EP0922117B1 - Device for coupling a blow lance with a header - Google Patents

Device for coupling a blow lance with a header Download PDF

Info

Publication number
EP0922117B1
EP0922117B1 EP97930463A EP97930463A EP0922117B1 EP 0922117 B1 EP0922117 B1 EP 0922117B1 EP 97930463 A EP97930463 A EP 97930463A EP 97930463 A EP97930463 A EP 97930463A EP 0922117 B1 EP0922117 B1 EP 0922117B1
Authority
EP
European Patent Office
Prior art keywords
coupling
lance
pressure
piston
collector
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
EP97930463A
Other languages
German (de)
French (fr)
Other versions
EP0922117A1 (en
Inventor
Hubert Stomp
Serge Devillet
Fred Parasch
Daniel Fries
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.)
Paul Wurth SA
Original Assignee
Paul Wurth SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Paul Wurth SA filed Critical Paul Wurth SA
Publication of EP0922117A1 publication Critical patent/EP0922117A1/en
Application granted granted Critical
Publication of EP0922117B1 publication Critical patent/EP0922117B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

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
    • C21C5/4606Lances or injectors
    • C21C5/462Means for handling, e.g. adjusting, changing, coupling

Definitions

  • the present invention relates to a device for coupling a lance metallurgical blowing to a manifold.
  • the blowing lances are used for example for the conversion of cast iron in steel by blowing oxygen on the metal bath in a converter.
  • the blowing lances are generally cooled with a coolant, for example water, which circulates in a cooling circuit.
  • a lance comprises in general two annular chambers which are arranged coaxially around the oxygen channel of the lance and connected in the region of the lance nose so forming an annular supply and return channel for the fluid cooling. It follows that during its operation, such a lance must be connected to at least three pipes carrying the coolants and blowing.
  • the blowing lances must be changed due to wear after a fixed duration of use.
  • many devices have been proposed to partially automate the connection of the lance to the pipes necessary for its operation, i.e. to allow connection concomitant of all the necessary conducts.
  • Such devices include a coupling head with a first coupling surface and a clamping device for sealingly pressing the first surface coupling on a second coupling surface of the lance.
  • the head coupling comprises several coaxial channels, the first end of which is connected to one of the pipes carrying the coolants and blowing and the second end of which opens into the first surface coupling.
  • the coaxial channels of the lance open in the second mating surface, so that after establishment tight contact between the two elements by means of the tightening a transfer of fluids is made possible at the head-lance junction.
  • Document DE-A-2512 487 therefore proposes a coupling device in which the lance is suspended from the coupling head and fixed to it using two clamping bolts and attached nuts.
  • the bolts are mounted on the level of the coupling head so as to tilt laterally and are engaged in two notches with a flange secured to the lance. Strength necessary for the tight connection between the two mating surfaces is then established by tightening the two nuts.
  • the object of the present invention is to provide a coupling device for a blowing lance, allowing to dynamically adapt the force of pressure between the manifold and the lance as a function of pressure variations in cooling and / or blowing fluids.
  • this objective is achieved by a coupling device from a blowing lance to a collector, in which the force necessary to a tight junction between the collector and the lance is exerted by the fluid of cooling and / or blowing fluid.
  • the strength of pressure between the lance and the collector is not fixedly exerted by a conventional clamping means but it is exerted dynamically by one of the fluids necessary for the operation of the lance. This makes the pressure force between the collector and the lance varies according to the pressure of the fluid in question. As a result, abrupt variations in fluid pressures can be dynamically compensated so that even very violent water hammer does not lead to a risk of rupture of the system seal.
  • said cooling fluid and / or blowing acts via a pressure surface on the junction between the collector and the lance. It is known that the pressure force between the collector and the lance is proportional to the pressure of the fluid and to the surface area of pressure. It is obvious that we are talking here about the effective area of the pressure surface. The value of the pressure force for a certain fluid pressure can therefore be predetermined by the dimensioning of said pressure surface.
  • the pressure surface is, for example, integral with a piston which transmits the force of pressure at said junction.
  • the lance presents a first mating surface
  • the manifold has a second mating surface and one of said two mating surfaces is integral with said piston and opposite the pressure surface.
  • the piston can also constitute part of the lance as the collector. It includes one of the two surfaces required for the connection and tightens it tightly against the other of said two mating surfaces.
  • the piston is embedded in a recess of the manifold so as to delimit by said pressure surface a pressure at the bottom of said recess.
  • the pressure chamber can be connected directly to the fluid supply line cooling and / or blowing. Integrating the piston into the manifold also reduces investment costs since a refining unit includes several lances for a single collector.
  • the piston is executed in such a way that said force of pressure exerted by said piston is greater than the reaction force acting on the junction plane between said manifold and said lance.
  • difference between the seal obtained by the pressure force and the seal necessary, which constitutes the safety margin increases progressively as the pressure of the cooling and / or blowing fluid increases.
  • a preferred embodiment of the invention consists of a coupling device from a blowing lance to a manifold which is connected to pipes carrying blowing and cooling fluids, the lance comprising first channels for said fluids which extend through said lance and which open at one end into a first surface coupling, the manifold comprising second channels for said fluids, each of said second channels being associated with one of said first channels, being in connection with one of said conduits and opening out to a end in a second mating surface, said second surface of coupling being associated with said first coupling surface and which can be pressed against it by means of a clamping means so forming a tight junction between said first and second channels associated.
  • Said manifold comprises a coupling head and said second mating surface is integral with a piston which is embedded in a axial recess of said coupling block so as to delimit by a surface pressure chamber a pressure chamber at the bottom of said recess, said surface pressure of the piston being opposite the second coupling surface.
  • a supply line is connected to said pressure chamber so that the fluid supplied by said supply line exerts pressure on said pressure surface and therefore the piston exerts a pressing force on said first coupling surface.
  • this device makes it possible to dynamically compensate for sudden variations in fluid pressures and adapt automatically at high speed, i.e. at high fluid pressures, while retaining a safety margin in the form of minimum sealing required established by the clamping means.
  • the device comprises means attachment to suspend the lance to said coupling head.
  • Said hooking means eg hooks which are mounted pivotally on said coupling head and which can engage journals extending radially from said lance.
  • said attachment means comprise locking rods which are pivotally mounted on said coupling head as well as a radial flange on said lance on the side of the first coupling surface, said radial flange having radial notches intended to receive the locking rods so that the heads of said locking rods take support on the side of said flange which is opposite the first surface coupling.
  • the attachment is faster and poses less risk to the staff. Fixing with locking rods is particularly advantageous because it makes it possible to minimize the piston stroke.
  • the lance must be moved certain distance towards the coupling head until the heads blocking rods can pass the lower edge of said flange in order to be spread laterally.
  • the piston rests on the lance, it must also be moved the same distance, which should be done if necessary against the action of the clamping means. It is therefore advisable to limit the distance of movement to limit the work to be done to move the piston by example against the action of the clamping means or its weight.
  • Said clamping means preferably comprises springs which are arranged between the coupling head and said piston, said springs being prestressed when attaching the lance to the coupling head.
  • one of said two mating surfaces advantageously comprises an edge axially projecting annular extending, said annular edge having a inner diameter which is substantially equal to the outer diameter of the other said coupling surfaces.
  • Figure 1 shows a vertical cross section of a coupling for blowing lances. It includes a coupling head 2 which is connected to cooling and blowing fluid lines (not shown) on which a blowing lance 4 is hung.
  • the lance 4 comprises a central channel 6 for a blowing gas, eg oxygen, which is coaxially surrounded by two chambers 8, 10 with annular sections. Both chambers 8 and 10 are connected in the region of the lance nose 4 (not shown) so as to form a supply channel 8 and a return channel 10 to annular sections for the coolant.
  • the spear could include additional channels for other blowing gases. These channels would then be located coaxially between the central channel and the cooling system channels.
  • channels 6, 8 and 10 open out in a first mating surface 12 which is associated with a second coupling surface 14 of the coupling head 2.
  • channels 6, 8 and 10 then form mouths coaxial annulars which are separated radially by the front faces annular tubular walls 16, 18 and 20 of the different channels.
  • the walls 16, 18 and 20 are reinforced in the region of the first mating surface 12 and their front faces are executed in the form of surfaces sealing.
  • the first coupling surface 12 In order to allow a transfer of the cooling and blowing fluids from the coupling head 2 towards the lance 4, the first coupling surface 12 must be pressed tightly against the second mating surface 14 and a connection between channels 6, 8 and 10 and the pipes carrying the respective cooling and blowing fluids must be established.
  • the coupling head 2 advantageously comprises a piston 22 which is mounted axially sliding in a recess 24 of the coupling head 2 and can establish tight contact with the first coupling surface 12 under the action of a clamping means 25.
  • This piston 22 then has the second coupling surface 14 on its end oriented towards lance 4 and includes channels 26, 28 and 30 for fluids cooling and blowing which are assigned to channels 6, 8 and 10 of the lance 4.
  • One end of each channel 26, 28 and 30 opens out in such a way way in the second mating surface 14 that the mouths of the channels 6, 8 and 10 in the first mating surface 12 and the mouths respective channels 26, 28 and 30 in the second coupling surface 14 are superimposed exactly during mating.
  • the mouths of channels 26, 28 and 30 in the second coupling surface 14 are separated, similarly to the mouths of channels 6, 8 and 10 in the first mating surface 12, by front faces annular tubular walls separating the different channels 26, 28 and 30.
  • These annular front faces are then also executed in the form of sealing surfaces and, during coupling, bear on the faces respective annular front faces in the first mating surface 12.
  • the clamping means 25 which presses the second coupling surface 14 of the piston 22 against the first mating surface 12 of the lance comprises preferably springs which are arranged in a groove on the surface front of the coupling head 2 and bear against a radial projection 27 piston. These springs 25 are then prestressed during the coupling of the lance 4 and thus exert a force on the piston 22 in the direction of the lance 4. It it is obvious that any other tightening means would be suitable for pressing the piston 22 against lance 4, eg hydraulic cylinders, actuated worms by any motor, etc. or a combination of these.
  • the piston 22 On its end opposite to the second coupling surface 14, the piston 22 has a pressure surface 32 through which it delimits a pressure 34 in the bottom of the recess 24.
  • this pressure chamber 34 which in the example shown is connected to the supply line in coolant through a connecting pipe 36, the lance 4 is supplied with cooling fluid.
  • channel 28 of coolant supply opens into the surface of pressure 32 so as to be in connection with the pressure chamber 34.
  • the channel 30 for return of the cooling fluid advantageously opens in an annular chamber 38, delimited by a circumferential groove 40 in the piston and the side wall of the recess 24.
  • This annular chamber 38 is then connected to a connection pipe to the return line of the cooling fluid 42.
  • the axial dimension of the groove circumferential 40 is greater than the axial dimension of the mouth of the drain hose 42 so that the mouth of drain hose 42 is not blocked by the lateral surface of the piston during the axial displacement of this one.
  • the channel 26 of the blowing fluid opens into the pressure surface 32 of the piston 22 and is extended tightly through the pressure chamber 34 via a tube 44, one end of which is embedded so sliding and sealed in said channel 26 and the other end of which extends through the bottom of the recess 24 to exit at the top of the coupling head 2, where it ends in a connecting pipe 46 to the fluid line blowing.
  • the junction between the tube 44 and the channel 26 is made waterproof using several annular seals 48 arranged around the end embedded in the tube 44.
  • the pressure chamber 34 and the chamber ring 38 are sealed using O-rings which are arranged eg in circumferential grooves of piston 22.
  • An alternative design for connection of channel 26 to the respective supply line consists in extending the channel 26 beyond the pressure surface 32 so that it passes through the pressure chamber 34 and extends through a bore in the bottom of the recess 24 to exit at the top of the coupling head 2.
  • the channel 26 is guided through the bore in the bottom of the recess of watertight and axially sliding. Outside the coupling head 2, the channel 26 can then be connected to the gas supply pipe for blowing through a flexible compensator, which allows a tight connection and able to adapt to the axial displacements of the channel 26.
  • the lance is brought by a bridge or an ad hoc manipulator which positions it with its surface coupling 12 below the coupling surface 14 of the head coupling 2 so that the axes of the lance 4 and the coupling head 2 are aligned.
  • the piston 22 and therefore the second coupling surface 14 is now in their lowest position relative to the head coupling 2.
  • the lance 4 is then lifted until the two mating surfaces 12 and 14 come into contact.
  • one of the two surfaces (in the fig.1 the first mating surface 12) includes an annular edge 48 which extends axially and has an inner diameter which is substantially equal to the outside diameter of the other of said coupling surfaces 14.
  • the lance 4 is raised further and the piston 22 is moved against the action of the springs 25.
  • the weight of the collector and its equipment device acts as a counterforce, so the springs 25 can be prestressed with a force substantially equivalent to this weight.
  • the lance 4 is then advantageously hooked by two locking rods 50 which are mounted on either side of the coupling head 2 and are received by two notches 52 of a radial flange 54 of the lance 4, so that the heads 56 of the locking rods 50 bear on the lower surface of the flange 54.
  • the locking rods 50 are mounted on the coupling head 2 pivotally so that their heads 56 can be moved laterally (as indicated on the fig.).
  • the piston may as well be subjected to pressure blowing gas only at coolant pressure.

