US20080169077A1 - Method of reinforcing low melting temperature cast metal parts - Google Patents

Method of reinforcing low melting temperature cast metal parts Download PDF

Info

Publication number
US20080169077A1
US20080169077A1 US11/652,305 US65230507A US2008169077A1 US 20080169077 A1 US20080169077 A1 US 20080169077A1 US 65230507 A US65230507 A US 65230507A US 2008169077 A1 US2008169077 A1 US 2008169077A1
Authority
US
United States
Prior art keywords
mold
molten metal
melting temperature
metal material
reinforcing
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.)
Abandoned
Application number
US11/652,305
Other languages
English (en)
Inventor
Yahya Hodjat
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Gates Corp
Original Assignee
Gates Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Gates Corp filed Critical Gates Corp
Priority to US11/652,305 priority Critical patent/US20080169077A1/en
Assigned to GATES CORPORATION, THE reassignment GATES CORPORATION, THE ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: HODJAT, YAHYA
Priority to CNA2008800020313A priority patent/CN101578149A/zh
Priority to PCT/US2008/000027 priority patent/WO2008085820A1/en
Priority to EP08712937A priority patent/EP2111315A1/de
Priority to JP2009545564A priority patent/JP2010515582A/ja
Priority to BRPI0806329-0A priority patent/BRPI0806329A2/pt
Priority to KR1020097015037A priority patent/KR20090095652A/ko
Publication of US20080169077A1 publication Critical patent/US20080169077A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • 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
    • B22D19/16—Casting in, on, or around objects which form part of the product for making compound objects cast of two or more different metals, e.g. for making rolls for rolling mills
    • 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
    • B22D19/14—Casting in, on, or around objects which form part of the product the objects being filamentary or particulate in form
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D21/00—Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D27/00—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
    • B22D27/02—Use of electric or magnetic effects

