unbonded state. The unbonded dry-vibratable material is able to absorb and
distribute local stresses without formation of cracks. However, the unbonded dry-vibratable
material remains capable of forming strong ceramic bonds in those areas where it may be
exposed to more severe operating conditions, for example, if molten metal or slag penetrates through the working lining and the bonded dry-vibratable material.
A liner of the present invention has been installed and tested in a dry bottom hot blast
cupola in an integrated steel manufacturing plant. This steelmaking operation required a
uninterrupted high volume supply of basic pig iron having consistent temperature and
chemistry over an extended operating period. At full production, the cupola was expected to
have a capacity in the range of about 100-150 tons of iron per hour or about 3000-3500 tons
per operating day. The desired campaign time (without requiring shutdown of the cupola to
repair or replace the hearth lining) was about 26 weeks or more, and preferably about 52
weeks or more.
The cupola designed for this plant contemplated the use of a conventional ramming
refractory liner. It soon became clear, however, that a conventional rammed liner would be consumed too quickly under the expected operating conditions (probably in about nine to
twelve weeks) and thus the cupola would not be capable of achieving the campaign time
desired. Although it was recognized that use of a castable refractory liner, and particularly an
ultra- low cement castable liner, might provide a longer operating life than noncastable
refractories such as ramming material and would also allow localized repair to be made to worn, contaminated or damaged portions of the lining, the brittle character of castable
refractory liners discouraged consideration of such a liner, particularly in view of the metal
burden and the stringent operating conditions.
The liner of the present invention provided a fluid refractory secondary lining in
combination with a rigid castable working lining. The resultant liner provides excellent
resistance to crack propagation and is easy to repair. The fluid secondary lining protects the
structural elements of the cupola from expansion of the rigid refractory. It also insulates the working lining, reducing the thermal gradient across the working lining. These features may
contribute to extending the operating life of the working lining.
Novel methods of installing the liner of the invention, described above, were
developed to allow installation of the dry-vibratable layer between the walls of the working
lining and the shell and to allow use of this liner in a shell that was designed for conventional
ramming and plastic refractories. A novel method also was developed to accommodate the
provision of large radial venting channels through the sides of the secondary lining and into
the bottom of the working lining to allow moisture, steam and other gases present in the working lining to escape during dryout and heatup. The venting channels were provided by installing stainless steel sleeves radially
through the openings in the sides of the shell, across the annular space defined by the shell
and the retainers, and through the retainers. The dry-vibratable material was installed in the
annular space after the sleeves were in position. Solid steel rods were then inserted through
the sleeves, extending into the center of the castable lining bottom. After the castable lining
was installed and cured, the solid rods were removed, leaving radial voids in the bottom of the castable lining. These voids allow moisture, steam and other gases present in the castable
lining to escape during dryout and heatup. The stainless steel sleeves remained in the side
walls of the secondary lining after the rods were removed to isolate the dry-vibratable material
from the venting channels and prevent it from leaking out of the openings in the shell. After drying, the channels were filled with refractory material. This helps to exclude air from the
lining and may reduce the oxidation of certain components of the refractory lining.
Although a specific embodiment of the invention has been described herein in detail, it
is understood that variations may be made thereto by those skilled in the art without departing
from the spirit of the invention or the scope of the appended claims.

