EP1673481B1 - Four industriel et buse associee - Google Patents

Four industriel et buse associee Download PDF

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Publication number
EP1673481B1
EP1673481B1 EP04790388A EP04790388A EP1673481B1 EP 1673481 B1 EP1673481 B1 EP 1673481B1 EP 04790388 A EP04790388 A EP 04790388A EP 04790388 A EP04790388 A EP 04790388A EP 1673481 B1 EP1673481 B1 EP 1673481B1
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EP
European Patent Office
Prior art keywords
nozzle
heat
element according
conducting elements
refractory material
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.)
Not-in-force
Application number
EP04790388A
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German (de)
English (en)
Other versions
EP1673481A2 (fr
Inventor
Uwe Zulehner
Hans Rinnhofer
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.)
Maerz Gautschi Industrieofenanlagen GmbH Germany
Original Assignee
Maerz Gautschi Industrieofenanlagen GmbH Germany
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 Maerz Gautschi Industrieofenanlagen GmbH Germany filed Critical Maerz Gautschi Industrieofenanlagen GmbH Germany
Priority to PL04790388T priority Critical patent/PL1673481T3/pl
Publication of EP1673481A2 publication Critical patent/EP1673481A2/fr
Application granted granted Critical
Publication of EP1673481B1 publication Critical patent/EP1673481B1/fr
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21C—PROCESSING OF PIG-IRON, e.g. REFINING, MANUFACTURE OF WROUGHT-IRON OR STEEL; TREATMENT IN MOLTEN STATE OF FERROUS ALLOYS
    • C21C5/00—Manufacture of carbon-steel, e.g. plain mild steel, medium carbon steel or cast steel or stainless steel
    • C21C5/28—Manufacture of steel in the converter
    • C21C5/42—Constructional features of converters
    • C21C5/46—Details or accessories
    • C21C5/48—Bottoms or tuyéres of converters
    • 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
    • F27D1/10—Monolithic linings; Supports therefor
    • 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
    • F27D1/12—Casings; Linings; Walls; Roofs incorporating cooling arrangements
    • 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
    • F27D1/141—Anchors therefor
    • 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
    • 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
    • F27D9/00—Cooling of furnaces or of charges therein
    • 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
    • F27D99/00—Subject matter not provided for in other groups of this subclass
    • F27D99/0001—Heating elements or systems
    • F27D99/0033—Heating elements or systems using burners

