WO2023087107A1 - Interior lining system for an electrolytic cell - Google Patents
Interior lining system for an electrolytic cell Download PDFInfo
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- WO2023087107A1 WO2023087107A1 PCT/CA2022/051698 CA2022051698W WO2023087107A1 WO 2023087107 A1 WO2023087107 A1 WO 2023087107A1 CA 2022051698 W CA2022051698 W CA 2022051698W WO 2023087107 A1 WO2023087107 A1 WO 2023087107A1
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- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25C—PROCESSES FOR THE ELECTROLYTIC PRODUCTION, RECOVERY OR REFINING OF METALS; APPARATUS THEREFOR
- C25C3/00—Electrolytic production, recovery or refining of metals by electrolysis of melts
- C25C3/06—Electrolytic production, recovery or refining of metals by electrolysis of melts of aluminium
- C25C3/08—Cell construction, e.g. bottoms, walls, cathodes
- C25C3/085—Cell construction, e.g. bottoms, walls, cathodes characterised by its non electrically conducting heat insulating parts
Definitions
- the present technology relates to coating systems for electrolytic cells, electrolytic cells equipped with such systems as well as aluminum smelters comprising electrolytic cells provided with such systems.
- the production of aluminum on an industrial scale is carried out in an aluminum smelter, and this by electrolysis from alumina according to the Hall-Héroult process.
- the implementation of this process requires an electrolytic cell comprising a casing typically constructed of steel and lined with an interior lining typically constructed of refractory materials.
- a bottom of the vessel comprises a cathode assembly having a cathode formed of at least one cathode block typically constructed of carbonaceous material, which is traversed by electrical conductors of the cathode assembly intended to collect therein an electrolysis current to conduct it to cathode outputs.
- the top of the cathode assembly and the coating define a crucible intended to contain a bath of molten cryolite, also called an electrolytic bath, in which the alumina can be dissolved to form an aluminum sheet at the bottom of the crucible, s accumulating on the cathode assembly.
- the electrolytic cell also comprises at least one anode block suspended from an anode support, such as a rod and a crosspiece, the anode block being partially immersed in the electrolytic bath, above the cathode blocks.
- An upstream electrical conductor carries electrolysis current to the anode assembly, either from a source or from a cathode outlet of an upstream electrolysis cell, as required for the electrolysis reaction can take place in the bath in the presence of a suitably positioned anode block and a suitable temperature, among other conditions.
- the passage of the electrolytic current to the cathode assembly takes place from the anode block, via the electrolytic bath and the sheet of metal.
- the vessel is often constructed and operated in such a way as to cause the formation of a solidified pool slope on the side walls of the vessel. The slope is usually formed by a cooling mechanism. As discussed below, a homogeneous berm formation along the vessel walls is desirable.
- French patent application No. 14/01518 teaches the use of internal facing blocks superimposed on an outer layer of the coating. However, even in the presence of these facing blocks, the management of the temperature of the electrolytic bath and the formation of the embankment vis-à-vis the metal remains an issue.
- French patent application no. 98/05040 teaches the use of means for evacuating and dissipating the heat produced by the electrolytic cell placed outside the box, presented in the form of means of blowing can be directed on the casing generally towards the interface between the sheet of metal and the bath of electrolyte.
- temperature management from inside the crucible is also decisive, particularly with regard to the formation of an appropriately distributed slope all around the crucible.
- excessive heat dissipation can induce excessive embankment formation that can possibly interfere with the descent of the anode blocks.
- insufficient heat dissipation can induce insufficient slope formation, exposing the side lining of the vessel to the aluminum ply, leaving room for premature wear of the lining blocks.
- a deficient distribution of the slope is therefore detrimental to the proper functioning of the electrolysis process, to the life of certain components of the tank, and thereby to the performance of the tank.
- the present technology proposes an electrolytic cell comprising an interior coating system configured to allow management of heat transfers from the inside of a crucible of the cell to the outside of a the tank, favoring a homogeneous creation of embankments inside the crucible adjoining an internal layer of said internal lining system.
- a second objective of at least one embodiment of the proposed technology is to evenly distribute the heat losses on the side walls all around the electrolysis cell in order to stabilize the heat balance of the cell, as well as the formation of a stable and uniform embankment which ensures a long service life of the cell.
- the present technology relates to an electrolytic cell comprising a casing comprising side walls including a pair of longitudinal walls and a pair of transverse walls, a cathode inside the casing, and a coating side including an inner layer on the periphery of the cathode and an outer layer adjoining the side walls of the casing on the periphery of the inner layer, the side coating extending vertically beyond the cathode, characterized in that the inner layer comprises segments including a nominal segment and a conductive segment arranged one after the other along a side wall of the side walls of the casing; the nominal segment having a nominal thermal conductivity and the conductive segment having a thermal conductivity greater than the nominal thermal conductivity, the conductive segment adjoining an area of increased thermal stress of the tank.
- the side wall is an upstream longitudinal wall of the pair of longitudinal walls located upstream of the cathode
- the nominal segment extends from a longitudinal center of the cathode towards an end of the longitudinal wall upstream
- the conductive segment extends from near the end of the upstream longitudinal wall toward the longitudinal center
- the conductive segment is located in an area having a flow normal to said side wall, said flow induced by a magneto-hydrodynamic field in the contents of the tank.
- the conductive segment is a first conductive segment
- a downstream longitudinal wall of the pair of longitudinal walls is located downstream of the cathode
- the segments include a second conductive segment extending from the center longitudinal from the cathode towards one end of the downstream longitudinal wall, the second conductive segment having a thermal conductivity greater than the nominal thermal conductivity.
- the segments include an insulating segment extending along said side wall, the insulating segment having a thermal conductivity lower than the nominal thermal conductivity.
- the first conductive segment has a first thermal conductivity and the second conductive segment has a second thermal conductivity lower than the first thermal conductivity.
- the segments include an insulating segment extending from near the end of the downstream longitudinal wall towards the longitudinal center of the cathode, the insulating segment having a thermal conductivity lower than the thermal conductivity nominal.
- the first conductive segment and the second conductive segment are axially offset relative to a transverse axis of the cathode.
- the insulating segment is constructed from a material of the anthracite, semi-graphitic or graphitic type.
- the nominal segment is a first nominal segment
- the segments include a second nominal segment disposed between the second conductive segment and the insulating segment, the second nominal segment having the nominal thermal conductivity.
- the segments include a transverse conductive segment extending from a transverse center of the cathode along a transverse wall of the pair of transverse walls and a nominal transverse segment located near a end of the transverse wall downstream of the transverse center, the transverse nominal segment having the nominal thermal conductivity and the transverse conductive segment having a thermal conductivity greater than the nominal thermal conductivity.
- the transverse nominal segment has the nominal conductivity and the transverse conductive segment has the second thermal conductivity.
- the nominal segment is constructed in a material of the semi-graphitic, graphitic or graphitized type
- the conductive segment is constructed in a material of the graphitic, graphitized or over-graphitized type.
- the present technology relates to an aluminum smelter characterized in that it comprises an electrolytic cell having the aforementioned characteristics.
- the aluminum smelter comprises a cooling means disposed outside the side walls of the box, characterized in that the cooling means is arranged at the internal layer of the side coating so that the means cooling has a greater density vis-à-vis a portion of the casing along the conductive segment than vis-à-vis a portion of the casing along the nominal segment.
- Figure 1 is a partial schematic view of an electrolytic cell according to one embodiment of the invention.
- Figure 2 is a horizontal sectional view of the interior of an electrolytic cell according to one embodiment of the invention.
- Figure 3 is a partial schematic view of a crucible of an electrolytic cell according to one embodiment of the invention.
- Figure 4 is a partial cross-sectional view of the interior of an electrolytic cell according to one embodiment of the invention.
- an electrolytic cell 10 is provided according to one embodiment of the technology.
- the tank 10 has an upstream side 10A, a downstream side 10B opposite the upstream side 10A extending along a longitudinal orientation of the tank 10, and a pair of head sides 10C opposite to each other and extending according to a transverse orientation of the tank 10.
- the upstream-downstream direction is oriented in the direction of the current in the electrolysis series.
- the tank 10 comprises a box 20, conventionally made of steel and falling within a rectangular perimeter.
- the box 20 has side walls, including a pair of longitudinal walls 22A, 22B and a pair of transverse walls 24G, 24D, as well as a bottom 26 whose interior surfaces are provided with a coating system 30.
- a cathode assembly 40 of the vessel 10 comprises a cathode typically consisting of a multitude of cathode blocks 42 of carbonaceous material, is supported above the bottom 26 of the box 20.
- the cathode blocks 42 extend symmetrically from a longitudinal center CL of the cathode assembly and along the X axis of the tank 10, and on either side of a transverse center CT of the cathode assembly and along the Y axis of the tank 10.
- the cathode blocks 42 together define an upper surface 44, or above, of the cathode assembly generally parallel to the XY plane. As illustrated in Figures 1 and 4, this upper surface 44 represents a bottom of a crucible C intended to contain the alumina and other substances required for the implementation of the electrolysis process.
- each cathode block is connected to an electrical output conductor 12 of the tank 10 intended to receive an electrolysis current I from the cathode assembly 40 to lead it out of the tank 10 according to the axis Y, therefore downstream of the tank 10
- the electrolysis current I is routed from the transverse center of the cathode to the downstream side 10B of the tank 10 through one of the longitudinal walls 22A, 22B of the box 20 being designated downstream wall 22B.
- One of the longitudinal walls 22A, 22B arranged opposite the downstream wall 22B is therefore designated the upstream wall 22A.
- Other electrical conductor configurations and vessel orientations are also possible. .
- a source or an output conductor from another tank carries the electrolysis current I to a conductor of electrical riser 14 of the tank 10.
- the riser conductor 14 is electrically connected to a series of anode assemblies 50 of the vessel 10 located above the cathode assembly 40.
- Each anode assembly 50 comprises at least one anode block 52 having a bottom defining a portion of a lower surface 54 of the anode assemblies 50.
- Each anode block 52 is suspended from an anode support, such as a conductive rod 56 and a crosspiece.
- the tank 10 also comprises a superstructure 60 extending above the box 20.
- This superstructure 60 consists in particular of at least one beam positioned in a longitudinal direction X of the tank 10 and held in position relative to the box 20, for example by means of feet (not shown) arranged on either side of the tank 10 at its transverse edges, also called heads.
- An opening O that can be closed by a cowling system 70 of the tank 10 extends longitudinally above the casing 20 on each side of the superstructure 60.
- the cowling system 70 is arranged on the casing 20 and on the superstructure 60 to close off each opening O reversibly, thus forming with box 20 a containment enclosure for vessel 10.
- Superstructure 60 is arranged to support other components of vessel 10, in particular anode assemblies 50 via an anode frame 62 attached to the superstructure 60.
- Each rod 56 is connected electrically to the electric rise conductor 14 of the tank 10 via the frame 62, which makes it possible to convey the electrolysis current I to the corresponding anode block 52.
