EP1325161A1 - Blowing lance nozzle - Google Patents

Blowing lance nozzle

Info

Publication number
EP1325161A1
EP1325161A1 EP01969081A EP01969081A EP1325161A1 EP 1325161 A1 EP1325161 A1 EP 1325161A1 EP 01969081 A EP01969081 A EP 01969081A EP 01969081 A EP01969081 A EP 01969081A EP 1325161 A1 EP1325161 A1 EP 1325161A1
Authority
EP
European Patent Office
Prior art keywords
front wall
central
depression
lance
passage
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
Application number
EP01969081A
Other languages
German (de)
French (fr)
Other versions
EP1325161B1 (en
Inventor
Jacques Thomas
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.)
Individual
Original Assignee
Individual
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Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of EP1325161A1 publication Critical patent/EP1325161A1/en
Application granted granted Critical
Publication of EP1325161B1 publication Critical patent/EP1325161B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • 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
    • C21C5/00Manufacture of carbon-steel, e.g. plain mild steel, medium carbon steel or cast steel or stainless steel
    • C21C5/28Manufacture of steel in the converter
    • C21C5/42Constructional features of converters
    • C21C5/46Details or accessories
    • 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
    • C21C5/00Manufacture of carbon-steel, e.g. plain mild steel, medium carbon steel or cast steel or stainless steel
    • C21C5/28Manufacture of steel in the converter
    • C21C5/42Constructional features of converters
    • C21C5/46Details or accessories
    • C21C5/4606Lances or injectors

Definitions

  • the present invention relates to a blowing lance nose, intended for the mixing of baths, comprising a central tube for supplying mixing gas, closed at one end facing the bath by a first front wall provided with at least one opening, an internal tube forming with the central tube a first annular cavity for the passage of a coolant and closed at one end facing the bath by a second front wall having a central opening and an opening for passage provided in said first front wall, an external tube forming with the internal tube a second annular cavity for the passage of coolant and closed at one end facing the bath by a third front wall having an outlet orifice by opening provided in said first wall front, a heat exchange space which is located between, on the one hand, said second fron wall tale and said third front wall and, on the other hand, said central opening and said second annular cavity, and in which the coolant flows, and an outlet conduit for the stirring gas leaving each opening in said first front wall and going to a corresponding aforesaid outlet orifice passing through a said aforesaid or
  • blowing lance nose has been known for a long time.
  • the lance noses work at a distance from the bath of 1 to 2.5 m, while the bath has a temperature of the order of 1400 ° C.
  • the temperature of the nose can rapidly increase to 400 ° C., and must remain in this environment for approximately 20 minutes. Then, when the lance is removed, the nose quickly returns to room temperature, that is to say at 20 ° C.
  • the front walls of the lance noses in a very good conductive material of heat, for example copper, to allow a heat exchange as efficient as possible with a coolant which flows at high speed the along this wall, inside the nose.
  • the already known lance noses have the drawback of offering cooling which is not uniform over the entire surface of this wall exposed to variations in extremely critical thermal conditions. This results in mechanical tensions between the different zones of the wall.
  • cavitation phenomena are frequently observed in the coolant as a result of local depressions therein. This cavitation has the effect of causing poor cooling between the coolant and the wall to be cooled, the heat exchanges being much less good between a gas phase and a solid phase than between a liquid phase and a solid phase.
  • the object of the present invention is to provide a lance nose which is capable of undergoing the significant stresses to which it is subjected, during a significant number of successive uses, while providing a lance nose which is simple to manufacture and of defensible cost.
  • a blowing lance nose as described at the start, in which said third front wall has a central depression which is directed towards said central opening and which has a relationship between depression height and vacuum base equal to or greater than 0.35, and the aforementioned heat exchange space has a section for the passage of the coolant which is substantially constant, so as to obtain a speed of passage of the coolant through this space which is approximately constant, in the presence of said depression.
  • said central depression has a ratio between height and base equal to or greater than 0.4, in particular 0.5, and preferably even 0.8.
  • section for the passage of coolant it is meant that the intended sections are taken perpendicular to the direction of flow of the coolant in the heat exchange space. In this way, at constant flow, the flow / section ratio remains constant and therefore the speed of passage of the liquid also remains constant.
  • a speed of passage of the flow liquid will be provided between 8 and 12 m / sec.
  • the lance nose comprises several said passage conduits arranged around a central axis and in that said central depression extends from said outlet orifices of these conduits.
  • the base of the depression is thus advantageously maximum and allows an improved efficiency of the heat exchange in the depression.
  • the third front wall has an external diameter and the base of said depression is a circle having a diameter equal to at least 0.25 x said external diameter, preferably to at least 0.33 x this external diameter .
  • the central depression is thus according to the invention in no way a small central recess arranged in the wall of the nose to reinforce the rigidity of the latter.
  • said third front wall has a central depression in the shape of a cone.
  • said second front wall has, around the central opening, a central deformation in the form of a truncated cone, which is directed towards said first front wall.
  • said cone and said truncated cone have a common axis and the central depression in the form of a cone forms with this axis an angle greater than the angle formed between this axis and the central deformation in the form of a truncated cone.
  • the central depression is covered at least partially with a protective screen made of a material with high thermal resistance. It can be a disc-shaped plate which is carried by the central depression or pressed against it and which therefore does not require any welding for its fixing.
  • the heat exchange between the coolant and the third front wall remains unchanged, while a large part of the area of the third front wall is protected from excessive overheating.
  • Figure 1 shows an axial sectional view of a blowing lance nose according to the invention.
  • FIG. 2 shows an axial sectional view of an alternative embodiment.
  • FIG. 3 shows a detail of a lance nose according to the invention, to illustrate the method of measuring the parameters necessary for the invention.
  • FIG 1 there is shown a nose 1 of blowing lance.
  • This nose includes a central tube 2 for supplying stirring gas.
  • This central tube 2 is closed by a front wall 3 which, in the example illustrated, is provided with several openings 4.
  • An internal tube 5 is arranged coaxially around the central tube 2 and these tubes form between them an annular cavity 6 which, in the example illustrated, is used for the supply of cooling water in the direction of the arrow F ⁇ Ce inner tube 5 is closed by a front wall 7 which is called a separator.