Claims

What is Claimed Is:
1. A liner for the shell of a vertical shaft metallurgical vessel, comprising:
a working lining within the shell; and
a secondary lining inteφosed between the shell and a portion of the working lining,
said secondary lining comprising a refractory exhibiting fluid properties.
2. The liner according to Claim 1, wherein said fluid refractory comprises a dry- vibratable refractory.
3. The liner according to Claim 1 , wherein said secondary lining extends over a
portion of the bottom of the shell.
4. The liner according to Claim 3, wherein said secondary lining further extends
over a portion of a wall of the shell.
5. The liner according to Claim 1, wherein said secondary lining extends over a portion of a wall of the shell.
6. The liner according to Claim 3, further comprising: a sealing layer inteφosed between a bottom portion of the secondary lining and a
corresponding portion of the working lining.
7. The liner according to Claim 5, further comprising:
a retainer inteφosed between a wall portion of the secondary lining and a
corresponding portion of the working lining.
8. The liner according to Claim 1, further comprising:
a web inteφosed between the shell and a portion of the secondary lining.
9. The liner according to Claim 1 , wherein said working lining comprises a
castable refractory.
10. The liner according to Claim 1 , wherein said working lining comprises
refractory blocks.
11. The liner according to Claim 1 , wherein said working lining comprises refractory bricks.
12. The liner according to Claim 1 , wherein said working lining comprises plastic
refractory.
13. The liner according to Claim 1, wherein said working lining comprises
ramming refractory.
14. A liner for the shell of a vertical shaft metallurgical vessel, comprising: a rigid refractory working lining within the shell; and
a secondary refractory lining inteφosed between the shell and a portion of the working lining, a portion of said secondary lining exhibiting fluid properties.
15. The liner according to Claim 14, wherein said secondary lining accommodates
expansion of said rigid working lining during heating of the rigid lining.
16. A liner for the shell of a vertical shaft metallurgical vessel, comprising: a working lining within the shell, said working lining extending over the bottom and a
portion of a wall of the shell;
a secondary lining inteφosed between the shell and a portion of the working lining,
said secondary lining comprising a refractory exhibiting fluid properties; a sealing layer inteφosed between a bottom portion of the secondary lining and a
corresponding portion of the working lining; and
a web inteφosed between the shell and a portion of the secondary lining.
17. The liner according to Claim 16, further comprising: a retainer inteφosed between a wall portion of the working lining and a corresponding
portion of the secondary lining.
18. The liner according to Claim 17, further comprising:
a coating layer covering the upper surface of the secondary lining located between the
retainer and a wall portion of the shell.
19. A liner for the shell of a hot blast cupola, comprising:
a working lining within the shell; and
a secondary lining inteφosed between the shell and a portion of the working lining, said secondary lining comprising a refractory exhibiting fluid properties.
20. The liner according to Claim 19, wherein said fluid refractory comprises a dry-
vibratable refractory.
21. A liner for the shell of hot blast cupola, comprising:
a working lining within the shell, said working lining extending over the bottom and a
portion of a wall of the shell;
a secondary lining interposed between the shell and a portion of the working lining,
said secondary lining comprising a refractory exhibiting fluid properties; a sealing layer inteφosed between a bottom portion of the secondary lining and a
corresponding portion of the working lining; and a web inteφosed between the shell and a portion of the secondary lining.
22. The liner according to Claim 21 , further comprising:
a retainer inteφosed between a wall portion of the working lining and a corresponding
portion of the secondary lining.
23. A liner for the slag separator of a vertical shaft metallurgical vessel,
comprising:
a working lining within the slag separator, said working lining extending over a
portion of an inner surface of the slag separator; and
a secondary lining inteφosed between the shell and a portion of the working lining,
said secondary lining comprising a refractory exhibiting fluid properties.
24. A liner for the transition area between the hearth and a slag separator of a vertical shaft metallurgical vessel, comprising:
a working lining within the transition area, said working lining extending over a
portion of an inner surface of the transition area; and
a secondary lining inteφosed between the shell and a portion of the working lining,
said secondary lining comprising a refractory exhibiting fluid properties.
25. A liner for a vertical shaft metallurgical vessel having a shell, said shell
including a hearth and an integral slag separator, said liner comprising:
a working lining, said working lining continuously extending over a portion of the hearth and a portion of the integral slag separator; and
a secondary lining inteφosed between the shell and a portion of the working lining,
said secondary lining comprising a refractory exhibiting fluid properties.
26. The liner according to Claim 25, wherein said secondary liner extends
continuously over a portion of the hearth and a portion of the integral slag separator.
27. A method for lining a vertical shaft metallurgical vessel having a shell, said
method comprising the steps of:
providing a working lining within the shell; and
providing a secondary lining between the shell and a portion of the working lining,
said secondary lining comprising a refractory exhibiting fluid properties.
28. The method according to Claim 27, wherein the step of providing a secondary
lining further comprises the step of:
installing a dry-vibratable refractory.
29. The method according to Claim 27, wherein the step of providing a secondary
lining further comprises the step of:
installing the secondary lining over a portion of the bottom of the shell.
30. The method according to Claim 27, wherein the step of providing a secondary lining further comprises the step of:
installing the secondary lining adjacent to a portion of a wall of the shell.
31. The method according to Claim 30, further comprising the step of:
providing a retainer between the secondary lining adjacent to a portion of a wall of the
shell and a corresponding portion of the working lining.
32. The method according to Claim 29, further comprising the step of:
providing a sealing layer between a bottom portion of the secondary lining and a
corresponding portion of the working lining.
33. The method according to Claim 27, further comprising the step of:
providing a web between the shell and a portion of the secondary lining.
34. The method according to Claim 27, wherein the step of providing a working lining further comprises the step of: selecting a refractory lining material from among: castable refractory, refractory
bricks, refractory blocks, ramming refractory, and plastic refractory.
35. The method according to Claim 34, wherein the step of providing a working lining further comprises the step of:
installing a castable refractory using forms.
36. The method according to Claim 34, wherein the step of providing a working
lining further comprises the step of:
installing a castable refractory using a formless method.
37. The method according to Claim 27, wherein the step of providing a secondary
lining further comprises the step of:
providing a structure that assists in shaping of the working lining.
38. A method for lining a hot blast cupola, comprising the steps of:
providing a working lining within the shell of the cupola; and
providing a secondary lining between the shell and a portion of the working lining,
said secondary lining comprising a refractory exhibiting fluid properties.
39. The method according to Claim 38, wherein the step of providing a secondary
lining further comprises the step of:
installing a dry-vibratable refractory.
40. A method for lining a vertical shaft metallurgical vessel having a shell, said
method comprising the steps of:
providing a working lining within the shell, said working lining extending over the bottom and at least a portion of the walls of the shell;
providing a secondary lining between the shell and a portion of the working lining,
said secondary lining comprising a refractory exhibiting fluid properties; and providing a sealing layer between a portion of secondary lining and a corresponding
portion of the working lining.
41. The method according to Claim 40, further comprising the steps of: installing the secondary lining adjacent to a portion of a wall of the shell; and
providing a retainer between a wall portion of the secondary lining and a
corresponding portion of the working lining.
42. The method according to Claim 40, further comprising the step of:
providing a web between the shell and a portion of the secondary lining.
PCT/US1997/005529 1996-04-04 1997-04-04 Refractory liner and lining method for a vertical shaft metallurgical vessel Ceased WO1997038140A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19780414T DE19780414T1 (en) 1996-04-04 1997-04-04 Refractory lining and lining method for a vertical shaft metallurgical container