Landscapes

  • 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)
  • Threshing Machine Elements (AREA)
  • Quick-Acting Or Multi-Walled Pipe Joints (AREA)
  • Treatment Of Steel In Its Molten State (AREA)
  • Waste-Gas Treatment And Other Accessory Devices For Furnaces (AREA)
  • Nozzles (AREA)
  • Small-Scale Networks (AREA)
  • Furnace Details (AREA)

Abstract

A device for coupling a blow lance with a header is disclosed, in which the force required for producing a sealing joint between the header (2) and the lance (4) is exerted by a cooling fluid and/or a blowing fluid. In a preferred embodiment, said cooling fluid and/or blowing fluid acts via a pressure surface (32) on the joint between the header (2) and the lance (4), the pressure surface being integral with a piston (22) which transmits the pressure to said joint. The lance has preferably a first coupling surface (12), while the header (2) has a second coupling surface (14), and one of said coupling surfaces (12 or 14) is integral with said piston (22).

Description

La présente invention concerne un dispositif d'accouplement d'une lance de soufflage métallurgique à un collecteur.The present invention relates to a device for coupling a lance metallurgical blowing to a manifold.

Les lances de soufflage sont utilisées par exemple pour la conversion de fonte en acier par insufflation d'oxygène sur le bain métallique dans un convertisseur. Pour éviter un endommagement précoce des lances dû aux températures élevées dans le convertisseur, les lances de soufflage sont généralement refroidies à l'aide d'un fluide de refroidissement, de l'eau par exemple, qui circule dans un circuit de refroidissement. A cette fin, une lance comporte en général deux chambres annulaires qui sont disposées coaxialement autour du canal d'oxygène de la lance et reliées dans la région du nez de lance de façon à former un canal d'alimentation et un canal de retour, annulaires, pour le fluide de refroidissement. Il s'en suit que pendant son fonctionnement, une telle lance doit être raccordée à au moins trois conduites véhiculant les fluides de refroidissement et de soufflage.The blowing lances are used for example for the conversion of cast iron in steel by blowing oxygen on the metal bath in a converter. To avoid early damage to the lances due to temperatures high in the converter, the blowing lances are generally cooled with a coolant, for example water, which circulates in a cooling circuit. To this end, a lance comprises in general two annular chambers which are arranged coaxially around the oxygen channel of the lance and connected in the region of the lance nose so forming an annular supply and return channel for the fluid cooling. It follows that during its operation, such a lance must be connected to at least three pipes carrying the coolants and blowing.