  • This front wall 7 is provided with a central opening 8 and an orifice 9 in alignment with each opening 4 in the central tube 2.
  • An external tube 10 is arranged coaxially around the central tube 2.
  • This external tube is generally made of steel and it forms with the internal tube 5 an annular cavity 11 which, in the example illustrated, is used for the outlet of water from cooling in the direction of arrow F 2 .
  • This external tube 10 is closed by a front wall 12 which faces the brewing bath and which is therefore subjected to critical thermal stresses, as explained above.
  • this front wall is made of a material which is a good conductor of heat, for example copper, to allow a heat exchange as efficient as possible between the front wall 12 heated and the cooling water passing through the heat exchange space 13 which is located between the front wall 7 of the inner tube 5 and the front wall 12 of the outer tube 10.
  • the cooling water coming from the cavity 6 passes through the central opening 8 in the heat exchange zone 13. There it flows in the direction of the arrow F 3 towards the outside, that is to say towards the cavity 11.
  • the front wall 12 is also provided with an outlet orifice 14 in alignment with each opening 4 provided in the front wall 3 and with each through orifice 9 provided in the front wall 7.
  • an outlet conduit 15 for the ejection of stirring gas outside the lance nose.
  • These conduits are advantageously made of an erosion-resistant material, for example bronze, and are directed obliquely to the axis 19 of the lance nose.
  • the outer front wall 12 is, according to the invention, provided in its center with a depression 16 in the form of a cone, which is directed towards the central opening.
  • this depression is sufficiently pronounced to present a ratio between the height of the internal wall of the cone (h) and the base diameter (B) equal to or greater than 0.35. In the illustrated case this ratio is equal to approximately 0.5. In this way, the heat exchange zone 13 is greatly increased for the same heat front undergone by the lance nose, hence an increased efficiency of the cooling of the front wall 12. It is entirely advantageous, as shown , that this depression 16 extends from the outlet conduits 15 and therefore forms a cone whose base is maximum. In the example illustrated, the ratio between the base B of the depression and the external diameter D of the front wall 12 is approximately 0.33. In addition, by the deep depression, the central area of the front wall outer 12, which is the most stressed thermally, is separated as far as possible from the surface of the bath.
  • FIG. 3 illustrates how the parameters h and B of the lance nose according to the invention must be measured.
  • the height h is calculated between, on the one hand, the lower tangent plane 30 of the lance nose perpendicular to the axis 19 and the parallel plane 31 tangent to the top of the depression. If an element foreign to the depression is provided at the top thereof, such as for example the tie 20 in FIG. 2, the plane 31 remains in the position it would have if this foreign element did not exist. The summit of the depression must then be considered as a virtual point to be taken into account in the measurement.
  • the base B is located in the lower tangent plane 30. It is circumscribed by the line 32 resulting from the crossing between this plane 30 and the extension 33 of the internal faces 34 of the depression. Rounding is therefore not taken into account.
  • the outer diameter of the front wall 12 is taken where its value is maximum.
  • This deformation 17 has the shape of a truncated cone open towards the high through the central opening 8.
  • This truncated cone 17 is coaxial with the cone formed by the depression 16, their common axis being the axis 19 of the lance nose.
  • the cone of the depression 16 forms with the axis 19 an angle greater than the angle formed between this axis and the imaginary extension of the truncated cone 17 to this axis.
  • the truncated cone is narrower. So the section of the heat exchange space between the front walls 7 and 12, which is measured in a plane perpendicular to the direction of flow of the coolant, remains constant even in the presence of the central depression 16 provided in the embodiment illustrated in FIG. 1. Furthermore, at the outlet conduits 15, the coolant can only pass through the interstices situated circumferentially between these conduits in the heat exchange space 13. Consequently, to maintain a constant passage section for the liquid at this location cooling and therefore a constant passage speed at a given flow rate, an inward bulge 18 in the front wall 7 serving as a separator is provided in each of the aforementioned interstices.
  • the lance nose according to the invention is therefore arranged so as to provide over the entire extent of the heat exchange zone 13 a constant passage section for the coolant.
  • a ratio is obtained between this flow rate (d) and the section (S) which remains constant during the operation of the lance, this ratio corresponding to a speed of passage of the flow liquid expressed in m / sec.
  • the flow rate and the section will be determined to obtain an approximately constant speed of passage of between 8 and 12 m / sec. The cavitation phenomenon can thus be avoided as much as possible, which greatly improves the efficiency of the heat exchange obtained in the nose.
  • a lance nose which differs from that shown in Figure 1 in that the depression 16 is more pronounced.
  • the top of the depression 16 projects through the opening 8 and therefore even opens into the space between the front walls 3 and 7, which makes it possible to obtain a ratio between h and B equal to or greater than 0.8.
  • a retaining element can be provided, for example a tie rod 20, between the top of the depression and a nut arranged on or in the front wall 3 of the central tube 2.
  • the depression central 16 is, in this embodiment, completely covered by a thermally resistant plate 21. In this way, while allowing an unchanged heat exchange between the cooling water and the cone formed by the depression 16, the central part of the lance nose is thermally insulated from the heat of the bath, which reinforces the efficiency of the heat exchange and allows a longer life of the lance nose.
  • the plate 21 is composite, that is to say that it has an outer layer of a refractory material, for example ceramic, or of refractory steel and an inner layer in a thermally insulating material, such as for example fibrous alumina.
  • a refractory material for example ceramic
  • a thermally insulating material such as for example fibrous alumina
  • this plate is simply clamped between the head 22 of a threaded rod 23 passing through the plate 21 and screwed into a thread provided in the head of the tie rod 20.
  • Other methods of fixing this plate could of course be planned.
  • the lifespan of a nose is calculated on the number of flows that could have been brewed before having to discard that nose. As can be seen from this table, the improvement in the average lifespan of the noses according to the invention is remarkable and completely unexpected.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Carbon Steel Or Casting Steel Manufacturing (AREA)
  • Treatment Of Steel In Its Molten State (AREA)
  • Furnace Charging Or Discharging (AREA)
  • Nozzles (AREA)
  • Furnace Housings, Linings, Walls, And Ceilings (AREA)
  • Furnace Details (AREA)
  • Heterocyclic Carbon Compounds Containing A Hetero Ring Having Oxygen Or Sulfur (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Low-Molecular Organic Synthesis Reactions Using Catalysts (AREA)

