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EP0759335B1 - Supporting device for the side walls of a continuous roll caster installation for the production of metallic strips - Google Patents

Supporting device for the side walls of a continuous roll caster installation for the production of metallic strips Download PDF

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Publication number
EP0759335B1
EP0759335B1 EP96401654A EP96401654A EP0759335B1 EP 0759335 B1 EP0759335 B1 EP 0759335B1 EP 96401654 A EP96401654 A EP 96401654A EP 96401654 A EP96401654 A EP 96401654A EP 0759335 B1 EP0759335 B1 EP 0759335B1
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EP
European Patent Office
Prior art keywords
thrust
cylinders
plate
thrust plate
face
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
EP96401654A
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German (de)
French (fr)
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EP0759335A1 (en
Inventor
Yann Breviere
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.)
Thyssen Stahl AG
USINOR SA
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Thyssen Stahl AG
USINOR SA
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Publication of EP0759335A1 publication Critical patent/EP0759335A1/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/06Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
    • B22D11/0637Accessories therefor
    • B22D11/0648Casting surfaces
    • B22D11/066Side dams

Definitions

  • the invention relates to the continuous casting of metals. More specifically, it concerns the devices for lateral containment of liquid metal in the ingot molds of thin strip continuous casting machines, the casting space of which is limited by the side surfaces close to two cylinders with horizontal axes, energetically internally cooled and rotated in opposite directions.
  • the object of the invention is to provide the operator with the means of imposing on the lateral face a controlled wear which would not be higher than what would be strictly necessary for the smooth running of the casting.
  • the invention relates to a device for supporting a lateral face of a continuous casting installation between cylinders of thin metal products of the type with two cooled cylinders with horizontal axes, two side faces applied against the edges of the rolls, said support device comprising a carriage movable on command in a direction parallel to the axes of the cylinders, a pushing device carried by said carriage, and a plate integral with the face lateral, connected to said pushing device via a pushing plate and thrust members bearing on said thrust plate and said plate, (see: EP-A-0698433).
  • Said plate comprises at least one tie rod passing through the plate thrust and the free end of which is fitted with a stop which can be applied against the rear face of said push plate.
  • the plate supporting the small face is equipped with one or more tie rods passing through the thrust plate, and the free ends can abut against the rear face of the thrust plate.
  • the thrust members which normally tend to move the plate away from the push plate to apply the side face against the cylinders causing its wear, see their action limited when this wear has become sufficiently pronounced so that this abutment is achieved. There is then only one minimal friction between the side face and the cylinders, and wear on the side face almost canceled.
  • Figure 1 shows a side part of a casting machine between two close cylinders with horizontal axes rotated and internally cooled, of which only one of the cylinders 1 is visible.
  • the other side of the machine is equipped in the same way.
  • the casting space defined by the two cylinders is closed laterally by a side face 2 of refractory material whose front face is applied against the edges 3 of the cylinders 1.
  • the lateral face 2 is fixed by its face rear on a plate 4 which is made of a material such as a metallic material. This plate 4 is preferably cooled to prevent it from being affected by deformations of purely thermal origin.
  • Displacement and bearing force on the cylinders 1 of the side face 2 are controlled by an assembly which acts on the plate 4 and which will be described in more detail detail.
  • it comprises a carriage 5 movable to control according to a direction parallel to the cylinder axes 1.
  • a device for thrust 6 such as a jack (or group of jacks) controlled by pressure or position, comprising a rod 7 which can be moved when ordered, always in the same direction parallel to the axes of the cylinders 1.
  • the rod 7 attacks a thrust plate 8, which itself carries a set of thrust members 9, 9 ', 9' ', 9' '', such as springs or jacks piloted, exerting their force on the rear face 10 of the plate 4.
  • thrust members 9, 9 ', 9' ', 9' '' such as springs or jacks piloted, exerting their force on the rear face 10 of the plate 4.
  • These members are distributed over an area whose shape preferably corresponds to that of the lateral face 2.
  • Their usual function is to strongly apply the side face 2 against the edges of the cylinders 1, via the plate 4.
  • a plurality tie rods 11, 11 ′ are fixed to the rear face of the plate 4 and oriented substantially perpendicular to it. These tie rods 11, 11 ′ pass through the thrust plate 8 thanks to passages 12, 12 'which are provided for this purpose, and their free end is equipped a stop 13, 13 'of dimensions greater than those of the passages 12, 12'.
  • the lengths of tie rods 11, 11 ' are chosen so that the stops 13, 13' can come to bear against the rear face 14 of the thrust plate 8 before the members 9, 9 ', 9' ', 9' ' thrust have reached their maximum possible extension.
  • the material tie rods must have good strength and stability properties dimensional to the temperatures encountered in this area of the machine. We recommend using, for example, stainless steel with a low coefficient of dilation.
  • FIG. 1 represents the installation in its initial state, at the start of the casting, with a side face 2 having a thickness (e).
  • the springs which, in the example shown, constitute the thrust members 9, 9 ', 9' ', 9' '', are in a state of compression corresponding to a distance (d) between the plate 4 and the thrust plate 8.
  • the stops 13, 13 ' tie rods 11, 11 ' are, in this initial state, at a distance (d') from the rear face 14 of the push plate 8.
  • FIG. 2 represents the same installation at a later instant in the casting.
  • the position of the pushing device 6 has not changed, but the face lateral 2 underwent progressive wear, due to its friction against the edges of cylinders 1.
  • This wear gradually increased the distance between the thrust plate 8 and the plate 4 under the action of the springs 9, 9 ', 9' ', 9' '' and the loosening of their state of compression.
  • This distance can be estimated for example using displacement sensors integrated into the organs 9, 9 ', 9' ', 9' '' thrust.
  • the side face 2-plate assembly 4 can retreat at least locally, this decline being all the more localized as this together has a certain flexibility and that the pushing members 9, 9 ', 9' ', 9' '' are more numerous.
  • the stop 13, 13 'of one or more tie rods 11, 11' is no longer in contact with the push plate 8, and the push member (s) 9, 9 '', 9 '', 9 '' 'closest to the infiltration area resume their function firm application of the side face 2 against the cylinders 1.
  • tie rods 13, 13 ' for example three
  • the side face 2-plate assembly 4 presents a certain flexibility or possibilities of travel in the three dimensions, it is possible to better take into account the local setbacks of the face lateral 2, as well as the misalignment of the edges of the cylinders 1 one on the other.
  • the invention is, moreover, perfectly compatible with the use of faces side 2 which, as it is known, would give an oscillating movement in the plane of the flat faces of the cylinders 1, 1 '.
  • the device according to the invention can be supplemented by one or more sensors position providing a value representative, at least at a given time, of the distance between the side face 2 and the cylinders 1. They make it possible to ensure that during the phases where wear of the side face 2 is sought, there is good contact between it and the cylindersl. On the other hand, during normal operation of the installation, may wish this contact not to be fully realized, and endeavor to maintain permanent play of 0.1 to 0.2 mm, small enough to prevent metal leakage liquid but making it possible to eliminate wear on the side face 2 by friction. Alone Corrosion by liquid metal would then remain as a cause of wear.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Continuous Casting (AREA)
  • Coating With Molten Metal (AREA)
  • Bending Of Plates, Rods, And Pipes (AREA)
  • Forging (AREA)
  • Rollers For Roller Conveyors For Transfer (AREA)
  • Paper (AREA)
  • Rolls And Other Rotary Bodies (AREA)
  • Structure Of Belt Conveyors (AREA)
  • Types And Forms Of Lifts (AREA)