Les lances de soufflage doivent être changées pour cause d'usure après une durée d'utilisation déterminée. En vue du remplacement rapide et facile d'une lance endommagée par une lance nouvelle, de nombreux dispositifs ont été proposés pour automatiser en partie le raccordement de la lance aux conduites nécessaires à son fonctionnement, c'est-à-dire pour permettre le raccordement concomitant de toutes les conduites nécessaires. De tels dispositifs comprennent une tête d'accouplement avec une première surface d'accouplement et un dispositif de serrage pour presser de manière étanche la première surface d'accouplement sur une deuxième surface d'accouplement de la lance. La tête d'accouplement comprend plusieurs canaux coaxiaux dont la première extrémité est reliée à une des conduites véhiculant les fluides de refroidissement et de soufflage et dont la deuxième extrémité débouche dans la première surface d'accouplement. De façon similaire, les canaux coaxiaux de la lance débouchent dans la deuxième surface d'accouplement, de sorte qu'après établissement du contact étanche entre les deux éléments au moyen du dispositif de serrage un transfert des fluides est rendu possible à la jonction tête-lance.The blowing lances must be changed due to wear after a fixed duration of use. For quick and easy replacement of a lance damaged by a new lance, many devices have been proposed to partially automate the connection of the lance to the pipes necessary for its operation, i.e. to allow connection concomitant of all the necessary conducts. Such devices include a coupling head with a first coupling surface and a clamping device for sealingly pressing the first surface coupling on a second coupling surface of the lance. The head coupling comprises several coaxial channels, the first end of which is connected to one of the pipes carrying the coolants and blowing and the second end of which opens into the first surface coupling. Similarly, the coaxial channels of the lance open in the second mating surface, so that after establishment tight contact between the two elements by means of the tightening a transfer of fluids is made possible at the head-lance junction.

Ainsi le document DE-A-2512 487 propose un dispositif d'accouplement dans lequel la lance est suspendue à la tête d'accouplement et fixée à celle-ci à l'aide de deux boulons de serrage et d'écrous adjoints. Les boulons sont montés au niveau de la tête d'accouplement de manière à basculer latéralement et sont engagés dans deux encoches d'une bride solidaire de la lance. La force nécessaire à la jonction étanche entre les deux surfaces d'accouplement est alors établie par serrage des deux écrous.Document DE-A-2512 487 therefore proposes a coupling device in which the lance is suspended from the coupling head and fixed to it using two clamping bolts and attached nuts. The bolts are mounted on the level of the coupling head so as to tilt laterally and are engaged in two notches with a flange secured to the lance. Strength necessary for the tight connection between the two mating surfaces is then established by tightening the two nuts.

Ce dispositif bien que très simple et compact présente cependant quelques inconvénients. En effet, le changement de la lance nécessite d'une part des travaux manuels, comme le desserrage et le serrage manuels des boulons, ce qui implique un risque d'accident compte tenu de l'environnement dans lequel ces travaux se situent et d'autre part, le caractère fixe de la manière d'étanchéification, c'est-à-dire le serrage direct des deux surfaces d'accouplement, pose un problème lors de variations brusques de pression des fluides de refroidissement et de soufflage. De telles variations qui se produisent par exemple en régime transitoire sous forme de coups de bélier se propagent à travers le système de refroidissement et peuvent provoquer une interruption passagère de l'étanchéité au niveau du joint entre la tête d'accouplement et la lance. Un remède contre une telle rupture serait de serrer davantage les écrous afin d'augmenter la force d'appui des deux surfaces d'accouplement. Cependant la force de serrage des deux surfaces d'accouplement ne peut pas être augmentée indéfiniment afin de ne pas détruire les surfaces d'étanchéité des surfaces d'accouplement.This device, although very simple and compact, nevertheless presents some disadvantages. Indeed, changing the lance requires on the one hand manual work, such as loosening and tightening the bolts manually, which implies a risk of accident taking into account the environment in which these works are located and on the other hand, the fixed nature of the sealing manner, i.e. direct clamping of the two mating surfaces, installation a problem with sudden changes in coolant pressure and blowing. Such variations that occur for example in transient regime in the form of water hammer spread through the cooling system and can cause a temporary interruption sealing at the joint between the coupling head and the lance. A remedy for such a break would be to tighten the nuts further so increase the contact force of the two mating surfaces. However the clamping force of the two mating surfaces cannot be increased indefinitely so as not to destroy the sealing surfaces of the surfaces coupling.

L'objet de la présente invention est de proposer un dispositif d'accouplement pour une lance de soufflage, permettant d'adapter dynamiquement la force de pression entre le collecteur et la lance en fonction des variations de pression dans les fluides de refroidissement et/ou de soufflage.The object of the present invention is to provide a coupling device for a blowing lance, allowing to dynamically adapt the force of pressure between the manifold and the lance as a function of pressure variations in cooling and / or blowing fluids.

Conformément à l'invention, cet objectif est atteint par un dispositif d'accouplement d'une lance de soufflage à un collecteur, dans lequel la force nécessaire à une jonction étanche entre le collecteur et la lance est exercée par le fluide de refroidissement et/ou fluide de soufflage. Dans un tel dispositif, la force de pression entre la lance et le collecteur n'est pas exercée de manière fixe par un moyen de serrage conventionnel mais elle est exercée de manière dynamique par un des fluides nécessaires au fonctionnement de la lance. Ceci fait que la force de pression entre le collecteur et la lance varie en fonction de la pression du fluide en question. En conséquence, des variations brusques dans les pressions des fluides peuvent être compensées de façon dynamique de sorte que même des coups de bélier très violents ne conduisent pas à un risque de rupture de l'étanchéité du système. De plus, aucun ajustement de la force de serrage du moyen de serrage n'est requis lors de l'utilisation du dispositif à régime élevé, c'est-à-dire à des pressions de fluides élevées. En effet, l'adaptation dynamique de la force d'appui des deux surfaces d'accouplement augmente la force de pression de manière automatique dès que la pression des fluides augmente et conserve ainsi une étanchéité de base préétablie avec une certaine marge de sécurité.According to the invention, this objective is achieved by a coupling device from a blowing lance to a collector, in which the force necessary to a tight junction between the collector and the lance is exerted by the fluid of cooling and / or blowing fluid. In such a device, the strength of pressure between the lance and the collector is not fixedly exerted by a conventional clamping means but it is exerted dynamically by one of the fluids necessary for the operation of the lance. This makes the pressure force between the collector and the lance varies according to the pressure of the fluid in question. As a result, abrupt variations in fluid pressures can be dynamically compensated so that even very violent water hammer does not lead to a risk of rupture of the system seal. In addition, no adjustment of the strength of tightening of the clamping means is not required when using the device to high speed, i.e. at high fluid pressures. Indeed, the adaptation dynamics of the support force of the two mating surfaces increases the pressure force automatically as soon as the pressure of the fluids increases and thus retains a pre-established basic seal with a some safety margin.

Dans une exécution préférée, ledit fluide de refroidissement et/ou fluide de soufflage agit par l'intermédiaire d'une surface de pression sur la jonction entre le collecteur et la lance. Il est connu, que la force de pression entre le collecteur et la lance est proportionnelle à la pression du fluide et à l'aire de la surface de pression. Il est évident qu'on parle ici de l'aire effective de la surface de pression. La valeur de la force de pression pour une certaine pression du fluide peut donc être prédéterminé par le dimensionnement de ladite surface de pression.In a preferred embodiment, said cooling fluid and / or blowing acts via a pressure surface on the junction between the collector and the lance. It is known that the pressure force between the collector and the lance is proportional to the pressure of the fluid and to the surface area of pressure. It is obvious that we are talking here about the effective area of the pressure surface. The value of the pressure force for a certain fluid pressure can therefore be predetermined by the dimensioning of said pressure surface.

