WO2001062992A1 - Nucleated casting systems and methods - Google Patents
Nucleated casting systems and methods Download PDFInfo
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- WO2001062992A1 WO2001062992A1 PCT/US2000/008548 US0008548W WO0162992A1 WO 2001062992 A1 WO2001062992 A1 WO 2001062992A1 US 0008548 W US0008548 W US 0008548W WO 0162992 A1 WO0162992 A1 WO 0162992A1
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- Prior art keywords
- casting
- reduced pressure
- metal
- casting system
- source
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D23/00—Casting processes not provided for in groups B22D1/00 - B22D21/00
- B22D23/06—Melting-down metal, e.g. metal particles, in the mould
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D23/00—Casting processes not provided for in groups B22D1/00 - B22D21/00
- B22D23/06—Melting-down metal, e.g. metal particles, in the mould
- B22D23/10—Electroslag casting
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22B—PRODUCTION AND REFINING OF METALS; PRETREATMENT OF RAW MATERIALS
- C22B9/00—General processes of refining or remelting of metals; Apparatus for electroslag or arc remelting of metals
- C22B9/16—Remelting metals
- C22B9/18—Electroslag remelting
Definitions
- the invention relates to nucleated casting systems and associated methods for forming the casting.
- the invention relates to reduced pressure nucleated cast systems and methods.
- Metals such as iron- (Fe), nickel- (Ni), titanium- (Ti), and cobalt- (Co) based alloys, are often used in turbine component applications, in which fine-grained microstructures, homogeneity, and essentially defect-free compositions are desired. Problems in superalloy castings and ingots are undesirable as the costs associated with superalloy formation are high, and results of these problems, especially in ingots formed into turbine components are undesirable. Conventional systems for producing castings have attempted to reduce the amount of impurities, contaminants, and other constituents, which may produce undesirable consequences in a casting made from the casting.
- Casting to form articles may include at least a step of electroslag refining (ESR) (such as disclosed in US Patent Nos. 5,160,532; 5,310,165; 5,325,906; 5,332,197; 5,348,566; 5,366,206; 5,472,177; 5,480,097;
- ESR electroslag refining
- a conventional electroslag refining method typically uses a refining vessel that contains a slag refining layer floating on a layer of molten refined metal. An ingot of unrefined metal is generally used as a consumable electrode and is lowered into the vessel to make contact with the molten electroslag layer.
- An electric current is passed through the slag layer to the ingot and causes surface melting at the interface between the ingot and the slag layer.
- oxide inclusions or impurities are exposed to the slag and removed at the contact point between the ingot and the slag.
- Droplets of refined metal are formed, and these droplets pass through the slag and are collected in a pool of molten refined metal beneath the slag.
- the electroslag refining apparatus may be dependent on a relationship between the individual method parameters, such as, but not limited to, an intensity of the refined current, specific heat input, and melting rate. This relationship involves undesirable interdependence between the rate of electroslag refining of the metal, metal ingot temperature, and rate at which the refined molten metal is cooled, all of which may result in poor metallurgical structure in the resultant casting.
- a deep melt pool may entrap air therein to cause undesirable voids and pores in the casting.
- the deep melt pool may cause a varied degree of ingredient macrosegregation in the metal that leads to a less desirable microstructure, such as a microstructure that is not a fine-grained microstructure, or segregation of the elemental species so as to form an inhomogeneous structure.
- a subsequent operation has been proposed in combination with the electroslag refining method to overcome this deep melt pool problem.
- This subsequent processing may be vacuum arc remelting (VAR). Vacuum arc remelting is initiated when an ingot is processed by vacuum arc steps to produce a relatively shallow melt pool, whereby an improved microstructure, which may also possess a lower hydrogen content, is produced.
- VAR vacuum arc remelting
- thermo-mechanical processing requires large, expensive equipment, as well as costly amounts of energy input.
- the vertical casting operation forms a relatively deep liquidus portion in the mold, in which the liquidus portion may entrap some gas in the casting as it solidifies, thus possibly resulting in undesirable voids and porosity in the casting.
- the voids and porosity may adversely impact a casting's microstructure and characteristics.
- An aspect of the invention sets forth a nucleated casting system for forming castings under reduced pressure.
- the casting system forms a casting comprising a liquidus portion that receives the refined liquid metal and a solidified portion, the casting further comprising a fine-grain, homogeneous microstructure that is essentially oxide- and sulfide-free and segregation defect free.
- the casting system comprises a source of refined liquid metal, the refined liquid metal having oxides and sulfides refined out of the metal; a reduced pressure system that provides a reduced pressure to at least a portion of the casting system; and a nucleated casting system for forming the casting.
- the reduced pressure system provides a sufficient reduced pressure for reducing entrapped air from the liquidus portion of the casting.
- a further aspect of the invention sets forth a nucleated casting method that forms castings under reduced pressure.
- the casting system forms a casting comprising a liquidus portion that receives the refined liquid metal and a solidified portion, the casting further comprising a fine-grain, homogeneous microstructure that is essentially oxide- and sulfide-free and segregation defect free.
- the casting system comprises a source of refined liquid metal, the refined liquid metal having oxides and sulfides refined out of the metal; a reduced pressure system that provides a reduced pressure to at least a portion of the casting system; and a nucleated casting system for forming the casting.
- the reduced pressure system provides a sufficient reduced pressure for reducing entrapped air from the liquidus portion of the casting.
- Figure 1 is a schematic illustration of a casting system with a reduced pressure system, as embodied by the invention
- Figure. 2 is a partial schematic, vertical sectional illustration of the casting system of Fig. 1 that illustrates details of an electroslag refining system portion of the casting system;
- FIG. 3 is a partial schematic, vertical section illustration in detail of the electroslag refining system portion.
- Figure 4 is a partial schematic, part sectional illustration of the electroslag refining system of the casting system for producing a casting. ;
- the casting systems and methods comprise a source of clean metal that can be provided as a liquid metal stream for a nucleated casting system (also known . as a "vertical casting system").
- the casting system as embodied by the invention, further provides for casting in a reduced pressure environment that can be produced by a reduced pressure system, as embodied by the invention.
- the reduced pressure system produces a relatively mild vacuum in the nucleated casting system, in which the vacuum removes entrapped gas from a liquidus portion of a casting.
- the relatively mild vacuum is applied in a pressure range from about 0.1 atmospheres to about 0.5 atmospheres. This range of reduced pressure in the casting system, as embodied by the invention, can produce an enhanced density in the casting, especially when compared to conventional nucleated casting systems.
- the casting method comprises steps of forming a source of clean liquid metal, for example from an electroslag refining system, delivering or supplying the clean metal to a nucleated casting system in a reduced pressure system, and producing a dense casting that results from entrapped gas being removed by the reduced pressure system, in which the casting includes but is not limited to, a casting, ingot, or preform, with an essentially oxide free and impurity free material.
- the term "essentially free” means that any constituents in the material do not adversely influence the material, for example its strength and related characteristics.
- the casting method produces castings in which segregation of defects has been reduced, especially when compared to castings produced by conventional melting methods, such as described above.
- the description of the invention will describe a casting formed by the casting methods and systems, however, this description is merely exemplary and not intended to limit the invention in any manner.
- the clean-liquid metal source can comprise an electroslag refining apparatus that provides a clean liquid metal, because of the electroslag refining steps.
- the electroslag refining apparatus comprises an electroslag refining system in cooperation with a cold-induction guide (CIG), for example as set forth in the above-mentioned patents to the Assignee of the instant invention.
- the nucleated casting system can comprise a system that permits molten metal to pass through a cooling zone, which is formed with a length sufficient to allow up to about 30 volume percent (on average) of each of the molten metal to solidify.
- the molten metal is then received by a mold and solidification of the molten metal is completed in the mold.
- the molten metal retains liquid characteristics and readily flow within the mold, when less than about 30 volume percent is solid.
- the reduced pressure system may be applied to the entire casting system, for example, but not limited to, surrounding the entire casting system.
- the reduced pressure system may surround only portions of the casting system to remove entrapped gas from the liquidus portion of a casting.
- the portion of the casting system that is surrounded by the reduced pressure system, as embodied by the invention is sufficient to remove entrapped gas from the liquidus portion of a casting during a casting operation.
- the term "surround" with respect to the reduced pressure system is intended to mean that the reduced pressure system encircles, encloses, envelops, and otherwise encases that reduced pressure system, as embodied by the invention.
- the casting methods and systems can produce a casting, which includes a homogeneous, fine-grained microstructure, for many metals and alloys, including but not limited to nickel- (Ni) and cobalt- (Co) based superalloys, iron- (Fe), titanium- (Ti), alloys, which are often used in turbine component applications.
- the castings formed by the casting methods and systems can be converted into a final casting, a billet, or directly forged with reduced processing and heat treatment steps, due to their homogeneous, fine-grained microstructure.
- the casting methods and systems can be used to produce high quality forgings that can be used in many applications, such as but not limited to rotating equipment applications, such as, but not limited to, disks, rotors, blades, vanes, wheel, buckets, rings, shafts, wheels, and other such elements, and other turbine component applications.
- rotating equipment applications such as, but not limited to, disks, rotors, blades, vanes, wheel, buckets, rings, shafts, wheels, and other such elements, and other turbine component applications.
- turbine components formed from castings however, this is merely exemplary of the applications within the scope of the invention.
- Fig. 1 illustrates a semi- schematic, part-sectional, elevational view of the casting system 3 with a reduced pressure system.
- Figures 2-4 illustrate details of casting system features illustrated in Fig. 1.
- the electroslag refining system 1 will be initially described, followed by a description of the casting system 3, and then by a description of the reduced pressure system to facilitate the understanding of the invention.
- the clean metal for the casting system 3 and its associated casting methods can be provided by an electroslag refining system 1.
- the clean metal is fed to a nucleated casting system 2.
- the electroslag refining system 1 and nucleated casting system 1 cooperate to form a casting system 3 with the reduced pressure system for forming a casting.
- the electroslag refining system 1 introduces a consumable electrode 24 of metal to be refined directly into an electroslag refining system 1, and refines the consumable electrode 24 to produce a clean, refined metal melt 46 (hereafter "clean metal").
- the source of metal for the electroslag refining system 1 as a consumable electrode 24 is merely exemplary, and the scope of the invention comprises, but is not limited to, the source metal comprising an ingot, melt of metal, powder metal, and combinations thereof.
- the description of the invention will refer to a consumable electrode, however this is merely exemplary and is not intended to limit the invention in any manner.
- the clean metal 46 is received and retained within a cold hearth structure 40 that is mounted below the electroslag refining apparatus 1.
- the clean metal 46 is dispensed from the cold hearth structure 40 through a cold finger orifice structure 80 that is mounted and disposed below the cold hearth structure 40.
- the electroslag refining system 1 can provide essentially steady state operation in supplying clean metal 46 if the rate of electroslag refining of metal and rate of delivery of refined metal to a cold hearth structure 40 approximates the rate at which molten metal 46 is drained from the cold hearth structure 40 through an orifice 81 of the cold finger orifice structure 80.
- the casting method can operate continuously for an extended period of time and, accordingly, can method a large bulk of metal.
- the casting method can be operated intermittently by intermittent operation of one or more of the features of the casting system 3.
- the clean metal 46 exits the electroslag refining system 1 through the cold finger orifice structure 80 as stream 56, it enters into the nucleated casting system 2 to form a casting 145.
- the stream 56 and the casting 145 which includes its liquidus portion 148, is enveloped by the reduced pressure system 200, as embodied by the invention.
- the casting 145 can be processed to produce a relatively large casting of refined metal.
- the casting 145 may be processed through to produce smaller castings, ingots, articles, or formed into continuous cast castings.
- the casting method and system, as embodied by the invention effectively eliminates many of the processing operations, such as those described above that, until now, have been necessary in order to produce a metal casting having a desired set of material characteristics and properties.
- Figure 1 generally illustrates a reduced pressure system 200 that provides a reduced pressure to portions of the casting system 3.
- the reduced pressure system 200 comprises a reduced pressure-generating device 201 that creates a reduced pressure in the casting system 3.
- the reduced pressure device 201 is connected by reduced pressure system lines 202 to a reduced pressure chamber that surrounds at least a portion of the casting system 3 to reduce pressure therein.
- the reduced pressure system 200 may create a reduced pressure in a chamber 225 (in dashed lines) that surrounds that entire casting system 3.
- the reduced pressure system 200 may comprise a chamber 235 that surrounds only portions of the casting system 3, such as the nucleated casting system 2, to remove entrapped gas from the casting 145.
- the chamber 235 will include appropriate seal structures (not illustrated) to various elements and components of the casting system 3 that are sufficient to maintain the reduced pressure in the reduced pressure system 200 while allowing the operation of the casting system 3.
- the reduced pressure-generating device 201 comprises any appropriately configured device that can reduce the pressure of an enclosed area, such as the chambers, as embodied by the invention.
- the reduced pressure generating device 201 comprises a vacuum pump, in which the vacuum pump can reduce the pressure in the chambers, as embodied by the invention, to a reduced pressure (also known as a "vacuum level") in a range between about 0.1 atmospheres (atm.) to about 0.5 atm.
- the reduced pressure system 200 as embodied by the invention, will create a reduced pressure in the casting system 3 that is sufficient to remove entrapped gas from the liquidus portion 148 of the casting 145.
- a resultant density of the casting 145 will increase, especially when compared to conventional nucleated casting systems.
- the increased density is desirable for many applications of the casting, for example, but not limited to, turbine component applications.
- a vertical motion control apparatus 10 is schematically illustrated.
- the vertical motion control apparatus 10 comprises a box 12 mounted to a vertical support 14 that includes a motive device (not illustrated), such as but not limited to a motor or other mechanism.
- the motive device is adapted to impart rotary motion to a screw member 16.
- An ingot support structure 20 comprises a member, such as but not limited to a member 22, that is threadedly engaged at one end to the screw member 16.
- the member 22 supports the consumable electrode 24 at its other end by an appropriate connection, such as, but not limited to, a bolt 26.
- An electroslag refining structure 30 comprises a reservoir 32 that is cooled by an appropriate coolant, such as, but not limited to, water.
- the reservoir 32 comprises a molten slag 34, in which an excess of the slag 34 is illustrated as the solid slag granules 36.
- the slag composition used in the casting method will vary with the metal being processed.
- a slag skull 75 may be formed along inside surfaces of an inner wall 82 of reservoir 32, due to the cooling influence of the coolant flowing against the outside of inner wall 82, as described hereinafter.
- a cold hearth structure 40 (Figs. 1-3) is mounted below the electroslag refining structure 30.
- the cold hearth structure 40 comprises a hearth 42, which is cooled by an appropriate coolant, such as water.
- the hearth 42 contains a skull 44 of solidified refined metal and a body 46 of refined liquid metal.
- the reservoir 32 may be formed integrally with the hearth 42. Alternatively, the reservoir 32 and hearth 42 may be formed as separate units, which are connected to form the electroslag refining system 1.
- a bottom orifice 81 of the electroslag refining system 1 is provided in the cold finger orifice structure 80, which is described with reference to Figs. 3 and 4.
- a clean metal 46 which is refined by the electroslag refining system 1 so as to be essentially free of oxides, sulfides, and other impurities, can traverse the electroslag refining system 1 and flow out of the orifice 81 of the cold finger orifice structure 80.
- a power supply structure 70 can supply electric refining current to the electroslag refining system 1.
- the power supply structure 70 can comprise an electric power supply and control mechanism 74.
- An electrical conductor 76 that is able to carry current to the member 22 and, in turn, carry current to the consumable electrode
- a conductor 78 is connected to the reservoir 32 to complete a circuit for the power supply structure 70 of the electroslag refining system 1.
- FIG 2 is a detailed part-sectional illustration of the electroslag refining structure 30 and the cold hearth structure 40 in which the electroslag refining structure 30 defines an upper portion of the reservoir 32 and the cold hearth structure 40 defines a lower portion 42 of the reservoir 32.
- the reservoir 32 generally comprises a double-walled reservoir, which includes an inner wall 82 and outer wall -84.
- a coolant 86 such as but not limited to water, is provided between the inner wall 82 and outer wall 84.
- the coolant 86 can flow to and through a flow channel, which is defined between the inner wall 82 and outer wall 84 from a supply 98 (Fig. 3) and through conventional inlets and outlets (not illustrated in the figures).
- the cooling water 86 that cools the wall 82 of the cold hearth structure 40 provides cooling to the electroslag refining structure 30 and the cold hearth structure 40 to cause the skull 44 to form on the inner surface of the cold hearth structure 40.
- the coolant 86 is not essential for operation of the electroslag refining system 1, casting system 3, or electroslag refining structure 30. Cooling may insure that the liquid metal 46 does not contact and attack the inner wall 82, which may cause some dissolution from the wall 82 and contaminate the liquid metal 46.
- the cold hearth structure 40 also comprises an outer wall 88, which may include flanged tubular sections, 90 and 92. Two flanged tubular sections 90 and 92 are illustrated in the bottom portion of Fig. 2.
- the outer wall 88 cooperates with the nucleated casting system 2 to form a controlled atmosphere environment 140, which is described hereinafter.
- the cold hearth structure 40 comprises a cold finger orifice structure 80 that is shown detail Figs. 3 and 4.
- the cold finger orifice structure 80 is illustrated in Fig. 3 in relation to the cold hearth structure 40 and a stream 56 of liquid melt 46 that exits the cold hearth structure 40 through the cold finger orifice structure 80.
- the cold finger orifice structure 80 is illustrated (Figs. 2 and 3) in structural cooperation with the solid metal skull 44 and liquid metal 46.
- Figure 4 illustrates the cold finger orifice structure 80 without the liquid metal or solid metal skull, so details of the cold finger orifice structure 80 are illustrated.
- the cold finger orifice structure 80 comprises the orifice 81 from which processed molten metal 46 is able to flow in the form of a stream 56.
- the cold finger orifice structure 80 is connected to the cold hearth structure 40 and the cold hearth structure 30. Therefore, the cold hearth structure 40 allows processed and generally impurity-free alloy to form the skulls 44 and 83 by contacting walls of the cold hearth structure 40.
- the skulls 44 and 83 thus act as a container for the molten metal 46.
- the skull 83 (Fig. 3), which is formed at the cold finger orifice structure 80, is controllable in terms of its thickness, and is typically formed with a smaller thickness than the skull 44.
- the thicker skull 44 contacts the cold hearth structure 40 and the thinner skull 83 contacts the cold finger orifice structure 80, and the skulls 44 and 83 are in contact with each other to form an essentially continuous skull.
- a controlled amount of heat may be provided to the skull 83 and thermally transmitted to the liquid metal body 46.
- the heat is provided from induction heating coils 85 that are disposed around the cold hearth structure.
- An induction-heating coil 85 can comprise a cooled induction-heating coil, by flow of an appropriate coolant, such as water, into it from a supply 87.
- Induction heating power is supplied from a power source 89, which is schematically illustrated in Fig. 3.
- the construction of the cold finger orifice structure 80 permits heating by induction energy to penetrate the cold finger orifice structure 80 and heat the liquid metal.46 and skull 83, and maintain the orifice 81 open so that the stream 56 may flow out of the orifice 81.
- the orifice may be closed by solidification of the stream 56 of liquid metal 46 if heating power is not applied to the cold finger orifice structure 80.
- the heating is dependent on each of the fingers of the cold finger orifice structure 80 being insulated from the adjoining fingers, for example being insulated by an air or gas gap or by a suitable insulating material.
- the cold finger orifice structure 80 is illustrated in Fig. 4, with both skulls 44 and 83 and the molten metal 46 are omitted for clarity.
- An individual cold finger 97 is separated from each adjoining finger, such as finger 92, by a gap 94.
- the gap 94 may be provided and filled with an insulating material, such as, but not limited to, a ceramic material or insulating gas.
- the molten metal 46 (not illustrated) that is disposed within the cold finger orifice structure 80 does not leak out through the gaps, because the skull 83 creates a bridge over the cold fingers and prevents passage of liquid metal 46 therethrough.
- Each gap extends to the bottom of the cold finger orifice structure 80, as illustrated in Fig. 4, which illustrates a gap 99 aligned with a viewer's line-of-sight.
- the gaps can be provided with a width in a range from about of 20 mils to about 50 mils, which is sufficient to provide an insulated separation of respective adjacent fingers.
- the individual fingers may be provided with a coolant, such as water, by passing coolant into a conduit 96 from a suitable coolant source (not shown). The coolant is then passed around and through a manifold 98 to the individual cooling tubes, such as cooling tube 100. Coolant that exits the cooling tube 100 flows between an outside surface of the cooling tube 100 and an inside surface of a finger.
- a coolant such as water
- the coolant is then collected in a manifold 102, and passed out of the cold finger orifice structure 80 through a water outlet tube 104.
- This individual cold finger water supply tube arrangement allows for cooling of the cold finger orifice structure 80 as a whole.
- the amount of heating or cooling that is provided through the cold finger orifice structure 80 to the skulls 44 and 83, as well as to the liquid metal 46, can be controlled to control the passage of liquid metal 46 through the orifice 81 as a stream 56.
- the controlled heating or cooling is done by controlling the amount of current and coolant that pass in the induction coils 85 to and through the cold finger orifice structure 80.
- the controlled heating or cooling can increase or decrease the thickness of the skulls 44 and 83, and to open or close the orifice 81, or to reduce or increase the passage of the stream 56 through the orifice 81.
- More or less liquid metal 46 can pass through the cold finger orifice structure 80 into the orifice 81 to define the stream 56 by increasing or decreasing the thickness of the skulls 44 and 83.
- the flow of the stream 56 can be maintained at a desirable balance, by controlling coolant water and heating current and power to and through the induction heating coil 85 to maintain the orifice 81 at a set passage size along with controlling the thickness of
- the electroslag refining system 1 can refine ingots that can include defects and impurities or that can be relatively refined.
- a consumable electrode 24 is melted by the electroslag refining system 1.
- the consumable electrode 24 is mounted in the electroslag refining system 1 in contact with molten slag in the electroslag refining system.
- Electrical power is provided to the electroslag refining system and ingot. The power causes melting of the ingot at a surface where it contacts the molten slag and the formation of molten drops of metal. The molten drops to fall through the molten slag.
- the drops are collected after they pass through the molten slag as a body of refined liquid metal in the cold hearth structure 40 below the electroslag refining structure 30.
- Oxides, sulfides, contaminants, and other impurities that originate in the consumable electrode 24 are removed as the droplets form on the surface of the ingot and pass through the molten slag.
- the molten drops are drained from the electroslag refining system 1 at the orifice 81 in the cold finger orifice structure 80 as a stream 56.
- the stream 56 that exits the electroslag refining system 1 of the casting system 3 that forms castings comprises a refined melt that is essentially free of oxides, sulfides, contaminants, and other impurities.
- the rate at which the metal stream 56 exits the cold finger orifice structure 80 can further be controlled by controlling a hydrostatic head of liquid metal 46 above the orifice 81.
- the liquid metal 46 and slag 44 and 83 that extend above the orifice 81 of the cold finger orifice structure 80 define the hydrostatic head. If a casting system 3 with an electroslag refining system 1 is operated with a given constant hydrostatic head and a constant sized orifice 81, an essentially constant flow rate of liquid metal can be established.
- the melt rate is generally equal to the removal rate from the casting system 3.
- the current applied to the casting system 3 can be adjusted to provide more or less liquid metal 46 and slag 44 and 83 above the orifice 81.
- the amount of liquid metal 46 and slag 44 and 83 above the orifice 81 is determined by the power that melts the ingot, and the cooling of the electroslag refining system 1, which create the skulls. By adjusting the applied current, flow through the orifice 81 can be controlled.
- the contact of the consumable electrode 24 with an upper surface of the molten slag 34 can be maintained in order to establish a steady state of operation 1.
- a rate of consumable electrode 24 descent into the melt 46 can be adjusted to ensure that contact of the consumable electrode 24 with the upper surface of the molten slag 34 is maintained for the steady state operation.
- a steady-state discharge from the stream 56 can be maintained in the casting system 3.
- the stream 56 formed in the electroslag refining system 1 of the casting system 3 exits electroslag refining system 1 and is fed to a nucleated casting system 2.
- the nucleated casting system 2 is schematically illustrated in Fig. 1 in cooperation with the electroslag refining system 1.
- the nucleated casting system 2 comprises a disruption site 134 that is positioned to receive the stream 56 from the electroslag refining system 1 of the clean metal nucleated casting system 3.
- the disruption site 134 converts the stream 56 into a plurality of molten metal droplets 138.
- the stream 56 can be fed to disruption site
- the controlled atmosphere environment 140 may include any gas or combination of gases, which do not react with the metal of the stream 56.
- the controlled atmosphere environment 140 presents an environment that prevents the droplets 138 from becoming a fire hazard.
- any noble gas or nitrogen is suitable for use in the controlled atmosphere environment 140 because these gases are generally non-reactive with most metals and alloys within the scope of the invention.
- nitrogen which is a low-cost gas, can be in the controlled atmosphere environment 140, except for metals and alloys that are prone to excessive nitriding.
- the controlled atmosphere environment 140 may comprise nitrogen, argon, and mixtures thereof. If the metal comprises nickel or steel, the controlled atmosphere environment 140 can comprises nitrogen or argon, or mixtures thereof.
- the disruption site 134 can comprise any suitable device for converting the stream 56 into droplets 138.
- the disruption site 134 can comprise a gas atomizer, which circumscribes the stream 56 with one or more jets 142. The flow of gas from the jets 142 that impinge on the stream can be controlled, so the size and velocity of the droplets 138 can be controlled.
- Another atomizing device within the scope of the invention, includes a high pressure atomizing gas in the form of a stream of the gas, which is used to form the controlled atmosphere environment 140.
- the stream of controlled atmosphere environment 140 gas can impinge the metal stream 56 to convert the metal stream 56 into droplets 138.
- Other exemplary types of stream disruption include magneto-hydrodynamic atomization, in which the stream 56 flows through a narrow gap between two electrodes that are connected to a DC power supply with a magnet perpendicular to the electric field, and mechanical-type stream disruption devices.
- the droplets 138 are broadcast downward (Fig. 1) from the disruption site 134 to form a generally diverging cone shape.
- the droplets 138 traverse a cooling zone 144, which is defined by the distance between the disruption site 134 and the upper surface 150 of the metal casting that is supported by the mold 146.
- the cooling zone 144 length is sufficient to solidify a volume fraction portion of a droplet by the time the droplet traverses the cooling zone 144 and impacts the upper surface 150 of the metal casting.
- the portion of the droplet 138 that solidifies (hereinafter referred to as the "solid volume fraction portion”) is sufficient to inhibit coarse dendritic growth in the mold 146 up to a viscosity inflection point at which liquid flow characteristics in the mold are essentially lost.
- the partially molten/partially solidified metal droplets collect in mold 146.
- the mold may comprise a unitary and one-piece mold, as illustrated in the broken lines of Fig. 1.
- the mold may comprises a withdrawal mold, which includes a retractable base 246 that can be withdrawn from sidewalls of the mold 146.
- the following description of the invention will discuss a withdrawal mold as an exemplary, non-limiting mold, and is not intended to limit the invention in any manner.
- the retractable base 246 can be connected to a shaft 241 to move base away from the sidewalls in the direction of arrow 242.
- the shaft 241 may rotate the retractable base 246 in the direction of arrow 243 to provide most portions of the mold to a cooling system, which is described hereinafter.
- the semisolid droplets behave like a liquid if the solid volume fraction portion is less than a viscosity inflection point, and the semisolid droplets exhibit sufficient fluidity to conform to the shape of the mold.
- an upper solid volume fraction portion limit that defines a viscosity inflection point is less than about 40% by volume.
- An exemplary solid volume fraction portion is in a range from about 5% to about 40%, and a solid volume fraction portion in a range from about 15% to about 30% by volume does not adversely influence the viscosity inflection point.
- the spray of droplets 138 creates a liquidus, upper portion 148 disposed proximate the surface of the casting 145 in the mold 146.
- the depth of the liquidus, upper portion 148 is dependent on cooling of the liquidus portion, the solidification rate thereof, and various clean metal nucleated casting system 3 factors, such as, but not limited to, the atomization gas velocity, droplet velocity, the cooling zone 144 length, the stream temperature, and droplet size.
- the liquidus, upper portion 148 can be created with a depth in the mold 146 in a range from about 0.005 inches to about 1.0 inches.
- An exemplary liquidus, upper portion 148 within the scope of invention comprises a depth in a range from about 0.25 to about 0.5 inches in the mold.
- the liquidus, upper portion 148 in the mold 146 should not be greater that a region of the casting, where the metal exhibits predominantly liquid characteristics.
- the mold 146 extracts heat from the casting by thermal conduction through the mold 146 walls and by convection off of the top surface 150 of the casting.
- the liquidus portion 148 reduces a thermal gradient of the casting by the inherent turbulent nature in the liquidus portion 148. The reduction of the thermal gradients reduces hot tears and dendritic coarsening of the casting, both of which are undesirable in castings.
- Heat is extracted from the casting 145 to complete the solidification and form castings. Sufficient nuclei can be formed in the casting 145 so that upon solidification, a fine equiaxed microstructure 149 can be formed in the casting 145 and the resultant article. Porosity and hot working cracking therein are reduced or substantially eliminated by the casting method, as embodied by the invention.
- the mold 146 can be formed of any suitable material for casting applications, such as but not limited to, graphite, cast iron, and copper.
- Graphite is a suitable mold 146 material since it is relatively easy to machine and exhibits satisfactory thermal conductivity for heat removal purposes. Cooling coils that can be embedded in the mold to circulate a coolant may enhance the removal of heat through the mold 146.
- the scope of the invention comprises other means for cooling the mold, as known in the art.
- the mold 146 may not need as much thermal protection as in conventional molds, since the semisolid metal may already be partially solidified. Thus, some heat has already been removed from the semisolid metal to partially solidify them and less heat needs to be removed when the semisolid metal is in the mold, compared to conventional castings formed entirely from liquid metals.
- Decreased heat removal can reduce thermally induced distortion of the mold 146, and this can lead to uniform heat removal rates from the casting to enhance casting uniformity and homogeneity.
- At least one of the electroslag refining system 1 or the mold 146 may be mounted on a moveable support and separated at a fixed rate to maintain a constant cooling zone 144 dimension. Thus, a generally consistent solid volume fraction portion in the metal is formed.
- Baffles 152 may be provided in the nucleated casting system 2 to extend the controlled atmosphere environment 140 from the electroslag refining system 1 to the mold 146. The baffles 152 can prevent oxidation of the partially molten metal and conserve the controlled atmosphere environment 140.
- the controlled atmosphere environment 140 and the cooling zone 144 can be enclosed within the reduced pressure system 200 for casting in a reduced pressure, as embodied by the invention.
- the casting system 3 inhibits undesirable dendritic growth, reduces solidification shrinkage porosity of the formed casting and casting, and reduces hot tearing both during casting and during subsequent hot working of the casting. Further, the casting system 3 produces a uniform, equiaxed structure in the casting which is a result of the minimal distortion of the mold during casting, the controlled transfer of heat during solidification of the casting in the mold, and controlled nucleation.
- the casting system 3 enhances ductility and fracture toughness of the casting compared to conventionally castings.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture And Refinement Of Metals (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP00919937A EP1263996A1 (en) | 2000-02-23 | 2000-03-30 | Nucleated casting systems and methods |
JP2001561800A JP2003523831A (ja) | 2000-02-23 | 2000-03-30 | 核生成鋳造装置及び方法 |
KR1020027010969A KR20020086910A (ko) | 2000-02-23 | 2000-03-30 | 감압 주조 시스템 및 방법 |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US51119700A | 2000-02-23 | 2000-02-23 | |
US09/511,197 | 2000-02-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2001062992A1 true WO2001062992A1 (en) | 2001-08-30 |
Family
ID=24033858
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2000/008548 WO2001062992A1 (en) | 2000-02-23 | 2000-03-30 | Nucleated casting systems and methods |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP1263996A1 (ja) |
JP (1) | JP2003523831A (ja) |
KR (1) | KR20020086910A (ja) |
WO (1) | WO2001062992A1 (ja) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2016142611A1 (fr) * | 2015-03-12 | 2016-09-15 | Snecma | Procédé de fabrication de pièces de turbomachine, ébauche et pièce finale |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8030082B2 (en) | 2006-01-13 | 2011-10-04 | Honeywell International Inc. | Liquid-particle analysis of metal materials |
CN112705677B (zh) * | 2020-12-16 | 2022-05-13 | 辽宁科技大学 | 一种旋转浇铸金属铸锭的装置及方法 |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3519059A (en) * | 1967-07-12 | 1970-07-07 | Viktor Grigorievich Voskoboini | Method of vacuum slag refining of metal in the course of continuous casting |
US4726840A (en) * | 1986-06-07 | 1988-02-23 | Leybold-Heraeus Gmbh | Method for the electroslag refining of metals, especially those having alloy components with an affinity for oxygen |
US5325906A (en) * | 1991-10-21 | 1994-07-05 | General Electric Company | Direct processing of electroslag refined metal |
US5381847A (en) * | 1993-06-10 | 1995-01-17 | Olin Corporation | Vertical casting process |
-
2000
- 2000-03-30 EP EP00919937A patent/EP1263996A1/en not_active Withdrawn
- 2000-03-30 JP JP2001561800A patent/JP2003523831A/ja active Pending
- 2000-03-30 KR KR1020027010969A patent/KR20020086910A/ko not_active Application Discontinuation
- 2000-03-30 WO PCT/US2000/008548 patent/WO2001062992A1/en not_active Application Discontinuation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3519059A (en) * | 1967-07-12 | 1970-07-07 | Viktor Grigorievich Voskoboini | Method of vacuum slag refining of metal in the course of continuous casting |
US4726840A (en) * | 1986-06-07 | 1988-02-23 | Leybold-Heraeus Gmbh | Method for the electroslag refining of metals, especially those having alloy components with an affinity for oxygen |
US5325906A (en) * | 1991-10-21 | 1994-07-05 | General Electric Company | Direct processing of electroslag refined metal |
US5381847A (en) * | 1993-06-10 | 1995-01-17 | Olin Corporation | Vertical casting process |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2016142611A1 (fr) * | 2015-03-12 | 2016-09-15 | Snecma | Procédé de fabrication de pièces de turbomachine, ébauche et pièce finale |
CN107405681A (zh) * | 2015-03-12 | 2017-11-28 | 赛峰航空器发动机 | 用于制造涡轮机部件、坯件以及最终部件的方法 |
US10760153B2 (en) | 2015-03-12 | 2020-09-01 | Safran Aircraft Engines | Method for manufacturing turbomachine components, blank and final component |
CN107405681B (zh) * | 2015-03-12 | 2020-12-22 | 赛峰航空器发动机 | 用于制造涡轮机部件、坯件以及最终部件的方法 |
Also Published As
Publication number | Publication date |
---|---|
JP2003523831A (ja) | 2003-08-12 |
KR20020086910A (ko) | 2002-11-20 |
EP1263996A1 (en) | 2002-12-11 |
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