Definitions

  • the invention relates to an industrial furnace for melting metals, in particular non-ferrous metals, and an associated nozzle element.
  • Appropriate treatment media are injected regularly through nozzles in the molten metal.
  • Such nozzles can be made up either as under-bath nozzles (in these the treatment medium is injected below the bath surface of the molten metal into them) or as over-bath nozzles (in these the treatment medium is injected into the interior of the furnace above the bath surface).
  • the nozzles used are usually from a metal tube, which is passed through the outer wall of the industrial furnace through into the interior of the furnace. On the furnace inside the nozzle is usually a nozzle insert plugged onto the metal tube.
  • the outer wall of corresponding industrial furnaces is constructed of an outer steel shell, which is delivered on an inner side with a refractory material. In the furnace interior formed by the refractory lining, the metal is melted.
  • the refractory material surrounding the nozzles in this area is regularly subjected to increased wear.
  • This increased wear finds its cause on the one hand in particular in increased temperature changes in the region of the nozzle orifice, which leads to flaking of the refractory lining.
  • increased flow movements of the partial melt occur in the region of the nozzle orifice, which leads to a mechanical erosion of the refractory lining.
  • US 3,330,645 discloses high temperature devices comprising fans, nozzles and buried burners which prevent erosion of the refractory lining by improved cooling of a porous block. Numerous fine channels (pores or holes), through which a coolant passes, pass through a refractory porous block. The coolant causes a protective layer of gas bubbles to be formed on the mating surface of the permeable refractory material with the molten metal and is constantly renewed.
  • the back of the porous block is provided with an annular Sammelrohusethlung with an inlet channel for thedefierstoff.
  • the groove is also associated with the pores or channels that pass through the porous block.
  • the lower end of the block may be equipped with a metal sleeve which also extends over the lower side part of the block. Holes are provided in a bottom plate for an extension which forms the inlet port of the central channel and for a second extension which is the inlet for the cooling fluid.
  • DE 1 246 782 A relates to a nozzle body which consists of pressed, highly heat-resistant material and contains metallic insert rings (wire or ribbon-shaped). Furthermore, the nozzle body is surrounded by a metal shell adapted to its outer surface, which in turn is surrounded by a spiral-shaped cooling tube.
  • the invention is based on the object, an industrial furnace for melting metals, in particular non-ferrous metals, as well as a associated nozzle element to provide, with the wear of the refractory material in the region of the nozzle can be reduced.
  • the assembly of the nozzle element according to the application is based on the finding that the wear of the refractory material in the region of the nozzle can be reduced, in particular, by the formation of a "batch" of solidified molten metal in the region of the nozzle on the hot side of the refractory material.
  • This "approach” consists essentially of slag and metal and protects the underlying refractory material in the area of the nozzle from closing.
  • heat-conducting elements For cooling the refractory material in the region of the nozzle, heat-conducting elements are provided, which consist of a material which has an increased thermal conductivity compared to the refractory material.
  • the heat-conducting elements are in contact with the metal shell on the cold side of the nozzle body, so that the heat-conducting receive heat and can forward quickly to the metal jacket. From the metal shell, the heat is released to the outside. To improve the heat output from the metal shell to the outside of the metal jacket is cooled, for example by a cooling medium.
  • the nozzle element may be formed as a separate element.
  • the hot side of the nozzle body of the nozzle member and the cold side are spaced and preferably also parallel to each other.
  • the hot side and the cold side of the nozzle body may have the same or different shapes.
  • the hot side and the cold side can each be designed round, oval, square or polygonal. If the hot side and the cold side each have a round shape, they may for example have the same diameter, so that the nozzle body has the overall shape of a cylinder, or the hot side may have a smaller diameter than the cold side, so that the nozzle body of the Cold side tapered to the hot side; thereby
  • the nozzle element can be easily inserted into a corresponding opening in the outer wall of an industrial furnace.
  • the nozzle body has the overall shape of a cuboid, that is, for example, the shape of a cube.
  • the cold side and the hot side connecting side surfaces of the nozzle body may be covered by a metal jacket.
  • hot side is understood to mean the side of the nozzle body which (in the installed state of the nozzle element in an industrial furnace) faces the interior of the furnace and therefore the molten metal.
  • cold side is correspondingly understood the opposite side of the nozzle body, ie the side facing away from the furnace interior of the nozzle body.
  • the nozzle element is designed to introduce gas or other media, for example solids such as powders or the like, into the molten metal.
  • the nozzle body may consist of any refractory material, such as an oxide ceramic or a non-oxide ceramic material, so for example an oxide ceramic refractory material.
  • the refractory material of the nozzle body is covered by a metal sheath.
  • This metal shell may for example consist of copper or steel, such as stainless steel, and be connected for example via anchors or a refractory mass with the refractory material of the nozzle body.
  • the metal shell may be dimensioned such that it - when inserting the nozzle element in the outer wall of an industrial furnace - flush with the outer metal shell of the furnace, so that the Metal shell of the nozzle element and the outer metal shell of the furnace form a continuous surface.
  • the metal shell is in contact (on its side facing the nozzle body) with heat conducting elements which extend into the refractory material and toward the hot side of the nozzle body.
  • the heat-conducting elements may have any shape, for example the shape of rods, prisms, webs or plates.
  • heat-conducting elements in the form of rods having a star-shaped cross-section can be used; corresponding rods have a relatively high surface, whereby a good heat transfer to the heat conducting elements can be effected.