La surface de pression est p.ex. solidaire d'un piston qui transmet la force de pression à ladite jonction. De préférence, la lance présente une première surface d'accouplement, le collecteur présente une deuxième surface d'accouplement et l'une desdites deux surfaces d'accouplement est solidaire dudit piston et opposée à la surface de pression. Le piston peut aussi bien constituer une partie de la lance que du collecteur. Il comprend une des deux surfaces d'accouplement nécessaires à la jonction et serre celle-ci de manière étanche contre l'autre desdites deux surfaces d'accouplement. The pressure surface is, for example, integral with a piston which transmits the force of pressure at said junction. Preferably, the lance presents a first mating surface, the manifold has a second mating surface and one of said two mating surfaces is integral with said piston and opposite the pressure surface. The piston can also constitute part of the lance as the collector. It includes one of the two surfaces required for the connection and tightens it tightly against the other of said two mating surfaces.

Dans une exécution préférée, le piston est encastré dans un évidement du collecteur de façon à délimiter par ladite surface de pression une chambre de pression au fond dudit évidement. De cette manière, la chambre de pression peut être connectée directement à la conduite d'alimentation du fluide de refroidissement et/ou de soufflage. Le fait d'intégrer le piston dans le collecteur permet par ailleurs de diminuer les coûts d'investissement étant donné qu'une unité d'affinage comprend plusieurs lances pour un seul collecteur.In a preferred embodiment, the piston is embedded in a recess of the manifold so as to delimit by said pressure surface a pressure at the bottom of said recess. In this way, the pressure chamber can be connected directly to the fluid supply line cooling and / or blowing. Integrating the piston into the manifold also reduces investment costs since a refining unit includes several lances for a single collector.

Avantageusement le piston est exécuté de telle manière que ladite force de pression exercée par ledit piston est supérieure à la force de réaction agissant sur le plan de jonction entre ledit collecteur et ladite lance. Dans ce cas, la différence entre l'étanchéité obtenue par la force de pression et l'étanchéité nécessaire, qui constitue la marge de sécurité, augmente au fur et à mesure que la pression du fluide de refroidissement et/ou de soufflage augmente.Advantageously, the piston is executed in such a way that said force of pressure exerted by said piston is greater than the reaction force acting on the junction plane between said manifold and said lance. In this case difference between the seal obtained by the pressure force and the seal necessary, which constitutes the safety margin, increases progressively as the pressure of the cooling and / or blowing fluid increases.

Une réalisation préférentielle de l'invention consiste en un dispositif d'accouplement d'une lance de soufflage à un collecteur qui est raccordée à des conduites véhiculant des fluides de soufflage et de refroidissement, la lance comprenant des premiers canaux pour lesdits fluides qui s'étendent à travers ladite lance et qui débouchent à une extrémité dans une première surface d'accouplement, le collecteur comprenant des deuxièmes canaux pour lesdits fluides, chacun desdits deuxièmes canaux étant associé à un desdits premiers canaux, étant en connexion avec une desdites conduites et débouchant à une extrémité dans une deuxième surface d'accouplement, ladite deuxième surface d'accouplement étant associée à ladite première surface d'accouplement et pouvant être pressée contre celle-ci à l'aide d'un moyen de serrage de manière à former une jonction étanche entre lesdits premiers et deuxièmes canaux associés. Ledit collecteur comprend une tête d'accouplement et ladite deuxième surface d'accouplement est solidaire d'un piston qui est encastré dans un évidement axial dudit bloc d'accouplement de façon à délimiter par une surface de pression une chambre de pression au fond dudit évidement, ladite surface de pression du piston étant opposée à la deuxième surface d'accouplement. Une conduite d'alimentation est en connexion avec ladite chambre de pression de telle sorte que le fluide alimenté par ladite conduite d'alimentation exerce une pression sur ladite surface de pression et que par conséquent le piston exerce une force de pression sur ladite première surface d'accouplement.A preferred embodiment of the invention consists of a coupling device from a blowing lance to a manifold which is connected to pipes carrying blowing and cooling fluids, the lance comprising first channels for said fluids which extend through said lance and which open at one end into a first surface coupling, the manifold comprising second channels for said fluids, each of said second channels being associated with one of said first channels, being in connection with one of said conduits and opening out to a end in a second mating surface, said second surface of coupling being associated with said first coupling surface and which can be pressed against it by means of a clamping means so forming a tight junction between said first and second channels associated. Said manifold comprises a coupling head and said second mating surface is integral with a piston which is embedded in a axial recess of said coupling block so as to delimit by a surface pressure chamber a pressure chamber at the bottom of said recess, said surface pressure of the piston being opposite the second coupling surface. A supply line is connected to said pressure chamber so that the fluid supplied by said supply line exerts pressure on said pressure surface and therefore the piston exerts a pressing force on said first coupling surface.

Dans ce dispositif, une partie seulement de la force d'appui nécessaire à la jonction étanche entre la tête d'accouplement et la lance est exercée par un moyen de serrage conventionnel, c'est-à-dire de manière fixe. Il s'agit d'une certaine force de pression de base qui garantit l'étanchéité minimale requise. Lors de l'affinage, la pression du fluide alimenté par la conduite en connexion avec la chambre de pression, de préférence le fluide de refroidissement, exerce une pression sur la surface de pression du piston et par conséquent le piston exerce une force de pression sur la première surface d'accouplement de la lance. En raison des surfaces de pressions effectives pour les fluides et de la perte de charge dans le système de refroidissement entre la conduite d'alimentation et la conduite de retour, cette force de pression est supérieure ou égale à la force de réaction exercée sur la jonction entre la tête d'accouplement et la lance. Il en résulte une augmentation de la force d'appui des deux surfaces d'accouplement et par conséquent de l'étanchéité de l'accouplement. Comme décrit plus haut, ce dispositif permet de compenser de façon dynamique des variations brusques dans les pressions de fluides et de s'adapter automatiquement à un régime élevé, c'est-à-dire à des pressions de fluides élevées, tout en conservant une marge de sécurité sous la forme de l'étanchéité minimale requise établie par les moyens de serrage.In this device, only part of the supporting force necessary for the tight connection between the coupling head and the lance is exerted by a conventional clamping means, that is to say in a fixed manner. It's about a certain basic pressing force which guarantees the minimum required tightness. During refining, the pressure of the fluid supplied by the connecting pipe with the pressure chamber, preferably the coolant, exerts pressure on the pressure surface of the piston and therefore the piston exerts a pressing force on the first mating surface of the launch. Due to the effective pressure surfaces for fluids and the pressure drop in the cooling system between the supply line and the return line, this pressing force is greater or equal to the reaction force exerted on the junction between the coupling head and launches it. This results in an increase in the bearing force of the two surfaces coupling and therefore the sealing of the coupling. As described above, this device makes it possible to dynamically compensate for sudden variations in fluid pressures and adapt automatically at high speed, i.e. at high fluid pressures, while retaining a safety margin in the form of minimum sealing required established by the clamping means.