Abstract

A blowing lance nozzle (1) having: a central tube (2) supplying stirring gas, an inner tube (5) for intake of a cooling liquid, an outer tube (10) for evacuation of the cooling liquid, a heat exchanging space (13), and an outlet conduit (15) for the stirring gas exiting from each orifice (4) in the front wall (3). The front wall (12) has a central recess (16) which is oriented towards the central orifice (8) and has a recess height/recess base ratio not less than 0.35. The heat exchanging space has a section for allowing passage of the cooling liquid through the space at a speed which is substantially constant, so as to obtain a cooling liquid passage speed, through the space, which is more or less constant.

Description

"Nez de lance de soufflage". "Blowing lance nose".
La présente invention est relative à un nez de lance de soufflage, destinée au brassage de bains, comprenant un tube central d'alimentation en gaz de brassage, fermé à une extrémité tournée vers le bain par une première paroi frontale pourvue d'au moins une ouverture, un tube interne formant avec le tube central une première cavité annulaire pour le passage d'un liquide de refroidissement et fermé à une extrémité tournée vers le bain par une deuxième paroi frontale présentant une ouverture centrale et un orifice de passage par ouverture prévue dans ladite première paroi frontale, un tube externe formant avec le tube interne une deuxième cavité annulaire pour le passage du liquide de refroidissement et fermé à une extrémité tournée vers le bain par une troisième paroi frontale présentant un orifice de sortie par ouverture prévue dans ladite première paroi frontale, un espace d'échange thermique qui est situé entre, d'une part, ladite deuxième paroi frontale et ladite troisième paroi frontale et, d'autre part, ladite ouverture centrale et ladite deuxième cavité annulaire, et dans lequel s'écoule le liquide de refroidissement, et un conduit de sortie pour le gaz de brassage partant de chaque ouverture dans ladite première paroi frontale et allant jusqu'à un orifice de sortie susdit correspondant en passant par un orifice de passage susdit correspondant d'une manière étanche au liquide de refroidissement. On connaît depuis longtemps des nez de lance de soufflage de ce genre. On peut citer à titre d'exemples les nez de lance de soufflage décrits dans la EP-A-0 340207, la WO-97/000973, et le US- A-4.432.534. Pour brasser avec des jets d'oxygène des bains de convertisseurs d'aciérie, les nez de lance travaillent à une distance du bain de 1 à 2,5 m, alors que le bain présente une température de l'ordre de 1400°C. Dans ces conditions opératoires, la température du nez peut croître rapidement à 400°C, et devoir rester dans cet environnement pendant environ 20 minutes. Ensuite, lorsque la lance est retirée, le nez retourne rapidement à la température ambiante, c'est-à-dire à 20°C.The present invention relates to a blowing lance nose, intended for the mixing of baths, comprising a central tube for supplying mixing gas, closed at one end facing the bath by a first front wall provided with at least one opening, an internal tube forming with the central tube a first annular cavity for the passage of a coolant and closed at one end facing the bath by a second front wall having a central opening and an opening for passage provided in said first front wall, an external tube forming with the internal tube a second annular cavity for the passage of coolant and closed at one end facing the bath by a third front wall having an outlet orifice by opening provided in said first wall front, a heat exchange space which is located between, on the one hand, said second fron wall tale and said third front wall and, on the other hand, said central opening and said second annular cavity, and in which the coolant flows, and an outlet conduit for the stirring gas leaving each opening in said first front wall and going to a corresponding aforesaid outlet orifice passing through a said aforesaid orifice in a sealed manner to the coolant. This type of blowing lance nose has been known for a long time. By way of example, mention may be made of the blowing lance noses described in EP-A-0 340207, WO-97/000973, and US-A-4,432,534. To brew with oxygen jets baths of steel converters, the lance noses work at a distance from the bath of 1 to 2.5 m, while the bath has a temperature of the order of 1400 ° C. Under these operating conditions, the temperature of the nose can rapidly increase to 400 ° C., and must remain in this environment for approximately 20 minutes. Then, when the lance is removed, the nose quickly returns to room temperature, that is to say at 20 ° C.
Il est donc prévu de construire les parois frontales des nez de lance en une matière très bonne conductrice de la chaleur, par exemple en cuivre, pour permettre un échange thermique aussi efficace que possible avec un liquide de refroidissement qui s'écoule à grande vitesse le long de cette paroi, à l'intérieur du nez. Toutefois, les nez de lance déjà connus présentent l'inconvénient d'offrir un refroidissement qui n'est pas uniforme sur toute la surface de cette paroi exposée à des variations de conditions thermiques extrêmement critiques. Il en résulte des tensions mécaniques entre les différentes zones de la paroi.It is therefore planned to build the front walls of the lance noses in a very good conductive material of heat, for example copper, to allow a heat exchange as efficient as possible with a coolant which flows at high speed the along this wall, inside the nose. However, the already known lance noses have the drawback of offering cooling which is not uniform over the entire surface of this wall exposed to variations in extremely critical thermal conditions. This results in mechanical tensions between the different zones of the wall.
Par ailleurs, on observe fréquemment des phénomènes de cavitation dans le liquide de refroidissement par suite de dépressions locales dans celui-ci. Cette cavitation a pour effet d'engendrer un mauvais refroidissement entre le liquide de refroidissement et la paroi à refroidir, les échanges thermiques étant beaucoup moins bons entre une phase gazeuse et une phase solide qu'entre une phase liquide et une phase solide.In addition, cavitation phenomena are frequently observed in the coolant as a result of local depressions therein. This cavitation has the effect of causing poor cooling between the coolant and the wall to be cooled, the heat exchanges being much less good between a gas phase and a solid phase than between a liquid phase and a solid phase.
De nombreuses tentatives ont été effectuées pour adoucir l'écoulement du liquide de refroidissement à l'intérieur du nez de lance, par exemple en pratiquant de légères dépressions dans la paroi frontale externe du nez (voir par exemple US-A-4.432.534 et WO 96/23082). Ces agencements présentent toutefois l'inconvénient de ne pas offrir une surface d'échange thermique suffisante, en particulier dans la zone centrale du nez. II est par ailleurs prévu, dans la zone centrale du nez de lance décrit dans la EP-A-0340207, une dépression importante sur laquelle sont dirigés des jets secondaires de liquide de refroidissement, ce qui a pour effet de provoquer un tourbillonnement dans l'écoulement du liquide. La présente invention a pour but de proposer un nez de lance qui soit capable de subir les sollicitations importantes auxquelles il est soumis, pendant un nombre significatif d'utilisations successives, tout en fournissant un nez de lance simple à fabriquer et de coût défendable.Many attempts have been made to soften the flow of coolant inside the lance nose, for example by making slight depressions in the front wall external of the nose (see for example US-A-4,432,534 and WO 96/23082). However, these arrangements have the disadvantage of not providing a sufficient heat exchange surface, in particular in the central region of the nose. It is also provided, in the central area of the lance nose described in EP-A-0340207, a significant depression on which are directed secondary jets of coolant, which has the effect of causing a swirl in the liquid flow. The object of the present invention is to provide a lance nose which is capable of undergoing the significant stresses to which it is subjected, during a significant number of successive uses, while providing a lance nose which is simple to manufacture and of defensible cost.
On résout ce problème, suivant l'invention, par un nez de lance de soufflage, tel que décrit au début, dans lequel ladite troisième paroi frontale présente une dépression centrale qui est dirigée vers ladite ouverture centrale et qui présente un rapport entre hauteur de dépression et base de dépression égal ou supérieur à 0,35, et l'espace d'échange thermique susdit présente une section pour le passage du liquide de refroidissement qui est sensiblement constante, de manière à obtenir une vitesse de passage du liquide de refroidissement à travers cet espace qui soit approximativement constante, en présence de ladite dépression.This problem is solved, according to the invention, by a blowing lance nose, as described at the start, in which said third front wall has a central depression which is directed towards said central opening and which has a relationship between depression height and vacuum base equal to or greater than 0.35, and the aforementioned heat exchange space has a section for the passage of the coolant which is substantially constant, so as to obtain a speed of passage of the coolant through this space which is approximately constant, in the presence of said depression.
