GB2107034A - Lance - Google Patents
Lance Download PDFInfo
- Publication number
- GB2107034A GB2107034A GB08226728A GB8226728A GB2107034A GB 2107034 A GB2107034 A GB 2107034A GB 08226728 A GB08226728 A GB 08226728A GB 8226728 A GB8226728 A GB 8226728A GB 2107034 A GB2107034 A GB 2107034A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tube
- sleeve
- lance
- anchoring means
- refractory
- 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.)
- Withdrawn
Links
- 238000004873 anchoring Methods 0.000 claims abstract description 23
- 239000011819 refractory material Substances 0.000 claims abstract description 12
- 239000002184 metal Substances 0.000 claims abstract description 10
- 229910052751 metal Inorganic materials 0.000 claims abstract description 10
- 230000000717 retained effect Effects 0.000 claims abstract description 4
- 229910000831 Steel Inorganic materials 0.000 claims description 7
- 239000010959 steel Substances 0.000 claims description 7
- 239000000463 material Substances 0.000 claims description 6
- 238000005266 casting Methods 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 claims description 3
- 238000000034 method Methods 0.000 claims description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000011810 insulating material Substances 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 229910000639 Spring steel Inorganic materials 0.000 description 1
- 229910000746 Structural steel Inorganic materials 0.000 description 1
- 230000004323 axial length Effects 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000011065 in-situ storage Methods 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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
- F27D3/00—Charging; Discharging; Manipulation of charge
- F27D3/16—Introducing a fluid jet or current into the charge
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Treatment Of Steel In Its Molten State (AREA)
Abstract
A lance comprises a metal tube (1) having a sleeve of a refractory material (shown by chain - dotted lines) mounted substantially co-axially therewith, the sleeve being retained upon the tube by means of two sets of anchoring means (3, 4) extending into the body of the refractory material, one set of anchoring means (3) being fixedly attached to the tube and the other set of anchoring means (4) being capable of axial movement relative to the tube. Preferably, the two sets of anchoring means are mounted upon different axial portions of the tube with the fixedly mounted set being located at the outlet end of the tube, i.e. that end of the tube which is to be inserted into the molten metal during use, the relatively moveable set being mounted on the tube over the remainder of its length. <IMAGE>
Description
SPECIFICATION
Lance
The present invention relates to lances used to inject gases or powdered solids into molten metals, notably into molten iron or steel.
During the production of many metals, it is desired to inject a gas or a powdered solid into the molten metal. This is conventionally achieved by means of a hollow tube whose end is inserted into the molten metal. For convenience, the term lance is used herein to denote such tubes. Such lances are usually constructed from a steel tube, protected from the molten metal by a refractory sleeve which surrounds the steel tube. However, probiems are encountered with such lances since cracks frequently develop in the refractory sleeve, causing premature failure of the lance.
In making lances, the refractory sleeve is fixed to the steel tube by means of a series of anchors which are fixed to the tube, e.g. by being welded thereto. The anchors are embedded in the refractory material, e.g. as it is cast around the tube, and provide a rigid linkage between the sleeve and the tube. However, we have found that the use of such anchors is a major cause of cracking of the refractory sleeve and we have devised a form of anchoring means which reduces this problem.
Accordingly, the present invention provides a lance which comprises a metal tube having a sleeve of a refractory material mounted substantially co-axially therewith, the sleeve being retained upon the tube by means of two sets of anchoring means extending into the body of the refractory material, one set of anchoring means being fixedly attached to the tube and the other set of anchoring means being capable of axial movement relative to the tube.
Preferably, the two sets of anchoring means are mounted upon different axial portions of the tube with the fixedly mounted set being located at the outlet end of the tube, i.e. that end of the tube which is to be inserted into the molten metal during use, and the relatively moveable set being mounted on the tube over the remainder of its length.
The tube can be of any desired cross-section, e.g. square, rectangular, circular or eliptical. If desired, tubes of a circular or eliptical crosssection can be supported and strengthened along part or all of their length, for example by locating them inside another close-fitting tube of a square or rectangular cross-section, or by welding an axial length of angle iron or other supporting element to the tube. The anchoring means and the refractory sleeve encompass the strengthening elements where present.
The anchoring means which are fixedly mounted on the tube can be of any suitable shape, e.g. T, L or hook shaped and can be bolted, welded or otherwise fixed to the tube. Preferably, this set of anchoring means is located at the outlet end of the tube and extend over the terminal 1 to 25% of the length of the tube at axial intervals of from 5 to 50, notably 10 to 20 cms.
Preferably, the anchoring means capable of axial movement with respect to the tube are in the form of coil springs having integral members extending outwardly from the tube in a generally radial direction. The coil(s) of the spring are a close fit on the tube so that they grip the tube and are thus located upon the tube. Desirably, the springs are single loop springs formed from a spring material, e.g. spring steel. The radially extending members are conveniently located at, or are provided by, the free ends of the spring coil. In addition to acting as anchorage points for the sleeve, they can serve the secondary function of acting as levers to assist in splaying the turns of the coil and thus enable the springs to be moved freely into position along the length of the tube.As indicated above, the springs are mounted over the majority, e.g. 99 to 75%, of the length of the tube extending from the inlet end of the tube and preferably at axial intervals of from 5 to 50 cms, notably 10 to 20 cms.
The sleeve can be made from a wide range of refractory materials and is preferably cast in situ around the tube during manufacture. The sleeve for example is from 10 to 30 cms thick and conveniently is of the same general cross-section as the tube around which it is formed.
In a preferred embodiment of the invention, a sleeve of insulating material is provided between the tube and the refractory sleeve, either as a sleeve of material extending continuously along the length of the tube or as a series of shorter sleeves extending between the anchoring means.