  • the heat-conducting elements may have a tree-like structure; In this embodiment, the heat-conducting element therefore branches in the direction of the hot side of the nozzle body. These "branches" can absorb the heat in the area of the hot side of the nozzle body well and forward over the (common) "trunk” to the metal shell.
  • the heat-conducting elements are arranged directly on the metal jacket and thereby, for example, integrally formed from the metal shell, for example in the form of "cooling fins".
  • the heat-conducting elements may for example also be connected directly to the metal jacket via a welding, screwing or other connection.
  • the heat-conducting elements are not in direct contact with the metal jacket but conduct heat intermediate areas of refractory material to the metal shell on.
  • Corresponding heat-conducting elements may for example consist of one, several or a plurality of individual bodies which are embedded in the refractory material.
  • a plurality of heat-conducting elements in the form of small bodies are provided, which are dispersedly embedded in the latter over the refractory material.
  • the thermal conductivity of the refractory material in this area is increased overall, so that the heat in the area distributed in the refractory material body is forwarded to the metal shell faster than in the areas of the refractory material, in which no corresponding bodies are arranged.
  • the ends of the heat-conducting elements facing the hot side of the nozzle body can terminate at a distance from the hot side, ie leak in the refractory material, or be led directly to the hot side and then form, for example, a flush surface with the hot side of the nozzle body.
  • the heat-conducting elements and the metal shell are preferably made of the same material, that is, for example, copper, steel or stainless steel.
  • a nozzle tube (hereinafter called "outer nozzle tube").
  • This outer nozzle tube is used - optionally in combination with one or more tubes for conducting gas - for supplying gas or other treatment media in the molten metal.
  • the outer nozzle tube may in particular consist of a metal, for example stainless steel, preferably has a circular inner (free) cross-sectional area and extends in particular along a linearly extending longitudinal axis.
  • the outer nozzle element can be connected to the nozzle body, for example via a refractory material.
  • inner nozzle tube In the outer nozzle tube, a further nozzle tube, hereinafter referred to as “inner nozzle tube” may be arranged.
  • the inner nozzle tube along its longitudinal axis, which extends for example coaxially to the longitudinal axis of the outer nozzle tube, be arranged displaceably in the outer nozzle tube.
  • a corresponding, along its longitudinal axis slidably disposed in the outer nozzle tube inner nozzle tube has a significant advantage: Instead of an inner nozzle tube, the previously used generic nozzles had a nozzle insert, which was placed on the hot side of the (outer) nozzle tube on this. Through this nozzle insert a defined nozzle shape could be adjusted on the hot side of the nozzle tube. Due to scaling of the nozzle insert this could only be used for a batch, so that the nozzle insert had to be broken out of the nozzle tube after each melting and replaced with a new nozzle insert. This replacement process was very time consuming. According to the application, an inner nozzle tube is now displaceably arranged in the outer nozzle tube, and according to its wear this can be continuously fed in from the outside. The previously necessary replacement process is eliminated.
  • the inner nozzle tube has a defined inner (free) cross-sectional area so that the conditions for introducing the gas introduced into the molten metal through the inner nozzle tube can be adjusted.
  • the inner nozzle tube is arranged at a distance from the outer nozzle tube in this. Characterized a gap is defined between the inner and outer nozzle tube, which can also be used to introduce gas into the molten metal.
  • Inner nozzle tube and outer nozzle tube can be kept at a distance via spacers. These spacers may for example be knob-like bulges, which are arranged on the inner nozzle tube surface facing the outer nozzle tube. On the inner nozzle tube surface facing the outer nozzle tube and such bulges can be arranged, which engage in corresponding guide elements, such as rails or grooves, which are arranged on the outer surface of the inner nozzle tube.
  • These guide elements can be arranged, for example, parallel to the longitudinal axis or also helically on the surface of the inner nozzle tube, so that the inner nozzle tube can be guided in the longitudinal direction or helically in the outer nozzle tube.
  • the outer peripheral surface of the inner nozzle tube has an external thread, which engages in internal thread, which is arranged on the inner nozzle tube surface facing the outer nozzle tube.
  • the outer and the inner nozzle tube are each formed such that the remaining between the outer and the inner nozzle tube gap or the inner free cross section of the inner nozzle tube in such Contact with a gas or other source of a medium can be brought that in the gap or the inner free cross section of the inner nozzle tube gas / medium can be introduced.
  • the tracking or movement of the inner nozzle tube in the outer nozzle tube can be done manually or automatically, for example, with electric, hydraulic or pneumatic drive.
  • the follow-up process can basically be gradual or continuous and be tuned to the metallurgical treatment time, for example, with a preset feed rate. In the case of a continuous residual strength measurement of the nozzle, the feed rate can be continuously adapted to the wear conditions of the inner nozzle tube.
  • the gap between the inner and outer nozzle tube may be provided with a suitable lubricant or lubricant, for example, to minimize the torsional stresses.
  • the outer peripheral surface of the inner nozzle tube and the surface of the outer nozzle tube facing this surface are in direct contact with each other. In this case, no gas is passed through this gap.
  • a provided in this gap lubricant or lubricant can then also serve for sealing.
  • the heat-conducting elements are arranged in such a way in the refractory material of the nozzle body, that they are arranged substantially annularly around the outer nozzle tube around.
  • the nozzle member according to the application can be made such that immediately adjacent to the mouth of the outer nozzle tube on the hot side of the nozzle body, a stronger approach can be formed than in the areas further away from the mouth.
  • thermal conductivity in the immediately adjacent to the outer nozzle tube portions of the nozzle body is higher than in the farther removed areas.
  • the heat-conducting elements are guided closer to the hot side of the nozzle body in the area of the nozzle body closer to the outer nozzle pipe than in the areas further away from the outer nozzle pipe.
  • the heat dissipation thereby increases toward the mouth of the outer nozzle tube at the hot side of the nozzle body. Accordingly, the strength of the approach in this direction is increasing.