Abstract

The support, designed for the lateral face of a continuous casting unit with two cooled cylinders (1) having horizontal axes, consists of a carriage (5) which can be moved parallel to the axes of the cylinders and has a thrust member (6) and a panel (4) joined to the lateral face of a cylinder through a thrust plate (8) and thrust elements (9, 9', 9", 9'"). The panel has at least one long bolt (11, 11') which passes through the thrust plate and has its free end equipped with a stop (13, 13') which can be applied against the rear face of the thrust plate. The long bolts can be three in number, distributed over an area corresponding to the shape of the lateral face, and the thrust elements (9, 9', 9", 9'") can be in the for of springs or power cylinders.

Description

L'invention concerne la coulée continue des métaux. Plus précisément, elle concerne les dispositifs de confinement latéral du métal liquide dans les lingotières des machines de coulée continue de bandes minces, dont l'espace de coulée est limité par les surfaces latérales rapprochées de deux cylindres à axes horizontaux, énergiquement refroidis intérieurement et mis en rotation en sens contraires.The invention relates to the continuous casting of metals. More specifically, it concerns the devices for lateral containment of liquid metal in the ingot molds of thin strip continuous casting machines, the casting space of which is limited by the side surfaces close to two cylinders with horizontal axes, energetically internally cooled and rotated in opposite directions.

Sur ce type de machine de coulée continue, dit "coulée entre cylindres", dont l'application industrielle à la coulée de bandes d'acier d'environ 2 à 10 mm d'épaisseur est actuellement en cours, le confinement latéral du métal liquide dans l'espace de coulée défini par les cylindres est assuré par des plaques qui sont appliquées contre les extrémités planes des cylindres, appelées "chants", par un dispositif approprié. Ces plaques sont habituellement désignées par les termes "faces latérales" ou "petites faces". Leur partie centrale destinée à être au contact du métal liquide est en matériau réfractaire, de même, en général, que leur périphérie qui frotte contre les cylindres en s'usant progressivement. Il est indispensable qu'elles soient en contact aussi étanche que possible avec les cylindres, car des infiltrations de métal liquide dans leur zone de contact auraient des effets désastreux sur la qualité des rives de la bande coulée. Celles-ci prendraient une forme dentelée, et seraient excessivement fragiles. Elles risqueraient alors de se séparer du reste de la bande et de rester collées aux cylindres. Si ce collage persistait pendant un tour complet des cylindres et si les lambeaux de rives pénétraient donc dans l'espace de coulée, cela pourrait donner lieu à de graves détériorations des surfaces des cylindres. Au pire, ces infiltrations de métal pourraient parvenir jusqu'à l'extérieur de la machine, ce qui imposerait l'arrêt immédiat de la coulée.On this type of continuous casting machine, called "casting between cylinders", of which industrial application to the casting of steel strips about 2 to 10 mm thick is currently in progress, the lateral confinement of the liquid metal in the space of casting defined by the cylinders is ensured by plates which are applied against flat ends of the cylinders, called "edges", by an appropriate device. These plates are usually referred to as "side faces" or "small faces ". Their central part intended to be in contact with liquid metal is made of material refractory, as well, in general, as their periphery which rubs against the cylinders in gradually wearing out. They must be in contact as tight as possible with cylinders, because liquid metal infiltration in their area of contact would have disastrous effects on the quality of the edges of the strip. These would take a serrated form, and would be excessively fragile. They would risk then separate from the rest of the strip and stay glued to the cylinders. If this collage persisted for a full revolution of the cylinders and if the shreds of the edges penetrated so in the casting space this could cause serious deterioration of the cylinder surfaces. At worst, these metal infiltrations could reach outside the machine, which would require the immediate stopping of the casting.

De tels défauts d'étanchéité peuvent avoir des causes multiples, parmi lesquelles on peut citer:

  • les déformations des cylindres et des faces latérales, dues aux sollicitations mécaniques et thermiques qu'ils subissent, en particulier au tout début de la coulée lors de leur mise en régime thermique;
  • l'usure progressive des faces latérales ou des cylindres, qui n'est pas toujours uniforme sur l'ensemble de leurs zones de contact;
  • l'usure instantanée des faces latérales provoquée par le passage d'une infiltration de métal solidifié.
Such leaks can have multiple causes, including:
  • the deformations of the cylinders and of the lateral faces, due to the mechanical and thermal stresses which they undergo, in particular at the very beginning of the casting when they are brought into thermal regime;
  • progressive wear of the lateral faces or of the cylinders, which is not always uniform over all of their contact zones;
  • the instantaneous wear of the lateral faces caused by the passage of an infiltration of solidified metal.

