US3401736A - Process for formation of non-abrasive refractory rubbing surface having high thermal conductivity by casting - Google Patents

Process for formation of non-abrasive refractory rubbing surface having high thermal conductivity by casting Download PDF

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Publication number
US3401736A
US3401736A US370282A US37028264A US3401736A US 3401736 A US3401736 A US 3401736A US 370282 A US370282 A US 370282A US 37028264 A US37028264 A US 37028264A US 3401736 A US3401736 A US 3401736A
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Prior art keywords
layer
core
metal
casting
abrasive
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Expired - Lifetime
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US370282A
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English (en)
Inventor
Imagawa Tameichi
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Bridgestone Cycle Co Ltd
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Bridgestone Cycle Co Ltd
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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D65/00—Parts or details
    • F16D65/02—Braking members; Mounting thereof
    • F16D65/10—Drums for externally- or internally-engaging brakes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00—Casting in, on, or around objects which form part of the product
    • B22D19/0009—Cylinders, pistons
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06—Metallic material
    • C23C4/067—Metallic material containing free particles of non-metal elements, e.g. carbon, silicon, boron, phosphorus or arsenic
    • C—CHEMISTRY; METALLURGY
    • C23—COATING 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
    • C23C—COATING 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
    • C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/18—After-treatment
    • C23C4/185—Separation of the coating from the substrate
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
    • F16D69/02—Composition of linings ; Methods of manufacturing
    • F16D69/027—Compositions based on metals or inorganic oxides
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D65/00—Parts or details
    • F16D65/02—Braking members; Mounting thereof
    • F16D2065/13—Parts or details of discs or drums
    • F16D2065/1304—Structure
    • F16D2065/132—Structure layered

