US2985442A - Refractory lining - Google Patents
Refractory lining Download PDFInfo
- Publication number
- US2985442A US2985442A US733445A US73344558A US2985442A US 2985442 A US2985442 A US 2985442A US 733445 A US733445 A US 733445A US 73344558 A US73344558 A US 73344558A US 2985442 A US2985442 A US 2985442A
- Authority
- US
- United States
- Prior art keywords
- lining
- permanent
- working
- magnesite
- furnace
- 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.)
- Expired - Lifetime
Links
- 239000011449 brick Substances 0.000 description 16
- 239000001095 magnesium carbonate Substances 0.000 description 15
- ZLNQQNXFFQJAID-UHFFFAOYSA-L magnesium carbonate Chemical compound [Mg+2].[O-]C([O-])=O ZLNQQNXFFQJAID-UHFFFAOYSA-L 0.000 description 15
- 229910000021 magnesium carbonate Inorganic materials 0.000 description 15
- 235000014380 magnesium carbonate Nutrition 0.000 description 15
- 239000000463 material Substances 0.000 description 10
- 238000006243 chemical reaction Methods 0.000 description 5
- 150000001875 compounds Chemical class 0.000 description 4
- 230000007935 neutral effect Effects 0.000 description 4
- BVKZGUZCCUSVTD-UHFFFAOYSA-L Carbonate Chemical compound [O-]C([O-])=O BVKZGUZCCUSVTD-UHFFFAOYSA-L 0.000 description 3
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- 229910052500 inorganic mineral Inorganic materials 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 235000010755 mineral Nutrition 0.000 description 2
- 239000011707 mineral Substances 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 239000011819 refractory material Substances 0.000 description 2
- 230000008646 thermal stress Effects 0.000 description 2
- 239000002253 acid Substances 0.000 description 1
- 230000002378 acidificating effect Effects 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- -1 for example Chemical compound 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 239000000395 magnesium oxide Substances 0.000 description 1
- CPLXHLVBOLITMK-UHFFFAOYSA-N magnesium oxide Inorganic materials [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 description 1
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 230000008439 repair process Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
Images
Classifications
-
- 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
- F27D1/0023—Linings or walls comprising expansion joints or means to restrain expansion due to thermic flows
-
- 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
Definitions
- the refractory lining structure of shaft furnaces comprises generally a so-called permanent lining next to the shell of the furnace, and a working lining, which is directly exposed to the burning material and to the furnace atmosphere.
- the usual lining is constructed of magnesite quality in the zone which is subjected to the greatest thermal stresses and partly also to the lgreatest mechanical stresses whereas the permanent lining consists of suitable fireclay.
- an annular gap filled with combustible materials such as cardboard or a space about 70-100 mm. wide and filled with ground iireclay is provided between the basic working lining and the permanent lining of iireclay.
- the two linings that is the working and the permanent linings, which are more or less directly in contact with each other just in the region of highest thermal stress consist of materials which give rise to chemical reactions at certain temperatures, whereby the adjoining layers of the lining may be destroyed.
- These reactions termed contact reactions, occur between two different solid materials, which are unable to react with one another at room or even slightly elevated temperatures, when their temperature is raised to a very high value.
- the resulting reaction forms a low melting flux.
- a basic material such as magnesium oxide and an acidic oxide such as alumina can and do often so react when heated to about l500 C.
- the heat-lagging layer consists also of shaped bodies, which suitably form compound blocks with the shaped bodies of the permanent lining lying before them.
- the accompanying drawing shows a sectional view of the entire lining for a portion of the furnace to show the several parts of the lining structure of a shaft furnace.
- 1 is the working lining, which. consists of basic or neutral bricks, e.g. magnesite bricks, and which is adjoined on the side facing the shell 6 of the furnace by an expansion joint 2 for compensating the thermal expansion of the refractory material.
- This joint is filled with combustible material when the lining is being prepared.
- 3 is the permanent lining, in which basic or neutral material, as in the working lining, is used according to the invention.
- the permanent lining '3 is adjoined by the heat-lagging layer 4 of high-grade insulating material.
- the drawing shows the permanent lining 3 and the heat-lagging layer 4 combined in the lform of compound blocks.
- An additional thin insulating layer 5, e.g. of Fibrosilex, is used in most cases-between the sheet metal shell 6 on the one hand, and the permanent lining 3 and the insulating layer 4, on the other hand,
- Example 1 (a) Working lining (1), 230 mm., of magnesite brick.