Dans une réalisation préférée de l'invention, le dispositif comprend des moyens d'accrochage pour suspendre la lance à ladite tête d'accouplement. Lesdits moyens d'accrochage comprennent p.ex. des crochets qui sont montés de manière pivotante sur ladite tête d'accouplement et qui peuvent enclencher des tourillons s'étendant radialement à partir de ladite lance. Dans une autre exécution, lesdits moyens d'accrochage comprennent des tiges de blocage qui sont montées de manière pivotante sur ladite tête d'accouplement ainsi qu'une bride radiale sur ladite lance du côté de la première surface d'accouplement, ladite bride radiale présentant des encoches radiales destinées à recevoir les tiges de blocage de sorte que les têtes desdites tiges de blocage prennent appui sur le côté de ladite bride qui est à l'opposé de la première surface d'accouplement. Ces deux exécutions de moyens d'accrochage suppriment la nécessité de travaux manuels tels que le serrage et le desserrage d'écrous. L'accrochage se fait plus rapidement et constitue moins de risques pour le personnel. La fixation à l'aide de tiges de blocage est particulièrement avantageuse du fait qu'elle permet de réduire au minimum la course du piston. En effet, pour remplacer une lance accrochée, la lance doit être déplacée d'une certaine distance en direction de la tête d'accouplement jusqu'à ce que les têtes des tiges de blocage puissent passer le bord inférieur de ladite bride afin d'être écartées latéralement. Comme le piston s'appuie sur la lance, il doit également être déplacé de la même distance, ce qui doit se faire le cas échéant contre l'action du moyen de serrage. Il convient donc de limiter la distance de déplacement afin de limiter le travail devant être effectué pour déplacer le piston par exemple contre l'action du moyen de serrage ou de son poids.In a preferred embodiment of the invention, the device comprises means attachment to suspend the lance to said coupling head. Said hooking means, eg hooks which are mounted pivotally on said coupling head and which can engage journals extending radially from said lance. In an other execution, said attachment means comprise locking rods which are pivotally mounted on said coupling head as well as a radial flange on said lance on the side of the first coupling surface, said radial flange having radial notches intended to receive the locking rods so that the heads of said locking rods take support on the side of said flange which is opposite the first surface coupling. These two executions of fastening means eliminate the the need for manual work such as tightening and loosening nuts. The attachment is faster and poses less risk to the staff. Fixing with locking rods is particularly advantageous because it makes it possible to minimize the piston stroke. In indeed, to replace a hanging lance, the lance must be moved certain distance towards the coupling head until the heads blocking rods can pass the lower edge of said flange in order to be spread laterally. As the piston rests on the lance, it must also be moved the same distance, which should be done if necessary against the action of the clamping means. It is therefore advisable to limit the distance of movement to limit the work to be done to move the piston by example against the action of the clamping means or its weight.

Ledit moyen de serrage comprend de préférence des ressorts qui sont disposés entre la tête d'accouplement et ledit piston, lesdits ressorts étant précontraints lors de l'accrochage de la lance à la tête d'accouplement.Said clamping means preferably comprises springs which are arranged between the coupling head and said piston, said springs being prestressed when attaching the lance to the coupling head.

Afin de faciliter la centrage desdites deux surfaces d'accouplement, l'une desdites deux surfaces d'accouplement comprend avantageusement un bord annulaire en saillie s'étendant axialement, ledit bord annulaire présentant un diamètre intérieur qui est sensiblement égal au diamètre extérieur de l'autre desdites surfaces d'accouplement.In order to facilitate the centering of said two coupling surfaces, one of said two mating surfaces advantageously comprises an edge axially projecting annular extending, said annular edge having a inner diameter which is substantially equal to the outer diameter of the other said coupling surfaces.

Un peu plus loin, un mode de réalisation préféré de l'invention est décrit à l'aide de la figure 1 qui montre une coupe transversale verticale d'un accouplement pour lances de soufflage. Il comprend une tête d'accouplement 2 qui est raccordée à des conduites de fluides de refroidissement et de soufflage (non représentées) sur laquelle une lance de soufflage 4 est accrochée. La lance 4 comprend un canal central 6 pour un gaz de soufflage, p.ex. l'oxygène, qui est entouré coaxialement par deux chambres 8, 10 à sections annulaires. Les deux chambres 8 et 10 sont reliées dans la région du nez de lance 4 (non représentée) de façon à former un canal d'alimentation 8 et un canal de retour 10 à sections annulaires pour le fluide de refroidissement. Il est à noter que la lance pourrait comprendre des canaux supplémentaires pour d'autres gaz de soufflage. Ces canaux se situeraient alors coaxialement entre le canal central et les canaux du circuit de refroidissement.A little further on, a preferred embodiment of the invention is described using in Figure 1 which shows a vertical cross section of a coupling for blowing lances. It includes a coupling head 2 which is connected to cooling and blowing fluid lines (not shown) on which a blowing lance 4 is hung. The lance 4 comprises a central channel 6 for a blowing gas, eg oxygen, which is coaxially surrounded by two chambers 8, 10 with annular sections. Both chambers 8 and 10 are connected in the region of the lance nose 4 (not shown) so as to form a supply channel 8 and a return channel 10 to annular sections for the coolant. Note that the spear could include additional channels for other blowing gases. These channels would then be located coaxially between the central channel and the cooling system channels.

Sur l'extrémité d'accouplement de la lance 4, les canaux 6, 8 et 10 débouchent dans une première surface d'accouplement 12 qui est associée à une deuxième surface d'accouplement 14 de la tête d'accouplement 2. Dans ladite première surface d'accouplement 12, les canaux 6, 8 et 10 forment alors des embouchures annulaires coaxiales qui sont séparées radialement par les faces frontales annulaires des parois tubulaires 16, 18 et 20 des différents canaux. Les parois 16, 18 et 20 sont renforcées dans la région de la première surface d'accouplement 12 et leurs faces frontales sont exécutées sous forme de surfaces d'étanchéité.On the coupling end of the lance 4, the channels 6, 8 and 10 open out in a first mating surface 12 which is associated with a second coupling surface 14 of the coupling head 2. In said first mating surface 12, channels 6, 8 and 10 then form mouths coaxial annulars which are separated radially by the front faces annular tubular walls 16, 18 and 20 of the different channels. The walls 16, 18 and 20 are reinforced in the region of the first mating surface 12 and their front faces are executed in the form of surfaces sealing.

Afin de permettre un transfert des fluides de refroidissement et de soufflage de la tête d'accouplement 2 vers la lance 4, la première surface d'accouplement 12 doit être pressée de manière étanche contre la deuxième surface d'accouplement 14 et une connexion entre les canaux 6, 8 et 10 et les conduites véhiculant les fluides de refroidissement et de soufflage respectives doit être établie.In order to allow a transfer of the cooling and blowing fluids from the coupling head 2 towards the lance 4, the first coupling surface 12 must be pressed tightly against the second mating surface 14 and a connection between channels 6, 8 and 10 and the pipes carrying the respective cooling and blowing fluids must be established.

Pour ce faire, la tête d'accouplement 2 comprend avantageusement un piston 22 qui est monté de manière axialement coulissante dans un évidement 24 de la tête d'accouplement 2 et peut établir un contact étanche avec la première surface d'accouplement 12 sous l'action d'un moyen de serrage 25. Ce piston 22 présente alors la deuxième surface d'accouplement 14 sur son extrémité orientée vers la lance 4 et comprend des canaux 26, 28 et 30 pour les fluides de refroidissement et de soufflage qui sont affectés aux canaux 6, 8 et 10 de la lance 4. Une des extrémités de chaque canal 26, 28 et 30 débouche de telle façon dans la deuxième surface d'accouplement 14 que les embouchures des canaux 6, 8 et 10 dans la première surface d'accouplement 12 et les embouchures des canaux 26, 28 et 30 respectives dans la deuxième surface d'accouplement 14 se superposent exactement lors de l'accouplement. Dans ce cas-ci, les embouchures des canaux 26, 28 et 30 dans la deuxième surface d'accouplement 14 sont séparées, semblablement aux embouchures des canaux 6, 8 et 10 dans la première surface d'accouplement 12, par des faces frontales annulaires de parois tubulaires séparant les différents canaux 26, 28 et 30. Ces faces frontales annulaires sont alors également exécutées sous forme de surfaces d'étanchéité et, lors de l'accouplement, prennent appui sur les faces frontales annulaires respectives dans la première surface d'accouplement 12.To do this, the coupling head 2 advantageously comprises a piston 22 which is mounted axially sliding in a recess 24 of the coupling head 2 and can establish tight contact with the first coupling surface 12 under the action of a clamping means 25. This piston 22 then has the second coupling surface 14 on its end oriented towards lance 4 and includes channels 26, 28 and 30 for fluids cooling and blowing which are assigned to channels 6, 8 and 10 of the lance 4. One end of each channel 26, 28 and 30 opens out in such a way way in the second mating surface 14 that the mouths of the channels 6, 8 and 10 in the first mating surface 12 and the mouths respective channels 26, 28 and 30 in the second coupling surface 14 are superimposed exactly during mating. In this case, the mouths of channels 26, 28 and 30 in the second coupling surface 14 are separated, similarly to the mouths of channels 6, 8 and 10 in the first mating surface 12, by front faces annular tubular walls separating the different channels 26, 28 and 30. These annular front faces are then also executed in the form of sealing surfaces and, during coupling, bear on the faces respective annular front faces in the first mating surface 12.