Il a déjà été proposé de résoudre ces problèmes d'étanchéité en provoquant une usure contrôlée des faces latérales par un frottement maítrisé de celles-ci contre les cylindres. On régénère ainsi en permanence les surfaces de contact des faces latérales, en les adaptant au mieux aux éventuelles évolutions de la forme des parties des cylindres sur lesquelles elles s'appuient. On peut citer, à cet égard, le document EP-A-546206. Il enseigne de presser tout d'abord fortement les faces latérales contre les cylindres en rotation avant le début de la coulée, afin de leur faire épouser la configuration initiale exacte des chants des cylindres. Ensuite on relâche un peu cette pression, puis on démarre la coulée en remettant temporairement une forte pression sur les faces latérales, de manière à créer délibérément une usure qui conforme les faces latérales aux chants des cylindres. En cours de coulée, on continue à appliquer les faces latérales contre les cylindres, en compensant leur usure par un déplacement à une vitesse modérée prédéterminée. On provoque ainsi une usure maítrisée assurant le renouvellement permanent des surfaces de contact entre les faces latérales et les cylindres.It has already been proposed to solve these sealing problems by causing controlled wear of the side faces by controlled friction of these against the cylinders. The contact surfaces of the lateral faces are thus constantly regenerated, by adapting them as best as possible to any changes in the shape of the parts of the cylinders on which they are based. Mention may be made, in this regard, of document EP-A-546206. He teaches first of all to strongly press the lateral faces against the cylinders in rotation before the start of the casting, in order to make them marry the exact initial configuration of the edges of the cylinders. Then we release this a little pressure, then start the casting by temporarily putting a strong pressure on the side faces, so as to deliberately create wear which conforms the faces lateral to the edges of the cylinders. During casting, we continue to apply the faces side against the cylinders, compensating for their wear by a displacement at a predetermined moderate speed. This causes controlled wear ensuring the permanent renewal of the contact surfaces between the lateral faces and the cylinders.

La demande de brevet français FR9408319 qui n'est pas publié à temps et qui correspond à EP-A-0698433, un docùment suivant l'Article 54(3) CBE. apporte une amélioration à ce mode opératoire et à ceux qui en dériveraient en prévoyant des moyens permettant de déformer légèrement les faces latérales en modulant la pression appliquée sur leurs différentes zones. Ainsi, on tient compte des inégalités temporaires ou permanentes dans les efforts exercés sur les différentes parties des faces latérales par les cylindres. De telles inégalités peuvent se produire, par exemple, en cas de solidification parasite de métal infiltré entre la face latérale et un cylindre, ou lorsque les deux chants des cylindres contre lesquels est appliquée la face latérale ne sont pas parfaitement coplanaires et orthogonaux aux axes des cylindres.French patent application FR9408319 which is not published in time and which corresponds to EP-A-0698433, a document under Article 54 (3) EPC. makes an improvement to this procedure and those who derive from it by providing means to slightly deform the lateral faces by modulating the pressure applied to their different areas. Thus, we take into account temporary or permanent inequalities in the forces exerted on the different parts of the lateral faces by the cylinders. Such inequalities can occur, for example, in the case of parasitic solidification of metal seeped between the side face and a cylinder, or when the two edges of the cylinders against which the side face is applied are not perfectly coplanar and orthogonal to the axes of the cylinders.

Ces modes opératoires ont cependant l'inconvénient d'imposer à chaque face latérale une usure par frottement qui est, certes, mesurable par l'intermédiaire de la vitesse d'avancement de la face latérale, mais qui n'est pas aisément contrôlable. Elle peut s'avérer inutilement importante dans le cas où la coulée se déroule sans incident particulier.However, these procedures have the disadvantage of imposing on each face lateral wear by friction which is certainly measurable by means of the forward speed of the side face, but which is not easily controllable. She can be unnecessarily important in the event that the casting takes place without incident particular.

Le but de l'invention est de procurer à l'opérateur les moyens d'imposer à la face latérale une usure contrôlée qui ne serait pas supérieure à ce qui serait strictement nécessaire au bon déroulement de la coulée.The object of the invention is to provide the operator with the means of imposing on the lateral face a controlled wear which would not be higher than what would be strictly necessary for the smooth running of the casting.

A cet effet, l'invention a pour objet un dispositif de support d'une face latérale d'une installation de coulée continue entre cylindres de produits métalliques minces du type comportant deux cylindres refroidis à axes horizontaux, deux faces latérales appliquées contre les chants des cylindres, ledit dispositif de support comportant un chariot déplaçable à la commande selon une direction parallèle aux axes des cylindres, un dispositif de poussée porté par ledit chariot, et une platine solidaire de la face latérale, reliée audit dispositif de poussée par l'intermédiaire d'une plaque de poussée et d'organes de poussée prenant appui sur ladite plaque de poussée et ladite platine, (voir: EP-A-0698433). Ladite platine comporte au moins un tirant traversant la plaque de poussée et dont l'extrémité libre est équipée d'une butée pouvant venir s'appliquer contre la face arrière de ladite plaque de poussée.To this end, the invention relates to a device for supporting a lateral face of a continuous casting installation between cylinders of thin metal products of the type with two cooled cylinders with horizontal axes, two side faces applied against the edges of the rolls, said support device comprising a carriage movable on command in a direction parallel to the axes of the cylinders, a pushing device carried by said carriage, and a plate integral with the face lateral, connected to said pushing device via a pushing plate and thrust members bearing on said thrust plate and said plate, (see: EP-A-0698433). Said plate comprises at least one tie rod passing through the plate thrust and the free end of which is fitted with a stop which can be applied against the rear face of said push plate.

