US3059295A - Composite mold for continuous casting - Google Patents

Composite mold for continuous casting Download PDF

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US3059295A
US3059295A US815901A US81590159A US3059295A US 3059295 A US3059295 A US 3059295A US 815901 A US815901 A US 815901A US 81590159 A US81590159 A US 81590159A US 3059295 A US3059295 A US 3059295A
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graphite
jacket
metal
liner
mold
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US815901A
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Vosskuehler Hugo
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Wieland Werke AG
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Wieland Werke AG
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/04Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds
    • B22D11/049Continuous casting of metals, i.e. casting in indefinite lengths into open-ended moulds for direct chill casting, e.g. electromagnetic casting

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  • This invention relates to molds for continuously casting metals and more particularly'to molds having a metal jacket and a graphite liner.
  • the present invention seeks to overcome the abovementioned disadvantages by adhering a metal layer integrally to the graphite liner so as to intimately bond the metal jacket to the graphite; and thus form a metal-tographite contact which can be separated only by destroying the mold.
  • the metal layer may be applied to the graphite in various ways, depending upon results desired; for example, the metal layer may be applied by spraying molten metal onto the surface of the graphite, or by dipping the graphite liner into molten metal.
  • the metal layer may be applied by spraying molten metal onto the surface of the graphite, or by dipping the graphite liner into molten metal.
  • the invention is preferred to adhere the metal to the graphite liner by' electroplating.
  • the invention is applicable to molds of different cross-sections including circular and rectangular, but it is particularly advantageous for rectangular molds where it is difiicult, if not impossible, in many cases to unite liner and jacket by a severe compression fit.
  • the mold according to the present invention increases the heat flow from the molten metal being cast to the 3,059,295 Patented Oct. 23, 1962 ice cooling medium appliedto the jacket and thus permits an increase in casting rate, resulting in improved grain structure and surface characteristics of the metal which is being continuously cast.
  • FIG. 1 is a longitudinalcross-section through a preferred form of circular mold according to the "invention
  • FIG. 2 is a plan view of FIG. 1;
  • FIG. 3 is an enlarged detail showing the graphite liner and the inner shell of the jacket which is plated onto the liner;
  • FIG. 4 is a transverse section taken on the line 4-4 of FIG. 3;
  • FIG. 5 is a transverse section, somewhat diagrammatically illustrating application of the invention to a mold of oblong cross-section
  • FIG. 6 is a section, on the line 66 of FIG. 5, illustrating very diagrammatically, the interlocking bond between graphite liner and metal jacket.
  • the mold 10 comprises a metal jacket 12 and graphite liner 13:. Cooling water is applied to inlet 14 and withdrawn at annular outlet 15. The cast product is indicated diagrammatically by 11; the cooling water issuing from annular outlet 15 impinges upon the cast product 11, as indicated. It will be understood that this mold may be mounted and used in a manner similar to the mold shown in the above-mentioned Wieland Patent No. 2,871,530.
  • the jacket 12 comprises two assemblies connected together by through bolts 24.
  • the first assembly comprises an upper ring 17 and a lower supporting plate 18 connected by outer cylindrical shell 16.
  • a well 19 is seated in an annular shoulder at the inner edge of the plate 18.
  • the second assembly comprises inner shell 22 having an upper shoulder 23 to .-which is suitably connected an upper plate 20.
  • the graphite liner 13 is bonded to and supported by inner shell 22, in a manner insuring excellent heat transfer as discussed more at length hereinafter.
  • the through bolts 24 are anchored in the bottom plate 18 and passed through upper plate 20. Upper nuts are applied to bolts 24 for suitably clamping the assemblies together.
  • the parts of each assembly are connected in any suitable way.
  • the inner shell 22 is spaced from well 19 and also from bottom plate '18; the latter spacing provides the annular outlet 15.
  • the well 19 provides a space 25 of reduced cross-section to promote increased how of cooling liquid -to overcome any film effect against inner shell 22.
