WO2003095697A1 - Method for manufacturing clad components - Google Patents

Method for manufacturing clad components Download PDF

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Publication number
WO2003095697A1
WO2003095697A1 PCT/US2003/013037 US0313037W WO03095697A1 WO 2003095697 A1 WO2003095697 A1 WO 2003095697A1 US 0313037 W US0313037 W US 0313037W WO 03095697 A1 WO03095697 A1 WO 03095697A1
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WIPO (PCT)
Prior art keywords
workpiece
metal
beads
preliminary
mold
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/US2003/013037
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French (fr)
Inventor
Xiaodi Huang
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Individual
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Individual
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Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to EP03728559A priority Critical patent/EP1501958A4/en
Priority to JP2004503685A priority patent/JP4409425B2/en
Priority to AU2003234247A priority patent/AU2003234247A1/en
Publication of WO2003095697A1 publication Critical patent/WO2003095697A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • 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
    • B22D19/0081Casting in, on, or around objects which form part of the product pretreatment of the insert, e.g. for enhancing the bonding between insert and surrounding cast metal
    • 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
    • B22D19/0027Cylinders, pistons 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
    • C23C26/00Coating not provided for in groups C23C2/00 - C23C24/00
    • C23C26/02Coating not provided for in groups C23C2/00 - C23C24/00 applying molten material to the substrate
    • 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
    • C23C6/00Coating by casting molten material on the substrate
    • 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
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/02Pretreatment of the material to be coated