Definitions

  • TAMEICHI IMAGAWA 60 260 3'00 4'00 560 oo W l I j ,7 TEMPERATURE 0 a-z/wh ETTORNEYS United States Patent 3,401,736 PROCESS FOR FORMATION OF NON-ABRASIVE REFRACTORY RUBBING SURFACE HAVING HIGH THERMAL CONDUCTIVITY BY CASTING Tameichi Imagawa, Omiya, Japan, assignor to Bridgestone Cycle Industry Company Limited, Tokyo, Japan, a corporation of Japan Filed May 26, 1964, Ser. No. 370,282 Claims priority, application Japan, Aug. 27, 1963, 38/45,124; Oct. 22, 1063, 38/56,623 5 Claims. (Cl.
  • a method of coatinga metal article having a layer of non-abrasive heat-resistant metal on a body of high thermal conductivity metal comprises spraying a first porous layer of a lower melting point metal on a sand core, spraying a second porous layer of higher melting point non-abrasive heat-resistant metal on the first layer, positioning the core in a casting mold, and pouring molten high thermal conductivity metal into the mold and over the core, the porosity of said layers permitting venting of entrapped air and gases therethrough and providing a good bond between the body and the layers.
  • the first layer may be removed to expose the layer of non-abrasive heat-resistant metal.
  • This invention relates to a process for the formation of a non-abrasive and heat-resistant metal layer on a body formed of a substance having refractory surface having high thermal conductivity which is applicable to frictional surfaces of relatively moving machine parts, such, for instance, as those of a high speed brake hub drum of vehicles or cylinder and piston of internal combustion engines.
  • the general object of the invention is to provide an improved process of forming a non-abrasive and heat resistant surface on a high thermal conductivity body of the relatively moving machine parts by casting.
  • a further object of the invention is to provide a very strong core capable of enduring rough handling and heat shock.
  • the inside surface of a machine part such as a cylinder of an internal combustion engine, in particular, an aluminum cylinder of an automobile or frictional surface of a brake evolving an extremely large amount of heat when exposed to a high temperature condition, such as damping hub drum must have a good heat resistance as well as a good thermal conductivity, otherwise, heat of friction is accumulated to cause over-heating, which results in an accident such as abrasion sticking of the frictional surface.
  • a light metal having a high thermal conductivity such as aluminum or aluminum alloy
  • a base material for the machine parts by casting using a core prepared from synthetic resin-coated casting sands for shell holding.
  • a non-abrasive and heat resistant metal layer is formed initially on the outer surface of the said core by spraying, and then the coated core is set in a casting mold and a melt of the above mentioned base material is poured in the mold and bonded to the non-abrasive and heat resistant metal layer, and the latter is transferred to the surface of the article made of the base metal.
  • a low melting point metal or alloy such Patented Sept. 17, 1968 ice as zinc aluminum, or an alloy thereof is applied as a 1st layer on the outer surface of the said core by metal spraying process, that is, by an electrically heated molten metal spraying process, and a non-abrasive and heat resistant metal which forms the frictional surface of the article is, as a 2nd layer, applied on the 1st layer by a molten metal spraying process by utilizing the fine irregularities of the surface of the 1st layer as holding means.
  • the thermal shock applied to the core is very low since the melt spray of the lower melting point metal has a small heat capacity so that the damage and the thermal deformation of the core can be positively prevented without necessity of great skill and large care as in the case of the direct spraying of the nonabrasive and heat resistant metal layer.
  • the core is reinforced such that it can sufliciently stand heat stress caused by the thermal shock at the spraying of metal for the 2nd layer and local heating by the metal spray, whereby the core is mechanically protected against rough handling which frequently happens in mass production, and the surface state of the 1st layer is an extremely effective layer of fine particles for welding of the 2nd layer by spraying, therefore, a desired metal can be coated as the 2nd layer easily with a uniform thickness and non-abrasive and heat resistant metal and wear resisting layer can be easily formed.
  • a 3rd layer of aluminum is, if necessary, formed by the molten metal spray on the 2nd layer on the surface of the treated core andthe core is then set in a casting mold. Then, a molten metal having high thermal conductivity such as aluminum or an aluminum alloy is poured in the mold and as the 2nd layer and the 3rd layer also have porous surface structures consisting of fine particles of spray metal, the poured base metal is very firmly adhered to the 3rd layer, the boundary layer forms an uneven structure and the combining surface areas are enlarged, which results in'increasing the thermal conductivity between layers. Also, since the surface of the core is only covered by the metal spray layers, gases can be easily vented in case of casting through the porous layers.
  • the layer fused onto the outer surface of the core is formed on the surface of the cast product and byremoving the 1st layer having a low melting point from thus obtained surface, the 2nd layer of the non-abrasive and heat resistant metal layer can be obtained for use as a non-abrasive surface.
  • FIG. 1 shows a cross-sectional view of ⁇ a core for casting light metal cylinder of an internal combustion engine by the method of the invention
  • FIG. 2 is a partial sectional view of for use in automobiles
  • FIG. 3 shows a microscopic structure of non-abrasive and heat resistant metal layer
  • FIG. 4 is a characteristic diagram wherein the hub drum according to the invention is compared with a conventional hub drum and shows that the decrease of hardness accompanied by the temperature rise of hub drum and a high performance can be expected over a wide temperature range.
  • reference numeral 1 represents a baked core prepared from synthetic resin-located casting sands for shell molding by a conventional means.