Comme on l'aura compris, selon l'invention la platine supportant la petite face est équipée de un ou plusieurs tirants traversant la plaque de poussée, et dont les extrémités libres peuvent venir en butée contre la face arrière de la plaque de poussée. Ainsi, les organes de poussée, qui tendent normalement à éloigner la platine de la plaque de poussée pour appliquer la face latérale contre les cylindres en provoquant son usure, voient leur action limitée lorsque cette usure est devenue suffisamment prononcée pour que cette venue en butée soit réalisée. Il n'y a plus alors qu'un frottement minimal entre la face latérale et les cylindres, et l'usure de la face latérale se trouve quasiment annulée.As will be understood, according to the invention the plate supporting the small face is equipped with one or more tie rods passing through the thrust plate, and the free ends can abut against the rear face of the thrust plate. Thus, the thrust members, which normally tend to move the plate away from the push plate to apply the side face against the cylinders causing its wear, see their action limited when this wear has become sufficiently pronounced so that this abutment is achieved. There is then only one minimal friction between the side face and the cylinders, and wear on the side face almost canceled.

L'invention sera mieux comprise à la lecture de la description qui suit, donnée en référence aux figures suivantes:

  • la figure 1 qui montre schématiquement vus de profil un dispositif selon l'invention et l'un des cylindres de coulée contre lesquels l'une des faces latérales de la machine de coulée entre cylindres est appliquée, les tirants étant en position telle qu'ils autorisent l'éloignement progressif de la platine par rapport à la plaque de poussée;
  • la figure 2 qui montre le même dispositif alors que les tirants sont en butée contre la face arrière de la plaque de poussée.
The invention will be better understood on reading the description which follows, given with reference to the following figures:
  • Figure 1 which schematically shows in profile a device according to the invention and one of the casting rolls against which one of the side faces of the casting machine between rolls is applied, the tie rods being in position such that allow the progressive displacement of the plate relative to the thrust plate;
  • Figure 2 which shows the same device while the tie rods are in abutment against the rear face of the thrust plate.

La figure 1 représente une partie latérale d'une machine de coulée entre deux cylindres rapprochés à axes horizontaux mis en rotation et refroidis intérieurement, dont seul un des cylindres 1 est visible. L'autre partie latérale de la machine est équipée de manière similaire. L'espace de coulée défini par les deux cylindres est obturé latéralement par une face latérale 2 en matériau réfractaire dont la face avant est appliquée contre les chants 3 des cylindres 1. La face latérale 2 est fixée par sa face arrière sur une platine 4 qui est en un matériau tel qu'un matériau métallique. Cette platine 4 est de préférence refroidie pour éviter qu'elle ne soit affectée par des déformations d'origine purement thermique.Figure 1 shows a side part of a casting machine between two close cylinders with horizontal axes rotated and internally cooled, of which only one of the cylinders 1 is visible. The other side of the machine is equipped in the same way. The casting space defined by the two cylinders is closed laterally by a side face 2 of refractory material whose front face is applied against the edges 3 of the cylinders 1. The lateral face 2 is fixed by its face rear on a plate 4 which is made of a material such as a metallic material. This plate 4 is preferably cooled to prevent it from being affected by deformations of purely thermal origin.

Les déplacements et la force d'appui sur les cylindres 1 de la face latérale 2 sont commandés par un ensemble qui agit sur la platine 4 et qui va être décrit plus en détail. De manière connue, il comprend un chariot 5 mobile à la commande selon une direction parallèle aux axes de cylindres 1. Sur ce chariot 5 est monté un dispositif de poussée 6 tel qu'un vérin (ou un groupe de vérins) asservi en pression ou en position, comportant une tige 7 déplaçable à la commande, toujours selon la même direction parallèle aux axes des cylindres 1. Comme dans la demande de brevet français FR9408319 déjà citée, la tige 7 attaque une plaque de poussée 8, qui porte elle-même un ensemble d'organes de poussée 9, 9', 9'', 9''', tels que des ressorts ou des vérins pilotés, exerçant leur effort sur la face arrière 10 de la platine 4. Ces organes sont répartis sur une zone dont la forme correspond de préférence à celle de la face latérale 2. Ils ont pour fonction habituelle d'appliquer fortement la face latérale 2 contre les chants des cylindres 1, par l'intermédiaire de la platine 4. Mais ils autorisent un léger recul d'au moins la portion de la face latérale 2 qui est située dans leur prolongement, lorsqu'une solidification parasite s'interpose entre elle et l'un des cylindres 1, sans pour autant que les conditions de contact entre le restant de la face latérale 2 et les cylindres 1 en soient fortement affectées. On se reportera au texte de la demande française précitée pour plus de détails.Displacement and bearing force on the cylinders 1 of the side face 2 are controlled by an assembly which acts on the plate 4 and which will be described in more detail detail. In known manner, it comprises a carriage 5 movable to control according to a direction parallel to the cylinder axes 1. On this carriage 5 is mounted a device for thrust 6 such as a jack (or group of jacks) controlled by pressure or position, comprising a rod 7 which can be moved when ordered, always in the same direction parallel to the axes of the cylinders 1. As in the French patent application FR9408319 already mentioned, the rod 7 attacks a thrust plate 8, which itself carries a set of thrust members 9, 9 ', 9' ', 9' '', such as springs or jacks piloted, exerting their force on the rear face 10 of the plate 4. These members are distributed over an area whose shape preferably corresponds to that of the lateral face 2. Their usual function is to strongly apply the side face 2 against the edges of the cylinders 1, via the plate 4. But they allow a slight receding of at least the portion of the lateral face 2 which is situated in their extension, when a parasitic solidification is interposed between it and one of the cylinders 1, without as much as the contact conditions between the rest of the side face 2 and the cylinders 1 are strongly affected. We will refer to the text of the French request above for more details.