- Heat lagging layer (4), 125 mm., of porous bricks obtained, for example, according to the Austrian Patent No. 175,535.
- the porous brick is formed by mixing a raw carbonate, for example, magnesite, with the heat-resisting material before the mass is fired.
- the carbonate upon heating loses carbon dioxide which is entrapped and lends porosity to the resulting brick.
- a carbonate is chosen which when heated will yield an oxide of high refractoriness.
- the heat-lagging layer (4) is preferably porous sintered magnesite.
- a refractory lining structure which comprises a working lining of magnesite bricks, a permanent lining of chromite bricks spaced from said working lining, and la heatlagging layer of non-acid shaped bodies' adjacent the side of said permanent lining which is remote from said working lining.
- a refractory lining structure which comprises a working lining of magnesite bricks, a permanent lining of chromite ,4 bricks spaced from s-aid working lining, and a heatlagging layer of porous maguesite bricks adjacent the side of said permanent lining which is remote from said working lining.
- a refractory lining *structurel which comprises a working lining of magnesite bricks, a permanent liningv of chromite bricks ⁇ spaced from said working lining, and a hat-lagging layer of porous magnesite bricks adjacent the side of said permanent lining which is remote' from said working lining, said permanent lining and heat-lagging layer being inthe form of a compound brick.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Furnace Housings, Linings, Walls, And Ceilings (AREA)
Description
A2,985,4 42 Patented May 23, 1961 United States Patent ce 2,985,442 REFRACTORY LINING Helmut Hlber, Vienna, Austria, assignor to Veitscher Magnesitwerke Adieu-Gesellschaft, Vienna, Austria, a corporation of Austria Filed May '6, 1958, Ser. No. 733,445 'Claims priority, application Austria May 11, 1957 3 Claims. (Cl. 26d-'43) This invention relates to a refractory lining structure as is used particularly in the combustion zone of shaft furnaces.
The refractory lining structure of shaft furnaces comprises generally a so-called permanent lining next to the shell of the furnace, and a working lining, which is directly exposed to the burning material and to the furnace atmosphere. The usual lining is constructed of magnesite quality in the zone which is subjected to the greatest thermal stresses and partly also to the lgreatest mechanical stresses whereas the permanent lining consists of suitable fireclay. To compensate the thermal expansion of the refractory bricks an annular gap filled with combustible materials such as cardboard or a space about 70-100 mm. wide and filled with ground iireclay is provided between the basic working lining and the permanent lining of iireclay.
In such a lining structure, the two linings, that is the working and the permanent linings, which are more or less directly in contact with each other just in the region of highest thermal stress consist of materials which give rise to chemical reactions at certain temperatures, whereby the adjoining layers of the lining may be destroyed. These reactions, termed contact reactions, occur between two different solid materials, which are unable to react with one another at room or even slightly elevated temperatures, when their temperature is raised to a very high value. The resulting reaction forms a low melting flux. For example, a basic material such as magnesium oxide and an acidic oxide such as alumina can and do often so react when heated to about l500 C. These contact reactions are particularly dangerous when a further period of operation Iis begun after the working lining of magnesite has been consumed to a considerable extent, when lateral fires occur in the case of au irregular furnace operation or when the furnace must be overloaded at times. In these cases, the magnesite working lining vw'll break down and the furnace must be shut down for repairs or relining; this involves a considerable loss of production. According to the invention these disadvantages are eliminated in that the permanent lining, which is spaced from the working lining only by the width of the expansion joint, consists also of basic or neutral shaped bodies and an additional heat-lagging layer is provided on the cold side. This measure enables the utilization of the Working lining except for smallest residual thicknesses and a much increased safety of operation even when the working lining has been considerably consumed and the period of operation is to be prolonged. Another advantage of the invention is to be seen in that furnaces for intermittent operation, as are used, e.g. in the sugar industry, may be provided with working linings of lower thickness than was previously usual because the 'danger of breakdowns is practically eliminated. Another highly advantageous and important improvement afforded by the invention resides in that the heat-lagging layer consists also of shaped bodies, which suitably form compound blocks with the shaped bodies of the permanent lining lying before them. By making the permanent lining of compound blocks, consisting of an insulating layer and a basic or neutral layer, a substantial simplification of the lining operation is achieved, whereby the time required for the lining operation is reduced.