Le moyen de serrage 25 qui presse la deuxième surface d'accouplement 14 du piston 22 contre la première surface d'accouplement 12 de la lance comprend de préférence des ressorts qui sont disposés dans une rainure de la surface frontale de la tête d'accouplement 2 et s'appuient contre une saillie radiale 27 du piston. Ces ressorts 25 sont alors précontraints lors de l'accouplement de la lance 4 et exercent ainsi une force sur le piston 22 en direction de la lance 4. Il est évident que tout autre moyen de serrage conviendrait pour presser le piston 22 contre la lance 4, p.ex. des vérins hydrauliques, des vis sans fin actionnées par un moteur quelconque, etc. ou une combinaison de ceux-ci.The clamping means 25 which presses the second coupling surface 14 of the piston 22 against the first mating surface 12 of the lance comprises preferably springs which are arranged in a groove on the surface front of the coupling head 2 and bear against a radial projection 27 piston. These springs 25 are then prestressed during the coupling of the lance 4 and thus exert a force on the piston 22 in the direction of the lance 4. It it is obvious that any other tightening means would be suitable for pressing the piston 22 against lance 4, eg hydraulic cylinders, actuated worms by any motor, etc. or a combination of these.

Sur son extrémité opposée à la deuxième surface d'accouplement 14, le piston 22 présente une surface de pression 32 par laquelle il délimite une chambre de pression 34 dans le fond de l'évidement 24. A travers cette chambre de pression 34, qui dans l'exemple représenté est connectée à la conduite d'alimentation en fluide de refroidissement par l'intermédiaire d'un tuyau de raccordement 36, la lance 4 est alimentée en fluide de refroidissement. A cette fin, le canal 28 d'alimentation en fluide de refroidissement débouche dans la surface de pression 32 de façon à être en connexion avec la chambre de pression 34. Le canal 30 de retour du fluide de refroidissement débouche avantageusement dans une chambre annulaire 38, délimitée par une gorge circonférentielle 40 dans le piston et la paroi latérale de l'évidement 24. Cette chambre annulaire 38 est alors connectée à un tuyau de raccordement à la conduite de retour du fluide de refroidissement 42. Il est à noter que la dimension axiale de la gorge circonférentielle 40 est supérieure à la dimension axiale de l'embouchure du tuyau d'évacuation 42 de sorte que l'embouchure du tuyau d'évacuation 42 n'est pas obturée par la surface latérale du piston lors du déplacement axial de celui-ci. On its end opposite to the second coupling surface 14, the piston 22 has a pressure surface 32 through which it delimits a pressure 34 in the bottom of the recess 24. Through this pressure chamber 34, which in the example shown is connected to the supply line in coolant through a connecting pipe 36, the lance 4 is supplied with cooling fluid. To this end, channel 28 of coolant supply opens into the surface of pressure 32 so as to be in connection with the pressure chamber 34. The channel 30 for return of the cooling fluid advantageously opens in an annular chamber 38, delimited by a circumferential groove 40 in the piston and the side wall of the recess 24. This annular chamber 38 is then connected to a connection pipe to the return line of the cooling fluid 42. It should be noted that the axial dimension of the groove circumferential 40 is greater than the axial dimension of the mouth of the drain hose 42 so that the mouth of drain hose 42 is not blocked by the lateral surface of the piston during the axial displacement of this one.

Le canal 26 du fluide de soufflage débouche dans la surface de pression 32 du piston 22 et est prolongé de manière étanche à travers la chambre de pression 34 par l'intermédiaire d'un tube 44, dont une extrémité est encastrée de manière coulissante et étanche dans ledit canal 26 et dont l'autre extrémité s'étend à travers le fond de l'évidement 24 pour sortir en haut de la tête d'accouplement 2, où il se termine dans un tuyau de raccordement 46 à la conduite du fluide de soufflage. Il est à noter que la jonction entre le tube 44 et le canal 26 est rendue étanche à l'aide de plusieurs joints annulaires 48 disposés autour de l'extrémité encastrée du tube 44. De même, la chambre de pression 34 et la chambre annulaire 38 sont rendues étanches à l'aide de joints toriques qui sont disposés p.ex. dans des rainures circonférentielles du piston 22. Une exécution alternative pour la connexion du canal 26 à la conduite d'alimentation respective consiste à prolonger le canal 26 au-delà de la surface de pression 32 de sorte qu'il traverse la chambre de pression 34 et s'étend à travers un alésage dans le fond de l'évidement 24 pour sortir en haut de la tête d'accouplement 2. Dans ce cas-ci le canal 26 est guidé à travers l'alésage dans le fond de l'évidement de manière étanche et axialement coulissant. A l'extérieur de la tête d'accouplement 2, le canal 26 peut ensuite être relié à la conduite d'alimentation du gaz de soufflage par l'intermédiaire d'un compensateur flexible, qui permet de réaliser une connexion étanche et capable à s'adapter aux déplacements axiaux du canal 26.The channel 26 of the blowing fluid opens into the pressure surface 32 of the piston 22 and is extended tightly through the pressure chamber 34 via a tube 44, one end of which is embedded so sliding and sealed in said channel 26 and the other end of which extends through the bottom of the recess 24 to exit at the top of the coupling head 2, where it ends in a connecting pipe 46 to the fluid line blowing. It should be noted that the junction between the tube 44 and the channel 26 is made waterproof using several annular seals 48 arranged around the end embedded in the tube 44. Similarly, the pressure chamber 34 and the chamber ring 38 are sealed using O-rings which are arranged eg in circumferential grooves of piston 22. An alternative design for connection of channel 26 to the respective supply line consists in extending the channel 26 beyond the pressure surface 32 so that it passes through the pressure chamber 34 and extends through a bore in the bottom of the recess 24 to exit at the top of the coupling head 2. In this in this case the channel 26 is guided through the bore in the bottom of the recess of watertight and axially sliding. Outside the coupling head 2, the channel 26 can then be connected to the gas supply pipe for blowing through a flexible compensator, which allows a tight connection and able to adapt to the axial displacements of the channel 26.

Pour accoupler une lance 4 à ce dispositif d'accouplement, la lance est amenée par un pont ou un manipulateur ad hoc qui la positionne avec sa surface d'accouplement 12 au-dessous de la surface d'accouplement 14 de la tête d'accouplement 2 de sorte que les axes de la lance 4 et de la tête d'accouplement 2 sont alignés. Sous l'action de son poids resp. du moyen de serrage 25, le piston 22 et par conséquent la deuxième surface d'accouplement 14 se trouvent à ce instant dans leur position la plus basse par rapport à la tête d'accouplement 2. La lance 4 est ensuite soulevée jusqu'à ce que les deux surfaces d'accouplement 12 et 14 entrent en contact. Pour faciliter le centrage des deux surfaces d'accouplement 12 et 14, l'une des deux surfaces (dans la fig.1 la première surface d'accouplement 12) comprend un bord annulaire 48 qui s'étend axialement et présente un diamètre intérieur qui est sensiblement égal au diamètre extérieur de l'autre desdites surfaces d'accouplement 14.To couple a lance 4 to this coupling device, the lance is brought by a bridge or an ad hoc manipulator which positions it with its surface coupling 12 below the coupling surface 14 of the head coupling 2 so that the axes of the lance 4 and the coupling head 2 are aligned. Under the action of its weight resp. clamping means 25, the piston 22 and therefore the second coupling surface 14 is are now in their lowest position relative to the head coupling 2. The lance 4 is then lifted until the two mating surfaces 12 and 14 come into contact. To facilitate centering of the two mating surfaces 12 and 14, one of the two surfaces (in the fig.1 the first mating surface 12) includes an annular edge 48 which extends axially and has an inner diameter which is substantially equal to the outside diameter of the other of said coupling surfaces 14.