Selon l'invention, dans l'exemple représenté sur les figures 1 et 2, une pluralité de tirants 11, 11' sont fixés à la face arrière de la platine 4 et orientés sensiblement perpendiculairement à elle. Ces tirants 11, 11' traversent la plaque de poussée 8 grâce à des passages 12, 12' qui y sont ménagés à cet effet, et leur extrémité libre est équipée d'une butée 13, 13' de dimensions supérieures à celles des passages 12, 12'. Les longueurs des tirants 11, 11' sont choisies de telle sorte que les butées 13, 13' puissent venir en appui contre la face arrière 14 de la plaque de poussée 8 avant que les organes de poussée 9, 9', 9'', 9''' n'aient atteint leur extension maximale possible. Le matériau des tirants doit présenter de bonnes propriétés de résistance et de stabilité dimensionnelle aux températures rencontrées dans cette zone de la machine. On recommande d'utiliser, par exemple, un acier inoxydable à faible coefficient de dilatation.According to the invention, in the example shown in Figures 1 and 2, a plurality tie rods 11, 11 ′ are fixed to the rear face of the plate 4 and oriented substantially perpendicular to it. These tie rods 11, 11 ′ pass through the thrust plate 8 thanks to passages 12, 12 'which are provided for this purpose, and their free end is equipped a stop 13, 13 'of dimensions greater than those of the passages 12, 12'. The lengths of tie rods 11, 11 'are chosen so that the stops 13, 13' can come to bear against the rear face 14 of the thrust plate 8 before the members 9, 9 ', 9' ', 9' '' thrust have reached their maximum possible extension. The material tie rods must have good strength and stability properties dimensional to the temperatures encountered in this area of the machine. We recommend using, for example, stainless steel with a low coefficient of dilation.

La figure 1 représente l'installation dans son état initial, au début de la coulée, avec une face latérale 2 présentant une épaisseur (e). Compte tenu de la position initiale du dispositif de poussée 6, les ressorts qui, dans l'exemple représenté, constituent les organes de poussée 9, 9', 9'', 9''', sont dans un état de compression correspondant à une distance (d) entre la platine 4 et la plaque de poussée 8. D'autre part, les butées 13, 13' des tirants 11, 11' sont, dans cet état initial, à une distance (d') de la face arrière 14 de la plaque de poussée 8.FIG. 1 represents the installation in its initial state, at the start of the casting, with a side face 2 having a thickness (e). Given the initial position of the pushing device 6, the springs which, in the example shown, constitute the thrust members 9, 9 ', 9' ', 9' '', are in a state of compression corresponding to a distance (d) between the plate 4 and the thrust plate 8. On the other hand, the stops 13, 13 ' tie rods 11, 11 'are, in this initial state, at a distance (d') from the rear face 14 of the push plate 8.

La figure 2 représente la même installation à un instant ultérieur de la coulée. Dans l'intervalle, la position du dispositif de poussée 6 n'a pas varié, mais la face latérale 2 a subi une usure progressive, du fait de son frottement contre les chants des cylindres 1. Cette usure a eu pour effet d'augmenter graduellement la distance séparant la plaque de poussée 8 et la platine 4 sous l'action des ressorts 9, 9', 9'', 9''' et du relâchement de leur état de compression. Cette distance, ou au moins ses variations, peut être estimée par exemple à l'aide de capteurs de déplacement intégrés aux organes de poussée 9, 9', 9'', 9'''. Lorsque cette usure a été telle que la face latérale a pris une épaisseur égale à (e-d'), la distance entre la plaque de poussée 8 et la platine 4 a pris une valeur égale à (d+d'), et les butées 13, 13' des tirants 11, 11' sont venues se mettre en appui sur la face arrière 14 de la plaque de poussée 8. Cela a eu pour effet d'interrompre l'avancée de la platine 4 vers les cylindres 1. A ce moment, en marche normale de l'installation, la face latérale 2 n'est plus appliquée contre les chants des cylindres 1 qu'avec une force très faible garantissant un frottement minimal entre eux, juste suffisant pour assurer l'étanchéité de l'espace de coulée. Ce frottement minimal permet de maintenir une usure très faible de la face latérale 2, et donc d'augmenter sa durée de vie.FIG. 2 represents the same installation at a later instant in the casting. In the meantime, the position of the pushing device 6 has not changed, but the face lateral 2 underwent progressive wear, due to its friction against the edges of cylinders 1. This wear gradually increased the distance between the thrust plate 8 and the plate 4 under the action of the springs 9, 9 ', 9' ', 9' '' and the loosening of their state of compression. This distance, or at least its variations, can be estimated for example using displacement sensors integrated into the organs 9, 9 ', 9' ', 9' '' thrust. When this wear has been such that the lateral face has taken a thickness equal to (e-d '), the distance between the push plate 8 and the plate 4 has taken a value equal to (d + d '), and the stops 13, 13' of the tie rods 11, 11 'have come to be resting on the rear face 14 of the push plate 8. This had the effect to interrupt the advancement of the plate 4 towards the cylinders 1. At this time, running normal installation, side face 2 is no longer applied against the edges of cylinders 1 with a very low force guaranteeing minimal friction between them, just enough to seal the pouring space. This minimal friction keeps very little wear on the side face 2, and therefore increases its lifetime.