Par une telle dépression, la surface d'échange thermique augmente fortement par rapport à une même surface du front de chaleur provenant du bain, et cela sans entraîner ni tourbillonnement, ni cavitation dans le liquide. Avantageusement, ladite dépression centrale présente un rapport entre hauteur et base égal ou supérieur à 0,4, en particulier à 0,5, et préférentiellement même à 0,8. Par l'expression "section pour le passage de liquide de refroidissement", il faut entendre que les sections visées sont prises perpendiculairement au sens d'écoulement du liquide de refroidissement dans l'espace d'échange thermique. De cette manière, à débit constant, le rapport débit/section reste constant et donc la vitesse de passage du liquide reste également constante. On peut ainsi assurer qu'à une vitesse de passage donnée, et à la température critique de la paroi frontale à refroidir, aucun phénomène de cavitation ne risque de se produire dans le liquide de refroidissement, lequel d'une manière générale est de l'eau. Avantageusement, pour les températures de paroi frontale indiquées plus haut on prévoira une vitesse de passage du liquide d'écoulement comprise entre 8 et 12 m/sec.By such a depression, the heat exchange surface greatly increases with respect to the same surface of the heat front coming from the bath, and this without causing either swirling or cavitation in the liquid. Advantageously, said central depression has a ratio between height and base equal to or greater than 0.4, in particular 0.5, and preferably even 0.8. By the expression "section for the passage of coolant", it is meant that the intended sections are taken perpendicular to the direction of flow of the coolant in the heat exchange space. In this way, at constant flow, the flow / section ratio remains constant and therefore the speed of passage of the liquid also remains constant. It can thus be ensured that at a given speed of passage, and at the critical temperature of the front wall to be cooled, no cavitation phenomenon is likely to occur in the coolant, which in general is of the water. Advantageously, for the front wall temperatures indicated above, a speed of passage of the flow liquid will be provided between 8 and 12 m / sec.
Par section sensiblement constante, il faut entendre, suivant l'invention, que la superficie de cette section ne puisse pas varier dans des limites supérieures à 10 %.By substantially constant section, it should be understood, according to the invention, that the area of this section cannot vary within limits greater than 10%.
Suivant une forme de réalisation de l'invention, le nez de lance comprend plusieurs conduits de passage susdits disposés autour d'un axe central et en ce que ladite dépression centrale s'étend depuis lesdits orifices de sortie de ces conduits. La base de la dépression est ainsi avantageusement maximale et permet une efficacité améliorée de l'échange thermique dans la dépression. D'une manière perfectionnée, la troisième paroi frontale présente un diamètre externe et la base de ladite dépression est un cercle présentant un diamètre égal à au moins 0,25 x ledit diamètre externe, de préférence à au moins 0,33 x ce diamètre externe. La dépression centrale n'est ainsi suivant l'invention en aucune façon un petit renfoncement central aménagé dans la paroi du nez pour renforcer la rigidité de celui-ci. Suivant une forme de réalisation avantageuse de l'invention, ladite troisième paroi frontale présente une dépression centrale en forme de cône.According to one embodiment of the invention, the lance nose comprises several said passage conduits arranged around a central axis and in that said central depression extends from said outlet orifices of these conduits. The base of the depression is thus advantageously maximum and allows an improved efficiency of the heat exchange in the depression. In an improved manner, the third front wall has an external diameter and the base of said depression is a circle having a diameter equal to at least 0.25 x said external diameter, preferably to at least 0.33 x this external diameter . The central depression is thus according to the invention in no way a small central recess arranged in the wall of the nose to reinforce the rigidity of the latter. According to an advantageous embodiment of the invention, said third front wall has a central depression in the shape of a cone.
Suivant une forme perfectionnée de réalisation de l'invention, ladite deuxième paroi frontale présente, autour de l'ouverture centrale, une déformation centrale en forme de tronc de cône, qui est dirigée vers ladite première paroi frontale. De préférence, ledit cône et ledit tronc de cône ont un axe commun et la dépression centrale en forme de cône forme avec cet axe un angle supérieur à l'angle formé entre cet axe et la déformation centrale en forme de tronc de cône. De cette manière, même dans l'espace d'échange thermique situé entre la dépression centrale de la troisième paroi frontale et la déformation centrale de la deuxième paroi frontale, la section peut rester constante et la vitesse de passage du liquide d'écoulement reste là aussi équivalente à celle obtenue le long de toute la troisième paroi frontale.According to an improved embodiment of the invention, said second front wall has, around the central opening, a central deformation in the form of a truncated cone, which is directed towards said first front wall. Preferably, said cone and said truncated cone have a common axis and the central depression in the form of a cone forms with this axis an angle greater than the angle formed between this axis and the central deformation in the form of a truncated cone. In this way, even in the heat exchange space located between the central depression of the third front wall and the central deformation of the second front wall, the section can remain constant and the speed of passage of the flow liquid remains there. also equivalent to that obtained along the entire third front wall.
Suivant une forme de réalisation particulière de l'invention, la dépression centrale est couverte au moins partiellement d'un écran protecteur en un matériau à haute résistance thermique. Il peut s'agir d'une plaque en forme de disque qui est portée par la dépression centrale ou serrée contre elle et qui ne nécessite donc aucun soudage pour sa fixation. L'échange thermique entre le liquide de refroidissement et la troisième paroi frontale reste inchangé, tandis qu'une grande partie de la superficie de la troisième paroi frontale est à l'abri d'une surchauffe excessive. D'autres formes de réalisation du nez de lance suivant l'invention sont indiquées dans les revendications annexées.According to a particular embodiment of the invention, the central depression is covered at least partially with a protective screen made of a material with high thermal resistance. It can be a disc-shaped plate which is carried by the central depression or pressed against it and which therefore does not require any welding for its fixing. The heat exchange between the coolant and the third front wall remains unchanged, while a large part of the area of the third front wall is protected from excessive overheating. Other embodiments of the lance nose according to the invention are indicated in the appended claims.
D'autres détails et particularités de l'invention ressortiront de la description donnée ci-après, à titre non limitatif, d'exemples de réalisation de l'invention, et en faisant référence aux dessins annexés. La figure 1 représente une vue en coupe axiale d'un nez de lance de soufflage suivant l'invention.Other details and particularities of the invention will emerge from the description given below, without implied limitation, of embodiments of the invention, and with reference to the attached drawings. Figure 1 shows an axial sectional view of a blowing lance nose according to the invention.
La figure 2 représente une vue en coupe axiale d'une variante de réalisation. La figure 3 représente un détail d'un nez de lance suivant l'invention, pour illustrer le mode de mesure des paramètres nécessaires à l'invention.Figure 2 shows an axial sectional view of an alternative embodiment. FIG. 3 shows a detail of a lance nose according to the invention, to illustrate the method of measuring the parameters necessary for the invention.