- a movable part of the frame 62 makes it possible to move the anode assembly 50 relative to the superstructure 60 in a vertical direction Z of the vessel 10, through the opening O, thus making it possible to immerse the anode block 52 in the crucible C while by controlling the position of the anode block 52 relative to the cathode and/or a surface of a sheet of metal forming at the bottom of the crucible C..
- a lower part 32 of the coating system 30 surrounds a base of the cathode receiving the electrical conductors 12 .
- the lower part 32 extends vertically to below the upper surface 44 of the cathode.
- An upper portion 34 of the coating system 30 surrounds the upper surface 44 of the cathode and extends vertically from the lower part 32 to beyond the upper surface 44.
- the upper part 34 of the coating system 30 forms a circumference of the crucible C extending vertically from the bottom of the crucible C.
- the coating system 30 serves both to form the contours of the crucible C and to protect the side walls of the box 20 with respect to the contents of the crucible C.
- the upper part 34 of the coating system 30 comprises an internal layer 80 located on the periphery of the cathode and an external layer 90 adjoining the side walls of the casing 20 on the periphery of the internal layer 80.
- a space on the periphery of the cathode and surrounded by the internal layer 80 is clogged with potlining paste 28.
- the contours of the crucible C are therefore formed by the upper surface 44 of the cathode, the potlining paste 28, the internal layer 80 of the coating system and the top of the external layer 90.
- the outer layer 90 typically consists of elements composed of refractory material based on silicon carbide (SiC) or other thermally refractory composition.
- the outer layer 90 includes a first stage and a second stage vertically superimposed on the first stage comprising respectively a series of elements 92, 94 affixed one after the other against the box 20.
- the elements 92 are refractory bricks and the elements 94 are SiC slabs.
- the elements 94 can be omitted.
- other insulating materials with mica can be added as needed.
- the inner layer 80 comprises a series of blocks 82 of internal facing affixed horizontally one after the other against the outer layer 90.
- Each of the blocks 82 of internal facing has a double vocation.
- each of the blocks 82 contributes to protecting both the wall portion 22A, 22B, 24G, 24D of the box 20 and the outer layer portion 90 located opposite it from wear by the aluminum and/or the molten electrolyte in the crucible C.
- Each of the blocks 82 of internal facing is constructed from a carbonaceous material.
- the blocks 82 include blocks 82 called "nominal", that is to say having a nominal thermal conductivity allowing a certain reference (or nominal) heat transfer which proves to be appropriate for several places around the periphery of the crucible C.
- a tank whose inner layer 80 of the coating system 30 was exclusively made of nominal blocks 82 does not perfectly meet the specific heat transfer requirements at certain places around the perimeter. of the crucible C. Indeed, electromagnetic characteristics specific to the vessel 10 induce localized thermal effects in the crucible C which can, in the presence of typical internal layer 80, have an adverse influence on the formation of slope T in the crucible C.
- the embankment T a formation including solidified electrolyte, is deposited on the periphery of crucible C as soon as the contents of crucible C, around 970°C at its center, undergoes cooling outwards.
- a nominal block 82 can, by its intrinsic characteristics, induce an adequate, excessive, or insufficient heat transfer. Excessive heat transfer can lead to excessive slope formation T, which can eventually coat the cathode and even interfere with the descent of an anode block 52 into crucible C. Insufficient heat transfer can lead to slope formation insufficient T, and even an absence of a slope T. When exposed to the contents of the crucible C in the absence of a slope T, the internal layer 80 of the coating system 30 is subject to premature degradation by a phenomenon similar to 'erosion.
- the series of blocks 82 of the inner layer 80 of the present technology is also intended to locally regulate the transfer of heat from the crucible C to the outer layer 90 and out of the box 20
- the horizontal series of blocks 82 comprises several types of blocks 82 differentiated among other things on the basis of their thermal conductivity, and arranged horizontally along the wall of the vessel so that their thermal conductivity meets a local need in heat transfer.
- the blocks 82 thus include so-called "specific" blocks, of thermal conductivity allowing a heat transfer other than the reference heat transfer, strategically placed over certain lengths of the internal layer 80 of the coating system 30 in alternation with other lengths traveled by nominal 82 blocks.
- Blocks 82 may include, depending on the embodiment, conductive blocks 82, with higher thermal conductivity than that of the nominal blocks 82, and/or insulating blocks 82 with lower thermal conductivity than that of the nominal blocks 82.
- Blocks 82 may be constructed of any of the following types of materials, listed in order of increasing thermal conductivity: anthracitic [ ⁇ 7W/m*K], semi-graphitic [ ⁇ 11 W/m*K] , graphitic [ ⁇ 20/m*K], graphitized [ ⁇ 110W/m*K], over-graphitized [ ⁇ 125W/m*K],
- the insulating blocks 82 are made of material anthracite
- the nominal blocks 82 are made of semi-graphitic material
- the conductive blocks 82 are made of graphitic and/or graphitized, or even over-graphitized material.
- insulating blocks 82 are of semi-graphitic material
- nominal blocks 82 are of graphitized
- the tank 10 is generally symmetrical with respect to the longitudinal center CL of the cathode and, similarly, the vortices V1, V3, and V2, V4 are respectively pairs of corresponding vortices formed in a generally symmetrical manner with respect to the longitudinal center CL when the inlets and current outputs in the tank are well balanced as well as the magnetic environment surrounding the tank.
- the vortices V1, V2 are formed in the right half of the tank 10 extending along X from the longitudinal center CL, while the vortices V3, V4 are formed in the left half of the tank 10.
- tank 10 is also generally symmetrical with respect to the transverse center CT of the cathode, the vortices V1, V2 are not distributed symmetrically with respect to the transverse center CT. It follows that the vortices V1, V2 can circulate around the coating 30 with more or less intensity on either side of the transverse center CT (at two positions along the Y axis) for the same position along the X axis.
- the tourbillon V1 circulates in the right half of the vessel 10 in a clockwise direction. From close to an end 22A' of the upstream wall 22A, the vortex V1 puts pressure on the upstream wall 22A and runs along the upstream wall 22A over a certain distance while heading towards the longitudinal center CL, creating a first zone Z1 of increased thermal stress on the vessel 10. Still according to the example of FIG. 2, the vortex V1 then takes off from the upstream wall 22A at a distance from the longitudinal center CL and branches off towards the downstream wall 22B.
- the vortex V1 puts pressure on the downstream wall 22B and runs along the downstream wall 22B over a certain distance while heading towards an end 22B' of the downstream wall 22B, creating a second zone Z2 of thermal stress. increased.
- the vortex V1 unhooks from the downstream wall 22B before going to rejoin the transverse wall 24D at a distance from opposite ends 24D′ of the transverse wall 24D, creating a zone ZR of thermal stress reduced to the junction between the downstream 22B and transverse 24D walls.
- the vortex V2 circulates in the zone ZR of reduced thermal stress counterclockwise and at a lower speed than the vortex V1, along the downstream wall 22B near the end 22B', inducing a low pressure on the downstream wall 22B. Then, the vortex V1 puts pressure on the transverse wall 24D on either side of the transverse center CT and runs along the transverse wall 24D at a distance from the upstream 22A and downstream 22B walls, creating a third zone Z3 of increased thermal stress.
- the zones Z1, Z2 see a normal flow to the side walls and therefore a greater heat flux than nominal where the flow is lateral.
- the Z3 zone can show counter-vortices which facilitate the formation of slopes and limit heat fluxes.
- the difference in heat flux, and more particularly the variations in heat exchange between the bath/metal and the embankment, in the various zones Z1, Z2, Z3 and ZR, can be observed by measuring the distribution of the embankment around the tank. A balancing of the heat fluxes in the various zones is therefore desirable in order to re-homogenize the thickness of the embankment around the tank 10.
- the internal layer 80 of the coating system 30 consists of segments, that is to say series of blocks 82 either nominal (or nominal segments 84), or conductive (or conductive segments 86), or either insulating (or insulating segments 88).
- Each of the segments 84, 86, 88 inherits the properties of the blocks 82 of which it is made, and can therefore be constructed, depending on the embodiment, of one or other of the following types of materials, listed in order of increasing thermal conductivity : anthracitic, semi-graphitic, graphitic, graphitized, or over-graphitized.
- each nominal segment 84 is constructed in a material of the semi-graphitic, graphitic or graphitized type
- each conductive segment 86 is constructed in a material of the graphitic, graphitized or over-graphitized type
- each insulating segment 88 is constructed of an anthracitic, semi-graphitic, or graphitic material such that conductive segments 86 have higher thermal conductivity than nominal segments 84, while insulating segments 88 have less thermal conductivity than nominal segments 84.
- the segments 84, 86, and 88 are alternately affixed along the side walls of box 20.
- segments 84, 86, and 88 may include more than one nominal segment 84, more than one conductive segment 86, and/or or more than one insulating segment 88 along a single side wall.
- a first nominal segment 84A extends from the longitudinal center CL towards an end 22A' of the upstream wall 22A.
- a first conductive segment 86A extends from near end 22A' toward longitudinal center CL.
- the first conductive segment 86A adjoins zone Z1.
- first nominal segment 84A is longer than first conductive segment 86A.
- the first conductive segment 86A has an equivalent length between 0 and 66% of the distance between the longitudinal center CL and the end 22k'.
- the length of the first conductive segment 86A may correspond to a distance covered by 2 to 8 cathode blocks 42 along the X axis, considering that the tank has 12 blocks between the longitudinal center CL and the end 22k' .
- a second conductive segment 86B extends from the longitudinal center CL towards an end 22B' of the downstream wall 22B.
- the second conductive segment 86B adjoins zone Z2.
- first nominal segment 84A is larger than second conductive segment 86B.
- the second conductive segment 86B has an equivalent length between 0 and 70% of the distance between the longitudinal center CL and the end 22B'.
- the inner layer 80 has a thermal conductivity equal to or less than nominal thermal conductivity.
- an insulating segment 88 extends from near the end 22B' towards the longitudinal center CL. Insulating segment 88 adjoins zone ZR.
- the insulating segment 88 has an equivalent length between 0 and 40% of the distance between the longitudinal center CL and the end 22B'.
- a second nominal segment 84B is disposed between the second conductive segment 86B and the insulating segment 88. In other embodiments, the insulating segment 88 is omitted, so that the second nominal segment 84B extends to near the end 22B'.
- a third conductive segment 86C extends from the transverse center CT to a distance from opposite ends 24D′ of the transverse wall 24D.
- the third conductive segment 86C has an equivalent length between 0 and 75% of the length of the transverse wall 24D.
- a pair of third nominal segments 84C, or transverse nominal segments, extend from either side of the third conducting segment 86C to the ends 24D'.
- the nominal segments 84A, 84B, 84C are made of graphite material.
- the first conductive segment 86A is made of over-graphitized material.
- the second conductive segment 86B and the third conductive segment 86C are made of graphitized material.
- the insulating segment 88 is made of semi-graphitic material.
- the nominal segments 84A, 84B, 84C are made of semi-graphitic material.
- the first conductive segment 86A is made of graphitized material.
- the second conductive segment 86B and the third conductive segment 86C are made of graphitic material.
- the insulating segment 88 is made of anthracite material.
- the segments of the inner layer 80 of the coating system 30 have in common to make possible a local heat transfer adequate for the formation of the embankment T, so that the embankment T will prove globally of an adequate and homogeneous dimension.
- homogeneous dimension is meant a slope thickness T being substantially the same horizontally (in the XY plane) throughout the inner layer 80.
- the vessel may be provided with evacuation means include means for cooling the aluminum smelter 1 arranged outside the vessel 10 and distributed around the box 20.
- the cooling means may include fins.
- the fins can advantageously be provided to have a greater density along the segments conductors 86A, 86B, 86C than along nominal segments 84A, 84B, 84C.
- a fin area ratio per unit length of conductive segments 86A, 86B, 86C is greater than a fin area ratio per unit length of nominal segments 84A, 84B, 84C.
- the cooling means may include blowing means suitable for directing a localized jet of air.
- the blowing means can advantageously be provided so that a blowing density is greater along the conductive segments 86A, 86B, 86C than along the nominal segments 84A, 84B, 84C.
- a ratio of incident air flow from the blowing means per unit length of conductive segments 86A, 86B, 86C is greater than a ratio of incident air flow from the blowing means per unit length of segments nominal 84A, 84B, 84C.
- the blowing means can be located opposite the conductive segments 86A, 86B, 86C or oriented towards the conductive segments 86A, 86B, 86C and/or away from the nominal segments 84A, 84B, 84C.
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Abstract
Description
SYSTÈME DE REVÊTEMENT INTÉRIEUR POUR CUVE D’ÉLECTROLYSE INTERNAL LINER SYSTEM FOR ELECTROLYSIS TANK
DOMAINE TECHNIQUE TECHNICAL AREA
[0001] La présente technologie concerne les systèmes de revêtement pour cuve d’électrolyse, les cuves d’électrolyse munies de tels systèmes ainsi que les alumineries comprenant des cuves d’électrolyses munies de tels systèmes. The present technology relates to coating systems for electrolytic cells, electrolytic cells equipped with such systems as well as aluminum smelters comprising electrolytic cells provided with such systems.
PRÉSENTATION DE L’ART ANTÉRIEUR PRESENTATION OF PRIOR ART
[0002] Communément, la production d’aluminium à l’échelle industrielle s’effectue en aluminerie, et ce par électrolyse à partir d’alumine selon le procédé de Hall-Héroult. La mise en œuvre de ce procédé requiert une cuve d’électrolyse comprenant un caisson typiquement construit d’acier et bordé d’un revêtement intérieur typiquement construit de matériaux réfractaires. Un fond de la cuve comprend un ensemble cathodique ayant une cathode formée d’au moins un bloc cathodique typiquement construit de matériau carboné, laquelle est parcourue par des conducteurs électriques de l’ensemble cathodique destinés à y collecter un courant d’électrolyse pour le conduire à des sorties cathodiques. Le dessus de l’ensemble cathodique et le revêtement définissent un creuset destiné à contenir un bain de cryolithe fondue, aussi appelé bain électrolytique, dans lequel l'alumine peut être dissoute pour donner forme à une nappe d’aluminium au fond du creuset, s’accumulant sur l’ensemble cathodique. La cuve d’électrolyse comprend également au moins un bloc anodique suspendu à un support anodique, tel qu’une tige et une traverse, le bloc anodique étant plongé partiellement dans le bain électrolytique, au- dessus des blocs cathodiques. Un conducteur électrique d’amont achemine le courant d’électrolyse jusqu'à l’ensemble anodique, soit depuis une source ou alors depuis une sortie cathodique d’une cuve d’électrolyse en amont, tel que requis pour que la réaction d’électrolyse puisse avoir lieu dans le bain en présence d’un bloc anodique adéquatement positionné et d’une température adéquate, entre autres conditions. En cours de réaction, le passage du courant électrolytique vers l’ensemble cathodique s’effectue depuis le bloc anodique, via le bain électrolytique et la nappe de métal. La cuve est souvent constituée et conduite de façon à entraîner la formation d’un talus de bain solidifié sur les parois latérales de la cuve. Le talus se forme généralement par un mécanisme de refroidissement. Tel que discuté ci-dessous, une formation homogène de talus le long des parois de la cuve est souhaitable. Commonly, the production of aluminum on an industrial scale is carried out in an aluminum smelter, and this by electrolysis from alumina according to the Hall-Héroult process. The implementation of this process requires an electrolytic cell comprising a casing typically constructed of steel and lined with an interior lining typically constructed of refractory materials. A bottom of the vessel comprises a cathode assembly having a cathode formed of at least one cathode block typically constructed of carbonaceous material, which is traversed by electrical conductors of the cathode assembly intended to collect therein an electrolysis current to conduct it to cathode outputs. The top of the cathode assembly and the coating define a crucible intended to contain a bath of molten cryolite, also called an electrolytic bath, in which the alumina can be dissolved to form an aluminum sheet at the bottom of the crucible, s accumulating on the cathode assembly. The electrolytic cell also comprises at least one anode block suspended from an anode support, such as a rod and a crosspiece, the anode block being partially immersed in the electrolytic bath, above the cathode blocks. An upstream electrical conductor carries electrolysis current to the anode assembly, either from a source or from a cathode outlet of an upstream electrolysis cell, as required for the electrolysis reaction can take place in the bath in the presence of a suitably positioned anode block and a suitable temperature, among other conditions. During the reaction, the passage of the electrolytic current to the cathode assembly takes place from the anode block, via the electrolytic bath and the sheet of metal. The vessel is often constructed and operated in such a way as to cause the formation of a solidified pool slope on the side walls of the vessel. The slope is usually formed by a cooling mechanism. As discussed below, a homogeneous berm formation along the vessel walls is desirable.
[0003] La demande de brevet français no 14/01518 enseigne l’utilisation de blocs de parement interne en superposition à une couche externe du revêtement. Toutefois, même en présence de ces blocs de parement, la gestion de la température du bain électrolytique et de la formation du talus en vis-à-vis du métal demeure un enjeu. French patent application No. 14/01518 teaches the use of internal facing blocks superimposed on an outer layer of the coating. However, even in the presence of these facing blocks, the management of the temperature of the electrolytic bath and the formation of the embankment vis-à-vis the metal remains an issue.
[0004] La demande de brevet français no 98/05040 enseigne l’utilisation de moyens d’évacuation et de dissipation de la chaleur produite par la cuve d’électrolyse mis en place à l’extérieur du caisson, présentés sous forme de moyens de soufflage pouvant être dirigés sur le caisson généralement vers l’interface entre la nappe de métal et le bain d’électrolyte. Néanmoins, la gestion de la température depuis l’intérieur du creuset est aussi déterminante, notamment en ce qui a trait à la formation d’un talus réparti de manière adéquate tout autour du creuset. Notamment, une dissipation thermique trop importante peut induire une formation de talus excessive pouvant éventuellement interférer avec la descente des blocs anodiques. D’autre part, une dissipation thermique insuffisante peut induire une formation insuffisante de talus, exposant le revêtement latéral de la cuve à la nappe d’aluminium, laissant place à une usure prématurée des blocs de revêtement.. Une répartition déficiente du talus est donc préjudiciable au bon fonctionnement du procédé d’électrolyse, à la durée de vie de certaines composantes de la cuve, et par le fait même au rendement de la cuve. [0004] French patent application no. 98/05040 teaches the use of means for evacuating and dissipating the heat produced by the electrolytic cell placed outside the box, presented in the form of means of blowing can be directed on the casing generally towards the interface between the sheet of metal and the bath of electrolyte. Nevertheless, temperature management from inside the crucible is also decisive, particularly with regard to the formation of an appropriately distributed slope all around the crucible. In particular, excessive heat dissipation can induce excessive embankment formation that can possibly interfere with the descent of the anode blocks. On the other hand, insufficient heat dissipation can induce insufficient slope formation, exposing the side lining of the vessel to the aluminum ply, leaving room for premature wear of the lining blocks. A deficient distribution of the slope is therefore detrimental to the proper functioning of the electrolysis process, to the life of certain components of the tank, and thereby to the performance of the tank.
RÉSUMÉ DE LA TECHNOLOGIE TECHNOLOGY SUMMARY
[0005] Un des buts de la présente technologie vise à pallier les inconvénients susmentionnés. Pour ce faire, la présente technologie propose une cuve d’électrolyse comprenant un système de revêtement intérieur configuré pour permettre une gestion des transferts de chaleur depuis l’intérieur d’un creuset de la cuve jusqu’à l’extérieur d’un caisson de la cuve, favorisant une création homogène de talus à l’intérieur du creuset jouxtant une couche interne dudit système de revêtement intérieur. [0005] One of the aims of the present technology aims to overcome the aforementioned drawbacks. To do this, the present technology proposes an electrolytic cell comprising an interior coating system configured to allow management of heat transfers from the inside of a crucible of the cell to the outside of a the tank, favoring a homogeneous creation of embankments inside the crucible adjoining an internal layer of said internal lining system.
[0006] Un second objectif d’au moins une réalisation de la technologie proposée est de répartir uniformément les pertes thermiques sur les parois latérales tout autour de la cellue d’électrolyse afin de stabiliser le bilan thermique de la cellule, ainsi que la formation d'un talus stable et uniforme qui assure une durée de vie élevée de la cellule. A second objective of at least one embodiment of the proposed technology is to evenly distribute the heat losses on the side walls all around the electrolysis cell in order to stabilize the heat balance of the cell, as well as the formation of a stable and uniform embankment which ensures a long service life of the cell.
[0007] Selon un aspect, la présente technologie a pour objet une cuve d’électrolyse comprenant un caisson comportant des parois latérales incluant une paire de parois longitudinales et une paire de parois transversales, une cathode à l’intérieur du caisson, et un revêtement latéral incluant une couche interne en périphérie de la cathode et une couche externe jouxtant les parois latérales du caisson en périphérie de la couche interne, le revêtement latéral s’étendant verticalement au-delà de la cathode, caractérisée en ce que la couche interne comprend des segments incluant un segment nominal et un segment conducteur disposés l’un à la suite de l’autre le long d’une paroi latérale des parois latérales du caisson; le segment nominal ayant une conductivité thermique nominale et le segment conducteur ayant une conductivité thermique supérieure à la conductivité thermique nominale, le segment conducteur jouxtant une zone de sollicitation thermique accrue de la cuve. According to one aspect, the present technology relates to an electrolytic cell comprising a casing comprising side walls including a pair of longitudinal walls and a pair of transverse walls, a cathode inside the casing, and a coating side including an inner layer on the periphery of the cathode and an outer layer adjoining the side walls of the casing on the periphery of the inner layer, the side coating extending vertically beyond the cathode, characterized in that the inner layer comprises segments including a nominal segment and a conductive segment arranged one after the other along a side wall of the side walls of the casing; the nominal segment having a nominal thermal conductivity and the conductive segment having a thermal conductivity greater than the nominal thermal conductivity, the conductive segment adjoining an area of increased thermal stress of the tank.
[0008] Selon un mode de réalisation, la paroi latérale est une paroi longitudinale amont de la paire de parois longitudinales située en amont de la cathode, le segment nominal s’étend depuis un centre longitudinal de la cathode vers une extrémité de la paroi longitudinale amont, et le segment conducteur s’étend depuis à proximité de l’extrémité de la paroi longitudinale amont vers le centre longitudinal. According to one embodiment, the side wall is an upstream longitudinal wall of the pair of longitudinal walls located upstream of the cathode, the nominal segment extends from a longitudinal center of the cathode towards an end of the longitudinal wall upstream, and the conductive segment extends from near the end of the upstream longitudinal wall toward the longitudinal center.
[0009] Selon un mode de réalisation, le segment conducteur est situé dans une zone présentant un écoulement normal à ladite paroi latérale, ledit écoulement induit par un champ magnéto- hydrodynamique dans le contenu de la cuve. [0009]According to one embodiment, the conductive segment is located in an area having a flow normal to said side wall, said flow induced by a magneto-hydrodynamic field in the contents of the tank.
[0010] Selon un mode de réalisation, le segment conducteur est un premier segment conducteur, une paroi longitudinale aval de la paire de parois longitudinales est située en aval de la cathode, et les segments incluent un deuxième segment conducteur s’étendant depuis le centre longitudinal de la cathode vers une extrémité de la paroi longitudinale aval, le deuxième segment conducteur ayant une conductivité thermique supérieure à la conductivité thermique nominale. According to one embodiment, the conductive segment is a first conductive segment, a downstream longitudinal wall of the pair of longitudinal walls is located downstream of the cathode, and the segments include a second conductive segment extending from the center longitudinal from the cathode towards one end of the downstream longitudinal wall, the second conductive segment having a thermal conductivity greater than the nominal thermal conductivity.
[0011] Selon un mode de réalisation, les segments incluent un segment isolant s’étendant le long de ladite paroi latérale, le segment isolant ayant une conductivité thermique inférieure à la conductivité thermique nominale. According to one embodiment, the segments include an insulating segment extending along said side wall, the insulating segment having a thermal conductivity lower than the nominal thermal conductivity.
[0012] Selon un mode de réalisation, le premier segment conducteur a une première conductivité thermique et le deuxième segment conducteur a une deuxième conductivité thermique inférieure à la première conductivité thermique. According to one embodiment, the first conductive segment has a first thermal conductivity and the second conductive segment has a second thermal conductivity lower than the first thermal conductivity.
[0013] Selon un mode de réalisation, les segments incluent un segment isolant s’étendant depuis à proximité de l’extrémité de la paroi longitudinale aval vers le centre longitudinal de la cathode, le segment isolant ayant une conductivité thermique inférieure à la conductivité thermique nominale. [0014] Selon un mode de réalisation, le premier segment conducteur et le deuxième segment conducteur sont axialement décalés relativement à un axe transversal de la cathode. According to one embodiment, the segments include an insulating segment extending from near the end of the downstream longitudinal wall towards the longitudinal center of the cathode, the insulating segment having a thermal conductivity lower than the thermal conductivity nominal. According to one embodiment, the first conductive segment and the second conductive segment are axially offset relative to a transverse axis of the cathode.
[0015] Selon un mode de réalisation, le segment isolant est construit d’un matériau de type anthracitique, semi-graphitique ou graphitique. [0015] According to one embodiment, the insulating segment is constructed from a material of the anthracite, semi-graphitic or graphitic type.
[0016] Selon un mode de réalisation, le segment nominal est un premier segment nominal, et les segments incluent un deuxième segment nominal disposé entre le deuxième segment conducteur et le segment isolant, le deuxième segment nominal ayant la conductivité thermique nominale. According to one embodiment, the nominal segment is a first nominal segment, and the segments include a second nominal segment disposed between the second conductive segment and the insulating segment, the second nominal segment having the nominal thermal conductivity.
[0017] Selon un mode de réalisation, les segments incluent un segment conducteur transversal s’étendant depuis un centre transversal de la cathode le long d’une paroi transversale de la paire de parois transversales et un segment nominal transversal situé à proximité d’une extrémité de la paroi transversale en aval du centre transversal, le segment nominal transversal ayant la conductivité thermique nominale et le segment conducteur transversal ayant une conductivité thermique supérieure à la conductivité thermique nominale. According to one embodiment, the segments include a transverse conductive segment extending from a transverse center of the cathode along a transverse wall of the pair of transverse walls and a nominal transverse segment located near a end of the transverse wall downstream of the transverse center, the transverse nominal segment having the nominal thermal conductivity and the transverse conductive segment having a thermal conductivity greater than the nominal thermal conductivity.
[0018] Selon un mode de réalisation, le segment nominal transversal a la conductivité nominale et le segment conducteur transversal a la deuxième conductivité thermique. According to one embodiment, the transverse nominal segment has the nominal conductivity and the transverse conductive segment has the second thermal conductivity.
[0019] Selon un mode de réalisation, le segment nominal est construit dans un matériau de type semi-graphitique, graphitique ou graphitisé, et le segment conducteur est construit dans un matériau de type graphitique, graphitisé ou sur-graphitisé. [0019]According to one embodiment, the nominal segment is constructed in a material of the semi-graphitic, graphitic or graphitized type, and the conductive segment is constructed in a material of the graphitic, graphitized or over-graphitized type.
[0020] Selon un autre aspect, la présente technologie a pour objet une aluminerie caractérisée en ce qu’elle comprend une cuve d’électrolyse ayant les caractéristiques précitées. According to another aspect, the present technology relates to an aluminum smelter characterized in that it comprises an electrolytic cell having the aforementioned characteristics.
[0021] Selon un mode de réalisation, l’aluminerie comprend un moyen de refroidissement disposé à l’extérieur des parois latérales du caisson, caractérisée en ce que le moyen de refroidissement est agencé à la couche interne du revêtement latéral de sorte que le moyen de refroidissement ait une densité plus grande vis-à-vis une portion du caisson longeant le segment conducteur que vis-à-vis une portion du caisson longeant le segment nominal. BRÈVE DESCRIPTION DES FIGURES [0021]According to one embodiment, the aluminum smelter comprises a cooling means disposed outside the side walls of the box, characterized in that the cooling means is arranged at the internal layer of the side coating so that the means cooling has a greater density vis-à-vis a portion of the casing along the conductive segment than vis-à-vis a portion of the casing along the nominal segment. BRIEF DESCRIPTION OF FIGURES
[0022] D’autres avantages et caractéristiques de la présente technologie ressortiront de la description ci-après de plusieurs variantes d’exécution données à titre d’exemples non limitatifs, dont certaines en référence aux dessins annexés dans lesquels : Other advantages and characteristics of this technology will emerge from the description below of several variant embodiments given by way of non-limiting examples, some of which with reference to the appended drawings in which:
[0023] La Figure 1 est une vue schématique partielle d’une cuve d’électrolyse selon un mode de réalisation de l’invention ; Figure 1 is a partial schematic view of an electrolytic cell according to one embodiment of the invention;
[0024] La Figure 2 est une vue en section horizontale de l’intérieur d’une cuve d’électrolyse selon un mode de réalisation de l’invention ; Figure 2 is a horizontal sectional view of the interior of an electrolytic cell according to one embodiment of the invention;
[0025] La Figure 3 est une vue schématique partielle d’un creuset d’une cuve d’électrolyse selon un mode de réalisation de l’invention, et [0025] Figure 3 is a partial schematic view of a crucible of an electrolytic cell according to one embodiment of the invention, and
[0026] La Figure 4 est une vue en section transversale partielle de l’intérieur d’une cuve d’électrolyse selon un mode de réalisation de l’invention. Figure 4 is a partial cross-sectional view of the interior of an electrolytic cell according to one embodiment of the invention.
DESCRIPTION DÉTAILLÉE DETAILED DESCRIPTION
[0027] En référence aux Figures 1 et 2, la présente technologie concerne des équipements destinés à servir dans une aluminerie dans le cadre d’un processus de transformation métallurgique industrielle pour production d’aluminium à partir d'alumine selon le procédé d’électrolyse de Hall-Héroult. À cet effet, on prévoit une cuve 10 d’électrolyse selon un mode de réalisation de la technologie. La cuve 10 a un côté amont 10A, un côté aval 10B opposé au côté amont 10A s’étendant selon une orientation longitudinale de la cuve 10, et une paire de côtés de tête 10C opposés l’un à l’autre et s’étendant selon une orientation transversale de la cuve 10. La direction amont-avale s’oriente dans le sens du courant dans la série d’électrolyse. La cuve 10 comprend un caisson 20, classiquement fabriqué en acier et s’inscrivant dans un périmètre rectangulaire. Le caisson 20 est doté de parois latérales, dont une paire de parois longitudinales 22A, 22B et une paire de parois transversales 24G, 24D, ainsi que d’un fond 26 dont les surfaces intérieures sont munies d’un système de revêtement 30. Tel qu’illustré aux Figures 2 et 3, un ensemble cathodique 40 de la cuve 10 comporte une cathode constituée typiquement d’une multitude de blocs cathodiques 42 en matériau carboné, est supportée au-dessus du fond 26 du caisson 20. Les blocs cathodiques 42 s’étendent symétriquement depuis un centre longitudinal CL de l’ensemble cathodique et selon l’axe X de la cuve 10, et de part et d’autre d’un centre transversal CT de l’ensemble cathodique et selon l’axe Y de la cuve 10. Les blocs cathodiques 42 définissent ensemble une surface supérieure 44, ou dessus, de l’ensemble cathodique généralement parallèle au plan XY. Tel qu’illustré aux Figures 1 et 4, cette surface supérieure 44 représente un fond d’un creuset C destiné à contenir l’alumine et autres substances requises pour la mise en œuvre du procédé d’électrolyse. En dessous de la surface supérieure 44, chaque bloc cathodique est relié à un conducteur de sortie 12 électrique de la cuve 10 destiné à recevoir un courant I d’électrolyse depuis l’ensemble cathodique 40 pour le conduire hors de la cuve 10 selon l’axe Y, donc en aval de la cuve 10Dit autrement, le courant I d’électrolyse est acheminé depuis le centre transversal de la cathode vers le côté aval 10B de la cuve 10 à travers l’une des parois longitudinales 22A, 22B du caisson 20 étant désignée paroi aval 22B. L’une des parois longitudinales 22A, 22B disposée à l’opposé de la paroi aval 22B est donc désignée paroi amont 22A. D’autres configurations de conducteur électrique et d’orientations de cuve sont aussi possibles. . With reference to Figures 1 and 2, the present technology relates to equipment intended for use in an aluminum smelter as part of an industrial metallurgical transformation process for the production of aluminum from alumina according to the electrolysis process. of Hall-Heroult. For this purpose, an electrolytic cell 10 is provided according to one embodiment of the technology. The tank 10 has an upstream side 10A, a downstream side 10B opposite the upstream side 10A extending along a longitudinal orientation of the tank 10, and a pair of head sides 10C opposite to each other and extending according to a transverse orientation of the tank 10. The upstream-downstream direction is oriented in the direction of the current in the electrolysis series. The tank 10 comprises a box 20, conventionally made of steel and falling within a rectangular perimeter. The box 20 has side walls, including a pair of longitudinal walls 22A, 22B and a pair of transverse walls 24G, 24D, as well as a bottom 26 whose interior surfaces are provided with a coating system 30. Such illustrated in Figures 2 and 3, a cathode assembly 40 of the vessel 10 comprises a cathode typically consisting of a multitude of cathode blocks 42 of carbonaceous material, is supported above the bottom 26 of the box 20. The cathode blocks 42 extend symmetrically from a longitudinal center CL of the cathode assembly and along the X axis of the tank 10, and on either side of a transverse center CT of the cathode assembly and along the Y axis of the tank 10. The cathode blocks 42 together define an upper surface 44, or above, of the cathode assembly generally parallel to the XY plane. As illustrated in Figures 1 and 4, this upper surface 44 represents a bottom of a crucible C intended to contain the alumina and other substances required for the implementation of the electrolysis process. Below the upper surface 44, each cathode block is connected to an electrical output conductor 12 of the tank 10 intended to receive an electrolysis current I from the cathode assembly 40 to lead it out of the tank 10 according to the axis Y, therefore downstream of the tank 10 In other words, the electrolysis current I is routed from the transverse center of the cathode to the downstream side 10B of the tank 10 through one of the longitudinal walls 22A, 22B of the box 20 being designated downstream wall 22B. One of the longitudinal walls 22A, 22B arranged opposite the downstream wall 22B is therefore designated the upstream wall 22A. Other electrical conductor configurations and vessel orientations are also possible. .
[0028] Tel qu’illustré à la Figure 1 , sur le côté amont 10A de la cuve 10, une source ou alors un conducteur de sortie d’une autre cuve (non montrée) achemine le courant I d’électrolyse vers un conducteur de montée 14 électrique de la cuve 10. Le conducteur de montée 14 est relié électriquement à une série d’ensembles anodiques 50 de la cuve 10 situés au-dessus de l’ensemble cathodique 40. Chaque ensemble anodique 50 comprend au moins un bloc anodique 52 ayant un dessous définissant une portion d’une surface inférieure 54 des ensembles anodiques 50. Chaque bloc anodique 52 est supendu à un support anodique, tel qu’une tige 56 conductrice et une traverse. Il convient de noter que le conducteur de montée est disposé à distance du caisson 20, surplombant la paroi amont 22A, de sorte que le courant I puisse descendre selon l’axe Z dans la cuve 10 par l’entremise des ensembles anodiques 50. Pour ce faire, la cuve 10 comprend aussi une superstructure 60 s'étendant au-dessus du caisson 20. Cette superstructure 60 est notamment constituée d’au moins une poutre positionnée selon une direction longitudinale X de la cuve 10 et maintenue en position relativement au caisson 20, par exemple par le biais de pieds (non-montrés) disposés de part et d’autre de la cuve 10 au niveau de ses bords transversaux, aussi appelés têtes. Une ouverture O refermable par un système de capotage 70 de la cuve 10 s’étend longitudinalement au dessus du caisson 20 de chaque côté de la superstructure 60. Le système de capotage 70 est agencé au caisson 20 et à la superstructure 60 pour obturer chaque ouverture O de manière réversible, formant ainsi avec le caisson 20 une enceinte de confinement de la cuve 10. La superstructure 60 est agencée pour supporter d’autres composantes de la cuve 10, notamment les ensembles anodiques 50 par le biais d’un cadre anodique 62 attaché à la superstructure 60. Chaque tige 56 est reliée électriquement au conducteur de montée 14 électrique de la cuve 10 via le cadre 62, ce qui permet d’acheminer le courant I d’électrolyse jusqu’au bloc anodique 52 correspondant. Une partie mobile du cadre 62 permet de déplacer l’ensemble anodique 50 par rapport à la superstructure 60 dans une direction verticale Z de la cuve 10, à travers l’ouverture O, permettant ainsi de plonger le bloc anodique 52 dans le creuset C tout en contrôlant la position du bloc anodique 52 par rapport à la cathode et/ou une surface d’une nappe de métal se formant au fond du creuset C.. [0028] As illustrated in Figure 1, on the upstream side 10A of the tank 10, a source or an output conductor from another tank (not shown) carries the electrolysis current I to a conductor of electrical riser 14 of the tank 10. The riser conductor 14 is electrically connected to a series of anode assemblies 50 of the vessel 10 located above the cathode assembly 40. Each anode assembly 50 comprises at least one anode block 52 having a bottom defining a portion of a lower surface 54 of the anode assemblies 50. Each anode block 52 is suspended from an anode support, such as a conductive rod 56 and a crosspiece. It should be noted that the rising conductor is arranged at a distance from the casing 20, overhanging the upstream wall 22A, so that the current I can descend along the Z axis in the tank 10 via the anode assemblies 50. For To do this, the tank 10 also comprises a superstructure 60 extending above the box 20. This superstructure 60 consists in particular of at least one beam positioned in a longitudinal direction X of the tank 10 and held in position relative to the box 20, for example by means of feet (not shown) arranged on either side of the tank 10 at its transverse edges, also called heads. An opening O that can be closed by a cowling system 70 of the tank 10 extends longitudinally above the casing 20 on each side of the superstructure 60. The cowling system 70 is arranged on the casing 20 and on the superstructure 60 to close off each opening O reversibly, thus forming with box 20 a containment enclosure for vessel 10. Superstructure 60 is arranged to support other components of vessel 10, in particular anode assemblies 50 via an anode frame 62 attached to the superstructure 60. Each rod 56 is connected electrically to the electric rise conductor 14 of the tank 10 via the frame 62, which makes it possible to convey the electrolysis current I to the corresponding anode block 52. A movable part of the frame 62 makes it possible to move the anode assembly 50 relative to the superstructure 60 in a vertical direction Z of the vessel 10, through the opening O, thus making it possible to immerse the anode block 52 in the crucible C while by controlling the position of the anode block 52 relative to the cathode and/or a surface of a sheet of metal forming at the bottom of the crucible C..
[0029] Selon l’exemple illustré aux Figures 3 et 4, une partie basse 32 du système de revêtement 30 ceinture une base de la cathode accueillant les conducteurs électriques 12 . Selon l’exemple illustré, la partie basse 32 s’étend verticalement jusqu’en deçà de la surface supérieure 44 de la cathode. Une partie haute 34 du système de revêtement 30 entoure la surface supérieure 44 de la cathode et s’étend verticalement depuis la partie basse 32 jusqu’au-delà de la surface supérieure 44. La partie haute 34 du système de revêtement 30 forme un pourtour du creuset C s’étendant verticalement depuis le fond du creuset C. According to the example illustrated in Figures 3 and 4, a lower part 32 of the coating system 30 surrounds a base of the cathode receiving the electrical conductors 12 . According to the example illustrated, the lower part 32 extends vertically to below the upper surface 44 of the cathode. An upper portion 34 of the coating system 30 surrounds the upper surface 44 of the cathode and extends vertically from the lower part 32 to beyond the upper surface 44. The upper part 34 of the coating system 30 forms a circumference of the crucible C extending vertically from the bottom of the crucible C.
[0030] Le système de revêtement 30 sert à la fois à former les contours du creuset C et à protéger les parois latérales du caisson 20 par rapport au contenu du creuset C. Notamment, en référence aux figures 3 et 4, la partie haute 34 du système de revêtement 30 comporte une couche interne 80 située en périphérie de la cathode et une couche externe 90 jouxtant les parois latérales du caisson 20 en périphérie de la couche interne 80. Un espace en périphérie de la cathode et ceinturé par la couche interne 80 est colmaté par de la pâte de brasque 28. Les contours du creuset C sont donc formés par la surface supérieure 44 de la cathode, la pâte de brasque 28, la couche interne 80 du système de revêtement et le haut de la couche externe 90. The coating system 30 serves both to form the contours of the crucible C and to protect the side walls of the box 20 with respect to the contents of the crucible C. In particular, with reference to Figures 3 and 4, the upper part 34 of the coating system 30 comprises an internal layer 80 located on the periphery of the cathode and an external layer 90 adjoining the side walls of the casing 20 on the periphery of the internal layer 80. A space on the periphery of the cathode and surrounded by the internal layer 80 is clogged with potlining paste 28. The contours of the crucible C are therefore formed by the upper surface 44 of the cathode, the potlining paste 28, the internal layer 80 of the coating system and the top of the external layer 90.
[0031] La couche externe 90 est typiquement constituée d’éléments composés de matériau réfractaire à base de carbure de silicium (SiC) ou autre composition thermiquement réfractaire. Dans le présent exemple, la couche externe 90 inclut un premier étage et un deuxième étage verticalement superposé au premier étage comprenant respectivement une série d’éléments 92, 94 apposés l’un à la suite de l’autre contre le caisson 20. Dans l’exemple, les éléments 92 sont des briques réfactaire et les éléments 94 sont des dalles de SiC. Il est à noter que selon certaines réalisations, les éléments 94 peuvent être omis. Également, d’autres matériaux isolants avec mica peuvent être ajoutés au besoin. Tel qu’illustré à la Figure 3, la couche interne 80 comprend une série de blocs 82 de parement internes apposés horizontalement l’un à la suite de l’autre contre la couche externe 90. Chacun des blocs 82 de parement interne a une double vocation. D’une part, chacun des blocs 82 contribue à protéger à la fois la portion de paroi 22A, 22B, 24G, 24D du caisson 20 et la portion de couche externe 90 situés vis-à-vis celui-ci de l’usure par l’aluminium et/ou l’électrolyte en fusion dans le creuset C. Chacun des blocs 82 de parement interne est construit en un matériau carboné. Les blocs 82 incluent des blocs 82 dits « nominaux », c’est-à-dire ayant une conductivité thermique nominale permettant un certain transfert de chaleur de référence (ou nominal) qui s’avère approprié pour plusieurs endroits du pourtour du creuset C. The outer layer 90 typically consists of elements composed of refractory material based on silicon carbide (SiC) or other thermally refractory composition. In the present example, the outer layer 90 includes a first stage and a second stage vertically superimposed on the first stage comprising respectively a series of elements 92, 94 affixed one after the other against the box 20. In the For example, the elements 92 are refractory bricks and the elements 94 are SiC slabs. It should be noted that according to certain embodiments, the elements 94 can be omitted. Also, other insulating materials with mica can be added as needed. As illustrated in Figure 3, the inner layer 80 comprises a series of blocks 82 of internal facing affixed horizontally one after the other against the outer layer 90. Each of the blocks 82 of internal facing has a double vocation. On the one hand, each of the blocks 82 contributes to protecting both the wall portion 22A, 22B, 24G, 24D of the box 20 and the outer layer portion 90 located opposite it from wear by the aluminum and/or the molten electrolyte in the crucible C. Each of the blocks 82 of internal facing is constructed from a carbonaceous material. The blocks 82 include blocks 82 called "nominal", that is to say having a nominal thermal conductivity allowing a certain reference (or nominal) heat transfer which proves to be appropriate for several places around the periphery of the crucible C.
[0032] Les inventeurs de la présente technologie ont fait la découverte qu’une cuve dont la couche interne 80 du système de revêtement 30 était exclusivement faite de blocs 82 nominaux ne répond pas parfaitement aux impératifs de transfert de chaleur spécifiques à certains endroits du pourtour du creuset C. En effet, des caractéristiques électromagnétiques propres à la cuve 10 induisent des effets thermiques localisés dans le creuset C pouvant, en présence de couche interne 80 typique, avoir une influence adverse sur la formation de talus T dans le creuset C. Le talus T, une formation incluant de l’électrolyte solidifié, se dépose sur le pourtour du creuset C dès lors que le contenu du creuset C, aux alentours de 970 °C en son centre, subit un refroidissement vers l’extérieur. Selon l’endroit sur le pourtour du creuset C, un bloc 82 nominal peut, de par ses caractéristiques intrinsèques, induire un transfert de chaleur adéquat, excessif, ou bien insuffisant. Un transfert de chaleur excessif peut mener à une formation excessive de talus T, laquelle peut éventuellement recouvrir la cathode et même interférer avec la descente d’un bloc anodique 52 dans le creuset C. Un transfert de chaleur insuffisant peut mener à une formation de talus T insuffisante, et même à une absence de talus T. Lorsqu’exposée au contenu du creuset C en absence de talus T, la couche interne 80 du système de revêtement 30 est asujettie à une dégradation prématurée par un phénomène s’apparentant à de l’érosion. [0032] The inventors of the present technology have discovered that a tank whose inner layer 80 of the coating system 30 was exclusively made of nominal blocks 82 does not perfectly meet the specific heat transfer requirements at certain places around the perimeter. of the crucible C. Indeed, electromagnetic characteristics specific to the vessel 10 induce localized thermal effects in the crucible C which can, in the presence of typical internal layer 80, have an adverse influence on the formation of slope T in the crucible C. The embankment T, a formation including solidified electrolyte, is deposited on the periphery of crucible C as soon as the contents of crucible C, around 970°C at its center, undergoes cooling outwards. Depending on the place on the periphery of the crucible C, a nominal block 82 can, by its intrinsic characteristics, induce an adequate, excessive, or insufficient heat transfer. Excessive heat transfer can lead to excessive slope formation T, which can eventually coat the cathode and even interfere with the descent of an anode block 52 into crucible C. Insufficient heat transfer can lead to slope formation insufficient T, and even an absence of a slope T. When exposed to the contents of the crucible C in the absence of a slope T, the internal layer 80 of the coating system 30 is subject to premature degradation by a phenomenon similar to 'erosion.
[0033] Ainsi donc, d’autre part, la série de blocs 82 de la couche interne 80 de la présente technologie a aussi pour vocation de réguler localement le transfert de chaleur depuis le creuset C vers la couche externe 90 et hors du caisson 20. Pour ce faire, la série horizontale de blocs 82 comprend plusieurs types de blocs 82 différenciés entre autres sur la base de leur conductivité thermique, et agencés horizontalement le long de la paroi de la cuve pour que leur conductivité thermique réponde à un besoin local en transfert de chaleur. Les blocs 82 incluent ainsi des blocs dits « spécifiques », de conductivité thermique permettant un transfert de chaleur autre que le transfert de chaleur de référence, disposés stratégiquement sur certaines longueurs de la couche interne 80 du système de revêtement 30 en alternance avec d’autres longueurs parcourues par des blocs 82 nominaux. Tel qu’il sera décrit plus bas, les blocs 82 spécifiques peuvent inclure, selon la réalisation, des blocs 82 conducteurs, à conductivité thermique plus élevée que celle des blocs 82 nominaux, et/ou des blocs 82 isolants à conductivité thermique moins élevée que celle des blocs 82 nominaux. Les blocs 82 peuvent être construits en l’un ou l’autre des types de matériaux suivants, énoncés en ordre de conductivité thermique croissante : anthracitique [~7W/m*K], semi-graphitique [~11 W/m*K], graphitique [~20/m*K], graphitisé [~110W/m*K], sur- graphitisé [~125W/m*K], Dans certaines implémentations basse puissance de la cuve 10, les blocs 82 isolants sont en matériau anthracitique, les blocs 82 nominaux sont en matériau semi- graphitique, et les blocs 82 conducteurs sont en matériau graphitique et/ou graphitisé, voire sur- graphitisé. Dans certaines implémentations haute puissance de la cuve 10, les blocs 82 isolants sont en matériau semi-graphitique, les blocs 82 nominaux sont en matériau graphitique, et les blocs 82 conducteurs sont en matériau graphitisé et/ou sur-graphitisé. Thus, on the other hand, the series of blocks 82 of the inner layer 80 of the present technology is also intended to locally regulate the transfer of heat from the crucible C to the outer layer 90 and out of the box 20 To do this, the horizontal series of blocks 82 comprises several types of blocks 82 differentiated among other things on the basis of their thermal conductivity, and arranged horizontally along the wall of the vessel so that their thermal conductivity meets a local need in heat transfer. The blocks 82 thus include so-called "specific" blocks, of thermal conductivity allowing a heat transfer other than the reference heat transfer, strategically placed over certain lengths of the internal layer 80 of the coating system 30 in alternation with other lengths traveled by nominal 82 blocks. As will be described below, specific 82 blocks may include, depending on the embodiment, conductive blocks 82, with higher thermal conductivity than that of the nominal blocks 82, and/or insulating blocks 82 with lower thermal conductivity than that of the nominal blocks 82. Blocks 82 may be constructed of any of the following types of materials, listed in order of increasing thermal conductivity: anthracitic [~7W/m*K], semi-graphitic [~11 W/m*K] , graphitic [~20/m*K], graphitized [~110W/m*K], over-graphitized [~125W/m*K], In certain low power implementations of the vessel 10, the insulating blocks 82 are made of material anthracite, the nominal blocks 82 are made of semi-graphitic material, and the conductive blocks 82 are made of graphitic and/or graphitized, or even over-graphitized material. In some high power implementations of vessel 10, insulating blocks 82 are of semi-graphitic material, nominal blocks 82 are of graphitic material, and conductive blocks 82 are of graphitized and/or over-graphitized material.
[0034] Les caractéristiques électromagnétiques de la cuve 10 influençant la formation de talus T seront maintenant résumées en référence à l’exemple des Figures 1 et 2. L’acheminement du courant I à travers la cuve 10, d’abord verticalement (selon l’axe Z) depuis les blocs anodiques 52 jusqu’aux blocs cathodiques 42 et ensuite horizontalement (selon l’axe Y) depuis les blocs cathodiques 42 jusqu’aux conducteurs de sortie 12, induit un champ magnéto-hydrodynamique dans le contenu du creuset C. Ce champ se manifeste par des tourbillons (ou champs de vélocité) V1 , V2, V3, V4 (Figure 2) observables à même la nappe de métal, entre autres à la hauteur de l’interface entre l’électrolyte en fusion avec la nappe de métal (aussi appelée interface bain- métal). La cuve 10 est généralement symétrique par rapport au centre longitudinal CL de la cathode et, similairement, les tourbillons V1 , V3, et V2, V4 sont respectivement des paires de tourbillons correspondants formés de manière généralement symétrique par rapport au centre longitudinal CL lorsque les entrées et sorties de courant dans la cuve sont bien équilibrées ainsi que l’environnement magnétique environnant la cuve. En pratique, il peut exister une différence entre les tourbillons et ces derniers ne sont pas toujours symétriquement agencés, notamment sur les cuves en bout de série. Généralement, les tourbillons V1 , V2 sont formés dans la moitié droite de la cuve 10 s’étendant selon X depuis le centre longitudinal CL, tandis que les tourbillons V3, V4 sont formés dans la moitié gauche de la cuve 10. Bien que la description qui suit portera principalement sur la moitié droite de la cuve 10 et sur les tourbillons V1 , V2 y étant formés, il est entendu que les caractéristiques de la moitié droite récitées s’appliquent, mutatis mutandis, à la moitié gauche de la cuve 10. Néanmoins, il est souligné qu’une différence de l’ordre d’environ 50% peut exister entre une dimension d’un élément situé dans la moitié droite et celle un élément symétrique correspondant situé dans la moitié gauche. Bien que la cuve 10 soit aussi généralement symétrique par rapport au centre transversal CT de la cathode, les tourbillons V1 , V2 ne sont pas répartis de manière symétriques par rapport au centre transversal CT. Il en découle que les tourbillons V1 , V2 puissent circuler aux abords du revêtement 30 avec plus ou moins d’intensité de part et d’autre du centre transversal CT (à deux positions selon l’axe Y) pour une même position selon l’axe X. The electromagnetic characteristics of the tank 10 influencing the formation of slope T will now be summarized with reference to the example of Figures 1 and 2. The routing of the current I through the tank 10, first vertically (according to the axis Z) from the anode blocks 52 to the cathode blocks 42 and then horizontally (along the Y axis) from the cathode blocks 42 to the output conductors 12, induces a magneto-hydrodynamic field in the contents of the crucible C This field is manifested by vortices (or velocity fields) V1, V2, V3, V4 (Figure 2) observable on the sheet of metal, among others at the height of the interface between the electrolyte in fusion with the sheet of metal (also called bath-metal interface). The tank 10 is generally symmetrical with respect to the longitudinal center CL of the cathode and, similarly, the vortices V1, V3, and V2, V4 are respectively pairs of corresponding vortices formed in a generally symmetrical manner with respect to the longitudinal center CL when the inlets and current outputs in the tank are well balanced as well as the magnetic environment surrounding the tank. In practice, there may be a difference between the whirlpools and the latter are not always symmetrically arranged, in particular on the tanks at the end of the series. Generally, the vortices V1, V2 are formed in the right half of the tank 10 extending along X from the longitudinal center CL, while the vortices V3, V4 are formed in the left half of the tank 10. Although the description which follows will relate mainly to the right half of tank 10 and to the vortices V1, V2 being formed there, it is understood that the characteristics of the recited right half apply, mutatis mutandis, to the left half of tank 10. Nevertheless, it is emphasized that a difference of the order of approximately 50% may exist between a dimension of an element situated in the right half and that of a corresponding symmetrical element situated in the left half. Although tank 10 is also generally symmetrical with respect to the transverse center CT of the cathode, the vortices V1, V2 are not distributed symmetrically with respect to the transverse center CT. It follows that the vortices V1, V2 can circulate around the coating 30 with more or less intensity on either side of the transverse center CT (at two positions along the Y axis) for the same position along the X axis.
Dans l’exemple illustré à la Figure 2, le tourbillon V1 circule dans la moitié droite de la cuve 10 en sens horaire. Depuis à proximité d’une extrémité 22A’ de la paroi amont 22A, le tourbillon V1 fait pression sur la paroi amont 22A et longe la paroi amont 22A sur une certaine distance en se dirigeant vers le centre longitudinal CL, créant une première zone Z1 de sollicitation thermique accrue de la cuve 10. Toujours selon l’exemple de la Figure 2, le tourbillon V1 décroche ensuite de la paroi amont 22A à distance du centre longitudinal CL et bifurque vers la paroi aval 22B. Depuis à proximité du centre longitudinal CL, le tourbillon V1 fait pression sur la paroi aval 22B et longe la paroi aval 22B sur une certaine distance en se dirigeant vers une extrémité 22B’ de la paroi aval 22B, créant une deuxième zone Z2 de sollicitation thermique accrue. À distance de l’extrémité 22B’, le tourbillon V1 décroche de la paroi aval 22B avant d’aller rejoindre la paroi transversale 24D à distance d’extrémités 24D’ opposées de la paroi transversale 24D, créant une zone ZR de sollicitation thermique réduite à la jonction entre les parois aval 22B et transversale 24D. Le tourbillon V2 circule dans la zone ZR de sollicitation thermique réduite en sens antihoraire et à vitesse plus faible que le tourbillon V1 , longeant la paroi aval 22B à proximité de l’extrémité 22B’, induisant une faible pression sur la paroi aval 22B. Ensuite, le tourbillon V1 fait pression sur la paroi transversale 24D de part et d’autre du centre transversal CT et longe la paroi transversale 24D à distance des parois amont 22A et aval 22B, créant une troisième zone Z3 de sollicitation thermique accrue. In the example illustrated in Figure 2, the tourbillon V1 circulates in the right half of the vessel 10 in a clockwise direction. From close to an end 22A' of the upstream wall 22A, the vortex V1 puts pressure on the upstream wall 22A and runs along the upstream wall 22A over a certain distance while heading towards the longitudinal center CL, creating a first zone Z1 of increased thermal stress on the vessel 10. Still according to the example of FIG. 2, the vortex V1 then takes off from the upstream wall 22A at a distance from the longitudinal center CL and branches off towards the downstream wall 22B. From close to the longitudinal center CL, the vortex V1 puts pressure on the downstream wall 22B and runs along the downstream wall 22B over a certain distance while heading towards an end 22B' of the downstream wall 22B, creating a second zone Z2 of thermal stress. increased. At a distance from the end 22B′, the vortex V1 unhooks from the downstream wall 22B before going to rejoin the transverse wall 24D at a distance from opposite ends 24D′ of the transverse wall 24D, creating a zone ZR of thermal stress reduced to the junction between the downstream 22B and transverse 24D walls. The vortex V2 circulates in the zone ZR of reduced thermal stress counterclockwise and at a lower speed than the vortex V1, along the downstream wall 22B near the end 22B', inducing a low pressure on the downstream wall 22B. Then, the vortex V1 puts pressure on the transverse wall 24D on either side of the transverse center CT and runs along the transverse wall 24D at a distance from the upstream 22A and downstream 22B walls, creating a third zone Z3 of increased thermal stress.
[0035] Toujours selon l’exemple de la Figure 2, les zones Z1 , Z2 voient un écoulement normal aux parois latérales et donc un flux thermique plus important qu’en nominal où l’écoulement est latéral. La zone Z3 peut montrer des contre-tourbillons qui facilitent la formation de talus et limitent les flux thermiques. La différence de flux thermique, et plus particulièrement les variations d’échanges thermiques entre le bain/métal et le talus, dans les divers zones Z1 , Z2, Z3 et ZR, peut être observée par la mesure de la répartition du talus autour de la cuve. Un équilibrage des flux thermiques dans les divers zones est donc souhaitable afin de ré-homogénéiser l’épaisseur du talus autour de la cuve 10. [0036] En référence à la Figure 2, afin de pallier les effets adverses de l’électromagnétisme de la cuve 10 sur la formation de talus T le long du pourtour du creuset C, la couche interne 80 du système de revêtement 30 est constituée de segments, c’est-à-dire de séries de blocs 82 soit nominaux (ou segments nominaux 84), soit conducteurs (ou segments conducteurs 86), ou soit isolants (ou segments isolants 88). Chacun des segments 84, 86, 88 hérite des propriétés des blocs 82 dont il est constitué, et peut donc être construit, selon la réalisation, en l’un ou l’autre des types de matériaux suivants, énoncés en ordre de conductivité thermique croissante: anthracitique, semi-graphitique, graphitique, graphitisé, ou sur-graphitisé. Ainsi, selon la réalisation, chaque segment nominal 84 est construit dans un matériau de type semi-graphitique, graphitique ou graphitisé, chaque segment conducteur 86 est construit dans un matériau de type graphitique, graphitisé ou sur-graphitisé, et chaque segment isolant 88 est construit dans un matériau anthracitique, semi-graphitique ou graphitique, de sorte que les segments conducteurs 86 ont une conductivité thermique plus élevée que les segments nominaux 84, alors que les segments isolants 88 ont une conductivité thermique moindre que les segments nominaux 84. Les segments 84, 86 et 88 sont apposés en alternance le long des parois latérales du caisson 20. Tout dépendant de la réalisation, les segments 84, 86 et 88 peuvent inclure plus d’un segment nominal 84, plus d’un segment conducteur 86 et/ou plus d’un segment isolant 88 le long d’une même paroi latérale. Dans l’exemple montré, le long de la paroi amont 22A, un premier segment nominal 84A s’étend depuis le centre longitudinal CL vers une extrémité 22A’ de la paroi amont 22A. Un premier segment conducteur 86A s’étend depuis à proximité de l’extrémité 22A’ vers le centre longitudinal CL. Le premier segment conducteur 86A jouxte la zone Z1 . Il est à noter que le premier segment nominal 84A est plus long que le premier segment conducteur 86A. Le premier segment conducteur 86A a une longueur équivalente entre 0 et 66% de la distance entre le centre longitudinal CL et l’extrémité 22k'. Sur l’exemple fourni, la longueur du premier segment conducteur 86A peut correspondre à une distance couverte par 2 à 8 blocs cathodiques 42 selon l’axe X, considérant que la cuve compte 12 blocs entre le centre longitudinal CL et l’extrémité 22k’. [0035] Still according to the example of Figure 2, the zones Z1, Z2 see a normal flow to the side walls and therefore a greater heat flux than nominal where the flow is lateral. The Z3 zone can show counter-vortices which facilitate the formation of slopes and limit heat fluxes. The difference in heat flux, and more particularly the variations in heat exchange between the bath/metal and the embankment, in the various zones Z1, Z2, Z3 and ZR, can be observed by measuring the distribution of the embankment around the tank. A balancing of the heat fluxes in the various zones is therefore desirable in order to re-homogenize the thickness of the embankment around the tank 10. [0036] With reference to Figure 2, in order to overcome the adverse effects of the electromagnetism of the tank 10 on the formation of slope T along the periphery of the crucible C, the internal layer 80 of the coating system 30 consists of segments, that is to say series of blocks 82 either nominal (or nominal segments 84), or conductive (or conductive segments 86), or either insulating (or insulating segments 88). Each of the segments 84, 86, 88 inherits the properties of the blocks 82 of which it is made, and can therefore be constructed, depending on the embodiment, of one or other of the following types of materials, listed in order of increasing thermal conductivity : anthracitic, semi-graphitic, graphitic, graphitized, or over-graphitized. Thus, depending on the embodiment, each nominal segment 84 is constructed in a material of the semi-graphitic, graphitic or graphitized type, each conductive segment 86 is constructed in a material of the graphitic, graphitized or over-graphitized type, and each insulating segment 88 is constructed of an anthracitic, semi-graphitic, or graphitic material such that conductive segments 86 have higher thermal conductivity than nominal segments 84, while insulating segments 88 have less thermal conductivity than nominal segments 84. The segments 84, 86, and 88 are alternately affixed along the side walls of box 20. Depending on the embodiment, segments 84, 86, and 88 may include more than one nominal segment 84, more than one conductive segment 86, and/or or more than one insulating segment 88 along a single side wall. In the example shown, along the upstream wall 22A, a first nominal segment 84A extends from the longitudinal center CL towards an end 22A' of the upstream wall 22A. A first conductive segment 86A extends from near end 22A' toward longitudinal center CL. The first conductive segment 86A adjoins zone Z1. Note that first nominal segment 84A is longer than first conductive segment 86A. The first conductive segment 86A has an equivalent length between 0 and 66% of the distance between the longitudinal center CL and the end 22k'. In the example provided, the length of the first conductive segment 86A may correspond to a distance covered by 2 to 8 cathode blocks 42 along the X axis, considering that the tank has 12 blocks between the longitudinal center CL and the end 22k' .
[0037] Le long de la paroi aval 22B, un deuxième segment conducteur 86B s’étend depuis le centre longitudinal CL vers une extrémité 22B’ de la paroi aval 22B. Le deuxième segment conducteur 86B jouxte la zone Z2. On remarquera que le premier segment nominal 84A est plus grand que le deuxième segment conducteur 86B. Le deuxième segment conducteur 86B a une longueur équivalente entre 0 et 70 % de la distance entre le centre longitudinal CL et l’extrémité 22B’. Entre le deuxième segment conducteur 86B et l’extrémité 22B’, la couche interne 80 a une conductivité thermique égale ou moindre à la conductivité thermique nominale. Dans le cas présent, un segment isolant 88 s’étend depuis à proximité de l’extrémité 22B’ vers le centre longitudinal CL. Le segment isolant 88 jouxte la zone ZR. Le segment isolant 88 a une longueur équivalente entre 0 et 40 % de la distance entre le centre longitudinal CL et l’extrémité 22B’. Un deuxième segment nominal 84B est disposé entre le deuxième segment conducteur 86B et le segment isolant 88. Dans d’autres réalisations, le segment isolant 88 est omis, de sorte que le deuxième segment nominal 84B s’étend jusqu’à proximité de l’extrémité 22B’. Along the downstream wall 22B, a second conductive segment 86B extends from the longitudinal center CL towards an end 22B' of the downstream wall 22B. The second conductive segment 86B adjoins zone Z2. Note that first nominal segment 84A is larger than second conductive segment 86B. The second conductive segment 86B has an equivalent length between 0 and 70% of the distance between the longitudinal center CL and the end 22B'. Between the second conductive segment 86B and the end 22B', the inner layer 80 has a thermal conductivity equal to or less than nominal thermal conductivity. In the present case, an insulating segment 88 extends from near the end 22B' towards the longitudinal center CL. Insulating segment 88 adjoins zone ZR. The insulating segment 88 has an equivalent length between 0 and 40% of the distance between the longitudinal center CL and the end 22B'. A second nominal segment 84B is disposed between the second conductive segment 86B and the insulating segment 88. In other embodiments, the insulating segment 88 is omitted, so that the second nominal segment 84B extends to near the end 22B'.
[0038] Le long de la paroi transversale 24D, un troisième segment conducteur 86C, ou segment conducteur transversal, s’étend depuis le centre transversal CT jusqu’à distance d’extrémités 24D’ opposées de la paroi transversale 24D. Le troisième segment conducteur 86C a une longueur équivalente entre 0 et 75 % de la longueur de la paroi transversale 24D. Une paire de troisièmes segments nominaux 84C, ou segments nominaux transverses, s’étendent de part et d’autre du troisième segment conducteur 86C jusqu’aux extrémités 24D’. [0038] Along the transverse wall 24D, a third conductive segment 86C, or transverse conductive segment, extends from the transverse center CT to a distance from opposite ends 24D′ of the transverse wall 24D. The third conductive segment 86C has an equivalent length between 0 and 75% of the length of the transverse wall 24D. A pair of third nominal segments 84C, or transverse nominal segments, extend from either side of the third conducting segment 86C to the ends 24D'.
[0039] Dans cet exemple, les segments nominaux 84A, 84B, 84C sont en matériau graphitique. Le premier segment conducteur 86A est en matériau sur-graphitisé. Le deuxième segment conducteur 86B et le troisième segment conducteur 86C sont en matériau graphitisé. Le segment isolant 88 est en matériau semi-graphitique. Dans d’autres réalisations de la cuve 10, les segments nominaux 84A, 84B, 84C sont en matériau semi-graphitique. Le premier segment conducteur 86A est en matériau graphitisé. Le deuxième segment conducteur 86B et le troisième segment conducteur 86C sont en matériau graphitique. Le segment isolant 88 est en matériau anthracitique. In this example, the nominal segments 84A, 84B, 84C are made of graphite material. The first conductive segment 86A is made of over-graphitized material. The second conductive segment 86B and the third conductive segment 86C are made of graphitized material. The insulating segment 88 is made of semi-graphitic material. In other embodiments of the tank 10, the nominal segments 84A, 84B, 84C are made of semi-graphitic material. The first conductive segment 86A is made of graphitized material. The second conductive segment 86B and the third conductive segment 86C are made of graphitic material. The insulating segment 88 is made of anthracite material.
[0040] En référence à la Figure 4, de par leur nature et leur positionnement eu égard aux tourbillons V1 , V2, les segments de la couche interne 80 du système de revêtement 30 ont en commun de rendre possible un transfert de chaleur local adéquat pour la formation du talus T, de sorte que le talus T s’avérera globalement d’une dimension adéquate et homogène. On entend par dimension homogène une épaisseur de talus T étant sensiblement la même horizontalement (dans le plan XY) tout au long de la couche interne 80. [0040] Referring to Figure 4, by their nature and their positioning with respect to the vortices V1, V2, the segments of the inner layer 80 of the coating system 30 have in common to make possible a local heat transfer adequate for the formation of the embankment T, so that the embankment T will prove globally of an adequate and homogeneous dimension. By homogeneous dimension is meant a slope thickness T being substantially the same horizontally (in the XY plane) throughout the inner layer 80.
[0041] Dans certaines réalisations, la cuve peut être munie de moyens d’évacuation incluent des moyens de refroidissement de l’aluminerie 1 disposés hors de la cuve 10 et répartis autour du caisson 20. Les moyens de refroidissement peuvent inclure des ailettes. Les ailettes peuvent avantageusement être prévues pour avoir une densité plus importante le long des segments conducteurs 86A, 86B, 86C que le long des segments nominaux 84A, 84B, 84C. Dit autrement, un ratio de superficie d’ailettes par unité de longueur de segment conducteurs 86A, 86B, 86C est plus grand qu’un ratio de superficie d’ailettes par unité de longueur de segments nominaux 84A, 84B, 84C. [0041] In some embodiments, the vessel may be provided with evacuation means include means for cooling the aluminum smelter 1 arranged outside the vessel 10 and distributed around the box 20. The cooling means may include fins. The fins can advantageously be provided to have a greater density along the segments conductors 86A, 86B, 86C than along nominal segments 84A, 84B, 84C. In other words, a fin area ratio per unit length of conductive segments 86A, 86B, 86C is greater than a fin area ratio per unit length of nominal segments 84A, 84B, 84C.
[0042] Les moyens de refroidissement peuvent inclure des moyens de soufflage adaptés pour diriger un jet d’air localisé. Les moyens de soufflage peuvent avantageusement être prévus pour qu’une densité de soufflage soit plus importante le long des segments conducteurs 86A, 86B, 86C que le long des segments nominaux 84A, 84B, 84C. Dit autrement, un ratio de débit d’air incident des moyens de soufflage par unité de longueur de segment conducteurs 86A, 86B, 86C est plus grand qu’un ratio de débit d’air incident des moyens de soufflage par unité de longueur de segments nominaux 84A, 84B, 84C. Les moyens de soufflage peuvent être situés vis-à-vis les segments conducteurs 86A, 86B, 86C ou orientés vers les segments conducteurs 86A, 86B, 86C et/ou au loin des segments nominaux 84A, 84B, 84C. [0042] The cooling means may include blowing means suitable for directing a localized jet of air. The blowing means can advantageously be provided so that a blowing density is greater along the conductive segments 86A, 86B, 86C than along the nominal segments 84A, 84B, 84C. In other words, a ratio of incident air flow from the blowing means per unit length of conductive segments 86A, 86B, 86C is greater than a ratio of incident air flow from the blowing means per unit length of segments nominal 84A, 84B, 84C. The blowing means can be located opposite the conductive segments 86A, 86B, 86C or oriented towards the conductive segments 86A, 86B, 86C and/or away from the nominal segments 84A, 84B, 84C.
[0043] D’autres changements pourraient être implémentés par une personne moyennement versée dans l’art en vue du présent document, lesquels seraient aussi compris dans la portée de la présente technologie. [0043] Other changes could be implemented by a person of ordinary skill in the art for the purposes of this document, which would also be within the scope of this technology.
Claims
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202280076660.0A CN118451217A (en) | 2021-11-18 | 2022-11-17 | Lining system for electrolytic cells |
| CA3238216A CA3238216A1 (en) | 2021-11-18 | 2022-11-17 | Interior lining system for an electrolytic cell |
| AU2022393598A AU2022393598A1 (en) | 2021-11-18 | 2022-11-17 | Interior lining system for an electrolytic cell |
| EP22894052.4A EP4433629A1 (en) | 2021-11-18 | 2022-11-17 | Interior lining system for an electrolytic cell |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR2112213A FR3129157B1 (en) | 2021-11-18 | 2021-11-18 | INTERIOR COATING SYSTEM FOR ELECTROLYSIS TANK |
| FRFR2112213 | 2021-11-18 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2023087107A1 true WO2023087107A1 (en) | 2023-05-25 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/CA2022/051698 Ceased WO2023087107A1 (en) | 2021-11-18 | 2022-11-17 | Interior lining system for an electrolytic cell |
Country Status (6)
| Country | Link |
|---|---|
| EP (1) | EP4433629A1 (en) |
| CN (1) | CN118451217A (en) |
| AU (1) | AU2022393598A1 (en) |
| CA (1) | CA3238216A1 (en) |
| FR (1) | FR3129157B1 (en) |
| WO (1) | WO2023087107A1 (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2103657A (en) * | 1981-07-18 | 1983-02-23 | British Aluminium Co Ltd | Electrolytic cell for the production of aluminium |
| US4737254A (en) * | 1985-09-06 | 1988-04-12 | Alcan International Limited | Linings for aluminium reduction cells |
| CA2893476A1 (en) * | 2012-12-13 | 2014-06-19 | Sgl Carbon Se | Side-wall block for a wall in an electrolytic cell for reducing aluminium |
| WO2016001743A1 (en) * | 2014-07-04 | 2016-01-07 | Rio Tinto Alcan International Limited | Side insulation coating for an electrolytic cell |
| CA3148080A1 (en) * | 2019-08-15 | 2021-02-18 | Obshchestvo S Ogranichennoy Otvetstvennost'yu "Obedinennaya Kompaniya Rusal Inzhenerno-Tekhnologicheskiy Tsentr" | Aluminium reduction cell with a heat insulated side lining |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1401518A (en) | 1963-05-21 | 1965-06-04 | Honeywell Regulator Co | Digital miscellaneous process control unit |
| FR2576920B1 (en) * | 1985-02-07 | 1987-05-15 | Pechiney Aluminium | HALL-HEROULT ELECTROLYSIS TANK WITH CATHODIC BARS AND INSULATED SHEATHING |
| EA201490507A1 (en) * | 2011-10-10 | 2014-09-30 | Гудтек Рекавери Текнолоджи Ас | METHOD AND DEVICE FOR REGULATING THE FORMATION OF A LAYER IN ELECTROLYSIS BATH FOR ALUMINUM |
| GB2564456A (en) * | 2017-07-12 | 2019-01-16 | Dubai Aluminium Pjsc | Electrolysis cell for Hall-Héroult process, with cooling pipes for forced air cooling |
-
2021
- 2021-11-18 FR FR2112213A patent/FR3129157B1/en active Active
-
2022
- 2022-11-17 AU AU2022393598A patent/AU2022393598A1/en active Pending
- 2022-11-17 EP EP22894052.4A patent/EP4433629A1/en active Pending
- 2022-11-17 WO PCT/CA2022/051698 patent/WO2023087107A1/en not_active Ceased
- 2022-11-17 CA CA3238216A patent/CA3238216A1/en active Pending
- 2022-11-17 CN CN202280076660.0A patent/CN118451217A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2103657A (en) * | 1981-07-18 | 1983-02-23 | British Aluminium Co Ltd | Electrolytic cell for the production of aluminium |
| US4737254A (en) * | 1985-09-06 | 1988-04-12 | Alcan International Limited | Linings for aluminium reduction cells |
| CA2893476A1 (en) * | 2012-12-13 | 2014-06-19 | Sgl Carbon Se | Side-wall block for a wall in an electrolytic cell for reducing aluminium |
| WO2016001743A1 (en) * | 2014-07-04 | 2016-01-07 | Rio Tinto Alcan International Limited | Side insulation coating for an electrolytic cell |
| CA3148080A1 (en) * | 2019-08-15 | 2021-02-18 | Obshchestvo S Ogranichennoy Otvetstvennost'yu "Obedinennaya Kompaniya Rusal Inzhenerno-Tekhnologicheskiy Tsentr" | Aluminium reduction cell with a heat insulated side lining |
Non-Patent Citations (1)
| Title |
|---|
| SONG YANG, PENG JIANPING, DI YUEZHONG, WANG YAOWU, FENG NAIXIANG: "Metal flow performance in aluminium electrolytic cells with different side-wall types", CANADIAN METALLURGICAL QUARTERLY, PERGAMON, CA, vol. 57, no. 3, 3 July 2018 (2018-07-03), CA , pages 253 - 261, XP093069361, ISSN: 0008-4433, DOI: 10.1080/00084433.2017.1414107 * |
Also Published As
| Publication number | Publication date |
|---|---|
| EP4433629A1 (en) | 2024-09-25 |
| CA3238216A1 (en) | 2023-05-25 |
| AU2022393598A1 (en) | 2024-05-23 |
| CN118451217A (en) | 2024-08-06 |
| FR3129157A1 (en) | 2023-05-19 |
| FR3129157B1 (en) | 2024-10-25 |
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