  • the core 1 has a substantial strength but is liable to be damaged if violently handled and is deformed if it is subject to a sudden thermal shock locally.
  • a low melting point metal or alloy such as zinc, aluminum or an alloy thereof is a brake hub drum applied on the outer surface of the core 1 by a metal spraying process, to form the 1st layer 2.
  • the core 1 is reinforced by the 1st layer 2 and its strength is increased,
  • compositions of aluminum alloys suitable as the base material of the cylinder are shown in Table 2.
  • the 1st layer 2 of a low melting point alloy or metal is ⁇ natal s uch as Wear reslsung steel or wear reslstmg alloy first formed on the outer surface of the core 1 by molten 1s apphed on the outer surface of the layer 2 by metal spraying process and then the 2nd layer 3 of a P Spray to form a layer
  • a sultalilefomposr non-abrasive and heat resistant material is formed on the tion of steel as the material for the 2nd layer 15 illustrated Surface of the 1st layer 2 the damage and the deforma Table tion of the core by external force, thermal shock 'and TABLE 1 heat stress caused by the melt spray of the 2nd layer 3 Percent can be extremely reduced, which makes the mass produc- C tion of such a kind of casting operation possible and Mn Q70 increases largely the production efiiciency.
  • the pres- P O'04 ence of the 1st layer 2 particularly facilitates the forma- S tion of the non-abrasive and heat resistant metal layer Fe 98'42 as the 2nd layer 3 on the surface of [the core 1 and
  • the thi k e of th 2 d layer 3 i 1 1,5 protects the core 1 from damage during the pouring time I thi case, lag th 2 d l e 3 i thoroughly i t of a molten metal thereon.
  • the second layer 2 may have sufficient thickness and can a layer is strongly joined With the poured base metal, heat be well adhe ed to the latt d as h h t f lt is effectively transferred from the 2nd layer 3 to the base metal spray is not directly applied to the core 1 by the material through the intimately combined portion and the presence of the 1st layer 2 having a high thermal conheat is p i iv ly r dia ed.
  • FIG' 2 designates a hub drum made tively applied to the case of casting a core having 3, Of aluminum or its alloy Shown in partial section, 9 iS its complicated shape as the core is sufficiently reinforced.
  • Tim P 10 a flange, 11 is the Surface layer of a high Further, if necessary, a lilght met l r a light alloy may heat resistant and non-abrasive material coated to the be a lied o th o ter rfa of th 2 d layer 3 b a inner peripheral surface of the rim 9, and 12 is an intermelt spray process t f r 3 d layer 4, mediate layer of base material aluminum, that is, which The thickness of the 3rd layer 4 may be about 0.5-1.0 firmly bonds alloy-like the Surface layer 11 to said Tim mm.
  • base metal- 13 represents a brake $1106, metal with the base material but in the case of applying 14 a brake lininga heat-treatment as after-treatment to diffuse the base
  • a brake lininga heat-treatment as after-treatment to diffuse the base
  • plete fusing or combination can be obtained by further applying the heat-treatment in the case of forming the 3rd layer 4 also.
  • the core 1 having thus sprayed layers is set in a casting mold for making a cylinder and a melt 'of base metal is poured in the mold to cast the cylinder body containing the 2nd layer 3 and the 3rd layer 4.
  • the outer sprayed layer 5 of the core 1 has the fine porous uneven surface, the poured base material is interconnected with the sprayed layer at the boundary and is combined strongly thereto.
  • the heat resistant and nonabrasive material as mentioned in Table 3 is sprayed to a thickness of 0.5 to 1 mm. on the surface of the shell molding core, which forms the inner periphery of the rim 9, to form the surface layer 11 (FIGS. 2 and 3) and an intermediate layer 12 of aluminum is sprayed thereon, the core is then put in a casting mold, a melt of an alloy of base material as exemplified in Table 4 is cast by a diecasting or conventional casting process and the coated layers on the core surface are cast together in the molten base metal or alloy.
  • the intermediate layer 12 of aluminum serves as a binder which fuses and firmly bonds the base material 16 and the surface layer 11 and fills the fine gaps between the coating particles of surface layer 11 to adhere perfectly.
  • the friction heat when produced is transmitted immediately to the base material 16 to produce no substantial temperature difference between both layers and the thermal expansion of the surface layer 11 is substantially equal to that of the base material 16.
  • the friction heat generated on sliding contact surface of hub drum is thus immediately dissipated without causing any trouble in the thin coated layer and defects as in the previous method owing to the accumulation of heat would never occur.
  • the surface layer 11 which forms a brake sliding contact surface, appears, the surface layer requires only a direct grinding processing without special machining operation and thus a hub drum of high performance can be produced without the increase in operating steps.
  • said lower melting point metal is selected from the group consisting of zinc, aluminum and an alloy thereof.
  • the method for forming a non-abrasive and heat resistant surface on a surface of a body cast from material having high thermal conductivity comprising the steps of forming a core from casting sand containing a synthetic resin binder to the desired shape and size and to define the surface of said body cast over said core, coating at least said surface defining portion of said core by spraying thereon a lower melting point metal in the form of molten particles prior to and followed by coating said sprayed surface with a porous layer of non-abrasive and heat resistant higher melting point metal by spraying said metal thereon in the form of molten particles, positioning said core in a casting mold, pouring molten metal having a high thermal conductivity into said mold and over said core to cast said body, and during casting to vent entrapped air and gases through said porous layer to permit said poured metal to penetrate into the interstices of said porous layer and to bond said metal of high thermal conductivity to said porous layer by said penetration, and separating said core from said cast body and leaving said cast body