Sur les différents dessins, les éléments identiques ou analogues sont désignés par les mêmes références. Sur la figure 1, on a représenté un nez 1 de lance de soufflage. Ce nez comprend un tube central 2 pour l'alimentation en gaz de brassage. Ce tube central 2 est fermé par une paroi frontale 3 qui, dans l'exemple illustré, est pourvue de plusieurs ouvertures 4.In the various drawings, identical or analogous elements are designated by the same references. In Figure 1, there is shown a nose 1 of blowing lance. This nose includes a central tube 2 for supplying stirring gas. This central tube 2 is closed by a front wall 3 which, in the example illustrated, is provided with several openings 4.
Un tube interne 5 est agencé de manière coaxiale autour du tube central 2 et ces tubes forment entre eux une cavité annulaire 6 qui, dans l'exemple illustré, sert à l'alimentation en eau de refroidissement dans le sens de la flèche F^ Ce tube interne 5 est fermé par une paroi frontale 7 que l'on appelle un séparateur. Cette paroi frontale 7 est pourvue d'une ouverture centrale 8 et d'un orifice 9 dans l'alignement de chaque ouverture 4 dans le tube central 2.An internal tube 5 is arranged coaxially around the central tube 2 and these tubes form between them an annular cavity 6 which, in the example illustrated, is used for the supply of cooling water in the direction of the arrow F ^ Ce inner tube 5 is closed by a front wall 7 which is called a separator. This front wall 7 is provided with a central opening 8 and an orifice 9 in alignment with each opening 4 in the central tube 2.
Un tube externe 10 est agencé de manière coaxiale autour du tube central 2. Ce tube externe est généralement en acier et il forme avec le tube interne 5 une cavité annulaire 11 qui, dans l'exemple illustré, sert à la sortie d'eau de refroidissement dans le sens de la flèche F2. Ce tube externe 10 est fermé par une paroi frontale 12 qui fait face au bain à brasser et qui est donc soumise à des sollicitations thermiques critiques, comme expliqué plus haut. Avantageusement, cette paroi frontale est en une matière bonne conductrice de la chaleur, par exemple en cuivre, pour permettre un échange thermique aussi efficace que possible entre la paroi frontale 12 chauffée et l'eau de refroidissement passant dans l'espace d'échange thermique 13 qui est situé entre la paroi frontale 7 du tube interne 5 et la paroi frontale 12 du tube externe 10. Dans l'exemple de réalisation illustré, l'eau de refroidissement venant de la cavité 6 passe par l'ouverture centrale 8 dans la zone d'échange thermique 13. Là elle s'écoule dans le sens'de la flèche F3 vers l'extérieur, c'est-à-dire vers la cavité 11.An external tube 10 is arranged coaxially around the central tube 2. This external tube is generally made of steel and it forms with the internal tube 5 an annular cavity 11 which, in the example illustrated, is used for the outlet of water from cooling in the direction of arrow F 2 . This external tube 10 is closed by a front wall 12 which faces the brewing bath and which is therefore subjected to critical thermal stresses, as explained above. Advantageously, this front wall is made of a material which is a good conductor of heat, for example copper, to allow a heat exchange as efficient as possible between the front wall 12 heated and the cooling water passing through the heat exchange space 13 which is located between the front wall 7 of the inner tube 5 and the front wall 12 of the outer tube 10. In the illustrated embodiment, the cooling water coming from the cavity 6 passes through the central opening 8 in the heat exchange zone 13. There it flows in the direction of the arrow F 3 towards the outside, that is to say towards the cavity 11.
La paroi frontale 12 est aussi pourvue d'un orifice de sortie 14 en alignement avec chaque ouverture 4 prévue dans la paroi frontale 3 et avec chaque orifice de passage 9 prévu dans la paroi frontale 7. Dans chacun de ces orifices et ouvertures alignés est agencé un conduit de sortie 15 pour l'éjection de gaz de brassage à l'extérieur du nez de lance. Ces conduits sont avantageusement réalisés en une matière résistant à l'érosion, par exemple en bronze, et sont dirigés en oblique par rapport à l'axe 19 du nez de lance. Ainsi qu'il ressort de l'exemple de réalisation illustré, la paroi frontale extérieure 12 est, suivant l'invention, pourvue en son centre d'une dépression 16 en forme de cône, qui est dirigée vers l'ouverture centrale. De préférence cette dépression est suffisamment prononcée pour présenter un rapport entre hauteur de la paroi interne du cône (h) et diamètre de base (B) égal ou supérieur à 0,35. Dans le cas illustré ce rapport est égal à environ 0,5. De cette manière, la zone d'échange thermique 13 est grandement augmentée pour un même front de chaleur subi par le nez de lance, d'où une efficacité augmentée du refroidissement de la paroi frontale 12. Il est tout à fait avantageux, comme représenté, que cette dépression 16 s'étende depuis les conduits de sortie 15 et forme donc un cône dont la base soit maximale. Dans l'exemple illustré, le rapport entre la base B de la dépression et le diamètre externe D de la paroi frontale 12 est d'environ 0,33. Par ailleurs, par la dépression profonde, la zone centrale de la paroi frontale extérieure 12, qui est thermiquement la plus sollicitée, est écartée au maximum de la surface du bain.The front wall 12 is also provided with an outlet orifice 14 in alignment with each opening 4 provided in the front wall 3 and with each through orifice 9 provided in the front wall 7. In each of these aligned orifices and openings is arranged an outlet conduit 15 for the ejection of stirring gas outside the lance nose. These conduits are advantageously made of an erosion-resistant material, for example bronze, and are directed obliquely to the axis 19 of the lance nose. As is apparent from the illustrated embodiment, the outer front wall 12 is, according to the invention, provided in its center with a depression 16 in the form of a cone, which is directed towards the central opening. Preferably, this depression is sufficiently pronounced to present a ratio between the height of the internal wall of the cone (h) and the base diameter (B) equal to or greater than 0.35. In the illustrated case this ratio is equal to approximately 0.5. In this way, the heat exchange zone 13 is greatly increased for the same heat front undergone by the lance nose, hence an increased efficiency of the cooling of the front wall 12. It is entirely advantageous, as shown , that this depression 16 extends from the outlet conduits 15 and therefore forms a cone whose base is maximum. In the example illustrated, the ratio between the base B of the depression and the external diameter D of the front wall 12 is approximately 0.33. In addition, by the deep depression, the central area of the front wall outer 12, which is the most stressed thermally, is separated as far as possible from the surface of the bath.
La figure 3 illustre comment il faut mesurer les paramètres h et B du nez de lance suivant l'invention. La hauteur h se calcule entre, d'une part, le plan tangent inférieur 30 du nez de lance perpendiculaire à l'axe 19 et le plan parallèle 31 tangent au sommet de la dépression. Si un élément étranger à la dépression est prévu au sommet de celle-ci, comme par exemple le tirant 20 sur la figure 2, le plan 31 reste dans la position qu'il aurait si cet élément étranger n'existait pas. Le sommet de la dépression doit être alors considéré comme un point virtuel à prendre en compte dans la mesure.FIG. 3 illustrates how the parameters h and B of the lance nose according to the invention must be measured. The height h is calculated between, on the one hand, the lower tangent plane 30 of the lance nose perpendicular to the axis 19 and the parallel plane 31 tangent to the top of the depression. If an element foreign to the depression is provided at the top thereof, such as for example the tie 20 in FIG. 2, the plane 31 remains in the position it would have if this foreign element did not exist. The summit of the depression must then be considered as a virtual point to be taken into account in the measurement.
La base B est située dans le plan tangent inférieur 30. Elle est circonscrite par la ligne 32 résultant du croisement entre ce plan 30 et le prolongement 33 des faces internes 34 de la dépression. On ne tient donc pas compte des arrondis.The base B is located in the lower tangent plane 30. It is circumscribed by the line 32 resulting from the crossing between this plane 30 and the extension 33 of the internal faces 34 of the depression. Rounding is therefore not taken into account.
Ainsi qu'on peut le voir sur la figure 1 , le diamètre externe de la paroi frontale 12 est pris là où sa valeur est maximale.As can be seen in Figure 1, the outer diameter of the front wall 12 is taken where its value is maximum.
La paroi frontale 7, servant de séparateur entre l'alimen- tation en eau et la sortie d'eau, présente elle aussi une déformation centrale 17 dirigée vers la paroi frontale 3. Cette déformation 17 a une forme de tronc de cône ouvert vers le haut par l'ouverture centrale 8.The front wall 7, serving as a separator between the water supply and the water outlet, also has a central deformation 17 directed towards the front wall 3. This deformation 17 has the shape of a truncated cone open towards the high through the central opening 8.
Ce tronc de cône 17 est coaxial au cône formé par la dépression 16, leur axe commun étant l'axe 19 du nez de lance. Le cône de la dépression 16 forme avec l'axe 19 un angle supérieur à l'angle formé entre cet axe et la prolongation imaginaire du tronc de cône 17 jusqu'à cet axe.This truncated cone 17 is coaxial with the cone formed by the depression 16, their common axis being the axis 19 of the lance nose. The cone of the depression 16 forms with the axis 19 an angle greater than the angle formed between this axis and the imaginary extension of the truncated cone 17 to this axis.
Il en résulte que le tronc de cône 17 est plus écarté du côneAs a result, the truncated cone 17 is further away from the cone
16 à son sommet qu'à sa base. Or, à son sommet, le tronc de cône est plus étroit. Donc, la section de l'espace d'échange thermique situé entre les parois frontales 7 et 12, qui est mesurée dans un plan perpendiculaire au sens d'écoulement du liquide de refroidissement, reste constante même en présence de la dépression centrale 16 prévue dans l'exemple de réalisation illustré sur la figure 1. Par ailleurs, au niveau des conduits de sortie 15, le liquide de refroidissement ne peut passer que dans les interstices situés circonférentiellement entre ces conduits dans l'espace d'échange thermique 13. Par conséquent, pour maintenir à cet endroit une section de passage constante pour le liquide de refroidissement et donc une vitesse de passage constante à un débit donné, un renflement vers l'intérieur 18 dans la paroi frontale 7 servant de séparateur est prévu dans chacun des interstices susdits.16 at its top than at its base. However, at its top, the truncated cone is narrower. So the section of the heat exchange space between the front walls 7 and 12, which is measured in a plane perpendicular to the direction of flow of the coolant, remains constant even in the presence of the central depression 16 provided in the embodiment illustrated in FIG. 1. Furthermore, at the outlet conduits 15, the coolant can only pass through the interstices situated circumferentially between these conduits in the heat exchange space 13. Consequently, to maintain a constant passage section for the liquid at this location cooling and therefore a constant passage speed at a given flow rate, an inward bulge 18 in the front wall 7 serving as a separator is provided in each of the aforementioned interstices.
Le nez de lance suivant l'invention est donc agencé de façon à prévoir sur toute l'étendue de la zone d'échange thermique 13 une section de passage constante pour le liquide de refroidissement. A un débit déterminé de l'alimentation en eau on obtient un rapport entre ce débit (d) et la section (S) qui reste constant pendant le fonctionnement de la lance, ce rapport correspondant à une vitesse de passage du liquide d'écoulement exprimée en m/sec. Avantageusement, le débit et la section seront déterminés pour obtenir une vitesse de passage approximativement constante et comprise entre 8 et 12 m/sec. Le phénomène de la cavitation peut ainsi être évité au maximum ce qui améliore grandement l'efficacité de l'échange thermique obtenu dans le nez. Dans l'exemple de réalisation illustré sur la figure 2, on a représenté un nez de lance qui se différencie de celui représenté sur la figure 1 par le fait que la dépression 16 est plus prononcée. Le sommet de la dépression 16 fait saillie à travers l'ouverture 8 et débouche donc même dans l'espace entre les parois frontales 3 et 7, ce qui permet d'obtenir un rapport entre h et B égal ou supérieur à 0,8. Pour mieux assurer la résistance mécanique de la dépression 16, on peut prévoir un élément de retenue, par exemple un tirant 20, entre le sommet de la dépression et un écrou agencé sur ou dans la paroi frontale 3 du tube central 2. Par ailleurs, la dépression centrale 16 est, dans cet exemple de réalisation, totalement couverte par une plaque 21 thermiquement résistante. De cette manière, tout en permettant un échange thermique inchangé entre l'eau de refroidissement et le cône formé par la dépression 16, la partie centrale du nez de lance est thermiquement isolée de la chaleur du bain, ce qui renforce l'efficacité de l'échange thermique et permet une plus longue durée de vie du nez de lance.The lance nose according to the invention is therefore arranged so as to provide over the entire extent of the heat exchange zone 13 a constant passage section for the coolant. At a determined flow rate of the water supply, a ratio is obtained between this flow rate (d) and the section (S) which remains constant during the operation of the lance, this ratio corresponding to a speed of passage of the flow liquid expressed in m / sec. Advantageously, the flow rate and the section will be determined to obtain an approximately constant speed of passage of between 8 and 12 m / sec. The cavitation phenomenon can thus be avoided as much as possible, which greatly improves the efficiency of the heat exchange obtained in the nose. In the embodiment illustrated in Figure 2, there is shown a lance nose which differs from that shown in Figure 1 in that the depression 16 is more pronounced. The top of the depression 16 projects through the opening 8 and therefore even opens into the space between the front walls 3 and 7, which makes it possible to obtain a ratio between h and B equal to or greater than 0.8. For better ensuring the mechanical resistance of the depression 16, a retaining element can be provided, for example a tie rod 20, between the top of the depression and a nut arranged on or in the front wall 3 of the central tube 2. Furthermore, the depression central 16 is, in this embodiment, completely covered by a thermally resistant plate 21. In this way, while allowing an unchanged heat exchange between the cooling water and the cone formed by the depression 16, the central part of the lance nose is thermally insulated from the heat of the bath, which reinforces the efficiency of the heat exchange and allows a longer life of the lance nose.
Dans l'exemple de réalisation illustré sur la figure 2, la plaque 21 est composite, c'est-à-dire qu'elle présente une couche externe en une matière réfractaire, par exemple en céramique, ou en acier réfractaire et une couche interne en une matière thermiquement isolante, comme par exemple l'alumine fibreuse.In the embodiment illustrated in FIG. 2, the plate 21 is composite, that is to say that it has an outer layer of a refractory material, for example ceramic, or of refractory steel and an inner layer in a thermally insulating material, such as for example fibrous alumina.
Dans l'exemple illustré, cette plaque est simplement serrée entre la tête 22 d'une tige filetée 23 traversant la plaque 21 et vissée dans un filetage prévu dans la tête du tirant 20. D'autres modes de fixation de cette plaque pourraient bien entendu être prévus.In the example illustrated, this plate is simply clamped between the head 22 of a threaded rod 23 passing through the plate 21 and screwed into a thread provided in the head of the tie rod 20. Other methods of fixing this plate could of course be planned.
Des essais comparatifs ont été réalisés dans les mêmes conditions dans des bains d'une aciérie.Comparative tests were carried out under the same conditions in baths of a steelworks.
Les essais ont été effectués avec des nez conventionnels de 3 firmes concurrentes (essais I à III sur le tableau ci-dessous), des nez fabriqués par la demanderesse avec une légère dépression centrale dont le rapport h/B = 0,15 et le rapport D/B = 0,15 (essai IV) et des nez suivant l'invention dont le rapport h/B = 0,44 et le rapport D/B = 0,30 (essai V). TableauThe tests were carried out with conventional noses from 3 competing firms (tests I to III in the table below), noses manufactured by the applicant with a slight central depression whose h / B ratio = 0.15 and the ratio D / B = 0.15 (test IV) and noses according to the invention, the h / B ratio = 0.44 and the D / B ratio = 0.30 (test V). Board
La durée de vie d'un nez est calculée sur le nombre de coulées qui ont pu être brassées avant de devoir mettre ce nez au rebut. Comme on peut le voir de ce tableau, l'amélioration de la durée moyenne de vie des nez suivant l'invention est remarquable et totalement inattendue.The lifespan of a nose is calculated on the number of flows that could have been brewed before having to discard that nose. As can be seen from this table, the improvement in the average lifespan of the noses according to the invention is remarkable and completely unexpected.
Il doit être entendu que la présente invention n'est en aucune façon limitée aux modes de réalisation décrits ci-dessus et que bien des modifications peuvent y être apportées sans sortir du cadre des revendications annexées. It should be understood that the present invention is in no way limited to the embodiments described above and that many modifications can be made thereto without departing from the scope of the appended claims.

Claims

REVENDICATIONS
1. Nez (1) de lance de soufflage, destinée au brassage de bains, comprenant : un tube central (2) d'alimentation en gaz de brassage, fermé à une extrémité tournée vers le bain par une première paroi frontale (3) pourvue d'au moins une ouverture (4), un tube interne (5) formant avec le tube central une première cavité annulaire (6) pour le passage d'un liquide de refroidissement et fermé à une extrémité tournée vers le bain par une deuxième paroi frontale (7) présentant une ouverture centrale (8) et un orifice de passage (9) par ouverture (4) prévue dans ladite première paroi frontale (3), un tube externe (10) formant avec le tube interne (5) une deuxième cavité annulaire (11) pour le passage du liquide de refroidissement et fermé à une extrémité tournée vers le bain par une troisième paroi frontale (12) présentant un orifice de sortie (14) par ouverture (4) prévue dans ladite première paroi frontale (3) , un espace d'échange thermique (13) qui est situé entre, d'une part, ladite deuxième paroi frontale (7) et ladite troisième paroi frontale (12) et, d'autre part, ladite ouverture centrale (8) et ladite deuxième cavité annulaire (11), et dans lequel s'écoule le liquide de refroidissement, et un conduit de sortie (15) pour le gaz de brassage partant de chaque ouverture (4) dans ladite première paroi frontale (3) et allant jusqu'à un orifice de sortie (14) susdit correspondant en passant par un orifice de passage (9) susdit correspondant d'une manière étanche au liquide de refroidissement, caractérisé en ce que ladite troisième paroi frontale (12) présente une dépression centrale (16) qui est dirigée vers ladite ouverture centrale (8) et qui présente un rapport entre hauteur de dépression et base de dépression égal ou supérieur à 0,35, et en ce que l'espace d'échange thermique (13) susdit présente une section pour le passage du liquide de refroidissement qui est sensiblement constante, de manière à obtenir une vitesse de passage du liquide de refroidissement à travers cet espace qui soit approximativement constante, en présence de ladite dépression.1. Nose (1) of blowing lance, intended for the mixing of baths, comprising: a central tube (2) for supplying mixing gas, closed at one end facing the bath by a first front wall (3) provided at least one opening (4), an internal tube (5) forming with the central tube a first annular cavity (6) for the passage of a coolant and closed at one end facing the bath by a second wall front (7) having a central opening (8) and a passage orifice (9) by opening (4) provided in said first front wall (3), an external tube (10) forming with the internal tube (5) a second annular cavity (11) for the passage of the coolant and closed at one end facing the bath by a third front wall (12) having an outlet orifice (14) by opening (4) provided in said first front wall (3 ), a heat exchange space (13) which is located e on the one hand, said second front wall (7) and said third front wall (12) and, on the other hand, said central opening (8) and said second annular cavity (11), and into which flows the coolant, and an outlet duct (15) for the stirring gas leaving each opening (4) in said first front wall (3) and going to a corresponding outlet outlet (14) above mentioned passing through an aforementioned passage orifice (9) corresponding in a sealed manner to the coolant, characterized in that said third front wall (12) has a central depression (16) which is directed towards said central opening (8) and which has a relationship between depression height and base vacuum equal to or greater than 0.35, and in that the aforementioned heat exchange space (13) has a section for the passage of the coolant which is substantially constant, so as to obtain a speed of passage of the coolant cooling through this space which is approximately constant, in the presence of said depression.
2. Nez de lance suivant la revendication 1 , caractérisé en ce qu'il comprend plusieurs conduits de passage (15) susdits disposés autour d'un axe central (19) et en ce que ladite dépression centrale (16) s'étend depuis lesdits orifices de sortie (14) de ces conduits.2. Lance nose according to claim 1, characterized in that it comprises several passage conduits (15) said above arranged around a central axis (19) and in that said central depression (16) extends from said outlet ports (14) for these conduits.
3. Nez de lance suivant la revendication 2, caractérisé en ce que la troisième paroi frontale présente un diamètre externe et en ce que la base de ladite dépression est un cercle présentant un diamètre égal à au moins 0,25 x ledit diamètre externe. 3. Lance nose according to claim 2, characterized in that the third front wall has an external diameter and in that the base of said depression is a circle having a diameter equal to at least 0.25 x said external diameter.
4. Nez de lance suivant l'une des revendications 1 à 3, caractérisé en ce que ladite deuxième paroi frontale (7) présente, autour de l'ouverture centrale (8), une déformation centrale (17) en forme de tronc de cône, qui est dirigée vers ladite première paroi frontale (3).4. lance nose according to one of claims 1 to 3, characterized in that said second front wall (7) has, around the central opening (8), a central deformation (17) in the form of a truncated cone , which is directed towards said first front wall (3).
5. Nez de lance suivant la revendication 4, caractérisé en ce que la dépression centrale (16) a une forme de cône, en ce que ledit cône et ledit tronc de cône ont un axe commun (19) et en ce que la dépression centrale (16) en forme de cône forme avec cet axe un angle supérieur à l'angle formé entre cet axe et la déformation centrale (17) en forme de tronc de cône. 5. Nose lance according to claim 4, characterized in that the central depression (16) has a cone shape, in that said cone and said truncated cone have a common axis (19) and in that the central depression (16) in the form of a cone forms with this axis an angle greater than the angle formed between this axis and the central deformation (17) in the form of a truncated cone.
6. Nez de lance suivant l'une quelconque des revendications 1 à 5, caractérisé en ce que la dépression centrale (16) fait saillie à travers l'ouverture centrale (8), vers ladite première paroi frontale (3).6. lance nose according to any one of claims 1 to 5, characterized in that the central depression (16) projects through the central opening (8), towards said first front wall (3).
7. Nez de lance suivant l'une quelconque des revendications 1 à 6, caractérisé en ce qu'il comprend un élément de retenue (20) qui fixe un sommet de la dépression centrale (16) à ladite première paroi frontale (3).7. Spear nose according to any one of claims 1 to 6, characterized in that it comprises an element of retainer (20) which fixes a top of the central depression (16) to said first front wall (3).
8. Nez de lance suivant l'une quelconque des revendications 1 à 7, caractérisé en ce que la dépression centrale (16) est couverte au moins partiellement d'un écran protecteur (21) en un matériau à haute résistance thermique.8. Lance nose according to any one of claims 1 to 7, characterized in that the central depression (16) is covered at least partially with a protective screen (21) of a material with high thermal resistance.
9. Nez de lance suivant la revendication 8, caractérisé en ce que l'écran protecteur (21) est porté sur une tige (23) fixée au sommet de la dépression centrale (16). 9. Lance nose according to claim 8, characterized in that the protective screen (21) is carried on a rod (23) fixed to the top of the central depression (16).
10. Nez de lance suivant l'une quelconque des revendications 1 à 9, caractérisé en ce qu'il comprend plusieurs conduits de passage (15) susdits séparés circonférentiellement par des interstices, et en ce que ladite deuxième paroi frontale présente à chaque interstice susdit un renflement (18) dirigé vers l'intérieur. 10. Nose lance according to any one of claims 1 to 9, characterized in that it comprises several passage conduits (15) above said circumferentially separated by interstices, and in that said second front wall has at each aforementioned interstice a bulge (18) directed inward.
11. Nez de lance suivant l'une quelconque des revendications 1 à 10, caractérisé en ce qu'il présente un rapport entre hauteur de dépression et base de dépression égal ou supérieur à 0,4, avantageusement à 0,5, de préférence à 0,8.11. lance nose according to any one of claims 1 to 10, characterized in that it has a ratio between height of depression and base of depression equal to or greater than 0.4, advantageously 0.5, preferably 0.8.
12. Nez de lance suivant l'une quelconque des revendications 1 à 11, caractérisé en ce que l'espace d'échange thermique (13) est alimenté en eau à un débit prédéterminé et en ce qu'il12. Lance nose according to any one of claims 1 to 11, characterized in that the heat exchange space (13) is supplied with water at a predetermined flow rate and in that it
présente un rapport entre ce débit et ladite section (—) donnant lieu àpresents a relationship between this flow and said section (-) giving rise to
une vitesse de passage du liquide d'écoulement comprise entre 8 et 12 m/sec. a flow speed of the flow liquid between 8 and 12 m / sec.
EP01969081A 2000-09-15 2001-09-11 Blowing lance nozzle Expired - Lifetime EP1325161B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
BE2000/0588A BE1013686A3 (en) 2000-09-15 2000-09-15 Blowing nose spear.
BE200000588 2000-09-15
PCT/BE2001/000148 WO2002022892A1 (en) 2000-09-15 2001-09-11 Blowing lance nozzle