  • the heat-conducting elements can be designed in a stepped manner, wherein the step height - with respect to the hot side of the nozzle body - decreases away from the outer nozzle tube.
  • the metal jacket is designed such that it can be cooled by a fluid, in particular water, or another cooling medium.
  • the metal shell may for example be provided with means by which a fluid can be conducted over the surface of the metal shell or through the metal shell.
  • the amount of heat dissipation from the metal jacket to the outside is adjustable by the cooling medium, for example over the temperature interval between (the warmer) metal shell and (the colder) cooling medium and / or the amount of cooling medium flowing past the metal shell and / or the choice of the cooling medium itself (Choice of a cooling medium with a certain specific heat capacity).
  • a higher heat dissipation from the metal jacket to the outside in this case has an increased heat dissipation from the hot side of the nozzle body to the outside to result, which is accompanied by an increased formation of deposits on the hot side.
  • the nozzle element according to the application is designed for installation in any industrial furnace for melting metals, but in particular for installation in an industrial furnace for melting non-ferrous metals.
  • the nozzle element can be designed both as an underbath nozzle and as a Kochbaddüse.
  • the application comprises an industrial furnace, in the outer wall of which a nozzle element according to the application is arranged.
  • the industrial furnace may have an opening in its outer wall into which a nozzle element according to the application can be inserted.
  • the Düserel-ement in Figure 1 is designated in its entirety by 1.
  • the nozzle body 3 of the nozzle element 1, which is formed from a refractory mass, has an overall cubic shape with a square hot side 5 and a square cold side 7.
  • the refractory material of the nozzle body 3 is covered by a metal jacket 9 made of copper.
  • Channel-like recesses 8 are introduced into the metal element 9 on the surface side of the metal element 9 facing away from the nozzle body 3.
  • the channel-like depressions 8 are covered by cover plates 10 to the outside, so that the channel-like depressions 8 are completely completed.
  • the cover plates 10 have an inlet opening 12 leading into the channel-like recesses 8 and an outlet opening 14 leading out of the recesses.
  • two rod-shaped heat-conducting elements 11, 13 can be seen, which extend perpendicularly from metal jacket 9 into the refractory material and in the direction of the hot side 5 of the nozzle body 3.
  • the rod-shaped heat conducting elements 11, 13 are stepped, wherein the nozzle tube 19 nearer heat conducting element 13 is guided directly to the hot side 5 of the nozzle body 3 and further from the outer nozzle tube 19 remote heat conducting element 11 expires at a distance from the hot side 5 in the refractory material.
  • the heat-conducting elements 11, 13 are inserted into the metal jacket 9.
  • the heat-conducting element 17, 17.1, 17.2 branches over two branches 17.1, 17.2 in the direction of the hot side 5.
  • the branches 17.1, 17.2 end at a distance to the hot side 5 in the refractory material.
  • the branches 17.1, 17.2 are also stepped, the step height of closer to the outer nozzle tube 19 arranged branch 17.1 to further away from the outer nozzle tube 19 branch 17.2 decreases.
  • heat-conducting elements 15 in the form of a plurality of individual geometric bodies 15, which are dispersedly distributed in the refractory material, can be seen on the left-hand side in FIG. Through these bodies 15, the heat conductivity of the refractory material of the nozzle body 3 in the area in which the bodies 15 are distributed, is increased overall. The heat conduction does not take place - as with the heat-conducting elements 11, 13, 17, 17.1, 17.2 - directly to the metal shell 9 but also over several intermediate areas of the refractory material.
  • a homogeneous combination of heat-conducting elements is preferably used.
  • different embodiments of heat-conducting elements can be used homogeneously distributed around the outer nozzle tube 19.
  • ring-shaped arranged around the outer nozzle tube 19 graded heat conducting elements in the form of rods and / or trees and / or Platt s of disperse distributed over the refractory heat conduction elements in the form of individual body 15 may be surrounded.
  • the outer nozzle tube 19 is made of stainless steel and runs rotationally symmetrical to its longitudinal axis A, which is perpendicular to the hot side 5 and cold side 7 of the nozzle body 3.
  • an inner nozzle tube 21 Concentric with the outer nozzle tube 19, an inner nozzle tube 21 is arranged in stainless steel in this.
  • the longitudinal axis A of the inner nozzle tube 21 extends coaxially to the longitudinal axis A of the outer nozzle tube 19.
  • Outer nozzle tube 19 and inner nozzle tube 21 are spaced apart, so that between the two tubes 19, 21 an annular gap 23 is defined.
  • knob-like bulges (not shown) arranged to hold the inner nozzle tube 21 and the outer nozzle tube 19 at a constant distance from each other.
  • the inner nozzle tube 21 is rotated on the one hand about the longitudinal axis A and on the other hand simultaneously displaced along its longitudinal axis A in the direction of the hot side 5.
  • FIG. 2 shows the nozzle element 1 according to FIG. 1 in a plan view of the hot side 5.
  • each gas can be conducted, which is in a molten metal, which is on the hot side 5 in contact with the nozzle member 1, can be introduced.
  • heat-conducting elements 11, 13, 15, 17, 17.1, 17.2 as well as further heat-conducting elements can be seen in FIG. 2, which surround the outer nozzle tube 21 in an annular manner.
  • the function of the illustrated nozzle element is as follows: If the hot side 5 of the nozzle body 3 is in contact with a molten metal during a melting process, a cooling medium is introduced through the inlet opening 12 into the channel-like depressions 8 in the metal shell 9 and discharged again through the outlet opening 14. As a result, the heat-conducting elements 11, 13, 15, 17, 17.1, 17.2 received and forwarded to the metal shell 9. Heat are dissipated quickly from the metal shell 9. Because of this effective heat dissipation in the region of the hot side 5, solidification of the molten metal occurs in this region. This solidified molten metal forms a projection 27 on the hot side 5 of the nozzle body 3. The underlying refractory material of the nozzle body 3 is protected by this approach 27 from wear.
  • gas in the gap 23 and in the free cross section 21i of the inner nozzle tube 21 is inserted through the Gap 23 and the free inner 21i passed to the hot side 5 of the nozzle body 3 and injected there into the molten metal.