The accompanying drawing shows a sectional view of the entire lining for a portion of the furnace to show the several parts of the lining structure of a shaft furnace.
In the drawing, 1 is the working lining, which. consists of basic or neutral bricks, e.g. magnesite bricks, and which is adjoined on the side facing the shell 6 of the furnace by an expansion joint 2 for compensating the thermal expansion of the refractory material. This joint is filled with combustible material when the lining is being prepared. 3 is the permanent lining, in which basic or neutral material, as in the working lining, is used according to the invention. The permanent lining '3 is adjoined by the heat-lagging layer 4 of high-grade insulating material. The drawing shows the permanent lining 3 and the heat-lagging layer 4 combined in the lform of compound blocks. An additional thin insulating layer 5, e.g. of Fibrosilex, is used in most cases-between the sheet metal shell 6 on the one hand, and the permanent lining 3 and the insulating layer 4, on the other hand,
'Ihe arrangement according to the invention enables the operation of the furnace until the working lining has been worked down to smallest thicknesses, even While Va portion of the permanent lining is directly exposed to the heat of the furnace, without endangering the safety of operation of the furnace. When a part of the permanent lining has been worn for certain reasons during the furnace campaign, this can be simply repaired with the aid of refractory materials when the Working lining is renewed whereas the former arrangement of permanent and working linings is retained.
Example 1 (a) Working lining (1), 230 mm., of magnesite brick.
(b) Air gap (2),` l0 mm., to take up the thermal expansion.
(c) Permanent lining (3), 125 mm., of chromite brick.
(d) Heat lagging layer (4), 125 mm., of porous bricks obtained, for example, according to the Austrian Patent No. 175,535. In that patent the porous brick is formed by mixing a raw carbonate, for example, magnesite, with the heat-resisting material before the mass is fired. The carbonate upon heating loses carbon dioxide which is entrapped and lends porosity to the resulting brick. A carbonate is chosen which when heated will yield an oxide of high refractoriness. The heat-lagging layer (4) is preferably porous sintered magnesite.
(e) Additional heatlagging layer between sheet metal shell and (4); this layer consists of a fill of ground tireclay.
Example 2 Particle Propor- Size, mm. tio
Component n,
percent Chromite Sintged magnesite n Fne1y-ground sintered magnesite Proi-V portion, V Percent Particle Size, mm.
Component dammi Dn Sintered magnesite Finely-ground sintered magnesite What is claimed is:
1. In a shaft furnace for burning mineral material, a refractory lining structure which comprises a working lining of magnesite bricks, a permanent lining of chromite bricks spaced from said working lining, and la heatlagging layer of non-acid shaped bodies' adjacent the side of said permanent lining which is remote from said working lining.
Z. In a shaft furnace for burning mineral material, a refractory lining structure which comprises a working lining of magnesite bricks, a permanent lining of chromite ,4 bricks spaced from s-aid working lining, and a heatlagging layer of porous maguesite bricks adjacent the side of said permanent lining which is remote from said working lining. t
3. In a shaft furnace for brningmineral material, a refractory lining *structurel which comprises a working lining of magnesite bricks, a permanent liningv of chromite bricks` spaced from said working lining, and a hat-lagging layer of porous magnesite bricks adjacent the side of said permanent lining which is remote' from said working lining, said permanent lining and heat-lagging layer being inthe form of a compound brick.