Publications (2)

Publication Number Publication Date
EP1325161A1 true EP1325161A1 (en) 2003-07-09
EP1325161B1 EP1325161B1 (en) 2005-04-27

Family

ID=3896669

Family Applications (1)

Application Number Title Priority Date Filing Date
EP01969081A Expired - Lifetime EP1325161B1 (en) 2000-09-15 2001-09-11 Blowing lance nozzle

Country Status (11)

Country Link
US (1) US6849228B2 (en)
EP (1) EP1325161B1 (en)
JP (1) JP2004524437A (en)
KR (1) KR20030046454A (en)
CN (1) CN1201024C (en)
AT (1) ATE294245T1 (en)
AU (1) AU2001289429A1 (en)
BE (1) BE1013686A3 (en)
BR (1) BR0113900A (en)
DE (1) DE60110446D1 (en)
WO (1) WO2002022892A1 (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7402274B2 (en) * 2005-12-07 2008-07-22 Berry Metal Company Metal making lance slag detection system
WO2007123986A2 (en) * 2006-04-21 2007-11-01 Berry Metal Company Metal making lance tip assembly
JP5379073B2 (en) * 2009-06-09 2013-12-25 三星ダイヤモンド工業株式会社 COOLING NOZZLE, COOLING METHOD USING THE COOLING NOZZLE, AND CRIMINATION METHOD FOR BRITTLE MATERIAL SUBSTRATE
BRPI1102243B1 (en) * 2011-05-20 2018-04-17 Magnesita Refratários S/A REFRIGERATED BOOM FOR INJECTION IN METALLURGICAL VASES
BE1023582B1 (en) * 2016-04-15 2017-05-09 Soudobeam Sa NOSE OF BLOWING LANCE
BE1023609B1 (en) 2016-04-15 2017-05-16 Soudobeam Sa Blowing spear nose
BE1023685B1 (en) * 2016-05-25 2017-06-14 Soudobeam Sa NOSE OF BLOWING LANCE
WO2017178608A1 (en) 2016-04-15 2017-10-19 Soudobeam Sa Blowing lance nozzle

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DE7337989U (en) * 1974-01-17 Thyssen Huette A Ag Blowing lance with cooled nozzle head for the oxygen inflation process
AT313945B (en) * 1969-08-14 1974-03-11 Voest Ag Nozzle head for oxygen blowing lances and burner lances and method for producing the same
DE2712745C2 (en) 1977-03-23 1979-03-15 Stahlwerke Peine-Salzgitter Ag, 3150 Peine Lance head for fresh lance
FR2521167B1 (en) * 1982-02-10 1987-04-30 Siderurgie Fse Inst Rech GAS INJECTION LANCE FOR METALLURGICAL CONVERTER
JPS61213311A (en) * 1985-03-18 1986-09-22 Nippon Kokan Kk <Nkk> Blowing lance for converter
DE3509795C1 (en) * 1985-03-19 1986-06-05 Klöckner CRA Technologie GmbH, 4100 Duisburg Water-cooled blowing lance for blowing oxygen onto a molten metal
AT389710B (en) * 1988-04-25 1990-01-25 Voest Alpine Ind Anlagen BLOWING
RU2051974C1 (en) * 1995-01-25 1996-01-10 Александр Леонидович Кузьмин Oxygen converter-type tuyere tip
JPH08302414A (en) * 1995-05-10 1996-11-19 Nippon Steel Corp Lance nozzle for blowing of converter
BE1009743A3 (en) * 1995-06-23 1997-07-01 Thomas Jacques Tuyere blowing oxygen steel.
DE29907794U1 (en) * 1999-05-03 1999-07-22 Impact Gesellschaft für Nichteisenmetallverarbeitung mbH, 47445 Moers Lance head for a water-cooled oxygen lance
US6217824B1 (en) * 1999-05-20 2001-04-17 Berry Metal Company Combined forged and cast lance tip assembly
US6599464B1 (en) * 1999-10-06 2003-07-29 Bernd Feldhaus Steelmaking lance with integral temperature probe

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Title
See references of WO0222892A1 *

Also Published As

Publication number Publication date
US6849228B2 (en) 2005-02-01
EP1325161B1 (en) 2005-04-27
US20030178186A1 (en) 2003-09-25
DE60110446D1 (en) 2005-06-02
KR20030046454A (en) 2003-06-12
CN1457368A (en) 2003-11-19
AU2001289429A1 (en) 2002-03-26
WO2002022892A1 (en) 2002-03-21
BE1013686A3 (en) 2002-06-04
CN1201024C (en) 2005-05-11
JP2004524437A (en) 2004-08-12
ATE294245T1 (en) 2005-05-15
BR0113900A (en) 2003-07-22

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