On peut, en conséquence, proposer une procédure de coulée qui serait la suivante. Préalablement à la coulée, on place l'installation dans la configuration précédemment décrite et représentée sur la figure 1. Puis on démarre la coulée, et par suite de l'usure progressive de la face latérale 2, on finit par se retrouver dans la configuration précédemment décrite et représentée sur la figure 2, où les butées 13, 13' des tirants 11, 11' sont en butée contre la face arrière 14 de la plaque de poussée 8. Le moment où on parvient à cet état peut être détecté grâce, par exemple, à des capteurs de déplacement intégrés aux organes de poussée 9, 9', 9'', 9'''. Si du métal solidifié vient s'insérer entre la face latérale 2 et l'un des cylindres 1, l'ensemble face latérale 2-platine 4 peut reculer au moins localement, ce recul étant d'autant plus localisé que cet ensemble présente une certaine souplesse et que les organes de poussée 9, 9', 9'', 9''' sont plus nombreux. A ce moment, la butée 13, 13' d'un ou de plusieurs tirants 11, 11' n'est plus au contact de la plaque de poussée 8, et le ou les organes de poussée 9, 9'', 9'', 9''' les plus proches de la zone où se trouve l'infiltration reprennent leur fonction d'application ferme de la face latérale 2 contre les cylindres 1. Cela dure jusqu'à la disparition de l'infiltration si sa présence n'est que temporaire, ou, si l'infiltration persiste durablement, jusqu'à ce que l'usure locale de la face latérale 2 entraíne la reprise du contact entre la ou les butées 13, 13' et la plaque de poussée 8.We can therefore propose a casting procedure which would be the next. Prior to casting, the installation is placed in the configuration previously described and shown in Figure 1. Then we start casting, and by following the progressive wear of the side face 2, we end up in the configuration previously described and shown in Figure 2, where the stops 13, 13 ' tie rods 11, 11 'are in abutment against the rear face 14 of the thrust plate 8. The when this state is reached can be detected, for example, by sensors displacement integrated in the thrust members 9, 9 ', 9' ', 9' ''. If solidified metal comes fit between the side face 2 and one of the cylinders 1, the side face 2-plate assembly 4 can retreat at least locally, this decline being all the more localized as this together has a certain flexibility and that the pushing members 9, 9 ', 9' ', 9' '' are more numerous. At this time, the stop 13, 13 'of one or more tie rods 11, 11' is no longer in contact with the push plate 8, and the push member (s) 9, 9 '', 9 '', 9 '' 'closest to the infiltration area resume their function firm application of the side face 2 against the cylinders 1. This lasts until the disappearance of the infiltration if its presence is only temporary, or, if the infiltration persists for a long time, until the local wear of the side face 2 causes the resumption of contact between the abutment (s) 13, 13 'and the thrust plate 8.

Afin de régénerer périodiquement la surface de la face latérale 2 qui est au contact des cylindres 1 et d'éviter ainsi que des usures locales trop prononcées ne détériorent les conditions d'étanchéité à son niveau, on prévoit de réaliser périodiquement une mise en mouvement de la tige 7 du dispositif de poussée 6 en direction des cylindres 1. On rapproche ainsi la plaque de poussée 8 des cylindres 1, ce qui a pour effet d'éloigner les butées 13, 13' de tous les tirants 11, 11' par rapport à la plaque de poussée 8 et de restaurer une application ferme de la face latérale 2 contre les cylindres 1 par les organes de poussée 9, 9', 9'', 9'''. Cette application ferme dure jusqu'à ce que l'usure de la face latérale 2 soit suffisamment prononcée pour que le contact entre les butées 13, 13' et la plaque de poussée 8 soit à nouveau réalisé, et qu'on retrouve ainsi les conditions de frottement minimal souhaitées. On peut choisir de réaliser cette opération de manière régulière, en imposant une vitesse moyenne de déplacement de l'ordre de 1 à 10 mm/h à la plaque de poussée 8. Cette vitesse de déplacement correspond à la vitesse d'usure que l'on souhaite imposer à la face latérale 2 en l'absence d'infiltrations de métal solidifié. Cette vitesse est notablement inférieure à celles qui sont habituellement imposées par les dispositifs classiques d'application des faces latérales contre les cylindres, et qui se chiffrent à quelques dizaines de mm/h. On peut également choisir de surimposer à ce déplacement périodique systématique de la tige 7 des déplacements épisodiques plus importants à des moments déterminés par l'opérateur ou l'automate qui gère le fonctionnement de l'installation. Cela peut être le cas lorsque, par exemple, on aura constaté des reculs de relativement fortes amplitudes sur une partie ou sur l'ensemble de la face latérale 2, qui seraient l'indice de la présence d'infiltrations de métal solidifié entre la face latérale 2 et les cylindres 1 susceptibles d'entraíner une usure exceptionnelle de la face latérale 2. Dans ces cas, il est souhaitable d'obtenir une régénération rapide de la surface de contact face latérale 2-cylindres 1, ce que permet un déplacement de la tige 7 spécialement réalisé dans cette intention.In order to periodically regenerate the surface of the side face 2 which is at contact of the cylinders 1 and thus avoid that too pronounced local wear does deteriorate the sealing conditions at its level, it is planned to carry out periodically setting the rod 7 of the pushing device 6 into motion direction of the cylinders 1. The thrust plate 8 is thus brought closer to the cylinders 1, this which has the effect of moving the stops 13, 13 'from all the tie rods 11, 11' relative to the push plate 8 and restore firm application of side face 2 against the cylinders 1 by the thrust members 9, 9 ', 9' ', 9' ''. This firm application lasts until the wear on the side face 2 is sufficiently pronounced for the contact between the stops 13, 13 ′ and the thrust plate 8 is again achieved, and that we thus find the desired minimum friction conditions. We can choose to perform this operation on a regular basis, imposing an average speed of displacement of the order of 1 to 10 mm / h at the thrust plate 8. This speed of displacement corresponds to the speed of wear which one wishes to impose on the face lateral 2 in the absence of infiltration of solidified metal. This speed is notably lower than those usually imposed by conventional devices of application of the lateral faces against the cylinders, which amount to a few tens of mm / h. We can also choose to superimpose this displacement systematic periodic of the rod 7 of the episodic displacements more important to moments determined by the operator or the automaton which manages the operation of the installation. This may be the case when, for example, there have been setbacks in relatively large amplitudes over part or all of the lateral face 2, which would be the indication of the presence of infiltrations of solidified metal between the side face 2 and the cylinders 1 likely to cause exceptional wear of the side face 2. In these cases, it is desirable to obtain rapid regeneration of the surface of the 2-cylinder side face contact 1, which allows displacement of the rod 7 specially made for this purpose.