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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)
  • Waste-Gas Treatment And Other Accessory Devices For Furnaces (AREA)
  • Vertical, Hearth, Or Arc Furnaces (AREA)
  • Furnace Charging Or Discharging (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Treatment Of Steel In Its Molten State (AREA)
  • Furnace Details (AREA)
  • Vending Machines For Individual Products (AREA)
  • Nozzles (AREA)
  • Crystals, And After-Treatments Of Crystals (AREA)
  • Continuous Casting (AREA)

Claims (12)

  1. Elément à buse pour l'introduction de gaz dans un four industriel pour la fusion de métaux, comprenant les caractéristiques suivantes :
    a) un corps de buse (3) en matériau réfractaire;
    b) une chemise métallique (9) recouvrant le matériau réfractaire du côté froid (7) du corps de buse (3) ;
    c) des éléments conducteurs thermiques (11, 13, 17/17.2) qui sont du moins partiellement en contact avec la chemise métallique (9) et s'étendent vers l'intérieur du matériau réfractaire;
    d) la chemise métallique (9) est conçue de manière à pouvoir être refroidie par refroidissement au moyen d'un réfrigérant ;
    e) un tube de buse extérieur (19) qui s'étend à travers la chemise métallique (9) et le corps de buse (3) du côté froid (7) au côté chaud (5) du corps de buse (3).
  2. Elément à buse selon la revendication 1, dans lequel la chemise métallique (9) et les éléments conducteurs thermiques (11, 13, 15, 17.1, 17.2) sont composés du même matériau.
  3. Elément à buse selon la revendication 1, comportant une chemise métallique (9) et des éléments conducteurs thermiques (11, 13, 15, 17.1, 17.2) en cuivre ou en acier inoxydable.
  4. Elément à buse selon la revendication 1, dans lequel les éléments conducteurs thermiques (11, 13, 15, 17.1, 17.2) sont disposés sensiblement en forme d'anneau autour du tube de buse extérieur (19).
  5. Elément à buse selon la revendication 1, comportant des éléments conducteurs thermiques (11, 13, 15, 17.1, 17.2) sous forme de barres, traverses ou plaques.
  6. Elément à buse selon la revendication 1, comportant un dispositif par lequel un fluide peut être guidé sur la surface de la chemise métallique (9) ou à travers la chemise métallique (9).
  7. Elément à buse selon la revendication 6, comportant un système en forme de canal (8) pour guider le fluide.
  8. Elément à buse selon la revendication 1, comportant un tube de buse intérieur (21) disposé de manière à pouvoir se déplacer dans le tube de buse extérieur (19) le long de son axe longitudinal (A).
  9. Elément à buse selon la revendication 1, dans lequel le tube de buse intérieur (21) est disposé à distance du tube de buse extérieur (19) dans celui-ci.
  10. Elément à buse selon la revendication 9, dans lequel le tube de buse intérieur (21) et le tube de buse extérieur (19) sont maintenus à distance par des écarteurs.
  11. Elément à buse selon la revendication 1, dans lequel la surface circonférentielle extérieure du tube de buse intérieur (21) comporte un filetage qui s'engrène dans un taraudage pratiqué sur la surface tournée vers le tube de buse intérieur (21) du tube de buse extérieur (19).
  12. Four industriel dans la paroi extérieure duquel est disposé un élément à buse selon la revendication 1.
EP04790388A 2003-10-15 2004-10-14 Four industriel et buse associee Not-in-force EP1673481B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL04790388T PL1673481T3 (pl) 2003-10-15 2004-10-14 Piec przemysłowy i odpowiedni element dyszowy