  • the discharge 15 is made smaller than inlet 14 so as to insure completely filling the jacket with water. The tangential connection of the inlet 14 further assists in providing improved cooling,
  • any well-known electroplating process may be used, which will bond the metal to the graphite in an intimate manner.
  • the following process sometimes'referred to as the Elmore process, may be used.
  • the graphite sleeve is placed in an electrolytic bath containing a copper electrolyte with the axis of the liner horizontal.
  • the upper of the liner is immersed in the bath.
  • the graphite tube is rota-ted, and as the copper is deposited on the outside surface of the tube, the surface is pressed by an agate stone which is reciprocated lengthwise of the liner axis. This polishes and packs the electro-deposited copper, preventing sprouts, needles and other projections, providing a smooth, hard, dense layer, making the deposited metal of the order of three times harder than ordinary electrolytic copper, and substantially more dense than ordinary electrolytic copper.
  • any conventional means may be provided to prevent electro-deposition on surfaces where no deposit is wanted; or,- if desired, the entire liner, both inside and out, may be coated with metal and the metal afterwards removed from the inside and other places where no metal deposit is wanted.
  • the copper inner shell 22 is machined to the shape shown.
  • a solid graphite rod may be used on which the copper may be deposited in the manner described above. After copper is deposited to the desired thickness, the solid rod may be bored to form a graphite cylinder.
  • any other process may be used, which will electro-deposit a dense, hard copper coat on the outside surface of the graphite.
  • the well known Cowper-Coles process may be used; here the cylindrical graphite cathode may be disposed vertically and completely immersed in the electrolytic bath, Electro-deposition may be carried out while the cathode rotates at extremely high speed.
  • the liner may be made of any grade or quality of graphite, including materials containing graphite, such as graphite-coated carbons which are suitable for casting the metal it is desired to continuously cast.
  • the jacket also may be made of any metal or alloy, but it is preferred to use copper for electro-deposition. It will be understood that the electrolytic process causes the copper ions to enter the pores of the graphite depositing below the surface and forming an adhering coat which is anchored and keyed to the graphite; this metal coat can be separated from the graphite only by destruction of the graphite. The bond is of such nature that the copper layer cannot be separated from the graphite by stripping.
  • the continuously cast billets may be from three to six inches in diameter
  • the electro-deposited copper layer may be five mm. in thickness (0.02")
  • the graphite liner may be two in thickness (0.008"). These are given by way of examples and not in any limitirig sense.
  • An important advantage of the plating operation is that the graphite liner may be made extremely thin after the metal is bonded to it since its adherence to the copper jacket obviates any necessity for the graphite to be self-supporting after the metal jacket is deposited.
  • the invention is shown applied to a cake mold having plane walls; the inner metal shell is denoted by 30 and the graphite liner by 31.
  • the jacket in this form may follow the construction of the jacket shown in the Wieland Patent No. 2,835,940, except that the plates forming the inner jacket shell are formed by plating metal onto the graphite liner plates.
  • FIG. 6 the interface between metal jacket 30 and graphite liner 31 is deliberately exaggerated to illustrate the tight interlocking bond between these members.
  • a mold in which the graphite liner and metal jacket are intimately bonded together.
  • This intimate bond eliminates air gaps, and also makes possible use of an extremely thin layer of graphite.
  • the efficiency of the bond is not limited to any particular crosssection of mold.
  • the intimacy of the bond is just as elfective in the case of a plane surface, as used in cake molds, as it is in the case of a cylindrical surface, as used in billet molds.
  • the improved efiiciency of heat transfer from liner to jacket makes possible continuous casting at high rates of speed, at the same time obtaining improved internal and external characteristics in the cast product.
  • a mold comprising a metal supporting jacket adapted to be cooled by fluid and a graphite liner defining a mold cavity within said jacket, characterized in that the metal jacket is plated onto the graphite liner to form a massive built-up metal coat.