Après établissement du contact entre les deux surfaces d'accouplement, la lance 4 est soulevée davantage et le piston 22 est déplacé contre l'action des ressorts 25. Il est à noter que le poids du collecteur et de son équipement périphérique agit ici comme contre-force, de sorte que les ressorts 25 peuvent être précontraints d'une force substantiellement équivalente à ce poids. La lance 4 est ensuite avantageusement accrochée par deux tiges de blocage 50 qui sont montées de part et d'autre de la tête d'accouplement 2 et sont reçues par deux encoches 52 d'une bride radiale 54 de la lance 4, de sorte que les têtes 56 des tiges de blocage 50 prennent appui sur la surface inférieure de la bride 54. Afin de pouvoir enlever la lance 4, les tiges de blocage 50 sont montées au niveau de la tête d'accouplement 2 de manière pivotante de sorte que leurs têtes 56 peuvent être écartées latéralement (comme indiqué sur la fig.).After establishing contact between the two mating surfaces, the lance 4 is raised further and the piston 22 is moved against the action of the springs 25. It should be noted that the weight of the collector and its equipment device here acts as a counterforce, so the springs 25 can be prestressed with a force substantially equivalent to this weight. The lance 4 is then advantageously hooked by two locking rods 50 which are mounted on either side of the coupling head 2 and are received by two notches 52 of a radial flange 54 of the lance 4, so that the heads 56 of the locking rods 50 bear on the lower surface of the flange 54. In order to be able to remove the lance 4, the locking rods 50 are mounted on the coupling head 2 pivotally so that their heads 56 can be moved laterally (as indicated on the fig.).

De cette manière, un accouplement "de base" est réalisé sous l'action des ressorts 25 qui présente une étanchéité minimale nécessaire pour démarrer l'alimentation en fluide de refroidissement. Lors de l'alimentation en fluide de refroidissement, la pression du fluide de refroidissement exerce une pression sur la surface de pression 32 du piston 22 et par conséquent le piston 22 exerce une force de pression sur la première surface d'accouplement 12 de la lance 4. Il sera évident pour l'homme de l'art de dimensionner le piston 22 de telle manière qu'en raison des surfaces de pressions effectives pour les fluides et de la perte de charge dans le système de refroidissement entre la conduite d'alimentation et la conduite de retour, la force de pression exercée par le piston soit supérieure ou égale à la force de réaction exercée sur la jonction entre la tête d'accouplement et la lance. Dans ce cas-ci, il en résulte une augmentation de la force d'appui des deux surfaces d'accouplement et par conséquent de l'étanchéité de l'accouplement. Ce dispositif permet donc de compenser de façon dynamique des variations brusques dans les pressions de fluides et de s'adapter automatiquement à un régime élevé. In this way, a "basic" coupling is achieved under the action of springs 25 which has a minimum seal necessary to start the coolant supply. When supplying cooling, the coolant pressure exerts a pressure on the pressure surface 32 of the piston 22 and consequently the piston 22 exerts a pressing force on the first coupling surface 12 of the lance 4. It will be obvious to those skilled in the art to size the piston 22 of in such a way that due to the effective pressure surfaces for the fluids and the pressure drop in the cooling system between the pipe supply and return line, the pressure force exerted by the piston is greater than or equal to the reaction force exerted on the junction between the coupling head and the lance. In this case, it results in a increase in the support force of the two mating surfaces and by consequently of the sealing of the coupling. This device therefore makes it possible to dynamically compensate for sudden changes in pressure from fluids and automatically adapt to a high regime.

Il faut encore remarquer que le piston peut aussi bien être soumis à la pression du gaz de soufflage qu'à la pression du fluide de refroidissement.It should also be noted that the piston may as well be subjected to pressure blowing gas only at coolant pressure.

Claims (12)

  1. Device for coupling a blowing lance to a collector, characterised in that the force necessary for an impervious junction between the collector (2) and the lance (4) is exerted by a cooling fluid and/or a blowing fluid.
  2. Coupling device according to Claim 1, characterised in that the said cooling fluid and/or the blowing fluid acts through the intermediary of a pressure surface (32) on the junction between the collector (2) and the lance (4).
  3. Coupling device according to Claim 2, characterised in that the pressure surface (32) is an integral part of a piston (22) which transmits the pressure force to the said junction.
  4. Coupling device according to Claim 3, characterised in that the lance (4) has a first coupling surface (12), in that the collector (2) has a second coupling surface (14), and in that one of the two coupling surfaces (12 or 14) is an integral part of the said piston (22).
  5. Coupling device according to Claim 3 or 4, characterised in that the piston (22) is embedded in a recess (24) in the collector, so that the said pressure surface (32) defines a pressure chamber (34) at the bottom of the said recess (24).
  6. Device according to one of Claims 3 to 5, characterised in that the piston (22) is made in such a way that the said pressure force exerted by the said piston (22) is greater than the reaction force acting on the plane of the junction between the said collector (2) and the lance (4).
  7. Device for coupling a blowing lance to a collector which is connected to ducts carrying blowing and cooling fluids, the lance (4) comprising first channels (6, 8, 10) for the said fluids which extend through the said lance (4) and which open at one end into a first coupling surface (12), the collector comprising second channels (26, 28, 30) for the said fluids, each of the said second channels (26, 28, 30) being associated with one of the said first channels (6, 8, 10), being connected to one of the said ducts and opening at one end into a second coupling surface (14), the said second coupling surface (14) being associated with the said first coupling surface (12) and being capable of being pressed against the latter using a clamping means (25) so as to form an impervious junction between the said first (6, 8, 10) and second (26, 28, 30) associated channels, characterised in that the said collector comprises a coupling head (2), in that the second coupling surface (14) is an integral part of a piston (22), which is embedded in an axial recess (24) in the said coupling head (2) so that a pressure surface (32) defines a pressure chamber (34) at the bottom of the said recess (24), the said pressure surface (24) of the piston (22) being opposite the second coupling surface (14), and in that a supply duct is connected with the said pressure chamber (34) in such a way that the fluid supplied through the said supply duct exerts a pressure on the said pressure surface (32) and so that the piston (22) exerts a pressure force on the said first coupling surface (12).
  8. Device according to Claim 7, characterised by coupling means to suspend the lance (4) from the said coupling head (2).
  9. Device according to Claim 8, characterised in that the coupling means comprise hooks which are mounted so that they pivot on the said coupling head and which may engage with trunnions extending radially from the said lance (4).
  10. Device according to Claim 8, characterised in that the coupling means comprise locking rods (50) which are mounted so that they pivot on the said coupling head (2) and a radial flange (54) on the said lance (4) on the side of the first coupling surface (12), the said radial flange (54) having radial notches (52) designed to receive the locking rods (50) so that the heads (56) of the said locking rods (50) bear on the side of the said flange (54) which is opposite the first coupling surface (12).
  11. Device according to one of Claims 7 to 10, characterised in that the said clamping means (25) comprise springs which are positioned between the coupling head (2) and the said piston (22), the said springs being prestressed during the coupling of the lance (4) to the coupling head (2).
  12. Device according to one of Claims 7 to 11, characterised in that one of the said two coupling surfaces (12 or 14) comprises a protruding annular edge (48) extending axially, the said annular edge (48) having an inner diameter which is roughly equal to the outer diameter of the other of the said coupling surfaces (14 or 12).
EP97930463A 1996-08-28 1997-07-01 Device for coupling a blow lance with a header Expired - Lifetime EP0922117B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
LU88808 1996-08-28
LU88808A LU88808A1 (en) 1996-08-28 1996-08-28 Device for coupling a blowing lance to a manifold
PCT/EP1997/003423 WO1998008983A1 (en) 1996-08-28 1997-07-01 Device for coupling a blow lance with a header