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Plasma & Fusion (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Inorganic Chemistry (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Braking Arrangements (AREA)
US370282A 1963-08-27 1964-05-26 Process for formation of non-abrasive refractory rubbing surface having high thermal conductivity by casting Expired - Lifetime US3401736A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP4512463 1963-08-27
JP5662363 1963-10-22

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US (1) US3401736A (de)
AT (1) AT271763B (de)
BE (1) BE652385A (de)
CH (1) CH449374A (de)
DE (1) DE1285680B (de)
FR (1) FR1398301A (de)
GB (1) GB1061573A (de)
NL (2) NL6408903A (de)
SE (1) SE313402B (de)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3648757A (en) * 1970-01-19 1972-03-14 Harold E Willingham Method of making centrifugal casting mold
US3692087A (en) * 1969-03-17 1972-09-19 Norton Co Metallic porous plates
US3797556A (en) * 1972-10-18 1974-03-19 T Imagawa Methods of producing accurate bore surfaces
US3797101A (en) * 1972-11-27 1974-03-19 Nl Industries Inc Method of making die castings having multi-layer coated surfaces
US3878880A (en) * 1973-06-25 1975-04-22 Curtiss Wright Corp Composite casting method
US3888296A (en) * 1974-05-30 1975-06-10 Gen Motors Corp Method for the manufacture of a composite article
US6044820A (en) * 1995-07-20 2000-04-04 Spx Corporation Method of providing a cylinder bore liner in an internal combustion engine
US20070286961A1 (en) * 2004-10-29 2007-12-13 Knorr-Bremse Systeme Fuer Nutzfahrzeuge Gmbh Wear-resistant brake disc or brake drum and method for producing same
US20100140033A1 (en) * 2008-12-05 2010-06-10 Gm Global Technology Operations, Inc. Component with inlay for damping vibrations

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2639294C2 (de) * 1976-09-01 1982-05-13 Mahle Gmbh, 7000 Stuttgart Gepreßter Aluminiumkolben für Verbrennungsmotoren mit Einlagen aus einem anderen Werkstoff
DE7913595U1 (de) * 1979-05-11 1979-12-20 Aluminium Walzwerke Singen Gmbh, 7700 Singen Bremstrommel fuer trommelbremse von fahrzeugen
JPS60171945U (ja) * 1984-04-24 1985-11-14 日本特殊陶業株式会社 断熱ポ−トライナ−
SE453968B (sv) * 1985-02-01 1988-03-21 Kanthal Ab Gjuten metallkropp och sett att framstella densamma
DE69702988T2 (de) * 1996-10-01 2001-03-01 Hubert Francois Verschleissfester verbundkörper