En principe, la présence d'un seul tirant, placé par exemple dans la région centrale de la platine 4 supportant la face latérale, est suffisante pour obtenir l'effet recherché. Toutefois, il est préférable de prévoir une pluralité de tirants 13, 13' (par exemple trois) répartis sur la platine 4 sur une zone de forme correspondant à celle de la face latérale 2. De cette façon, en particulier lorsque l'ensemble face latérale 2-platine 4 présente une certaine souplesse ou des possibilités de débattement dans les trois dimensions, il est possible de mieux prendre en compte les reculs localisés de la face latérale 2, de même que les défauts d'alignement des chants des cylindres 1 l'un sur l'autre. Afin que, lors des débattements de la platine 4 qui ne seraient pas strictement parallèles à l'axe des cylindres 1, les déplacements des tirants 11, 11' ne soient pas gênés, il faut prévoir un jeu suffisamment important entre eux et les parois des passages 12, 12' ménagés à leur intention dans la plaque de poussée 8.In principle, the presence of a single tie rod, placed for example in the region central of the plate 4 supporting the lateral face, is sufficient to obtain the effect research. However, it is preferable to provide a plurality of tie rods 13, 13 '(for example three) distributed on the plate 4 over a zone of shape corresponding to that of the side face 2. In this way, in particular when the side face 2-plate assembly 4 presents a certain flexibility or possibilities of travel in the three dimensions, it is possible to better take into account the local setbacks of the face lateral 2, as well as the misalignment of the edges of the cylinders 1 one on the other. So that, during the deflections of the plate 4 which would not be strictly parallel to the axis of the cylinders 1, the displacements of the tie rods 11, 11 'are not embarrassed, there must be a sufficiently large clearance between them and the walls of the passages 12, 12 'provided for them in the push plate 8.

L'invention est, par ailleurs, parfaitement compatible avec l'utilisation de faces latérales 2 auxquelles, comme il est connu, on imprimerait un mouvement d'oscillation dans le plan des faces planes des cylindres 1, 1'.The invention is, moreover, perfectly compatible with the use of faces side 2 which, as it is known, would give an oscillating movement in the plane of the flat faces of the cylinders 1, 1 '.

Le dispositif selon l'invention peut être complété par un ou des capteurs de position fournissant une valeur représentative, au moins à un instant donné, de la distance entre la face latérale 2 et les cylindres 1. Ils permettent de s'assurer que pendant les phases où une usure de la face latérale 2 est recherchée, il y a bien contact entre elle et les cylindresl. D'autre part, en fonctionnement normal de l'installation, on peut désirer que ce contact ne soit pas tout à fait réalisé, et s'efforcer de maintenir en permanence un jeu de 0,1 à 0,2 mm, suffisamment faible pour éviter les fuites de métal liquide mais permettant de supprimer l'usure de la face latérale 2 par frottement. Seule subsisterait alors comme cause d'usure la corrosion par le métal liquide. Il est avantageux d'intégrer ces capteurs (par exemple du type capacitif) aux butées 13, 13' des tirants 11, 11' pour mesurer leur distance à la plaque de poussée 8. Ainsi, lorsque les organes de poussée 9, 9', 9'''', 9''' ont une extension réglable à la commande (si par exemple ce sont des vérins pilotés), on peut, après que les butées 13, 13' sont venues au contact de la plaque de poussée 8, faire reculer la face latérale 2 en diminuant l'extension des organes de poussée 9, 9', 9'', 9''' d'une distance correspondant à ce jeu.The device according to the invention can be supplemented by one or more sensors position providing a value representative, at least at a given time, of the distance between the side face 2 and the cylinders 1. They make it possible to ensure that during the phases where wear of the side face 2 is sought, there is good contact between it and the cylindersl. On the other hand, during normal operation of the installation, may wish this contact not to be fully realized, and endeavor to maintain permanent play of 0.1 to 0.2 mm, small enough to prevent metal leakage liquid but making it possible to eliminate wear on the side face 2 by friction. Alone Corrosion by liquid metal would then remain as a cause of wear. It is advantageous to integrate these sensors (for example of the capacitive type) with the stops 13, 13 ′ tie rods 11, 11 'for measuring their distance from the thrust plate 8. Thus, when the thrust members 9, 9 ', 9' '' ', 9' '' have an adjustable extension when ordered (if by example they are piloted jacks), we can, after the stops 13, 13 'have come in contact with the push plate 8, roll back the side face 2 while decreasing the extension of the thrust members 9, 9 ', 9' ', 9' '' by a distance corresponding to this clearance.

