US20070227689A1 - Method of Casting an Article - Google Patents

Method of Casting an Article Download PDF

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Publication number
US20070227689A1
US20070227689A1 US11/759,440 US75944007A US2007227689A1 US 20070227689 A1 US20070227689 A1 US 20070227689A1 US 75944007 A US75944007 A US 75944007A US 2007227689 A1 US2007227689 A1 US 2007227689A1
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Prior art keywords
mold
article
halogen
containing compound
mold cavity
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US11/759,440
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Nicholas Green
Andrew Tomkinson
Jonathan Evans
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Mahle Powertrain Ltd
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Mahle Powertrain Ltd
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Publication of US20070227689A1 publication Critical patent/US20070227689A1/en
Assigned to MAHLE POWERTRAIN LIMITED reassignment MAHLE POWERTRAIN LIMITED ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: EVANS, JONATHAN PAUL, TOMKINSON, ANDREW MARK, GREEN, NICHOLAS RUSSELL
Abandoned legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/02Sand moulds or like moulds for shaped castings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C9/00Moulds or cores; Moulding processes
    • B22C9/06Permanent moulds for shaped castings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • B22D19/0009Cylinders, pistons
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00Coating starting from inorganic powder
    • C23C24/02Coating starting from inorganic powder by application of pressure only
    • C23C24/06Compressing powdered coating material, e.g. by milling
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • C23C24/10Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C30/00Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/01Selective coating, e.g. pattern coating, without pre-treatment of the material to be coated
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/10Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
    • C23C4/11Oxides

Definitions

  • the present invention relates to a method of casting an article, particularly, but not exclusively to a method of sand-casting an aluminum alloy engine block.
  • an engine block is made by sand casting an aluminum alloy.
  • a tubular cast iron liner In order to provide a suitable low friction, wear resistant, reciprocating surface, it is known to line the surface of each cylinder in the engine block in which a piston reciprocates, with a tubular cast iron liner.
  • Such liners increase the weight of the engine and, as cast iron has a lower thermal conductivity than aluminum based alloys, the use of such liners is detrimental to the removal of heat from the engine cylinders.
  • This method has a number of disadvantages, however. Removal of the brass inserts can be difficult, particularly in a V-engine where the cylinders are inclined relative to the engine block, and adds an extra, relatively labor-intensive step in the manufacturing process. Moreover, the brass inserts are susceptible to mechanical damage, particularly after repeated exposure to molten aluminum alloy has caused the brass to anneal and soften, and must be replaced at regular intervals, which further increases the cost of the casting process.
  • a method of casting an article using a mold including a mold cavity.
  • the method includes the steps of providing a compound containing a halogen at at least a portion of a surface of the mold adjacent the mold cavity, pouring molten metal into the mold cavity, allowing the metal to cool and solidify, and removing the article from the mold.
  • the halogen is fluorine.
  • the coating may include, for example, dipotassium fluorotitanate.
  • the halogen may be chlorine, and may be, for example, a potassium chloride-magnesium chloride eutectic.
  • the halogen containing compound is provided in a coating applied to at least a portion of the mold surface which forms at least part of the mold cavity.
  • the method further includes the step of subjecting the article to isostatic pressure.
  • the method further includes the step of heating the article to a temperature at which the entire article remains solid while applying the isostatic pressure.
  • the metal is preferably predominantly aluminum.
  • the metal may be an aluminum-silicon alloy, and is preferably a hypoeutectic aluminum-silicon alloy.
  • the coating is sprayed onto the mold surface.
  • the mold is made predominantly from sand.
  • the article may be an engine block.
  • the coated portions of the mold form cylinders in the engine block.
  • FIG. 1 is a schematic illustration of the method of making an article according to the invention.
  • the method is applied to sand casting an engine block 10 from a conventional hypoeutectic aluminum-silicon alloy, such as the 356 or 354 alloys detailed in Tables 1 and 2 (below): TABLE 1 (356 Alloy) Min. Max.
  • a conventional hypoeutectic aluminum-silicon alloy such as the 356 or 354 alloys detailed in Tables 1 and 2 (below): TABLE 1 (356 Alloy) Min. Max.
  • a mold 12 is formed from first 12 a and second 12 b mold parts made from zircon or silicon sand using conventional sand-casting techniques.
  • the cylindrical portions of an upper mold part 12 a, which form cylindrical cavities, i.e., the cylinders in the engine block, are then coated with a coating 14 containing a halogen, such as fluorine.
  • a halogen such as fluorine
  • the halogen is fluorine
  • the coating material contains dipotassium fluorotitanate powder (K 2 TiF 6 ).
  • Other halogen containing compounds such as a mixed potassium chloride—magnesium chloride eutectic, potassium borofluoride, or aluminum chloride may alternatively be used.
  • the K 2 TiF 6 powder is mixed with a solvent, a filler material such as zircon powder, and a gelling agent.
  • the coating material may comprise 60 weight percent powder (the powder comprising 25 weight percent zircon flour and 75 weight percent K 2 TiF 6 dry milled powder) and 40 weight percent IPA solvent.
  • the coating is typically sprayed onto the mold surface, but may also be painted onto the mold. Alternatively, dry K 2 TiF 6 powder may be rubbed onto the mold surface, or even added directly to the sand used to form the mold at levels of approximately 0.5 weight percent K 2 TiF 6 .
  • the mold parts 12 a and 12 b are clamped together to form a mold cavity, and molten aluminum-silicon alloy is pored into the mold cavity. The mold is then allowed to cool until the alloy has solidified. The as-cast engine block 10 is then removed from the mold 12 .
  • the coating reduces transfer of hydrogen ions into the molten alloy and therefore significantly reduces the surface and sub-surface microporosity of the casting. It is believed that this occurs because the fluorine in the coating reacts with the hydrogen ions before they can dissolve in the molten alloy.
  • the surface of the casting adjacent the coating in this example the interior surfaces of the cylinders in the engine block, may be machined and coated as described above without surface microporosity having a deleterious effect on the integrity of the coating.
  • Such a casting will, however, include internal pores, formed not as a result of reaction with the mold as described above, but as a result of the relatively low cooling rate associated with sand casting.
  • the internal pores may be exposed at the article surface during machining of the casting, and therefore it is desirable to eliminate these pores in addition to the surface microporosity.
  • the as-cast engine block is therefore subjected to hot isostatic pressing using a conventional, commercially available Al HIPPING process, the Bodycote Densal® II process, for example.
  • the engine block is placed in a container of fluid, heated to a temperature close to the melting temperature of the alloy but at which the alloy remains solid (e.g., 40° C. below the solidus temperature of the alloy), and the fluid pressurized (e.g., to 1,000 atmospheres of pressure).
  • the engine block is typically retained in the pressurized, heated fluid for forty five minutes to one hour.
  • the combination of fluid pressure and elevated temperature causes the internal pores to cave in and the material formerly surrounding each pore to diffusion bond.
  • the internal pores are substantially eliminated and the mechanical integrity of the casting improved.
  • the casting may thus be machined with substantially reduced risk of exposing internal pores at the casting surface.
  • HIPPING cannot be used to remedy surface microporosity, since the pressurized fluid would fill the surface pores and provide internal support preventing the pore from caving in. Moreover, HIPPING is ineffective in eliminating sub-surface microporosity, since the layer of aluminum alloy separating each pore from the article surface is relatively thin, and is easily ruptured under the pressure of the pressurized fluid, thus exposing the pore interior to the pressurized fluid and preventing consolidation of the material around the pore. In order to address the problem of surface/sub-surface porosity and internal porosity, it is therefore necessary to use a mold coated with or containing a halogen containing compound in addition to HIPPING.
  • the casting is then machined to the required dimensions and surface roughness.
  • the interior surfaces of the cylinders are machined in preparation for the application of a low friction, wear resistant coating using plasma transfer wire arc coating, electro-plating, or similar processes.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)
  • Mold Materials And Core Materials (AREA)

Abstract

A method of casting an article using a mold including a mold cavity, the method including the steps of providing a compound containing a halogen at at least a portion of a surface of the mold adjacent the mold cavity, pouring molten metal into the mold cavity and allowing the metal to cool and solidify, and removing the article from the mold.

Description

    CROSS-REFERENCE TO PRIORITY APPLICATIONS
  • This application hereby claims the benefit of pending International Application No. PCT/GB2005/004712, filed Dec. 8, 2005, (and published Jun. 22, 2006, as WO 2006/064188 A1), which itself claims the benefit of pending United Kingdom Application No. 0427501.2, filed Dec. 16, 2004, (and published Jun. 21, 2006, as GB 2,421,207 A). These applications are hereby incorporated by reference in their entirety. International Application No. PCT/GB2005/004712 designates the United States and, accordingly, this U.S. non-provisional application is a continuation thereof.
  • FIELD OF THE INVENTION
  • The present invention relates to a method of casting an article, particularly, but not exclusively to a method of sand-casting an aluminum alloy engine block.
  • BACKGROUND OF THE INVENTION
  • Typically, an engine block is made by sand casting an aluminum alloy. In order to provide a suitable low friction, wear resistant, reciprocating surface, it is known to line the surface of each cylinder in the engine block in which a piston reciprocates, with a tubular cast iron liner. Such liners increase the weight of the engine and, as cast iron has a lower thermal conductivity than aluminum based alloys, the use of such liners is detrimental to the removal of heat from the engine cylinders.
  • Thus, in order to remove the need for cast iron liners, various processes of coating the inner surface of each cylinder with a metal that is harder than aluminum to provide a low friction, wear resistant reciprocating surface have been developed, and these include electro-coating, plasma transfer wire arc coating, and laser alloying. For example, the plasma-spraying of a ferrous coating is described in U.S. Pat. No. 6,548,195, and use of laser alloying is described in U.S. Pat. No. 6,390,050 and European Publication No. EP 1041173 A1. Unfortunately, such processes only produce a satisfactory coating if applied to a relatively smooth substrate, and even after machining, the surface of a sand cast engine block includes significant porosity.
  • This problem has been addressed in U.S. Pat. No. 5,931,213, which discloses a method of casting an engine block of aluminum in which cylindrical brass inserts are inserted into a sand mold, the brass inserts forming the cylinders in the engine block. As a result of the use of such high thermal conductivity inserts, the cooling rate of the aluminum alloy around the inserts is significantly higher than the cooling rate of the aluminum alloy elsewhere in the mold cavity. Consequently, the porosity in the resultant casting is significantly reduced in the volumes around the inserts, and, once the inserts are removed, machining of the interior of each cylinder produces a surface that is suitable for coating using the above-mentioned methods.
  • This method has a number of disadvantages, however. Removal of the brass inserts can be difficult, particularly in a V-engine where the cylinders are inclined relative to the engine block, and adds an extra, relatively labor-intensive step in the manufacturing process. Moreover, the brass inserts are susceptible to mechanical damage, particularly after repeated exposure to molten aluminum alloy has caused the brass to anneal and soften, and must be replaced at regular intervals, which further increases the cost of the casting process.
  • SUMMARY OF THE INVENTION
  • According to a first aspect of the invention, we provide a method of casting an article using a mold, including a mold cavity. The method includes the steps of providing a compound containing a halogen at at least a portion of a surface of the mold adjacent the mold cavity, pouring molten metal into the mold cavity, allowing the metal to cool and solidify, and removing the article from the mold.
  • By virtue of the provision of such a compound, porosity formed by reaction at the surface of the casting adjacent the relevant portion of mold is reduced, and once machined, this surface provides a suitable substrate for electro-plating, plasma transfer wire arc coating etc. to produce a low friction, wear resistant surface.
  • Preferably, the halogen is fluorine. The coating may include, for example, dipotassium fluorotitanate. Alternatively, the halogen may be chlorine, and may be, for example, a potassium chloride-magnesium chloride eutectic.
  • Preferably, the halogen containing compound is provided in a coating applied to at least a portion of the mold surface which forms at least part of the mold cavity.
  • Preferably, the method further includes the step of subjecting the article to isostatic pressure. In this case, preferably, the method further includes the step of heating the article to a temperature at which the entire article remains solid while applying the isostatic pressure.
  • Subjecting the article to an isostatic pressure, particularly at high pressure, generally eliminates internal pores within the cast article, which improves the mechanical integrity of the article and reduces the risk of any such pores being exposed at the article surface during machining of the article.
  • The metal is preferably predominantly aluminum. The metal may be an aluminum-silicon alloy, and is preferably a hypoeutectic aluminum-silicon alloy.
  • Preferably, the coating is sprayed onto the mold surface.
  • Preferably, the mold is made predominantly from sand.
  • The article may be an engine block. In this case, preferably, the coated portions of the mold form cylinders in the engine block.
  • According to a second aspect of the invention, we provide an article cast using the method of the first aspect of the invention.
  • BRIEF DESCRIPTION OF THE DRAWING
  • FIG. 1 is a schematic illustration of the method of making an article according to the invention.
  • DETAILED DESCRIPTION
  • In accordance with an exemplary embodiment of the invention and as depicted in FIG. 1, the method is applied to sand casting an engine block 10 from a conventional hypoeutectic aluminum-silicon alloy, such as the 356 or 354 alloys detailed in Tables 1 and 2 (below):
    TABLE 1
    (356 Alloy)
    Min. Max.
    Element (weight fraction) (weight fraction) Ideal Content
    Cu 0.2% N/A
    Mg 0.4% 0.6% >0.5%
    Si 6.5% 7.5% >7.00%
    Fe 0.5% N/A
    Mn 0.3% >0.2%
    Ni 0.1% N/A
    Zn 0.10% N/A
    Pb 0.10% N/A
    Sn 0.05% N/A
    Ti  0.05% 0.15% >0.10%
    Sr 200 ppm 350 ppm 250 ppm
    P  20 ppm N/A
    Na  20 ppm N/A
    Ca 100 ppm N/A
    Sb 200 ppm N/A
    Li  2 ppm N/A
    Al + additional Balance Balance Balance
    impurities
  • TABLE 2
    (354 Alloy)
    Min. Max.
    Element (weight fraction) (weight fraction) Ideal Content
    Cu 1.5% 2.0% 1.80%
    Mg 0.5% 0.6% 0.55%
    Si 8.5% 9.5% 9.00%
    Fe 0.15% 0.10%
    Mn 0.05% 0.00
    Ni 100 ppm 0.00
    Zn 0.05% 0.00
    Pb 100 ppm 0.00
    Sn 100 ppm 0.00
    Ti 0.11% 0.14% 0.12%
    Sr 200 ppm 250 ppm 225 ppm
    P  20 ppm 0.00
    Na 100 ppm 0.00
    Ca 100 ppm 0.00
    Sb  20 ppm 0.00
    Li 100 ppm 0.00
    Al + additional Balance Balance Balance
    impurities
  • It should be appreciated, however, that the method may equally be applied to the making of any cast article using any metal or metal alloy, such as an aluminum-magnesium alloy, or magnesium based alloys.
  • A mold 12 is formed from first 12 a and second 12 b mold parts made from zircon or silicon sand using conventional sand-casting techniques. The cylindrical portions of an upper mold part 12 a, which form cylindrical cavities, i.e., the cylinders in the engine block, are then coated with a coating 14 containing a halogen, such as fluorine. In this example, the halogen is fluorine, and the coating material contains dipotassium fluorotitanate powder (K2TiF6). Other halogen containing compounds, such as a mixed potassium chloride—magnesium chloride eutectic, potassium borofluoride, or aluminum chloride may alternatively be used.
  • The K2TiF6 powder is mixed with a solvent, a filler material such as zircon powder, and a gelling agent. The coating material, for example, may comprise 60 weight percent powder (the powder comprising 25 weight percent zircon flour and 75 weight percent K2TiF6 dry milled powder) and 40 weight percent IPA solvent.
  • The coating is typically sprayed onto the mold surface, but may also be painted onto the mold. Alternatively, dry K2TiF6 powder may be rubbed onto the mold surface, or even added directly to the sand used to form the mold at levels of approximately 0.5 weight percent K2TiF6.
  • The mold parts 12 a and 12 b are clamped together to form a mold cavity, and molten aluminum-silicon alloy is pored into the mold cavity. The mold is then allowed to cool until the alloy has solidified. The as-cast engine block 10 is then removed from the mold 12.
  • Usually during sand-casting of an alloy such as a hypoeutectic aluminum-silicon (Al—Si) alloy, hydrogen ions migrate from the mold 12 into the liquid metal adjacent the mold surface. As the molten metal solidifies, dissolved hydrogen is ejected from the solidification front into the remaining liquid metal, which results in the formation of a plurality of sub-surface elongate micropores that extend into the casting, generally perpendicular to the surface of the casting, up to a depth of 3 to 4 mm. The inclusion of strontium in the alloy is believed to enhance this process. Conventionally, during machining of the cast article, less than 3 mm of material is removed from the article surface, and therefore such machining exposes these pores at the article surface, and renders the surface unsuitable for coating using plasma transfer wire arc coating, electro-plating and similar processes.
  • Where the K2TiF6 coating is present, however, the coating reduces transfer of hydrogen ions into the molten alloy and therefore significantly reduces the surface and sub-surface microporosity of the casting. It is believed that this occurs because the fluorine in the coating reacts with the hydrogen ions before they can dissolve in the molten alloy. As a result, the surface of the casting adjacent the coating, in this example the interior surfaces of the cylinders in the engine block, may be machined and coated as described above without surface microporosity having a deleterious effect on the integrity of the coating.
  • Even where a K2TiF6 coating is used, such a casting will, however, include internal pores, formed not as a result of reaction with the mold as described above, but as a result of the relatively low cooling rate associated with sand casting. The internal pores may be exposed at the article surface during machining of the casting, and therefore it is desirable to eliminate these pores in addition to the surface microporosity.
  • The as-cast engine block is therefore subjected to hot isostatic pressing using a conventional, commercially available Al HIPPING process, the Bodycote Densal® II process, for example. In such a process, the engine block is placed in a container of fluid, heated to a temperature close to the melting temperature of the alloy but at which the alloy remains solid (e.g., 40° C. below the solidus temperature of the alloy), and the fluid pressurized (e.g., to 1,000 atmospheres of pressure). The engine block is typically retained in the pressurized, heated fluid for forty five minutes to one hour.
  • The combination of fluid pressure and elevated temperature causes the internal pores to cave in and the material formerly surrounding each pore to diffusion bond. Thus, the internal pores are substantially eliminated and the mechanical integrity of the casting improved. The casting may thus be machined with substantially reduced risk of exposing internal pores at the casting surface.
  • It should be appreciated that HIPPING cannot be used to remedy surface microporosity, since the pressurized fluid would fill the surface pores and provide internal support preventing the pore from caving in. Moreover, HIPPING is ineffective in eliminating sub-surface microporosity, since the layer of aluminum alloy separating each pore from the article surface is relatively thin, and is easily ruptured under the pressure of the pressurized fluid, thus exposing the pore interior to the pressurized fluid and preventing consolidation of the material around the pore. In order to address the problem of surface/sub-surface porosity and internal porosity, it is therefore necessary to use a mold coated with or containing a halogen containing compound in addition to HIPPING.
  • After HIPPING, the casting is then machined to the required dimensions and surface roughness. In this example, the interior surfaces of the cylinders are machined in preparation for the application of a low friction, wear resistant coating using plasma transfer wire arc coating, electro-plating, or similar processes.
  • When used in this specification and claims, the terms “comprises” and “comprising” and variations thereof mean that the specified features, steps or integers are included. The terms are not to be interpreted to exclude the presence of other features, steps or components.
  • The features disclosed in the foregoing description, or the following claims, or the accompanying drawings, expressed in their specific forms or in terms of a means for performing the disclosed function, or a method or process for attaining the disclosed result, as appropriate, may, separately, or in any combination of such features, be utilized for realizing the invention in diverse forms thereof.

Claims (21)

1. A method of casting an article using a mold including a mold cavity, comprising:
providing a halogen-containing compound at at least a portion of a surface of the mold adjacent the mold cavity;
pouring molten metal into the mold cavity;
cooling and solidifying the metal; and
removing the article from the mold.
2. A method according to claim 1, wherein the halogen comprises fluorine.
3. A method according to claim 2, wherein the halogen-containing compound comprises dipotassium fluorotitanate.
4. A method according to claim 1, wherein the halogen comprises chlorine.
5. A method according to claim 4, wherein the halogen-containing compound comprises a potassium chloride-magnesium chloride eutectic.
6. A method according to claim 1, wherein the halogen-containing compound is provided in a coating applied to at least a portion of a surface of the mold forming at least part of the mold cavity.
7. A method according to claim 1, wherein the method further comprises the step of subjecting the article to isostatic pressure.
8. A method according to claim 7, wherein the method further comprises the step of maintaining the article at an elevated temperature at which the entire article remains solid while applying the isostatic pressure.
9. A method according to claim 1, wherein the step of providing a halogen-containing compound at at least a portion of a surface of the mold comprises spraying the halogen-containing compound onto the mold.
10. A method according to claim 1, wherein the mold is made predominantly from sand.
11. A method according to claim 1, wherein the article is an engine block.
12. A method according to claim 11, wherein the portions of the mold cavity surface that are coated with the halogen-containing compound form cylinders in the engine block.
13. A method of casting an article using a mold including a mold cavity, comprising:
providing a halogen-containing compound at at least a portion of a surface of the mold adjacent the mold cavity;
pouring molten metal into the mold cavity, the metal mostly comprising aluminum;
cooling and solidifying the metal; and
removing the article from the mold.
14. A method according to claim 13, wherein the metal comprises an aluminum-silicon alloy.
15. A method according to claim 14, wherein the metal comprises a hypoeutectic aluminum-silicon alloy.
16. A method according to claim 13, wherein the halogen-containing compound comprises dipotassium fluorotitanate.
17. A method according to claim 13, wherein the halogen-containing compound comprises a potassium chloride-magnesium chloride eutectic.
18. A method according to claim 13, wherein the halogen-containing compound is provided in a coating applied to at least a portion of a surface of the mold forming at least part of the mold cavity.
19. A method according to claim 13, wherein the method further comprises the step of subjecting the article to isostatic pressure.
20. A method according to claim 19, wherein the method further comprises the step of maintaining the article at an elevated temperature at which the entire article remains solid while applying the isostatic pressure.
21. A cast article formed according to the following steps:
providing a mold defining a mold cavity;
providing a halogen-containing compound at at least a portion of a surface of the mold adjacent the mold cavity;
pouring molten metal into the mold cavity;
cooling and solidifying the metal; and
removing the article from the mold.
US11/759,440 2004-12-16 2007-06-07 Method of Casting an Article Abandoned US20070227689A1 (en)

Applications Claiming Priority (3)

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GB0427501.2 2004-12-16
GB0427501A GB2421207A (en) 2004-12-16 2004-12-16 Casting with a halogen containing compound provided on the mould surface
PCT/GB2005/004712 WO2006064188A1 (en) 2004-12-16 2005-12-08 Method of casting an article

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PCT/GB2005/004712 Continuation WO2006064188A1 (en) 2004-12-16 2005-12-08 Method of casting an article

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EP (1) EP1841553A1 (en)
JP (1) JP2008523994A (en)
KR (1) KR20070099603A (en)
CN (1) CN101090784A (en)
GB (1) GB2421207A (en)
WO (1) WO2006064188A1 (en)

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US20210070328A1 (en) * 2017-12-18 2021-03-11 Lothar Thoni Bogie frame for rail vehicles made from an aluminum casting

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US11390824B2 (en) * 2018-01-29 2022-07-19 Purdue Research Foundation Compositions for use as lubricants in die casting, methods of using the same, and products produced therewith
CN108607996B (en) * 2018-07-27 2021-01-05 共享智能铸造产业创新中心有限公司 Arc spraying equipment applied to 3D printing technology
CN111534768B (en) * 2020-06-15 2021-08-03 中北大学 Hierarchical hot isostatic pressing method for Cu-containing cast Al-Si-Mg aluminum alloy casting

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Publication number Publication date
KR20070099603A (en) 2007-10-09
GB0427501D0 (en) 2005-01-19
WO2006064188A1 (en) 2006-06-22
EP1841553A1 (en) 2007-10-10
CN101090784A (en) 2007-12-19
JP2008523994A (en) 2008-07-10
GB2421207A (en) 2006-06-21

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