The insulating material can, for example, be formed from ceramic fibres in a bonding matrix.
Alternatively, cardboard or other combustible material sleeves can be provided between the refractory sleeve and the tube. During use of the lance, the cardboard or other material will burn away to form an air gap between the refractory sleeve and the tube.
A preferred form of the lance of the invention will now be described by way of illustration with respect to the accompanying drawings in which:
Figure 1 is a side view of the lance;
Figure 2 is an enlarged cross-section of the lance of Figure 1 on the line 1-1; and
Figure 3 is a cross-section of a lance using a square section tube.
A lance comprises a steel tube 1 enclosed in a refractory sleeve 2 (shown by broken lines).
Welded to tube 1 at its outlet end is a series of eight hook shaped members 3 located in pairs displaced circumferentially by 900 from one another. Located over the remaining length of the tube 1 are a number of single coil steel springs 4.
These springs are orientated upon the tube so that the radially extending free ends 5 on a spring are displaced by 900 circumferentially from the free ends on the adjacent springs. The springs 4 are mounted on tube 1 at axial intervals of approximately 1 5 cms along the length of the tube, although only four such springs are shown in the drawing.
Springs 4 are mounted upon tube 1 by pressing the free ends 5 of the spring together, thereby increasing the diameter of the ring part of the spring and permitting it to be slipped onto tube 1 and moved freely into position. On releasing the free ends 5, the spring firmly grips the tube.
When the springs 5 are in position, the tube is positioned in a cylindrical box shaped mould and a refractory material is cast around the tube using conventional materials and techniques. Preferably, the mould is vibrated during casting.
The casting forms a refractory sleeve around the tube 1 in which members 3 and 5 are embedded and act as reinforcement for the sleeve as well as holding the sleeve in position on the tube. Members 3 are fixed and retain sleeve 2 in position on the tube. Springs 4 on the other hand can move axially and can accommodate relative movement between the sleeve and the tube which can occur during setting of the refractory material during casting or during use of the lance.
Claims (9)
1. A lance which comprises a metal tube (1) having a sleeve (2) of a refractory material mounted substantially co-axially therewith, the sleeve (2) being retained upon the tube (1) by means of two sets of anchoring means (3), (4) extending into the body of the refractory material, one set of anchoring means (3) being fixedly attached to the tube (1) and the other set (4) of anchoring means being capable of axial movement relative to the tube (1).
2. A lance as claimed in claim 1 wherein the two sets of anchoring means (3), (4) are mounted upon different axial portions of the tube (1), the fixedly mounted set (3) being located in the portion adjacent the outlet of the tube (1), the moveable set (4) being located in the remaining length of the tube (1 ).
3. A lance as claimed in either of claims 1 or 2 wherein the moveable anchoring means (4) comprise coil springs substantially co-axially mounted on the tube and having members (5) extending radially outward from the tube (1).
4. A lance as claimed in any of the preceding claims wherein an insulating sleeve is provided between the refractory sleeve (2) and the tube (1).
5. A lance as claimed in claim 4 wherein a sleeve of combustible material is provided which is capable of being burnt away during use of the lance to form an air gap between the refractory sleeve (2) and the tube (1).
6. A lance which comprises a steel tube (1) having mounted substantially co-axially thereon a sleeve (2) of a refractory material, the sleeve (2) being retained upon the tube (1 ) by means of two sets of anchoring means (3), (4) extending radially outwardly from the tube (1) and embedded in the refractory sleeve (2), one set being provided by members (3) fixedly attached to the tube (1) over the terminal 1 to 25% of the length of the tube (1) adjacent the outlet of the tube, the other set (4) being provided by single coil springs substantially co-axially mounted on the tube (1) within the remaining length of the tube and capable of relative movement axially upon the tube, the coils (4) having members (5) integral therewith which extend radially into the refractory sleeve (2).
7. A method for producing a lance a claimed in claim 1 which method comprises mounting the relatively moveable set of anchoring means (4) upon a tube (1) provided with the fixed anchoring means (3); and casting a refractory material around the tube (1) to form the refractory sleeve (2).
8. A tube for use in the method of claim 7 which comprises a tubular member (1) having fixedly mounted thereon over the terminal 1 to 25% of the length thereof from the outlet of the tubular member anchoring means comprising members (3) extending radially outward from the tubular member (1); in association with members comprising coil springs (4) adapted to be mounted substantially co-axially upon the tubular member (1) and having members (5) extending radially from the coil spring (4).
9. A lance as claimed in claim 1 substantially as hereinbefore described.
1 0. A lance substantially as hereinbefore described with respect to and as shown in the accompanying drawings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB08226728A GB2107034A (en) | 1981-09-30 | 1982-09-20 | Lance |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB8129560 | 1981-09-30 | ||
| GB08226728A GB2107034A (en) | 1981-09-30 | 1982-09-20 | Lance |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB2107034A true GB2107034A (en) | 1983-04-20 |
Family
ID=26280858
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB08226728A Withdrawn GB2107034A (en) | 1981-09-30 | 1982-09-20 | Lance |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2107034A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2016166189A1 (en) | 2015-04-16 | 2016-10-20 | Vesuvius Crucible Company | Lance for top injection in metallurgical vessels and process for manufacturing same |
-
1982
- 1982-09-20 GB GB08226728A patent/GB2107034A/en not_active Withdrawn
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2016166189A1 (en) | 2015-04-16 | 2016-10-20 | Vesuvius Crucible Company | Lance for top injection in metallurgical vessels and process for manufacturing same |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |