Classifications

• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
  • B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
  • B22D11/04—Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
  • B22D11/041—Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds for vertical casting
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
  • B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
  • B22D11/04—Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
  • B22D11/0401—Moulds provided with a feed head
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B22—CASTING; POWDER METALLURGY
  • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
  • B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
  • B22D11/12—Accessories for subsequent treating or working cast stock in situ
  • B22D11/124—Accessories for subsequent treating or working cast stock in situ for cooling

Definitions

• the invention relates to a head of a continuous casting mold in charge "of a metallurgical product, in such a bloom, a billet or slab steel
• continuous casting under load which in fact constitutes an improvement on the general process of continuous casting, is implemented in such a way that the meniscus (free surface of the cast metal) is carried upstream of the level or begins the solidification of the metal inside the head of the ingot mold
• the usual copper tubular element of the ingot mold cooled by internal circulation of re rc ⁇ c ⁇ ssement water, is overcome , in a perfectly contiguous manner, by an uncooled extension in heat-insulating refractory material serving as a reserve of molten metal supplied by the casting jet from a distributor placed at the top at a short distance
• the meniscus of liquid metal is established there, during the casting inside the refractory riser, while the solidification of the metal begins only at the level of the cooled metallic tubular element, which, like in conventional continuous casting, calibrates the shape and size of the cast product.
• This gas injection has the effect of shearing the heterogeneous parasitic solidification veil which could form above against the interior wall of the refractory riser and thus create the conditions favorable to a frank and regular start of solidification at the level of the cool copper element located just below.
• the object of the present invention is precisely to propose a solution making it possible to reduce, or even completely eliminate these solidification defects in the corners of the cast products obtained.
• the subject of the invention is a mold for continuous casting in charge of molten metals, comprising a cooled metallic tubular element of quadrangular shape defining the shape and size of the cast product and in which the molten metal solidifies on contact of the cooled inner metal wall, said cooled tubular element being surmounted by an uncooled riser made of heat-insulating refractory material defining a reserve of molten metal to be solidified, a slot for injecting a shearing fluid (in particular a gas inert under pressure, such as argon preferably) along the inner periphery of the mold being formed between the cooled metal element and the refractory riser, mold characterized in that it is provided with flow reduction means of shear fluid in the corners.
• a shearing fluid in particular a gas inert under pressure, such as argon preferably
• these means are constituted by an element constituting an obstacle to the passage of gas in the injection slot and placed in each of the corners of the slot.
• the invention results from the following considerations. To obtain a satisfactory shearing effect from the gas flow injected at the base of the riser, it is necessary to maintain a gas flow rate all along the slot so that it there are no dead zones on which fragments of undesirable solidification would therefore persist. However, even if one feeds the slit from a peripheral distributor of pressurized gas, thus ensuring equal pressure drops and, consequently, a constant linear output flow over the entire length of slit, one does not however obtain a flow of gas injected equal at any point of the perimeter of the poured product.
• FIG. 1 is a schematic half-view, in axial section, of the upper part of the ingot mold, along the plane 1-1 of FIG. 3.
• FIG. 2 is a schematic half-view in axial section of the upper part of the mold, according to plane 2-2 of FIG. 3.
• Figure 3 is a top view of the lower part of the mold, along the plane 3-3 of Figure 1 or Figure 2.
• a Continuous casting ingot mold generally designated by the reference 1 which comprises a tubular element of cooled copper 6 extended upward, and in a very joi ⁇ tive manner to avoid infiltration of molten metal, by an extension 5 made of refractory material not cooled.
• the cooled metallic element 6 and the refractory riser 5 delimit, in their internal part, an internal casting space 3 in which the casting and solidification of a molten metal 4 such as steel is carried out.
• the internal casting space 3 has a cross section of square shape with rounded angles, the radius of which has been deliberately exaggeratedly enlarged in order to better reveal the characteristic constituent elements of the invention which will be specified again below.
• the tubular element cooled in copper 6 constitutes the main element of the mold.
• the riser 5 a specific component of the so-called "laden" casting, its essential function is to serve as a reserve 4 of molten metal .
• This metal arrives by a pouring jet 12 coming from a distributor 14 placed a short distance above and brought by a nozzle 13 mounted on the outlet orifice of the distributor
• the reserve 4 constitutes a buffer mass, which has a role determining in terms of hydrodynamics by allowing the often violent eddies of liquid metal due to the large amount of movement of the steel jet 12 to develop there freely and therefore to absorb it.
• the liquid steel which then arrives in the c ⁇ stailisoir 6 to solidify therein is in a much calmer state and above all distant from the meniscus 15, the agitation of which is often at the origin of the solidification heterogeneities of the extreme skin in a conventional continuous casting mold Below the reserve 4, the flow of molten metal approaches a flow of “piston” type, that is to say without marked gradient of the speed vector in the section, which is extremely favorable for the good completion of the solidification process
• the extension in refractory material 5 generally comprises - but not shown in the figures - a main upper part in a fibrous refractory material chosen for its thermal insulation qualities in order to keep the reserve of molten metal 4 in the liquid state, for example the material sold under the name A120K by the firm KAPYROK and a lower annular insert chosen from a dense refractory material, such as SiAION® to ensure better mechanical strength in the immediate vicinity of the cooled copper element 6 stressed by the start of solidification
• extension is fixed in a well aligned position with the tubular element 6 by means of centering pins not shown and of an assembly flange 9 with tie rod 9 ′, this flange bearing on a metal plate 5a covering the part A refractory plate 10 is advantageously provided for the passage of the tie rods and to ⁇ gidifier the assembly
• parasitic solidification films 16 of more or less extensive cast metal can form on the interior wall of the riser. Even localized around the periphery, they can be harmful to the good. solidification procedure in the c 6 filler as long as these fragments 16 manage to extend to the level of the edge of the cooled element 6 where solidification begins To break off before this stage the possible unwanted solidification veil prematurely forms in the enhancement, a base injection of a shearing fluid is practiced at the base thereof.
• a gas is preferably used in this respect, and more preferably a gas chemically inert with respect to the cast metal, such as argon
• a slot 18, of thin thickness for example of the order of 0.2 mm, is formed between the extension 5 and the copper element re cooled 6
• This slot opens freely towards the inside of the ingot mold and opens at its other end into a sealed annular chamber 19 formed in the extension
• This chamber 19, which runs along the slot 18 all along, serves to distribute the linear flow rate of gas leaving the slit It is connected by a line 20 to an external source of pressurized gas 21
• the slit 18 has an annular shape analogous to the quadrangular shape of the mold, therefore of that which takes the cast product 7 once solidified as a skin within the copper element 6 In particular, it therefore has a four-angle contour as shown in FIG. 3, where the rounding of the angles has been deliberately exaggerated for the aforementioned reasons
• the shearing gas introduced into the casting space 3 is brought from two sides at right angles to the slot 18, the supply bidirection- ⁇ elle and convergent corner areas of the casting space 3 produces a gas blowing in these areas, causing a risk of local distancing of the cast metal from the copper wall 11 at the upper edge thereof, where the extreme skin is formed, and consequently, of the lack of solidified metal, compared to the rest of the periphery, in the vicinity of the edges of the cast product being solidified within the copper element 6. due to the lack of effective cooling of the product in these places.
• the obstructing elements 17, placed in the corners of the gap 18, can be constituted by balls of flexible fibrous refractory material which, after tightening the riser against the top of the metallic element 6, stop off locally the passage by crushing., from the outside to the inside of the mold.
• Each of the obstruction elements 17 is then advantageously delimited towards the outside by the internal contour of the distribution chamber 19, towards the inside by an angle of the casting space 3, and laterally by two rectilig ⁇ es sides converging in the direction of the casting space 3, making an angle ⁇ with the perpendicular to the flat internal surface of the casting space 3, at the corresponding end of the rounded angle 3a (or 3b, 3c, 3d, respectively) of the casting space delimiting inwardly the obstruction element 17.
• the width of the obstruction element 17, in its least wide area, adjacent to an angle of the casting space should preferably be between 4 and 6.5 mm. If this width is less than 4 mm, it is difficult to remove the local gas overflow injected into the corner. If the width is greater than 6.5 mm, there is an area around the corner, where the linear flow rate of injected gas is zero.
• the angle between the rectilinear side of the obstruction element 17 and the perpendicular to the internal surface of the casting space will advantageously be between 0 and 45 °.
• the linear flow rate of injected gas that is to say the flow rate per unit length of the internal contour of the ingot mold at the level of the slot 18 cancels in an area near the corners.
• the two lateral ribs rectilinear obstructing elements 17 can make angles ⁇ and ⁇ 'different with the perpendiculars to the flat internal surface of the internal casting space 3, at the ends of the angles
• the invention is not limited to the embodiment which has been described.
• the slot 18 in its corner areas and to suppress the gas flow in these areas by providing a slight excess thickness of the extension 5 in the corner areas extending along the width of the slot 18, between the internal casting space 3 and the distribution chamber 19
• This additional thickness can be produced by machining, for example by milling, of the underside of the extension 5 adjacent to the element 6
• the additional angle may be provided on element 6, the upper face of which is turned towards the extension 5 for this purpose.
• the area in excess thickness will have a shape analogous to the shape of the obstructing elements 17 as shown in FIG.
• additional thickness may preferably be of the order of 0.2 mm It is also possible to partially obstruct the distribution chamber 19 in areas close to its angles, so as to limit or s remove supply from the corner areas of the slot 18
• the obstruction of the distribution chamber can be achieved, for example, by inserting plugs through the channels in the direction into the corner areas of the distribution chamber gas circulation in the distribution chamber or caps with a certain porosity
• the invention applies to any mold head more continuous casting laden in charge of a metallurgical product, such as a billet, * a bloom or a slab, preforms of shape already close to the finished product (beams, rails, various profiles, ). Furthermore, it can be applied both in the case of continuous casting of steel and in the case of continuous casting of non-ferrous metals.

