GB2080928A - Improvements relating to refractory components for furnaces - Google Patents
Improvements relating to refractory components for furnaces Download PDFInfo
- Publication number
- GB2080928A GB2080928A GB8122898A GB8122898A GB2080928A GB 2080928 A GB2080928 A GB 2080928A GB 8122898 A GB8122898 A GB 8122898A GB 8122898 A GB8122898 A GB 8122898A GB 2080928 A GB2080928 A GB 2080928A
- Authority
- GB
- United Kingdom
- Prior art keywords
- component
- refractory
- face
- channel
- section
- 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.)
- Granted
Links
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
- F27D1/14—Supports for linings
- F27D1/144—Supports for ceramic fibre materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F27—FURNACES; KILNS; OVENS; RETORTS
- F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
- F27D1/00—Casings; Linings; Walls; Roofs
- F27D1/0003—Linings or walls
- F27D1/0006—Linings or walls formed from bricks or layers with a particular composition or specific characteristics
- F27D1/0009—Comprising ceramic fibre elements
-
- 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
- F27D1/04—Casings; Linings; Walls; Roofs characterised by the form, e.g. shape of the bricks or blocks used
- F27D1/06—Composite bricks or blocks, e.g. panels, modules
- F27D1/08—Bricks or blocks with internal reinforcement or metal backing
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Furnace Housings, Linings, Walls, And Ceilings (AREA)
Abstract
A refractory component which is vacuum-formed from ceramic fibres and which is to be mounted on the external casing or frame structure of a furnace to form part of heat-resisting lining is provided with an internal reinforcement 19 in those parts of the component nearest the casing or frame structure and by which the component is to be mounted on the casing or frame structure. The reinforcement is embedded in the component during formation thereof and is of stiff open mesh form extending in a plane parallel to the general plane of the part of the casing or frame structure on which the component is mounted. The reinforcement is made from heat- resisting metal alloy, refractory clay or recrystallized alumina and is preferably of channel-section or other three dimensional form to increase its stiffness. <IMAGE>
Description
SPECIFICATION
Improvements relating to refractory components for furnaces
This invention relates to the reinforcement of refractory components which are vacuum formed from ceramic fibres and which are required to be mounted on the exterior structure of a furnace thus forming parts of the heat resisting refractory lining of the furnace. Such reinforced components may be, for example, modules, burner blocks, tube blocks, peep and access door frames and supports for electric heating elements.
According to this invention, there is provided a refractory component vacuum formed from ceramic fibre to be mounted on the exterior structure of the furnace (whether it be for example casings, columns or joists) wherein there is embedded during the vacuum forming process one or more reinforcing members of stiff openmesh form disposed in that region of the component which will eventually be placed nearest to said structure and in a plane or planes generally parallel to the said structure and from which region the component is to be anchored to the structure, the reinforcing member being made of heat resisting metal alloy, refractory clay or recrystallized alumina.
In practice the material from which the reinforcing member or members are formed depends upon the weight of the component, the temperature and chemistry of the furnace gases and the vibration encountered by the furnace in service.
Each of the said reinforcing members of openmesh form, hereinafter called reinforcements, is preferably made of three-dimensional shape to add to the inherent resistance to bending of the material from which they are made, first, so that during forming of the component the reinforcements will not yield under vacuum and, in springing back when the vacuum ceases, distort the wet and soft component, and second, so that the reinforcements can transform the point loading of the anchors into a dispersed loading over the area of the component in which the reinforcements are embedded both by reason of the added strength acquired by shaping and by the multiplying of the planes in the fibre where shear is resisted. This may be accomplished by making the reinforcements of channel, trough, T or L section.
When such sections are employed and the component is mounted on the supporting structure, the reinforcement is best disposed so that one flange of the channel or the foot of the T or L section runs along the colder edge of the component parallel to that portion of the structure to which it is to be anchored. The web, in the case of a channel, is best disposed approximately centrally in the wall of the component so that the other flange is nearer the hot face of the furnace wall by the width of the web.