References Cited in the le of this patent UNITED STATES PATENTS 1,410,739 BalZ Mar. 2K8, 1922 2,230,141 Heller 1311.28, 1941 2,683,052v Hartman July 6, 1954 FOREIGN PATENTS 448,663 Great Britain Junel 12, 1936
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT2985442X | 1957-05-11 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2985442A true US2985442A (en) | 1961-05-23 |
Family
ID=3690582
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US733445A Expired - Lifetime US2985442A (en) | 1957-05-11 | 1958-05-06 | Refractory lining |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2985442A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3779699A (en) * | 1973-03-15 | 1973-12-18 | Aluminum Co Of America | Furnace structure |
| FR2296485A1 (en) * | 1974-12-30 | 1976-07-30 | Daussan Jean | Ladles for molten metal with refractory lining - contg layer with high thermal insulation which reduces heat losses |
| FR2379497A1 (en) * | 1977-02-08 | 1978-09-01 | Zytan Thermochemi Verfahrenste | PLANT FOR THE MANUFACTURING OF SHAPED BODIES IN GRANULAR CERAMIC MATERIALS |
| US4202538A (en) * | 1977-03-02 | 1980-05-13 | Nippon Kokan Kabushiki Kaisha | Casting vessel having basic lining and usage thereof |
| US4734031A (en) * | 1985-10-30 | 1988-03-29 | Micropore International Limited | Vessel for holding high temperature bulk materials |
| US4754591A (en) * | 1978-06-02 | 1988-07-05 | Hoogovens Ijmuiden B.V. | Construction and repair of refractory structures, in particular heated structures |
| US4803933A (en) * | 1984-10-30 | 1989-02-14 | Dresser Industries, Inc. | Refractory brick having an increased insulating value |
| US4840131A (en) * | 1986-09-13 | 1989-06-20 | Foseco International Limited | Insulating linings for furnaces and kilns |
| US4997366A (en) * | 1990-02-05 | 1991-03-05 | Micro Control Company | Rear wall construction for burn-in environmental systems |
| US20080286709A1 (en) * | 2007-05-14 | 2008-11-20 | Bailey James G | Kiln Removable Ceramic Element Holder |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1410739A (en) * | 1919-04-15 | 1922-03-28 | Dunwell Stephen Hoyt | Process for treating waxed paper stock |
| GB448663A (en) * | 1935-09-09 | 1936-06-12 | Henry Victor Allen | Improvements relating to heat-insulating bricks or blocks for use in furnaces, kilns and the like |
| US2230141A (en) * | 1939-10-24 | 1941-01-28 | Gen Refractories Co | Rotary kiln lining |
| US2683032A (en) * | 1951-02-14 | 1954-07-06 | Meehanite Metal Corp | Basic lined cupola |
-
1958
- 1958-05-06 US US733445A patent/US2985442A/en not_active Expired - Lifetime
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1410739A (en) * | 1919-04-15 | 1922-03-28 | Dunwell Stephen Hoyt | Process for treating waxed paper stock |
| GB448663A (en) * | 1935-09-09 | 1936-06-12 | Henry Victor Allen | Improvements relating to heat-insulating bricks or blocks for use in furnaces, kilns and the like |
| US2230141A (en) * | 1939-10-24 | 1941-01-28 | Gen Refractories Co | Rotary kiln lining |
| US2683032A (en) * | 1951-02-14 | 1954-07-06 | Meehanite Metal Corp | Basic lined cupola |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3779699A (en) * | 1973-03-15 | 1973-12-18 | Aluminum Co Of America | Furnace structure |
| FR2296485A1 (en) * | 1974-12-30 | 1976-07-30 | Daussan Jean | Ladles for molten metal with refractory lining - contg layer with high thermal insulation which reduces heat losses |
| FR2379497A1 (en) * | 1977-02-08 | 1978-09-01 | Zytan Thermochemi Verfahrenste | PLANT FOR THE MANUFACTURING OF SHAPED BODIES IN GRANULAR CERAMIC MATERIALS |
| US4202538A (en) * | 1977-03-02 | 1980-05-13 | Nippon Kokan Kabushiki Kaisha | Casting vessel having basic lining and usage thereof |
| US4754591A (en) * | 1978-06-02 | 1988-07-05 | Hoogovens Ijmuiden B.V. | Construction and repair of refractory structures, in particular heated structures |
| US4803933A (en) * | 1984-10-30 | 1989-02-14 | Dresser Industries, Inc. | Refractory brick having an increased insulating value |
| US4734031A (en) * | 1985-10-30 | 1988-03-29 | Micropore International Limited | Vessel for holding high temperature bulk materials |
| US4840131A (en) * | 1986-09-13 | 1989-06-20 | Foseco International Limited | Insulating linings for furnaces and kilns |
| US4997366A (en) * | 1990-02-05 | 1991-03-05 | Micro Control Company | Rear wall construction for burn-in environmental systems |
| US20080286709A1 (en) * | 2007-05-14 | 2008-11-20 | Bailey James G | Kiln Removable Ceramic Element Holder |
| US7564007B2 (en) | 2007-05-14 | 2009-07-21 | Bailey James G | Kiln removable ceramic element holder |
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