Description

Oct. 23, 1962 H. VOSSKUEHLER COMPOSITE MOLD FOR CONTINUOUS CASTING Filed May 26, 1959 INVENTOR. Huqo VOSSKUEHLEE United States Patent 01 COMPOSITE MOLD non coNTINUoUs CASTING Hugo Vosskuehler, Wullenstettcn, Germany, assignor to Wieland-Werke A.G., Ulm, Germany, a corporation of Germany Filed May 26, 1 959, Ser. No. 815,901 Claims priority, application Germany June 12, 1958 r 7 Claims. (Cl. 22--57.2)
This invention relates to molds for continuously casting metals and more particularly'to molds having a metal jacket and a graphite liner.
Considerable study has been given over the years to improving the heat transfer between the graphite liner and the metal jacket of moldsfor continuously casting metal. Under the temperature changes occurring in successive continuous casting cycles, there is a great tendency for the metal jacket and graphite liner to separate, destroying perfect solid-to-solid contact between their surfaces. Tests have shown that, if contact between the liner and jacket is reduced or destroyed, flow of heat is seriously impaired, inasmuch as even an extremely thin gap or gas layer possesses a remarkable heat-insulating capacity. For example, it can be shown that 0001 of an inch of air space is equivalent to about 16 inches of copper and to about /2 inches of graphite with respect to thermal conductivity.
Various efforts have been made in the past to improve the heat transfer between the copper jacket and the graphite liner. For example, in Wieland Patent No. 2,871,530, the graphite liner of a billet mold is placed within the jacket with a severe compression fit. The compression fit may be obtained either by pressing an oversize graphite tube into the metal jacket, or by shrinking a heated metal jacket onto the graphite liner. 7
In Wieland Patent No. 2,835,940 intimate thermal contact between the graphite liner and metal jacket of a cake mold is obtained by making the jacket and liner of separate pieces. The jacket pieces are connected by articulated joints so arranged that the jacket may warp or dis tort under the temperature variations of continuous casting. The liner is in the form of relatively thin, separate plates which are so mounted that they may freely follow the changes in shape of the jacket, thereby to maintain good thermal relationship between the liner and jacket.
The above prior practices have, in general, given excellent performance when used for the purposes intended, but have certain limitations for other purposes. For example, the compression fit is useful mainly with cylindical molds and is not especially adapted for rectangular or cake molds. Furthermore, with both types of mold there is a tendency for thermal relationship between jacket and liner to deteriorate after prolonged use, with consequent loss in efiiciency of heat transfer.
The present invention seeks to overcome the abovementioned disadvantages by adhering a metal layer integrally to the graphite liner so as to intimately bond the metal jacket to the graphite; and thus form a metal-tographite contact which can be separated only by destroying the mold. The metal layer may be applied to the graphite in various ways, depending upon results desired; for example, the metal layer may be applied by spraying molten metal onto the surface of the graphite, or by dipping the graphite liner into molten metal. However, it
is preferred to adhere the metal to the graphite liner by' electroplating. The invention is applicable to molds of different cross-sections including circular and rectangular, but it is particularly advantageous for rectangular molds where it is difiicult, if not impossible, in many cases to unite liner and jacket by a severe compression fit.
The mold according to the present invention increases the heat flow from the molten metal being cast to the 3,059,295 Patented Oct. 23, 1962 ice cooling medium appliedto the jacket and thus permits an increase in casting rate, resulting in improved grain structure and surface characteristics of the metal which is being continuously cast.
Other objects and features of the invention will be more apparent from the following description when considered with the following drawings, in which:
FIG. 1 is a longitudinalcross-section through a preferred form of circular mold according to the "invention;
FIG. 2 is a plan view of FIG. 1;
FIG. 3 is an enlarged detail showing the graphite liner and the inner shell of the jacket which is plated onto the liner;
FIG. 4 is a transverse section taken on the line 4-4 of FIG. 3;
FIG. 5 is a transverse section, somewhat diagrammatically illustrating application of the invention to a mold of oblong cross-section;
FIG. 6 is a section, on the line 66 of FIG. 5, illustrating very diagrammatically, the interlocking bond between graphite liner and metal jacket.