Claims (8)

  1. Device for supporting a side wall (2) of an installation for the twin-roll continuous casting of thin metal products of the type including two cooled rolls (1) with horizontal axes, two side walls (2) applied against the sides (3) of the rolls (1), the said support device including a carriage (5) which can be displaced on command in a direction parallel to the axes of the rolls (1), a thrust device (6) carried by the said carriage (5) and a panel (4), integral with the side wall (2), connected to the said thrust device (6) by means of a thrust plate (8) and thrust members (9, 9', 9'', 9''') bearing on the said thrust plate (8) and the said panel (4), characterized in that the said panel (4) includes at least one tie (11, 11') passing through the thrust plate (8) and the free end of which is equipped with a stop (13, 13') which can be applied against the rear face (14) of the said thrust plate (8).
  2. Device according to Claim 1, characterized in that the said plate (4) includes three ties (13, 13').
  3. Device according to Claim 1 or 2, characterized in that the said ties (13, 13') are distributed over a zone with a shape corresponding to that of the side wall (2).
  4. Device according to one of Claims 1 to 3, characterized in that the said thrust members (9, 9', 9'', 9''') are springs.
  5. Device according to one of Claims 1 to 3, characterized in that the said thrust members (9, 9', 9'', 9''') are controlled rams.
  6. Device according to one of Claims 1 to 5, characterized in that it includes one or more position sensors supplying a representative value, at least at a given instant, of the distance between the side wall (2) and the rolls (1).
  7. Device according to Claim 6, characterized in that the said position sensor or sensors are adapted to the measurement of the distances between the stops (13, 13') of the ties (11, 11') and the thrust plate (8).
  8. Device according to Claim 6 or 7, characterized in that the said position sensor or sensors is/are of the capacitive type.
EP96401654A 1995-08-18 1996-07-25 Supporting device for the side walls of a continuous roll caster installation for the production of metallic strips Expired - Lifetime EP0759335B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9509907A FR2737859B1 (en) 1995-08-18 1995-08-18 SUPPORT DEVICE FOR A SIDE FACE OF A CONTINUOUS CASTING PLANT OF METAL BANDS BETWEEN CYLINDERS
FR9509907 1995-08-18

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EP0759335A1 EP0759335A1 (en) 1997-02-26
EP0759335B1 true EP0759335B1 (en) 1999-10-27

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EP (1) EP0759335B1 (en)
JP (1) JPH0957402A (en)
KR (1) KR100369256B1 (en)
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AT (1) ATE185992T1 (en)
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DE (1) DE69604874T2 (en)
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FR (1) FR2737859B1 (en)
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MX (1) MX9603413A (en)
PL (1) PL180625B1 (en)
RO (1) RO117157B1 (en)
RU (1) RU2149075C1 (en)
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FR2787360B1 (en) 1998-12-21 2001-02-02 Usinor SIDE SIDE FOR CONTINUOUS CASTING INSTALLATION OF METAL STRIPS
EP1287926B1 (en) * 2001-08-29 2006-03-01 DANIELI & C. OFFICINE MECCANICHE S.p.A. Device for lateral containment of liquid steel between crystallizing rolls of a casting machine for a steel strip
US7556084B2 (en) * 2006-03-24 2009-07-07 Nucor Corporation Long wear side dams
ITUD20070047A1 (en) * 2007-03-02 2008-09-03 Danieli Off Mecc SUPPORTING STRUCTURE FOR CONTINUOUS CASTING MACHINE
DE102008010653B4 (en) * 2008-02-22 2019-04-04 Outokumpu Nirosta Gmbh Method and two-roll casting machine for producing cast from a molten metal strip
US7888158B1 (en) * 2009-07-21 2011-02-15 Sears Jr James B System and method for making a photovoltaic unit
KR101104196B1 (en) * 2009-11-25 2012-01-09 중앙대학교 산학협력단 Lactobacillus casei CB264, useful for preparing fermented milk, and fermented milk comprising the same
US10046384B2 (en) 2015-09-30 2018-08-14 Nucor Corporation Side dam with pocket
WO2017181231A1 (en) * 2016-04-19 2017-10-26 Nucor Corporation Method of operation of twin roll strip caster to reduce chatter
US11027330B2 (en) * 2016-08-10 2021-06-08 Nucor Corporation Method of thin strip casting
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JPH02104447A (en) * 1988-10-07 1990-04-17 Nisshin Steel Co Ltd Apparatus for continuously casting sheet metal
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JPH0741376B2 (en) * 1990-06-11 1995-05-10 新日本製鐵株式会社 Thin strip continuous casting method
FR2670143A1 (en) * 1990-12-11 1992-06-12 Usinor Sacilor DEVICE FOR CONTINUOUS CASTING A THIN STRIP OF METAL, IN PARTICULAR STEEL.
FR2670142A1 (en) * 1990-12-11 1992-06-12 Usinor Sacilor METHOD AND DEVICE FOR CONTINUOUS CASTING A METAL THIN STRIP AND SIDE SHUTTER PLATE OF SUCH CONTINUOUS CASTING DEVICE
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FR2721843B1 (en) * 1994-06-30 1996-08-30 Unisor Sacilor CONTINUOUS CASTING ARRANGEMENT BETWEEN CYLINDERS WITH APPLIED SIDE SHUTTER WALLS

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AU699790B2 (en) 1998-12-17
AU6080396A (en) 1997-02-20
BR9603447A (en) 1998-05-12
EP0759335A1 (en) 1997-02-26
KR100369256B1 (en) 2003-03-15
ATE185992T1 (en) 1999-11-15
CN1066081C (en) 2001-05-23
RU2149075C1 (en) 2000-05-20
RO117157B1 (en) 2001-11-30
DE69604874T2 (en) 2000-05-25
CA2181765A1 (en) 1997-02-19
KR970009934A (en) 1997-03-27
SK281772B6 (en) 2001-07-10
FR2737859A1 (en) 1997-02-21
PL180625B1 (en) 2001-03-30
MX9603413A (en) 1997-03-29
PL315734A1 (en) 1997-03-03
US5704414A (en) 1998-01-06
UA41391C2 (en) 2001-09-17
FR2737859B1 (en) 1997-09-12
CN1150920A (en) 1997-06-04
JPH0957402A (en) 1997-03-04
DK0759335T3 (en) 2000-04-25
CZ241196A3 (en) 1997-03-12
ES2140802T3 (en) 2000-03-01
CZ285964B6 (en) 1999-12-15
DE69604874D1 (en) 1999-12-02
ZA966867B (en) 1997-02-19
GR3032327T3 (en) 2000-04-27
TW308558B (en) 1997-06-21
SK102996A3 (en) 1998-01-14
TR199600668A2 (en) 1997-03-21

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