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB189612552A (en) * 1896-06-08 1897-06-08 Timothy Shepherd Improvements relating to the Jointing of Aluminium and other Tubes, Rods, and the like into Velocipede or other Frames and similar Structures.
US1561287A (en) * 1923-10-20 1925-11-10 Doehler Die Casting Co Method and apparatus for die casting
US2281634A (en) * 1940-05-29 1942-05-05 Otto Stossel Production of spray metal negatives of models
US2390805A (en) * 1943-03-10 1945-12-11 Westinghouse Electric Corp Method of making metallic articles
US2629907A (en) * 1949-04-19 1953-03-03 Us Rubber Co Method of making molds
US2903375A (en) * 1956-08-08 1959-09-08 Renault Method of coating a mould for use in a foundry
CA621055A (en) * 1961-05-30 G. House James Casting metallic inserts in castings of light metal
US3083424A (en) * 1959-05-07 1963-04-02 Nat Lead Co Method for producing coated die castings
US3099869A (en) * 1953-12-02 1963-08-06 Hoover Co Process of bonding metals
US3186678A (en) * 1961-10-19 1965-06-01 Monarch Aluminum Mfg Co Metal casting art

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA621055A (en) * 1961-05-30 G. House James Casting metallic inserts in castings of light metal
GB189612552A (en) * 1896-06-08 1897-06-08 Timothy Shepherd Improvements relating to the Jointing of Aluminium and other Tubes, Rods, and the like into Velocipede or other Frames and similar Structures.
US1561287A (en) * 1923-10-20 1925-11-10 Doehler Die Casting Co Method and apparatus for die casting
US2281634A (en) * 1940-05-29 1942-05-05 Otto Stossel Production of spray metal negatives of models
US2390805A (en) * 1943-03-10 1945-12-11 Westinghouse Electric Corp Method of making metallic articles
US2629907A (en) * 1949-04-19 1953-03-03 Us Rubber Co Method of making molds
US3099869A (en) * 1953-12-02 1963-08-06 Hoover Co Process of bonding metals
US2903375A (en) * 1956-08-08 1959-09-08 Renault Method of coating a mould for use in a foundry
US3083424A (en) * 1959-05-07 1963-04-02 Nat Lead Co Method for producing coated die castings
US3186678A (en) * 1961-10-19 1965-06-01 Monarch Aluminum Mfg Co Metal casting art

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3692087A (en) * 1969-03-17 1972-09-19 Norton Co Metallic porous plates
US3648757A (en) * 1970-01-19 1972-03-14 Harold E Willingham Method of making centrifugal casting mold
US3797556A (en) * 1972-10-18 1974-03-19 T Imagawa Methods of producing accurate bore surfaces
US3797101A (en) * 1972-11-27 1974-03-19 Nl Industries Inc Method of making die castings having multi-layer coated surfaces
US3878880A (en) * 1973-06-25 1975-04-22 Curtiss Wright Corp Composite casting method
US3888296A (en) * 1974-05-30 1975-06-10 Gen Motors Corp Method for the manufacture of a composite article
US6044820A (en) * 1995-07-20 2000-04-04 Spx Corporation Method of providing a cylinder bore liner in an internal combustion engine
US20070286961A1 (en) * 2004-10-29 2007-12-13 Knorr-Bremse Systeme Fuer Nutzfahrzeuge Gmbh Wear-resistant brake disc or brake drum and method for producing same
US20100140033A1 (en) * 2008-12-05 2010-06-10 Gm Global Technology Operations, Inc. Component with inlay for damping vibrations
US9500242B2 (en) * 2008-12-05 2016-11-22 GM Global Technology Operations LLC Component with inlay for damping vibrations

Also Published As

Publication number Publication date
NL138822B (nl) 1973-05-15
FR1398301A (fr) 1965-05-07
SE313402B (de) 1969-08-11
AT271763B (de) 1969-06-10
BE652385A (de) 1964-12-16
DE1285680B (de) 1968-12-19
CH449374A (fr) 1967-12-31
NL6408903A (de) 1965-03-01
NL6901144A (de) 1969-04-25
GB1061573A (en) 1967-03-15

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