Definitions

  • the present invention is in the field of metal parts forming .
  • the aluminum MMC is very brittle, with about a 90% reduction in ductility with 10-15 vol . % ceramic particles in an aluminum matrix. As a result, monolithic aluminum MMC components are more prone to sudden catastrophic failure. This would likely cause serious liability problems if MMC was used for safety- sensitive parts such as a brake rotor and drum. In addition, it is difficult to machine aluminum MMC to final specifications .
  • the SiC or alumina in the aluminum MMC wears cutting tools very fast.
  • aluminum MMC brake rotors do not stand the friction heat well, causing adhesive wear and galling on the rotor rubbing surfaces .
  • U.S. Patent 5,183,632 discloses a method of manufacturing an aluminum disc rotor with aluminum composite rubbing surfaces which consists of aluminum and ceramic powders that are bonded to the aluminum rotor body by heating and pressing.
  • U.S. Patent 5,224,572 discloses a lightweight brake rotor with a thin ceramic coating on rubbing surfaces.
  • U.S. Patent 5,884,388 discloses a method of manufacturing a friction-wear aluminum part by thermally arc- spraying a mixture of aluminum and stainless steel onto the wear surface .
  • U.S. Patent Application Pub. No. 2001/0045332 Al discloses a titanium or aluminum brake disc bonded with stainless steel on the rubbing surfaces by brazing.
  • Japanese Patent Application No. JP-A No. H9-42339 discloses an aluminum brake disc bonded with an alloy steel on the rubbing surfaces by explosive cladding.
  • the present invention is a method for manufacturing a clad component in which a cladding workpiece having a section comprising a first metal onto which a number of metal beads are rigidly bonded is inserted into a mold. A molten second metal is poured into the mold, where it flows about and covers the beads and is then permitted to cool. This process forms an article made of the second metal, which is mechanically interlocked to the beads, clad by the first metal.
  • the first metal is a high-melting point strong metal, such as steel
  • the second metal is a lower- melting point, weaker, but lighter metal, such as aluminum.
  • FIG. 1 shows the mechanical interlocking mechanism disclosed by this invention.
  • FIG. 2 shows the bonding structure of a steel-capped aluminum piston.
  • a preliminary cladding workpiece 1 that is 0.5-20 mm thick, preferably l-5mm thick, and made of a strong, high- melting point metal, such as steel, is manufactured by blanking, cutting, bending and/or drawing from a metal sheet.
  • preliminary workpiece 1 may be manufactured by metal casting, powder metallurgy, extrusion, forging, welding, machining, or other means.
  • workpiece 1 is manufactured from a laminated metal sheet.
  • the laminated metal sheet consists of metal bonded to a "surface material," such as a different metal or a composite consisting of a metal matrix and particles of ceramic or graphite or both, or whisker or fiber reinforcement.
  • a binder preferably organic, such as rosin, gum, glue, dextrin, acrylic, cellulose, phenolic or polyurethane, is applied to a portion of the preliminary cladding workpiece 1 (FIG. 1) evenly or in a certain pattern.
  • the binder is blended with additives. These additives may consist of metal and/or carbon particles in the size range from 0.1-500Dm, preferably 25-147C]m, in the binder and additive ratio up to 1:10, preferably either 50:1 to 10:1 or 1:1 to 1:6.
  • Metal beads 2 which may be of either regular or irregular shapes, adhere on the binder-applied surface 5 of the cladding work piece 1.
  • the regular or irregular shapes may include spherical, cylindrical, polyhedral, ellipsoidal, T-shape, I-shape, L-shape, V-shape, screw, cone, staple, and other shapes which can generate mechanical interlocking. Equal-size metal spheres of 0.5-20 mm in diameter have been found to yield good results.
  • These metal beads 2 adhere on the binder-bearing surface 5 by a random distribution or in a certain distribution pattern.
  • binder may be applied to the beads 2, rather than, or in addition to, the surfaces 5 of the cladding workpiece 1.
  • the distance between beads is preferably 1.5-10 times of the bead's diameter.
  • the metal beads 2 adhere on the entire binder-bearing surface 5 in one layer.
  • the metal beads 2 adhere on the binder-applied surface 5 in more than one layer, with binder applied between the layers to bind the layers of beads together.
  • the workpiece 1, now including the binder and the beads 2, is loaded into a furnace.
  • the transient metal liquid forms necks 3 (FIG. 1) on the beads 2. Due to atomic diffusion of elements in the metal necks to adjacent regions, the metal necks become solid at the elevated temperature.
  • the cross-sectional diameter of a metal neck 3 is smaller than the bead's diameter, preferably 1/3-2/3 of the bead's diameter.
  • the binder itself forms metal liquid and builds metal necks at an elevated temperature. The metal necks become solid after cooling.
  • metal beads 2 bonded on the binder-bearing surface 5 in more than one layer form a porous metal layer on the preliminary cladding workpiece 1.
  • the beads are held together by the transient metal liquid during heating in a furnace. After cooling, this porous metal layer is firmly bonded on the thin article 1 by way of the solidified transient metal liquid. The pores in the porous metal layer are interconnected.
  • Carburizing and nitriding may be conducted on the cladding work piece 1 during heating by controlling the atmosphere of the furnace during the heating procedure .
  • Other heat treatments such as annealing, normalizing, quenching and tempering also can be performed during heating in the furnace .
  • the cladding workpiece can be further shaped by bending, punching, drawing or welding.
  • the metal beads 2 can be deformed by pressing to form them into shapes better adapted for mechanical interlocking.
  • the cladding workpiece can be coated or plated with a material partially or entirely by chemical vapor deposition, physical vapor deposition, thermal spray coating, plating, spraying, brushing, or dipping.
  • the cladding workpiece can be treated by flame hardening, laser surface hardening, or electron beam surface hardening.
  • Second metal 4 (FIG. 1) is melted and cast into this mold to form a component with the cladding workpiece 1.
  • Any metal casting methods commonly used by the metal casting industry such as green sand casting, die casting, squeeze casting, coremaking and inserting, investment casting, lost foam casting, and others, can be used in this invention.
  • metallurgical bonding may exist, the first metal surface, including the surface of the beads 2 and the necks 3 and the cladding workpiece surface 5 bonds with the second metal body 4 primarily by mechanical interlocking, such as the second metal catches the necks of beads 3 or penetrates into the pores of the porous layer.
  • the resulting component is machined, if necessary, to produce the final product with the required dimension accuracy and enhanced properties on the working surface/surfaces.
  • the critical surface/surfaces can be roughened by sand blasting, drilled, slotted, or machined by other means.
  • the critical surface/surfaces can be hardened by chemical vapor deposition, physical vapor deposition, laser surface hardening, or electron beam surface hardening.
  • FIG. 2 illustrates the structure of a steel-capped aluminum piston.
  • Dynamometer test results demonstrate that a steel-surfaced aluminum brake rotor produced by the methods described above presents equivalent braking performance in comparison with a cast iron rotor that weighs about twice as much.
  • the steel-surfaced aluminum brake rotor has the same dimensions and was tested under the identical conditions as the cast iron rotor. During a destruction fade test, the steel-surfaced aluminum brake rotor worked until the rotor surface temperature was over 1400DF. Parts made according to this method are projected for use in various applications for which light weight is desirable, but which also require enhanced surface properties such as wear resistance, thermal barrier, higher operation temperatures, and a desirable coefficient of friction. These applications include steel surfaced aluminum brake rotors, drums, pistons, gears, army tank tracks and clutch components. Projected applications also include steel surfaced magnesium components, steel surfaced titanium components, and other multiple material systems .
  • the present invention finds applications in the forming of metal parts having reduced weight for an equal degree of wear resistance. Particular application is found in the automotive industry.

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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)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

A method for manufacturing a clad component in which a cladding workpiece having a section (1) comprising a first metal onto which a number of metal beads (2) are rigidly bonded is inserted into a mold. A molten second metal (4) is poured into the mold, where it flows about and covers the beads (2) and is then permitted to cool. This process forms an article made of the second metal (4), which is mechanically interlocked to the beads (2), clad by the first metal (1). Typically the first metal (1) is a high-melting point strong metal, such as steel, and the second metal (4) is a lower-melting point, weaker, but lighter metal, such as aluminum.

Description

METHOD FOR MANUFACTURING CLAD COMPONENTS
TECHNICAL FIELD
The present invention is in the field of metal parts forming .
BACKGROUND ART
Driven by the desire to reduce automobile weight and improve fuel efficiency, the auto industry has dramatically increased aluminum use in automobiles in recent years. To further reduce weight, more iron and steel components need to be replaced with aluminum. Aluminum and its alloys have many attractive properties. Poor wear resistance, however, and low working temperature limit its potential wider uses. To solve the above noted problems, various methods of manufacturing lightweight components made of ceramic-reinforced aluminum metal matrix composites (MMC) or so-called ceramic metal composites (CMC) have been disclosed. In these methods, molten aluminum mixed with ceramic particles is poured into a mold to produce a component, or molten aluminum infiltrates a porous ceramic preform to produce a component. The aluminum MMC does improve wear resistance, but creates other problems. The aluminum MMC is very brittle, with about a 90% reduction in ductility with 10-15 vol . % ceramic particles in an aluminum matrix. As a result, monolithic aluminum MMC components are more prone to sudden catastrophic failure. This would likely cause serious liability problems if MMC was used for safety- sensitive parts such as a brake rotor and drum. In addition, it is difficult to machine aluminum MMC to final specifications . The SiC or alumina in the aluminum MMC wears cutting tools very fast. Also, aluminum MMC brake rotors do not stand the friction heat well, causing adhesive wear and galling on the rotor rubbing surfaces . Finally, aluminum MMC material is also expensive. U.S. Patent 5,183,632 discloses a method of manufacturing an aluminum disc rotor with aluminum composite rubbing surfaces which consists of aluminum and ceramic powders that are bonded to the aluminum rotor body by heating and pressing.
U.S. Patent 5,224,572 discloses a lightweight brake rotor with a thin ceramic coating on rubbing surfaces.
U.S. Patent 5,884,388 discloses a method of manufacturing a friction-wear aluminum part by thermally arc- spraying a mixture of aluminum and stainless steel onto the wear surface .
U.S. Patent Application Pub. No. 2001/0045332 Al discloses a titanium or aluminum brake disc bonded with stainless steel on the rubbing surfaces by brazing. Japanese Patent Application No. JP-A No. H9-42339 discloses an aluminum brake disc bonded with an alloy steel on the rubbing surfaces by explosive cladding.
DISCLOSURE OF THE INVENTION The present invention is a method for manufacturing a clad component in which a cladding workpiece having a section comprising a first metal onto which a number of metal beads are rigidly bonded is inserted into a mold. A molten second metal is poured into the mold, where it flows about and covers the beads and is then permitted to cool. This process forms an article made of the second metal, which is mechanically interlocked to the beads, clad by the first metal. Typically the first metal is a high-melting point strong metal, such as steel, and the second metal is a lower- melting point, weaker, but lighter metal, such as aluminum.
The foregoing and other objectives, features and advantages of the invention will be more readily understood upon consideration of the following detailed description of the preferred embodiment (s) , taken in conjunction with the accompanying drawings .
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 shows the mechanical interlocking mechanism disclosed by this invention.
FIG. 2 shows the bonding structure of a steel-capped aluminum piston.
BEST MODES FOR CARRYING OUT THE INVENTION
A preliminary cladding workpiece 1 that is 0.5-20 mm thick, preferably l-5mm thick, and made of a strong, high- melting point metal, such as steel, is manufactured by blanking, cutting, bending and/or drawing from a metal sheet. Alternatively, preliminary workpiece 1 may be manufactured by metal casting, powder metallurgy, extrusion, forging, welding, machining, or other means. In another alternative embodiment, workpiece 1 is manufactured from a laminated metal sheet. The laminated metal sheet consists of metal bonded to a "surface material," such as a different metal or a composite consisting of a metal matrix and particles of ceramic or graphite or both, or whisker or fiber reinforcement.
A binder, preferably organic, such as rosin, gum, glue, dextrin, acrylic, cellulose, phenolic or polyurethane, is applied to a portion of the preliminary cladding workpiece 1 (FIG. 1) evenly or in a certain pattern. As an alternative embodiment, the binder is blended with additives. These additives may consist of metal and/or carbon particles in the size range from 0.1-500Dm, preferably 25-147C]m, in the binder and additive ratio up to 1:10, preferably either 50:1 to 10:1 or 1:1 to 1:6.
Metal beads 2 (FIG. 1) , which may be of either regular or irregular shapes, adhere on the binder-applied surface 5 of the cladding work piece 1. The regular or irregular shapes may include spherical, cylindrical, polyhedral, ellipsoidal, T-shape, I-shape, L-shape, V-shape, screw, cone, staple, and other shapes which can generate mechanical interlocking. Equal-size metal spheres of 0.5-20 mm in diameter have been found to yield good results. These metal beads 2 adhere on the binder-bearing surface 5 by a random distribution or in a certain distribution pattern. Alternatively, binder may be applied to the beads 2, rather than, or in addition to, the surfaces 5 of the cladding workpiece 1. The distance between beads is preferably 1.5-10 times of the bead's diameter. As an alternative embodiment, the metal beads 2 adhere on the entire binder-bearing surface 5 in one layer. As another alternative embodiment, the metal beads 2 adhere on the binder-applied surface 5 in more than one layer, with binder applied between the layers to bind the layers of beads together.
The workpiece 1, now including the binder and the beads 2, is loaded into a furnace. At an elevated temperature, the binder and possibly a portion of the beads 2 and the cladding workpiece surface material 5, form a transient metal liquid. The transient metal liquid forms necks 3 (FIG. 1) on the beads 2. Due to atomic diffusion of elements in the metal necks to adjacent regions, the metal necks become solid at the elevated temperature. The cross-sectional diameter of a metal neck 3 is smaller than the bead's diameter, preferably 1/3-2/3 of the bead's diameter. After cooling, the beads 2 are welded onto the preliminary cladding workpiece 1 through the metal necks 3. As an alternative embodiment, the binder itself forms metal liquid and builds metal necks at an elevated temperature. The metal necks become solid after cooling. As an alternative embodiment, metal beads 2 bonded on the binder-bearing surface 5 in more than one layer form a porous metal layer on the preliminary cladding workpiece 1. The beads are held together by the transient metal liquid during heating in a furnace. After cooling, this porous metal layer is firmly bonded on the thin article 1 by way of the solidified transient metal liquid. The pores in the porous metal layer are interconnected.
As an alternative, several workpieces are prepared simultaneously by following the above method using a larger original preliminary cladding workpiece, which is then cut into pieces after the beads are firmly adhered to it. At least some of the pieces are then used as cladding workpieces in the final steps of the process.
Carburizing and nitriding may be conducted on the cladding work piece 1 during heating by controlling the atmosphere of the furnace during the heating procedure . Other heat treatments such as annealing, normalizing, quenching and tempering also can be performed during heating in the furnace . The cladding workpiece can be further shaped by bending, punching, drawing or welding. The metal beads 2 can be deformed by pressing to form them into shapes better adapted for mechanical interlocking. The cladding workpiece can be coated or plated with a material partially or entirely by chemical vapor deposition, physical vapor deposition, thermal spray coating, plating, spraying, brushing, or dipping. In addition, the cladding workpiece can be treated by flame hardening, laser surface hardening, or electron beam surface hardening.
The cladding workpiece is then inserted into a sand or metal mold. Second metal 4 (FIG. 1) is melted and cast into this mold to form a component with the cladding workpiece 1. Any metal casting methods commonly used by the metal casting industry, such as green sand casting, die casting, squeeze casting, coremaking and inserting, investment casting, lost foam casting, and others, can be used in this invention. Although metallurgical bonding may exist, the first metal surface, including the surface of the beads 2 and the necks 3 and the cladding workpiece surface 5 bonds with the second metal body 4 primarily by mechanical interlocking, such as the second metal catches the necks of beads 3 or penetrates into the pores of the porous layer. The resulting component is machined, if necessary, to produce the final product with the required dimension accuracy and enhanced properties on the working surface/surfaces.
To enhance performance, the critical surface/surfaces can be roughened by sand blasting, drilled, slotted, or machined by other means. To further enhance the surface properties, the critical surface/surfaces can be hardened by chemical vapor deposition, physical vapor deposition, laser surface hardening, or electron beam surface hardening.
FIG. 2 illustrates the structure of a steel-capped aluminum piston.
Dynamometer test results demonstrate that a steel-surfaced aluminum brake rotor produced by the methods described above presents equivalent braking performance in comparison with a cast iron rotor that weighs about twice as much. The steel-surfaced aluminum brake rotor has the same dimensions and was tested under the identical conditions as the cast iron rotor. During a destruction fade test, the steel-surfaced aluminum brake rotor worked until the rotor surface temperature was over 1400DF. Parts made according to this method are projected for use in various applications for which light weight is desirable, but which also require enhanced surface properties such as wear resistance, thermal barrier, higher operation temperatures, and a desirable coefficient of friction. These applications include steel surfaced aluminum brake rotors, drums, pistons, gears, army tank tracks and clutch components. Projected applications also include steel surfaced magnesium components, steel surfaced titanium components, and other multiple material systems .
INDUSTRIAL APPLICABILITY
The present invention finds applications in the forming of metal parts having reduced weight for an equal degree of wear resistance. Particular application is found in the automotive industry.
The terms and expressions that have been employed in the foregoing specification are used as terms of description and not of limitation. There is no intention, in the use of such terms and expressions, of excluding equivalents of the features shown and described or portions thereof, it being recognized that the scope of the invention is defined and limited only by the claims which follow.

Claims

CLAIMS :
1. A method for manufacturing a clad component comprising:
(a) providing a cladding workpiece having a section comprising a first metal, said section having an external surface area and wherein a multiplicity of metal beads are rigidly bonded to at least a portion of said external surface area; (b) inserting said workpiece into a mold;
(c) providing a molten second metal; and
(d) pouring said molten second metal into said mold so that it flows about and covers said beads and permitting said molten second metal to cool, thereby forming an article made of said second metal, which is mechanically interlocked to said beads, clad by said first metal.
2. The method of claim 1 wherein said cladding workpiece is provided by being produced in a process comprising: (a) providing said preliminary workpiece made of a first metal and having a preliminary workpiece external surface area;
(b) providing a binder;
(c) providing a set of metal beads; (d) using said binder to adhere said set of metal beads over at least a portion of said preliminary workpiece external surface area; and (e) heating said preliminary workpiece and permitting said preliminary workpiece to cool, wherein said heating and cooling is sufficient to form a rigid bond between said metal beads and said portion of said preliminary workpiece external surface area, thereby forming a final preliminary workpiece.
3. The method of claim 2 wherein said final preliminary workpiece is used as said cladding workpiece.
4. The method of claim 2 wherein said final preliminary workpiece is cut into sections, one of said sections being used as said cladding workpiece.
5. The method of claim 2, wherein said binder ' includes metal particles .
6. The method of claim 2, wherein said binder includes carbon particles.
7. The method of claim 2, wherein said metal beads are spheroids.
8. The method of claim 2, wherein said step of heating said workpiece causes necks to form between said beads and said portion of said external surface area.
9. The method of claim 8, wherein the cross-sectional diameter of said necks is smaller than the diameter of said beads .
10. The method of claim 2, wherein said step of heating said workpiece also includes carburizing said workpiece .
11. The method of claim 2, wherein said step of heating said workpiece also includes nitriding said workpiece.
12. The method of claim 2, wherein said step of heating said workpiece also includes annealing said workpiece.
13. The method of claim 2, wherein said step of heating said workpiece also includes normalizing said workpiece.
14. The method of claim 1, wherein said mold is a sand mold.
15. The method of claim 1, wherein said mold is a metal mold.
16. The method of claim 2, further including a step of machining said final preliminary workpiece.
17. The method of claim 2, further comprising shaping said final preliminary workpiece.
18. The method of claim 2, further comprising deforming said metal beads by pressing said metal beads of said -final preliminary workpiece.
19. The method of claim 2, further comprising coating said final preliminary workpiece.
20. 'The method of claim 16, further comprising coatirg said, final preliminary workpiece aftβr maphining.
21. 'The method of claim 1, further comprising machiη÷Lng said clad compqnent to a specified ghόφe haviηg specified surface charact.er^st cs .
PCT/US2003/013037 2002-05-07 2003-04-28 Method for manufacturing clad components Ceased WO2003095697A1 (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
EP03728559A EP1501958A4 (en) 2002-05-07 2003-04-28 Method for manufacturing clad components
JP2004503685A JP4409425B2 (en) 2002-05-07 2003-04-28 Clad component manufacturing method
AU2003234247A AU2003234247A1 (en) 2002-05-07 2003-04-28 Method for manufacturing clad components

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US10/140,239 US7066235B2 (en) 2002-05-07 2002-05-07 Method for manufacturing clad components
US10/140,239 2002-05-07

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WO2003095697A1 true WO2003095697A1 (en) 2003-11-20

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EP (1) EP1501958A4 (en)
JP (1) JP4409425B2 (en)
AU (1) AU2003234247A1 (en)
WO (1) WO2003095697A1 (en)

Families Citing this family (60)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2003095129A1 (en) * 2002-05-13 2003-11-20 Honda Giken Kogyo Kabushiki Kaisha Cast iron internal chill member and method of producing the same
US7937819B2 (en) * 2005-09-19 2011-05-10 GM Global Technology Operations LLC Method of manufacturing a friction damped disc brake rotor
US8163399B2 (en) * 2004-10-08 2012-04-24 GM Global Technology Operations LLC Damped products and methods of making and using the same
US7644750B2 (en) * 2005-09-20 2010-01-12 Gm Global Technology Operations, Inc. Method of casting components with inserts for noise reduction
US8245758B2 (en) * 2006-10-30 2012-08-21 GM Global Technology Operations LLC Coulomb damped disc brake rotor and method of manufacturing
US7775332B2 (en) * 2005-09-15 2010-08-17 Gm Global Technology Operations, Inc. Bi-metal disc brake rotor and method of manufacturing
US7975750B2 (en) * 2004-10-08 2011-07-12 GM Global Technology Operations LLC Coulomb friction damped disc brake rotors
US7594568B2 (en) 2005-11-30 2009-09-29 Gm Global Technology Operations, Inc. Rotor assembly and method
DE102006004769B4 (en) * 2006-02-02 2022-05-25 Mercedes-Benz Group AG Surface conditioning for thermal spray coatings
US9174274B2 (en) 2006-05-25 2015-11-03 GM Global Technology Operations LLC Low mass multi-piece sound dampened article
US8056233B2 (en) 2006-06-27 2011-11-15 GM Global Technology Operations LLC Method of manufacturing an automotive component member
US20090020383A1 (en) * 2006-06-27 2009-01-22 Gm Global Technology Operations, Inc. Damped part
DE102007029307A1 (en) * 2007-06-22 2008-12-24 Daimler Ag Piston for an internal combustion engine and method for its production
US20100122880A1 (en) * 2008-11-17 2010-05-20 Gm Global Technology Operations, Inc. Surface configurations for damping inserts
US7950441B2 (en) * 2007-07-20 2011-05-31 GM Global Technology Operations LLC Method of casting damped part with insert
US8758902B2 (en) * 2007-07-20 2014-06-24 GM Global Technology Operations LLC Damped product with an insert having a layer including graphite thereon and methods of making and using the same
US9534651B2 (en) * 2007-07-20 2017-01-03 GM Global Technology Operations LLC Method of manufacturing a damped part
US9527132B2 (en) 2007-07-20 2016-12-27 GM Global Technology Operations LLC Damped part with insert
US7938378B2 (en) * 2007-08-01 2011-05-10 GM Global Technology Operations LLC Damped product with insert and method of making the same
US7823763B2 (en) 2007-08-01 2010-11-02 Gm Global Technology Operations, Inc. Friction welding method and products made using the same
US20090035598A1 (en) * 2007-08-03 2009-02-05 Gm Global Technology Operations, Inc. Product with metallic foam and method of manufacturing the same
EP2022951A1 (en) * 2007-08-08 2009-02-11 Siemens Aktiengesellschaft Method for manufacturing a turbine casing and turbine casing
US8118079B2 (en) * 2007-08-17 2012-02-21 GM Global Technology Operations LLC Casting noise-damped, vented brake rotors with embedded inserts
US8020300B2 (en) 2007-08-31 2011-09-20 GM Global Technology Operations LLC Cast-in-place torsion joint
US8210232B2 (en) 2007-09-20 2012-07-03 GM Global Technology Operations LLC Lightweight brake rotor and components with composite materials
US7836938B2 (en) * 2007-09-24 2010-11-23 Gm Global Technology Operations, Inc. Insert with tabs and damped products and methods of making the same
US8028739B2 (en) 2007-10-29 2011-10-04 GM Global Technology Operations LLC Inserts with holes for damped products and methods of making and using the same
US8091609B2 (en) * 2008-01-04 2012-01-10 GM Global Technology Operations LLC Method of forming casting with frictional damping insert
US8104162B2 (en) 2008-04-18 2012-01-31 GM Global Technology Operations LLC Insert with filler to dampen vibrating components
US8960382B2 (en) 2008-04-18 2015-02-24 GM Global Technology Operations LLC Chamber with filler material to dampen vibrating components
US20090260931A1 (en) * 2008-04-18 2009-10-22 Gm Global Technology Operations, Inc. Filler material to dampen vibrating components
US9163682B2 (en) * 2008-07-24 2015-10-20 GM Global Technology Operations LLC Friction damped brake drum
US8006740B2 (en) * 2008-10-08 2011-08-30 Synergen, Inc High performance brake rotor
US9500242B2 (en) * 2008-12-05 2016-11-22 GM Global Technology Operations LLC Component with inlay for damping vibrations
US8534344B2 (en) * 2009-03-31 2013-09-17 Alcoa Inc. System and method of producing multi-layered alloy products
US9127734B2 (en) * 2009-04-08 2015-09-08 GM Global Technology Operations LLC Brake rotor with intermediate portion
US20100276236A1 (en) * 2009-05-01 2010-11-04 Gm Global Technology Operations, Inc. Damped product and method of making the same
US20100282550A1 (en) * 2009-05-07 2010-11-11 Gm Global Technology Operations, Inc. Mode altering insert for vibration reduction in components
US20100294063A1 (en) * 2009-05-22 2010-11-25 Gm Global Technology Operations, Inc. Friction damped gears
US8408369B2 (en) * 2009-09-08 2013-04-02 GM Global Technology Operations LLC Bimetallic brake rotor
US9103358B2 (en) * 2010-03-16 2015-08-11 Eaton Corporation Corrosion-resistant position measurement system and method of forming same
JP5572847B2 (en) * 2010-03-17 2014-08-20 株式会社Moresco Cylinder liner and manufacturing method thereof
US8714232B2 (en) 2010-09-20 2014-05-06 GM Global Technology Operations LLC Method of making a brake component
DE102011012320B4 (en) * 2011-02-25 2015-05-28 Daimler Ag Method for producing a brake disk
US8992696B2 (en) * 2011-05-23 2015-03-31 GM Global Technology Operations LLC Method of bonding a metal to a substrate
US8889226B2 (en) * 2011-05-23 2014-11-18 GM Global Technology Operations LLC Method of bonding a metal to a substrate
US9038271B2 (en) * 2012-04-18 2015-05-26 Xiaodi Huang High thermal conductivity disk brakes
US9776241B2 (en) 2012-04-18 2017-10-03 Xiaodi Huang High thermal conductivity disk brakes
US8800526B2 (en) 2012-12-21 2014-08-12 Caterpillar, Inc. Instrumented piston for an internal combustion engine
CN103354210B (en) * 2013-06-27 2016-08-10 清华大学 A kind of bonding method and use the bonding structure that this bonding method formed
WO2015157846A1 (en) * 2014-04-15 2015-10-22 Changize Sadr Structural assembly and method
DE102015016259B4 (en) 2015-12-15 2018-09-06 INPRO Innovationsgesellschaft für fortgeschrittene Produktionssysteme in der Fahrzeugindustrie mbH Method for producing a plastic-metal hybrid component
DE102016225934A1 (en) * 2016-12-22 2018-06-28 Bayerische Motoren Werke Aktiengesellschaft Die-cast component
CN108580852B (en) * 2018-05-14 2020-04-24 重庆大学 Method for enhancing AlFe composite casting bonding interface by lattice material
CN108620561B (en) * 2018-05-14 2020-04-24 重庆大学 Method for strengthening bonding interface of MgFe composite casting
US11898808B2 (en) 2019-04-18 2024-02-13 Apple Inc. Support plate thin cladding
US20200332400A1 (en) * 2019-04-18 2020-10-22 Apple Inc. Optimized weld strength for dissimilar materials
DE102021208965A1 (en) * 2021-08-16 2023-02-16 HPL Technologies GmbH Workpiece for coating with a finishing layer, and a calibration method for a workpiece
CN115158997B (en) * 2022-07-16 2023-09-12 西安强盛耐磨机械有限公司 Double-metal liquid composite casting spiral auger and manufacturing method thereof
USD1121575S1 (en) 2022-07-29 2026-04-07 Uusi, Llc Fluid heating thermal transfer extrusion

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5207776A (en) * 1991-10-04 1993-05-04 The Babcock & Wilcox Company Bi-metallic extrusion billet preforms and method and apparatus for producing same

Family Cites Families (31)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1960042A (en) * 1930-06-18 1934-05-22 Smith Corp A O Securing protective covering to metallic surfaces
US3112541A (en) * 1960-09-23 1963-12-03 Gen Motors Corp Method of making a composite article
US4023613A (en) * 1971-12-29 1977-05-17 Toyo Kogyo Co., Ltd. Method of making a composite metal casting
US3920360A (en) * 1974-05-30 1975-11-18 Gen Motors Corp Aluminum-iron composite rotor housing for a rotary combustion engine and method of making the same
JPS52138017A (en) * 1976-05-14 1977-11-17 Taiho Kogyo Co Ltd Compound material of aluminium group casting base and ferrous group annexation and its production method
SE431723B (en) * 1980-06-23 1984-02-27 Sandvik Ab WELDABLE Wear Part with High Durability
US4807728A (en) * 1986-03-20 1989-02-28 Hitachi Metals, Ltd. Brake member and method of manufacturing same
US4854496A (en) * 1987-01-16 1989-08-08 Dynamet, Inc. Porous metal coated implant and method for producing same
US5226469A (en) * 1987-07-01 1993-07-13 Kawasaki Jukogyo Kabushiki Kaisha Composite structures and methods of manufacturing the same
ATE91326T1 (en) * 1990-02-14 1993-07-15 Jurid Werke Gmbh FRICTION LINING FOR DISC BRAKES, PARTICULARLY FOR ROAD VEHICLES AND RAIL VEHICLES.
US5190091A (en) * 1990-08-08 1993-03-02 Deere & Company Method of impregnation of aluminum alloy with a wear-resistant material
JPH04293705A (en) * 1991-03-20 1992-10-19 Akebono Brake Res & Dev Center Ltd Production of disk rotor of aluminum-based composite material
US5224572A (en) * 1991-07-29 1993-07-06 Smolen Jr George W Lightweight brake rotor with a thin, heat resistant ceramic coating
US5620042A (en) * 1993-06-30 1997-04-15 Kelsey-Hayes Company Method of casting a composite disc brake rotor
US6295716B1 (en) * 1994-10-28 2001-10-02 American Superconductor Corporation Production and processing of (Bi,Pb) SCCO superconductors
US5884388A (en) * 1995-05-12 1999-03-23 Aluminum Company Of America Method for manufacturing a friction-wear aluminum part
JPH0942339A (en) 1995-08-04 1997-02-10 Asahi Chem Ind Co Ltd Brake disc consisting of composite metal layers
DE19545025A1 (en) * 1995-12-02 1997-06-05 Abb Research Ltd Method for applying a metallic adhesive layer for ceramic thermal insulation layers on metallic components
US5862892A (en) * 1996-04-16 1999-01-26 Hayes Lemmerz International Inc. Composite rotor for caliper disc brakes
DE19626175C2 (en) * 1996-06-29 2000-01-13 Honsel Ag Method and device for producing a brake drum or a brake disc
DE19649919C2 (en) * 1996-12-02 1999-05-06 Actech Gmbh Adv Casting Tech Brake members made of composite casting, namely brake drum, brake disc or the like, and composite casting method for the production of brake members
US6216826B1 (en) * 1999-01-19 2001-04-17 Michael John Botzet Bank hoist braking apparatus
US6136374A (en) * 1999-10-14 2000-10-24 Reuscher; Craig J. Method and apparatus for coating vented brake rotors
JP4627346B2 (en) * 2000-03-31 2011-02-09 本田技研工業株式会社 brake disc
DE20011435U1 (en) * 2000-07-05 2000-11-30 Honeywell Bremsbelag GmbH, 21509 Glinde Friction lining for disc brakes, especially for road and rail vehicles
US6357557B1 (en) * 2000-12-20 2002-03-19 Kelsey-Hayes Company Vehicle wheel hub and brake rotor and method for producing same
DE10117127B4 (en) * 2001-04-06 2009-12-31 Alstom Technology Ltd. Composite construction between metallic and non-metallic materials
DE10117128A1 (en) * 2001-04-06 2002-10-10 Alstom Switzerland Ltd Process for the production of composite structures between metallic and non-metallic materials
EP1275748A3 (en) * 2001-07-13 2004-01-07 ALSTOM (Switzerland) Ltd High temperature resistant coating with locally embedded protrusions and its application process
WO2003095129A1 (en) * 2002-05-13 2003-11-20 Honda Giken Kogyo Kabushiki Kaisha Cast iron internal chill member and method of producing the same
US20040178029A1 (en) * 2003-03-13 2004-09-16 J. L. French Automotive Castings, Inc. Lightweight brake rotor with cooling passageways

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5207776A (en) * 1991-10-04 1993-05-04 The Babcock & Wilcox Company Bi-metallic extrusion billet preforms and method and apparatus for producing same

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP1501958A4 *

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US20060246701A1 (en) 2006-11-02
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US7066235B2 (en) 2006-06-27
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