In reinforcements made of heat resisting metal alloys the mesh is diamond shaped, as commonly supplied in expanded metal. In reinforcements made from refractory the mesh may be oval or diamond shaped. These aperture shapes are much to be preferred because in them all of the strands of the mesh are load bearing in the sense that they resist loads tending to pull the mesh through the fabric of the fibre, whereas a square mesh cut parallel to the side of the squares would be load bearing on only half its strands.
The size of the apertures and the coarseness of the strands are governed by the general length of the fibres being vacuum formed. The general fibre length is in turn determined by the size and delicacy of the component. This walls of smaller components can be advantageously formed of generally short fibres and these will form around and through smaller apertures. Larger components are of generally longer fibre lengths and require larger apertures if the fibre is to form without voids.
The length of the reinforcement extends along the wall of the component approaching the corners where the fabric is thicker and so stronger.
However it is visualized that in certain applications the reinforcement may be bent in forming and take its position in a corner or corners of the component.
Applied to vacuum formed ceramic fibre burner blocks or fire face modules both of which are roughly five sided boxes with one open side (the colder side), four narrower sides the width of which constitutes a part of the thickness of the furnace wall, and the larger fifth side being the fire face, the invention provides the aforementioned reinforcement in one or more of the four narrower sides which are perpendicular, or nearly so to the fire face and in the positions described above.
One embodiment of the invention will now be described by way of example with reference to the accompanying drawing in which:
Figure 1 is a front view of a refractory burner block for use in a furnace, which block embodies the invention,
Figure 2 is a sectional view on the plane 2-2 of Figure 1,
Figure 3 is a sectional end elevation on the plane 3-3 of Figure 1, and
Figure 4 illustrates a form of fastener or anchor.
The drawings show a refractory burner block moulded in one piece from ceramic fibre by a vacuum forming technique which involves drawing into a mould cavity in the shape of the block, by means of powerful vacuum, a water slurry containing ceramic fibres of a required average length, bonding agents, organic or inorganic or both (starch and/or colloidal silica) and sometimes a quantity of filler such as tabular alumina the solid materials and a determinable amount of the bonding agents being retained. The solid material is retained in the mould cavity by filters forming part of the mould and the liquid being discharged from the cavity.The moulded block has a front wall 10 with a central aperture 1 Oa and rearwardly extending-side walls 11, 12, 13 and 14 and an inner side wall 1 5 about the aperture, which together form a box open at the rear. In use, the block is mounted by its side walls on the inner side of a steel furnace casing structure (not shown) in sealing side-wall to sidewall relationship with other furnace lining components in such a manner that the front wall 10 of the block define part of the furnace chamber.Additional refractory and/or heatinsulating material which may be desirable in order to increase the temperature gradient from the hot to the cold sides of the block may be placed in the two cavities enclosed by the side walls 1 1, 12, 13, 14 and side wall 15 and is held in place by an insulating back plate (not shown).
The burner block is secured to the steel casing of the furnace by anchors 1 6, one of which is shown in Figure 4, in the manner described in more detail in our Patent Specification No. 1544407, which extend inward between the side walls 12 of the two adjoining components and have oppositely directed teeth 1 6a which are pressed into the soft material of the two components. The rearward outer end portion 1 6b of the fastener is directed laterally and has a slot 1 6c in it which can be engaged by a stud welded to the casing 17 to enable the fastener to be secured to the casing.
The outer end portion 1 6b may alternatively be welded to the casing 17. The inner ends of the fasteners are positioned sufficiently far outward from the hot front wall 10 not to be weakened to an unacceptable extent by the temperature to which they are exposed; the fasteners are protected by the body of ceramic fibre disposed between their teeth and the furnace chamber and by refractory sealing strips disposed between the side walls of the components and are cooled by conduction through the metal to the furnace casing structure.