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US62628696A 1996-04-04 1996-04-04
US08/626,286 1996-04-04

Publications (1)

Publication Number Publication Date
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MX (1) MX9709437A (en)
WO (1) WO1997038140A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150136001A1 (en) * 2013-11-15 2015-05-21 Allied Mineral Products, Inc. High temperature reactor refractory systems
CN113446860A (en) * 2021-06-07 2021-09-28 山西太钢不锈钢股份有限公司 Method for repairing plastic material of side wall of stepping heating furnace

Citations (5)

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Publication number Priority date Publication date Assignee Title
US397376A (en) * 1889-02-05 Device for protecting furnaces or like structures
US2423898A (en) * 1944-02-18 1947-07-15 Carnegie Illinois Steel Corp Refractory bottom for metallurgical furnaces
US2912740A (en) * 1958-04-09 1959-11-17 United States Steel Corp Method of retarding disintegration of blast-furnace lining
US3202486A (en) * 1961-12-21 1965-08-24 Shell Oil Co Reaction vessel with refractory lining
US4157815A (en) * 1978-04-28 1979-06-12 Inland Steel Company Furnace bottom construction with seal

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US397376A (en) * 1889-02-05 Device for protecting furnaces or like structures
US2423898A (en) * 1944-02-18 1947-07-15 Carnegie Illinois Steel Corp Refractory bottom for metallurgical furnaces
US2912740A (en) * 1958-04-09 1959-11-17 United States Steel Corp Method of retarding disintegration of blast-furnace lining
US3202486A (en) * 1961-12-21 1965-08-24 Shell Oil Co Reaction vessel with refractory lining
US4157815A (en) * 1978-04-28 1979-06-12 Inland Steel Company Furnace bottom construction with seal

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20150136001A1 (en) * 2013-11-15 2015-05-21 Allied Mineral Products, Inc. High temperature reactor refractory systems
US10190823B2 (en) * 2013-11-15 2019-01-29 Allied Mineral Products, Inc. High temperature reactor refractory systems
CN113446860A (en) * 2021-06-07 2021-09-28 山西太钢不锈钢股份有限公司 Method for repairing plastic material of side wall of stepping heating furnace

Also Published As

Publication number Publication date
DE19780414T1 (en) 1998-06-18
MX9709437A (en) 1998-06-28

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