In the accompanying drawings and in the description forming part of this specification, certain specific disclosure of the invention is made for purposes of explanation, but it will be understood that the details may be modified in various respects without departure from the broad aspect of the invention.
Referring to the drawings and more particularly to FIGS. 1 to 4, one preferred form of mold will now be described. The mold 10 comprises a metal jacket 12 and graphite liner 13:. Cooling water is applied to inlet 14 and withdrawn at annular outlet 15. The cast product is indicated diagrammatically by 11; the cooling water issuing from annular outlet 15 impinges upon the cast product 11, as indicated. It will be understood that this mold may be mounted and used in a manner similar to the mold shown in the above-mentioned Wieland Patent No. 2,871,530.
The jacket 12 comprises two assemblies connected together by through bolts 24. The first assembly comprises an upper ring 17 and a lower supporting plate 18 connected by outer cylindrical shell 16. A well 19 is seated in an annular shoulder at the inner edge of the plate 18.
The second assembly comprises inner shell 22 having an upper shoulder 23 to .-which is suitably connected an upper plate 20. The graphite liner 13 is bonded to and supported by inner shell 22, in a manner insuring excellent heat transfer as discussed more at length hereinafter. The through bolts 24 are anchored in the bottom plate 18 and passed through upper plate 20. Upper nuts are applied to bolts 24 for suitably clamping the assemblies together. The parts of each assembly are connected in any suitable way.
It will be noted that the inner shell 22 is spaced from well 19 and also from bottom plate '18; the latter spacing provides the annular outlet 15. The well 19 provides a space 25 of reduced cross-section to promote increased how of cooling liquid -to overcome any film effect against inner shell 22. The discharge 15 is made smaller than inlet 14 so as to insure completely filling the jacket with water. The tangential connection of the inlet 14 further assists in providing improved cooling,
A preferred method of adhering the inner shell to the graphite liner will now be described. Any well-known electroplating process may be used, which will bond the metal to the graphite in an intimate manner. For example, the following process, sometimes'referred to as the Elmore process, may be used. The graphite sleeve is placed in an electrolytic bath containing a copper electrolyte with the axis of the liner horizontal. The upper of the liner is immersed in the bath. As the electrodeposition proceeds, the graphite tube is rota-ted, and as the copper is deposited on the outside surface of the tube, the surface is pressed by an agate stone which is reciprocated lengthwise of the liner axis. This polishes and packs the electro-deposited copper, preventing sprouts, needles and other projections, providing a smooth, hard, dense layer, making the deposited metal of the order of three times harder than ordinary electrolytic copper, and substantially more dense than ordinary electrolytic copper.
It will be understood that any conventional means may be provided to prevent electro-deposition on surfaces where no deposit is wanted; or,- if desired, the entire liner, both inside and out, may be coated with metal and the metal afterwards removed from the inside and other places where no metal deposit is wanted. In any event, after the electro-deposition, the copper inner shell 22 is machined to the shape shown.
Instead of starting the electrolytic deposition with a graphite tube, a solid graphite rod may be used on which the copper may be deposited in the manner described above. After copper is deposited to the desired thickness, the solid rod may be bored to form a graphite cylinder.
Instead of the Elmore process, any other process may be used, which will electro-deposit a dense, hard copper coat on the outside surface of the graphite. For example, the well known Cowper-Coles process may be used; here the cylindrical graphite cathode may be disposed vertically and completely immersed in the electrolytic bath, Electro-deposition may be carried out while the cathode rotates at extremely high speed.
The liner may be made of any grade or quality of graphite, including materials containing graphite, such as graphite-coated carbons which are suitable for casting the metal it is desired to continuously cast. The jacket also may be made of any metal or alloy, but it is preferred to use copper for electro-deposition. It will be understood that the electrolytic process causes the copper ions to enter the pores of the graphite depositing below the surface and forming an adhering coat which is anchored and keyed to the graphite; this metal coat can be separated from the graphite only by destruction of the graphite. The bond is of such nature that the copper layer cannot be separated from the graphite by stripping.