In order to increase the secureness of its attachment to the casing structure the illustrated burner block has its four side walls 11 to 14 reinforced by having rigid refractory mesh embedded therein. The reinforcement in each of these side walls comprises a rigid channel-section length 18 having a stiff mesh, which is made from heat-resisting alloy, recrystallized alumina or a refractory clay, extending along the side wall but in this instance terminating short of the corners of the block which are naturally stronger than the middle portions of the side wall.The width dimension of the web 19 of the channel extends in an inward and outward direction whilst the two flanges 20, 21 of the channel extend in a direction through the thickness of the side wall, flange 21 of the channel being disposed at the rear edge of the side wall since this flange 21 is used in securing the reinforcement channel 1 8 in the mould during manufacture of the component. As shown in
Figure 2, the mesh is of diamond or lozenge form and the reinforcement is so cut and disposed that each of the lengths of material defining the mesh apertures is inclined with respect to the inward and outward direction.In order to avoid the formation of voids in the region of the reinforcement during the moulding process and to bind the reinforcement securely into the fibre, the fibre strands should extend through the apertures and then fill them and for this reason it is preferable to use mesh with fairly large apertures; the longer the fibres the larger the apertures should be. The teeth of the fasteners preferably extend just outside the channel but close to the inner flange 20 of the channel,:but may where the teeth are of a small and compact'crnsssection extend through apertures in the web of the channel.
The above-mentioned inclination of the lengths of refractory material defining the apertures ensures that substantially all of the material of the channel serves to spread what would otherwise be point compression loads exerted by the teethover the greater part of the fabric of the wall.
The reinforcing members may be made fr13in refractory clay or similar cheaper refractory N materials if the furnace operating conditions permit.
It will be understood that the same method of reinforcement can be used for wall modules and other components for a furnace which components are made from fibre by a vacuum moulding technique and are secured to the furnace casing by the same general type of fastener as is described above and as is illustrated in our Patent Specification No. 1544407.
It will be seen that the invention also provides a furnace component vacuum-formed from refractory fibre and having formed integrally therewith a support portion by which the component is to be supported from the exterior of a furnace, which support portion has embedded therein a reinforcing member of stiff open-mesh form and made from heat-resistant metal alloy or a refractory material. e.g. re-crystallized alumina or refractory clay, said member comprising a first part extending along said support portion from a position spaced outwardly from the "hot" or inner end or face of the component to a position adjacent the "cold" or outer end or face of said support portion, and a second part rigidly connected to and extending transversely of the first part at a location spaced from both the hot and cold ends or faces of the component Thus when the component is mounted on the casing, the said first part of the reinforcing member extends along the support portion towards the casing, and the said second part extends in the direction of the thickness of the support portion and, preferably, generally parallel to the adjacent part of the inner furnace of the furnace.
The term "wall" used herein in relation to a furnace is intended to include the roof and floor of the furnace in addition to the side wall thereof.
Claims (9)
1. A refractory component vacuum formed from ceramic fibre to be mounted on the exterior structure.of the furnace (whether it be for example casings, columns or joists) wherein there is embedded during-the vacùum Wtint prows one or more reinforcing members of stiff openmesh form disposed in that region of the component which will eventually be placed nearest to said structure and in a plane or planes generally parallel to the said structure and from which region the component is to be anchored to the structure, the reinforcing member being made of heat resisting metal alloy, refractory clay or recrystallized alumina.
2. A refractory component as claimed in claim 1, wherein each of the open-mesh reinforcing members is of three dimensional form.
3. A reinforcing component as claimed in claim 2, wherein the reinforcing member or members are of channel-section, the two side flanges of the channel extending parallel to the plane of the cold face of the component.
4. A refractory component as claimed in claim 3, wherein one of said side flanges is disposed substantially in the cold face of the component.
5. A refractory component as claimed in claim 2, wherein the reinforcing member or members are of T-section, the foot of the section being disposed substantially in the colder face of the component and the cross-piece of the section extending parallel to the plane of the cold face of the component.
6. A refractory component as claimed in claim 2, wherein the reinforcing member or members are of L-section, one of the two webs of the section extending substantially in the plane of the cold face of the component, and the other of the webs projecting away from said -cold face, having its free edge substantially in the colder face of the component.
7. A refractory component as clairmed in any one of claims 1 to 6, wherein the reinforcing member or members are of diamond or oval mesh.