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• Engineering & Computer Science (AREA)
• Mechanical Engineering (AREA)
• Continuous Casting (AREA)
• Refinement Of Pig-Iron, Manufacture Of Cast Iron, And Steel Manufacture Other Than In Revolving Furnaces (AREA)
• Mold Materials And Core Materials (AREA)
• Casting Support Devices, Ladles, And Melt Control Thereby (AREA)
• Confectionery (AREA)
• Formation And Processing Of Food Products (AREA)

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• 1998
  • 1998-12-18 FR FR9816055A patent/FR2787359B1/fr not_active Expired - Fee Related
• 1999
  • 1999-12-16 US US09/622,228 patent/US6354363B1/en not_active Expired - Fee Related
  • 1999-12-16 BR BR9908047-8A patent/BR9908047A/pt active Search and Examination
  • 1999-12-16 EP EP99959484A patent/EP1056559B1/de not_active Expired - Lifetime
  • 1999-12-16 JP JP2000589295A patent/JP2002532257A/ja active Pending
  • 1999-12-16 SK SK1210-2000A patent/SK12102000A3/sk unknown
  • 1999-12-16 TR TR2000/02392T patent/TR200002392T1/xx unknown
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  • 1999-12-16 RU RU2000123769/02A patent/RU2211743C2/ru not_active IP Right Cessation
  • 1999-12-16 CA CA002320841A patent/CA2320841A1/fr not_active Abandoned
  • 1999-12-16 SI SI9920019A patent/SI20311A/sl unknown
  • 1999-12-16 KR KR1020007008997A patent/KR20010034498A/ko not_active Application Discontinuation
  • 1999-12-16 CZ CZ20003009A patent/CZ20003009A3/cs unknown
  • 1999-12-16 DE DE69909974T patent/DE69909974D1/de not_active Expired - Lifetime
  • 1999-12-16 MX MXPA00007935A patent/MXPA00007935A/es not_active Application Discontinuation
  • 1999-12-16 CN CN99803091A patent/CN1291122A/zh active Pending
  • 1999-12-16 AT AT99959484T patent/ATE246060T1/de not_active IP Right Cessation
  • 1999-12-16 WO PCT/FR1999/003166 patent/WO2000037197A1/fr not_active Application Discontinuation
• 2000
  • 2000-08-07 ZA ZA200004013A patent/ZA200004013B/en unknown

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