The invention is applicable to a wide variation of dimensions. For example, the continuously cast billets may be from three to six inches in diameter, the electro-deposited copper layer may be five mm. in thickness (0.02"), and the graphite liner may be two in thickness (0.008"). These are given by way of examples and not in any limitirig sense. An important advantage of the plating operation is that the graphite liner may be made extremely thin after the metal is bonded to it since its adherence to the copper jacket obviates any necessity for the graphite to be self-supporting after the metal jacket is deposited.
Referring now to FIG. 5, the invention is shown applied to a cake mold having plane walls; the inner metal shell is denoted by 30 and the graphite liner by 31. The jacket in this form may follow the construction of the jacket shown in the Wieland Patent No. 2,835,940, except that the plates forming the inner jacket shell are formed by plating metal onto the graphite liner plates. In FIG. 6 the interface between metal jacket 30 and graphite liner 31 is deliberately exaggerated to illustrate the tight interlocking bond between these members.
Thus a mold is provided in which the graphite liner and metal jacket are intimately bonded together. This intimate bond eliminates air gaps, and also makes possible use of an extremely thin layer of graphite. The efficiency of the bond is not limited to any particular crosssection of mold. The intimacy of the bond is just as elfective in the case of a plane surface, as used in cake molds, as it is in the case of a cylindrical surface, as used in billet molds. The improved efiiciency of heat transfer from liner to jacket makes possible continuous casting at high rates of speed, at the same time obtaining improved internal and external characteristics in the cast product.
While certain novel features have been disclosed and are pointed out in the annexed claims, it will be understood that various omissions, substitutions and changes may be made by those skilled in the art without departing from the spirit of the invention.
What is claimed is:
1. In a system for continuously casting metal, a mold comprising a metal supporting jacket adapted to be cooled by fluid and a graphite liner defining a mold cavity within said jacket, characterized in that the metal jacket is plated onto the graphite liner to form a massive built-up metal coat.
2. The system according to claim 1, in which the jacket and liner are circular and cylindrical.
3. The system according to claim 1, in which the jacket and liner have flat walls.
4. The system according to claim 1, in which the metal jacket comprises densified and hardened electrolytically deposited metal.
5. The system according to claim 1, in which the metal jacket is applied to the graphite liner by spraying.
6. The system according to claim 1 in which the metal jacket is applied by dipping the graphite liner in molten metal.
7. The system according to claim 1, in which the graphite liner is so thin as to require adherence to the jacket for support.
References Cited in the file of this patent UNITED STATES PATENTS 1,630,688 Becket May 31, 1927 1,984,925 Gahn Dec. 18, 1934 2,023,517 Creager Dec. 10, 1935 2,289,791 Loftis July 14, 1942 2,609,576 Roush et al. Sept. 9, 1952 2,871,534 Wieland Feb. 3, 1959
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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3210812A (en) * 1962-12-31 1965-10-12 Scovill Manufacturing Co Continuous casting mold
US3302251A (en) * 1962-10-18 1967-02-07 Mannesmann Ag Molybdenum lined mold for continuous casting
US3307228A (en) * 1963-11-01 1967-03-07 Albert W Scribner Continuous casting control method and apparatus