8. A refractory cornponent as claimed in claim 1, wherein the component is in the form of a hollow rectangular box which is open at one face (the cold face) and has a front wall providing a hot face and four rearwardly-extending side walls which terminate at the cold face, each of said side walls having embedded therein a reinforcing member which is of diamond mesh and of rectangular channel section, one side flange of the channel being disposed substantially in the plane of the cold face, the other side flange of the channel extending parallel to the cold face, and the web of the channel being disposed substantially centrally of the thickness of said side wall.
9. A refractory component substantially as hereinbefore described with reference to and as illustrated in Figures 1 to 3 of the accompanying drawings.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8122898A GB2080928B (en) | 1980-07-29 | 1981-07-24 | Improvements relating to refractory components for furnaces |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8024816 | 1980-07-29 | ||
GB8122898A GB2080928B (en) | 1980-07-29 | 1981-07-24 | Improvements relating to refractory components for furnaces |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2080928A true GB2080928A (en) | 1982-02-10 |
GB2080928B GB2080928B (en) | 1984-09-19 |
Family
ID=26276383
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8122898A Expired GB2080928B (en) | 1980-07-29 | 1981-07-24 | Improvements relating to refractory components for furnaces |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2080928B (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2522801A1 (en) * | 1982-03-02 | 1983-09-09 | Isolite Babcock Refractories | Ceramic fibre block-securing equipment - comprises oblong support with ends inserted in adjacent block fixed to plate |
EP0123165A1 (en) * | 1983-04-23 | 1984-10-31 | Didier-Werke Ag | Device for fastening electical heating elements to lining blocks |
FR2558243A1 (en) * | 1984-01-13 | 1985-07-19 | Lafarge Refractaires | OVEN COMPARTMENT COMPRISING A PASSAGE FOR GAS FROM A BURNER AND PROCESS FOR OBTAINING THE SAME |
EP1528343A1 (en) * | 2003-10-27 | 2005-05-04 | Siemens Aktiengesellschaft | Refractory tile with reinforcing members embedded therein, as liner for gas turbine combustion chamber |
-
1981
- 1981-07-24 GB GB8122898A patent/GB2080928B/en not_active Expired
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2522801A1 (en) * | 1982-03-02 | 1983-09-09 | Isolite Babcock Refractories | Ceramic fibre block-securing equipment - comprises oblong support with ends inserted in adjacent block fixed to plate |
EP0123165A1 (en) * | 1983-04-23 | 1984-10-31 | Didier-Werke Ag | Device for fastening electical heating elements to lining blocks |
FR2558243A1 (en) * | 1984-01-13 | 1985-07-19 | Lafarge Refractaires | OVEN COMPARTMENT COMPRISING A PASSAGE FOR GAS FROM A BURNER AND PROCESS FOR OBTAINING THE SAME |
EP0151543A1 (en) * | 1984-01-13 | 1985-08-14 | Kerlane | Oven part constituting a duct for the exhaust gases of a burner and process for its fabrication |
EP1528343A1 (en) * | 2003-10-27 | 2005-05-04 | Siemens Aktiengesellschaft | Refractory tile with reinforcing members embedded therein, as liner for gas turbine combustion chamber |
WO2005043058A2 (en) * | 2003-10-27 | 2005-05-12 | Siemens Aktiengesellschaft | Ceramic thermal shield with integrated reinforcing elements, especially for lining the wall of a gas turbine combustion chamber |
WO2005043058A3 (en) * | 2003-10-27 | 2005-08-11 | Siemens Ag | Ceramic thermal shield with integrated reinforcing elements, especially for lining the wall of a gas turbine combustion chamber |
JP2007510121A (en) * | 2003-10-27 | 2007-04-19 | シーメンス アクチエンゲゼルシヤフト | Heat shield element |
US7540710B2 (en) | 2003-10-27 | 2009-06-02 | Siemens Aktiengesellschaft | Turbine blade for use in a gas turbine |
US7805945B2 (en) | 2003-10-27 | 2010-10-05 | Siemens Aktiengesellschaft | Thermal shield, especially for lining the wall of a combustion chamber |
US8857190B2 (en) | 2003-10-27 | 2014-10-14 | Siemens Aktiengesellschaft | Heat shield element, in particular for lining a combustion chamber wall |
Also Published As
Publication number | Publication date |
---|---|
GB2080928B (en) | 1984-09-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19960724 |