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10347947A DE10347947B4 (de) 2003-10-15 2003-10-15 Industrieofen und zugehöriges Düsenelement
PCT/EP2004/011525 WO2005038372A2 (fr) 2003-10-15 2004-10-14 Four industriel et buse associee

Publications (2)

Publication Number Publication Date
EP1673481A2 EP1673481A2 (fr) 2006-06-28
EP1673481B1 true EP1673481B1 (fr) 2007-03-14

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Family Applications (1)

Application Number Title Priority Date Filing Date
EP04790388A Not-in-force EP1673481B1 (fr) 2003-10-15 2004-10-14 Four industriel et buse associee

Country Status (13)

Country Link
US (1) US7611663B2 (fr)
EP (1) EP1673481B1 (fr)
JP (1) JP4499725B2 (fr)
CN (1) CN100385017C (fr)
AT (1) ATE356889T1 (fr)
AU (1) AU2004282334B2 (fr)
BR (1) BRPI0415346B1 (fr)
CA (1) CA2538618C (fr)
DE (2) DE10347947B4 (fr)
ES (1) ES2282912T3 (fr)
MX (1) MXPA06003547A (fr)
PL (1) PL1673481T3 (fr)
WO (1) WO2005038372A2 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8212173B2 (en) * 2008-03-12 2012-07-03 Hypertherm, Inc. Liquid cooled shield for improved piercing performance
CN101462154B (zh) * 2008-11-28 2011-05-18 苏州明志科技有限公司 插入式热芯盒用水冷射嘴结构
US11305142B2 (en) * 2018-01-12 2022-04-19 Carrier Corporation End cap agent nozzle
JP7009245B2 (ja) * 2018-02-05 2022-01-25 パンパシフィック・カッパー株式会社 銅製錬転炉

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US2933259A (en) * 1958-03-03 1960-04-19 Jean F Raskin Nozzle head
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JPS58135456U (ja) * 1982-03-09 1983-09-12 住友金属工業株式会社 溶鋼内吹込みランス
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PL1673481T3 (pl) 2007-08-31
CA2538618A1 (fr) 2005-04-28
BRPI0415346B1 (pt) 2014-07-22
WO2005038372A3 (fr) 2005-11-03
DE10347947A1 (de) 2005-06-09
ES2282912T3 (es) 2007-10-16
AU2004282334B2 (en) 2007-03-22
DE502004003243D1 (de) 2007-04-26
EP1673481A2 (fr) 2006-06-28
DE10347947B4 (de) 2007-04-12
BRPI0415346A (pt) 2006-12-05
JP2007506063A (ja) 2007-03-15
WO2005038372A2 (fr) 2005-04-28
AU2004282334A1 (en) 2005-04-28
MXPA06003547A (es) 2006-06-05
CN100385017C (zh) 2008-04-30
US20060273500A1 (en) 2006-12-07
CA2538618C (fr) 2009-04-07
CN1867684A (zh) 2006-11-22
JP4499725B2 (ja) 2010-07-07
US7611663B2 (en) 2009-11-03
ATE356889T1 (de) 2007-04-15

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