Publications (2)

Publication Number Publication Date
EP0922117A1 EP0922117A1 (en) 1999-06-16
EP0922117B1 true EP0922117B1 (en) 2000-05-10

Family

ID=19731622

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97930463A Expired - Lifetime EP0922117B1 (en) 1996-08-28 1997-07-01 Device for coupling a blow lance with a header

Country Status (15)

Country Link
US (1) US6086818A (en)
EP (1) EP0922117B1 (en)
JP (1) JP2000516998A (en)
CN (1) CN1076399C (en)
AT (1) ATE192781T1 (en)
AU (1) AU714387B2 (en)
BR (1) BR9711249A (en)
CZ (1) CZ65699A3 (en)
DE (1) DE69701992T2 (en)
ES (1) ES2146105T3 (en)
LU (1) LU88808A1 (en)
PL (1) PL184089B1 (en)
PT (1) PT922117E (en)
RU (1) RU2199592C2 (en)
WO (1) WO1998008983A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9825428D0 (en) * 1998-11-19 1999-01-13 Kvaerner Metals Davy Ltd A quick change blow lance
US20050067743A1 (en) * 2003-09-29 2005-03-31 Eric Hatfield Internal bubble cooling unit and method for extruded thin wall thermoplastic sheet

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
LU69797A1 (en) * 1974-04-05 1974-11-21
US4083540A (en) * 1977-05-09 1978-04-11 Pullman Berry Company Gas and oxygen steel making lance
LU87387A1 (en) * 1988-11-16 1990-06-12 Wurth Paul Sa AUTOMATIC LANCES CHANGER
LU87425A1 (en) * 1989-01-16 1989-12-11 Wurth Paul Sa AUTOMATIC LANCES CHANGER
LU87761A1 (en) * 1990-07-04 1992-03-11 Wurth Paul Sa DEVICE FOR AUTOMATICALLY COUPLING AN INSUFFLATION LANCE TO A CONNECTING HEAD
LU88057A1 (en) * 1992-01-24 1993-08-17 Paul Wurth S.A. BLOWING HANGING WITH COMBINED MEDIA SUPPLY

Also Published As

Publication number Publication date
PL184089B1 (en) 2002-08-30
AU714387B2 (en) 1999-12-23
DE69701992T2 (en) 2000-10-05
CN1228816A (en) 1999-09-15
ES2146105T3 (en) 2000-07-16
JP2000516998A (en) 2000-12-19
DE69701992D1 (en) 2000-06-15
PT922117E (en) 2000-10-31
RU2199592C2 (en) 2003-02-27
EP0922117A1 (en) 1999-06-16
CZ65699A3 (en) 1999-10-13
AU3440897A (en) 1998-03-19
BR9711249A (en) 1999-08-17
US6086818A (en) 2000-07-11
CN1076399C (en) 2001-12-19
WO1998008983A1 (en) 1998-03-05
PL331943A1 (en) 1999-08-16
ATE192781T1 (en) 2000-05-15
LU88808A1 (en) 1998-03-02

Similar Documents

Publication Publication Date Title
EP0360946B1 (en) Coupling for butt-joining tubes
EP0922117B1 (en) Device for coupling a blow lance with a header
EP1034310B1 (en) Method for cooling a shaft furnace loading device
FR3102826A1 (en) Quick disconnect fitting with internal valves
EP0428433B1 (en) Device for fixation of upper spider guide plate in a nuclear reactor vessel
LU87730A1 (en) DEVICE FOR INJECTING PREHEATED AIR IN A TANK OVEN
EP0060835A1 (en) Pivot joint
FR2740525A1 (en) HYDRODYNAMIC TORQUE CONVERTER INCLUDING PASSAGE IN CRANKCASE COVER
EP0876872B1 (en) Device for the extraction of the tubes of heat exchangers with tube bundles and double plates
JP2000084759A (en) Nut fastening device and method
EP0783085A1 (en) Flexible piece for mounting into a bore
FR2504993A1 (en) REPAIRABLE PRESSURE TANK
FR2776305A1 (en) Lance carrier incorporating a multifunctional securing head
EP0015812B1 (en) Removable and tight closure device for an opening of a nuclear reactor vessel
EP0498187A1 (en) Clay gun for a machine for plugging tapping holes in shaft furnaces
FR2635768A1 (en) FOUNDRY PIECE ARRANGEMENT, IN PARTICULAR MOLDED STEEL, ON A MOLDED STRUCTURE BONDING NODE
FR2496695A1 (en) METALLURGICAL VESSEL PARTICULARLY STEEL CONVERTER
JPH10132093A (en) Valve system
FR3045773A1 (en) MAIN CONDUIT OF A FLUID CIRCUIT CIRCUIT COMPRISING A FLUID SAMPLE ELEMENT
FR2673870A1 (en) ELECTRODE SUPPORT FOR COMPRESSION BUT-A-BUT WELDING MACHINE AND END-TO-BIT SPINNING WELDING.
FR3007882A1 (en) SHUTTER ASSEMBLY AND ASSOCIATED MAINTENANCE METHOD
FR2678350A1 (en) Collar for live tapping on cement pipe with sheet metal core
MA56276A1 (en) METHOD FOR MANUFACTURING A PIPE ARRANGEMENT AND PIPE ARRANGEMENT
FR2560659A1 (en) Mechanical seal between rotary components
EP0582496A1 (en) Internal pouring tube made from refractory material for metallurgical vessels

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19990125

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE DE ES FI FR GB IT NL PT SE

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

17Q First examination report despatched

Effective date: 19990929

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT BE DE ES FI FR GB IT NL PT SE

REF Corresponds to:

Ref document number: 192781

Country of ref document: AT

Date of ref document: 20000515

Kind code of ref document: T

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FI

Payment date: 20000530

Year of fee payment: 4

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20000510

REF Corresponds to:

Ref document number: 69701992

Country of ref document: DE

Date of ref document: 20000615

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2146105

Country of ref document: ES

Kind code of ref document: T3

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: BE

Payment date: 20000719

Year of fee payment: 4

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: SE

Payment date: 20000725

Year of fee payment: 4

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: PT

Payment date: 20000726

Year of fee payment: 4

ITF It: translation for a ep patent filed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: SE

Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT

Effective date: 20000810

REG Reference to a national code

Ref country code: PT

Ref legal event code: SC4A

Free format text: AVAILABILITY OF NATIONAL TRANSLATION

Effective date: 20000726

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FI

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20010701

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20010731

REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

BERE Be: lapsed

Owner name: S.A. PAUL WURTH

Effective date: 20010731

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: PT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20020131

REG Reference to a national code

Ref country code: PT

Ref legal event code: MM4A

Free format text: LAPSE DUE TO NON-PAYMENT OF FEES

Effective date: 20020131

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20020614

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 20020619

Year of fee payment: 6

Ref country code: AT

Payment date: 20020619

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20020704

Year of fee payment: 6

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: ES

Payment date: 20020807

Year of fee payment: 6

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20030701

Ref country code: AT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20030701

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20030702

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20040201

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20030701

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20040331

NLV4 Nl: lapsed or anulled due to non-payment of the annual fee

Effective date: 20040201

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20030702

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.

Effective date: 20050701

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20110615

Year of fee payment: 15

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20130201

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 69701992

Country of ref document: DE

Effective date: 20130201