US3412784A (en) * 1965-06-18 1968-11-26 Wieland Werke Ag A mold for continuous casting of flat bars having an oval graphical insert surrounded by a cooled rectangular jacket
US3435881A (en) * 1967-01-03 1969-04-01 Carbone Corp Anisotropic continuous casting mold
US3459255A (en) * 1966-12-07 1969-08-05 Ascast Corp Graphite continuous casting mold
US3596707A (en) * 1967-06-29 1971-08-03 Cegedur Gp Apparatus for continuous vertical casting
US3665999A (en) * 1970-07-30 1972-05-30 Wagstaff Machine Works Inc Continuous casting mould
JPS4825008U (en) * 1971-07-31 1973-03-24
US3763924A (en) * 1968-06-21 1973-10-09 Cegedur Gp Apparatus for continuous vertical casting
US3780789A (en) * 1969-10-08 1973-12-25 Alusuisse Apparatus for the vertical multiple continuous casting of aluminum and aluminum alloys
US3885617A (en) * 1972-06-14 1975-05-27 Kaiser Aluminium Chem Corp DC casting mold assembly
US3908746A (en) * 1973-03-30 1975-09-30 Clark Automation Inc Continuous casting machine
US4120930A (en) * 1974-08-08 1978-10-17 Lemelson Jerome H Method of coating a composite mold
US4510989A (en) * 1981-03-23 1985-04-16 Mayer Frederic C Production of metal rods

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1630688A (en) * 1924-12-01 1927-05-31 Electro Metallurg Co Chromium-plated carbon article
US1984925A (en) * 1933-01-16 1934-12-18 Erie Resistor Corp Resistor
US2023517A (en) * 1932-07-19 1935-12-10 Rca Corp Electrical resistance device
US2289791A (en) * 1940-07-20 1942-07-14 Henrite Products Corp Electrical resistor
US2609576A (en) * 1949-12-06 1952-09-09 Thompson Prod Inc Method of making hollow shapes
US2871534A (en) * 1956-04-20 1959-02-03 Wieland Werke Ag Method of continuous casting

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1630688A (en) * 1924-12-01 1927-05-31 Electro Metallurg Co Chromium-plated carbon article
US2023517A (en) * 1932-07-19 1935-12-10 Rca Corp Electrical resistance device
US1984925A (en) * 1933-01-16 1934-12-18 Erie Resistor Corp Resistor
US2289791A (en) * 1940-07-20 1942-07-14 Henrite Products Corp Electrical resistor
US2609576A (en) * 1949-12-06 1952-09-09 Thompson Prod Inc Method of making hollow shapes
US2871534A (en) * 1956-04-20 1959-02-03 Wieland Werke Ag Method of continuous casting

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3302251A (en) * 1962-10-18 1967-02-07 Mannesmann Ag Molybdenum lined mold for continuous casting
US3210812A (en) * 1962-12-31 1965-10-12 Scovill Manufacturing Co Continuous casting mold
US3307228A (en) * 1963-11-01 1967-03-07 Albert W Scribner Continuous casting control method and apparatus
US3412784A (en) * 1965-06-18 1968-11-26 Wieland Werke Ag A mold for continuous casting of flat bars having an oval graphical insert surrounded by a cooled rectangular jacket
US3459255A (en) * 1966-12-07 1969-08-05 Ascast Corp Graphite continuous casting mold
US3435881A (en) * 1967-01-03 1969-04-01 Carbone Corp Anisotropic continuous casting mold
US3596707A (en) * 1967-06-29 1971-08-03 Cegedur Gp Apparatus for continuous vertical casting
US3763924A (en) * 1968-06-21 1973-10-09 Cegedur Gp Apparatus for continuous vertical casting
US3780789A (en) * 1969-10-08 1973-12-25 Alusuisse Apparatus for the vertical multiple continuous casting of aluminum and aluminum alloys
US3665999A (en) * 1970-07-30 1972-05-30 Wagstaff Machine Works Inc Continuous casting mould
JPS4825008U (en) * 1971-07-31 1973-03-24
JPS5042117Y2 (en) * 1971-07-31 1975-11-29
US3885617A (en) * 1972-06-14 1975-05-27 Kaiser Aluminium Chem Corp DC casting mold assembly
US3908746A (en) * 1973-03-30 1975-09-30 Clark Automation Inc Continuous casting machine
US4120930A (en) * 1974-08-08 1978-10-17 Lemelson Jerome H Method of coating a composite mold
US4510989A (en) * 1981-03-23 1985-04-16 Mayer Frederic C Production of metal rods

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