Definitions

  • the invention relates to a process and a part made using the process, namely, reinforcing low melting temperature cast metal parts using high melting point fibers or powders applied or dispersed to predetermined portions of the mold casting.
  • Aluminum and magnesium alloys are used commonly in manufacturing industrial products. Although there are many uses for these alloys, they cannot be used for high strength and high wear applications except if there are made of two parts joint together, an aluminum core and a case made of a higher strength material, e.g. steel. A good example is aluminum block engines require a steel sleeve. To improve pure metal properties, alloys are made by adding different metals to the base metal and creating intermetalic compositions and phases in the atomic scale. However, for aluminum and magnesium even their alloys do not have sufficient strength and wear resistance for many applications, even though their low densities and relatively low melting points are very attractive features. A known art to strengthen aluminum and magnesium alloys is addition of ceramics to these alloys.
  • Ceramics do not mix with alloys in the atomic scale; rather, they reinforce these alloys in a macro scale.
  • the problem with ceramic added alloys is the fact that they are extremely difficult to machine. And since castings are almost never net-shape, they are only suited for certain applications that do not need finish machining.
  • U.S. Pat. No. 4,586,554 discloses a process is provided for the production of fibre-reinforced light-metal castings by die casting.
  • a fibre moulding is introduced into an auxiliary mould and the auxiliary mould is heated to an optimum temperature above the melting point of the light metal.
  • the auxiliary mould is then inserted with positive fit into a die casting mould corresponding to the outer contour of the auxiliary mould and filled with light metal under pressure.
  • the fibre moulding can optionally be stabilized by means of a temporary organic binder which decomposes when the auxiliary mould is heated.
  • the primary aspect of the invention is to provide a method of reinforcing low melting temperature cast metal parts using high melting point fibers or powders applied or dispersed to predetermined portions of the mold casting.
  • the invention comprises a method of reinforcing a low melting temperature cast metal part comprising preparing a molten metal material having a melting temperature, mixing a reinforcing material having a melting temperature greater than the melting temperature of the molten metal material into the molten metal material, pouring the molten metal material into the mold, applying a force to the reinforcing material causing the reinforcing material to occupy a predetermined portion of the mold and thereby a predetermined portion of the cast metal part, and solidifying the molten metal material.
  • FIG. 1 is a perspective view of a first method.
  • FIG. 2 is a perspective view of a magnetic mold.
  • FIG. 3 is a perspective view of the magnetic mold.
  • FIG. 4 is a perspective view of the finished part.
  • FIG. 5 is a perspective view of the centrifugal mold.
  • FIG. 6 is a perspective view of an armature machine.
  • FIG. 7 is a perspective view of a finished part.
  • FIG. 8 is a side view of a part formed using gravity separation.
  • FIG. 9 is a perspective view showing application of powder or fiber to a mold.
  • FIG. 10 is a perspective view of the mold with poured metal.
  • FIG. 11 is a perspective view of a finished part.
  • FIG. 12 is a perspective view of the magnetic mold with the fibers or powder applied before pouring.
  • FIG. 13 is a perspective view of the filled mold.
  • FIG. 14 is a perspective view of the finished part.
  • FIG. 15 is a perspective view of the two step mold.
  • FIG. 16 is a perspective view of the two step mold with the core removed.
  • FIG. 17 is a perspective view of the two step mold.
  • FIG. 18 is a perspective view of the dam mold.
  • FIG. 19 is a perspective view of the mold with the dam.
  • FIG. 20 is a perspective view of the finished part.
  • the invention provides a method, and a product using the method, for reinforcing for durability and/or strength enhancement of aluminum, magnesium, zinc or tin castings or any other low melting point metal casting using stainless steel fiber or powder or other high melting point alloy fibers and/or powders mixed within the host metal material. It also comprises a method of reinforcing low melting temperature alloys by mixing a reinforcing powder or material into the molten metal, and subsequently separating the fiber/powder from the molten metal by external forces such as magnetism, centrifugal or gravitational.
  • the method comprises use of a metal host alloy into which the reinforcing fibers or powders are added to form a metal matrix mix.
  • the metal matrix mix comprises a mechanically reinforced alloy. When the mix is cast into a product it will have enhanced mechanical strength (for example, tensile, compressive, fatigue, bending, and so on) and higher wear resistance.
  • This process disclosed herein can be used in making high strength, wear resistant aluminum sprockets, without the need of hard chrome plating or ceramic coating.
  • the disclosed process is superior to coatings because coatings generally consist of mechanical or chemical bonds which are not as strong as a part manufactured using the inventive process since there is no need for “bonding” between layers and so the part is essentially one piece.
  • the inventive process comprises use of mechanical or other means of separating or segregating the fiber and/or powder in the molten host metal matrix material in a predetermined manner.
  • This can include use of centripetal force, gravitational force, magnetic force or a static electric charge.
  • concentration of fibers and/or powder in the outer layer (or other desired locations) of a part in the molten stage can be manipulated and increased. This improves the mechanical properties for parts in specific predetermined locations giving higher strength and/or higher wear resistance on the surface or other locations, without increasing the fiber usage in the entire part, thereby reducing the cost and weight.
  • the fibers or powders are not necessarily uniformly distributed through the metal matrix as one might expect in a pure mixing process. Instead, the powders or fibers are selectively concentrated in areas where either durability or strength enhancements are desired. The concentration of the metal fibers and/or powders is performed during the casting process.
  • the metal matrix may comprise aluminum, magnesium, zinc or tin or a combination of two or more of the foregoing.
  • the fibers and powders comprise metal materials having a higher melting point than the metal matrix, including stainless steel, alloy steel, low carbon steel, or other materials that have a very high melting point compared to molten aluminum, magnesium, zinc or tin.
  • the melting point of pure iron is 1537° C.
  • the melting point of pure aluminum is 660° C. and melting point of pure magnesium is 650° C.
  • the melting point of pure zinc is 420° C. and the melting point of pure tin is 232° C.
  • the stainless steel fibers or powder do not melt in the molten metal matrix, rather, an intermetalic boundary layer comprising a combination of iron and the host metal is formed at the fiber or powder interface.
  • the melt is agitated before and sometimes depending on the part design after casting (in-mold agitation) to prevent the fibers or powder from settling down in the host molten metal matrix as the density of iron is about three times as much as the density of aluminum or magnesium.
  • the agitation can be done simply by mechanical means or by magnetic forces. Casting is generally done in closed molds and sometimes under pressure (i.e. in die casting). This helps to better fill the mold.
  • the percentage of fibers, size and shape of fibers, and material composition (alloy) of fibers can vary depending on the required performances of the part.
  • a typical mix will have a fiber or powder content in the range of approximately 5% to 50% by volume, and fiber sizes of approximately one micron to 10 mm long and approximately 1 micron to 1.0 mm (1 to 1000 microns) in cross sectional diameter.
  • the cross section can be any shape, but for simplicity, it has been considered basically round.
  • the range of sizes, although given only as an example, will allow easy die casting of the reinforced alloy.
  • the powder can also vary in the range of approximately one micron to one millimeter size, but is not limited to this range.
  • the size of fibers and powder can be larger both in length and diameter. Choosing powder, fiber, or a combination of both is a matter of achieving the desired properties in the finished part.
  • the percentage of fiber/powder in the selected enriched area of parts can be as high as 95%, but not limited to this amount.
  • the enriched layer applied on the mold in the mold coating process can have some aluminum powder mixed with it to assure that it melts and creates the homogeneous enriched layer after casting.
  • Example fibers include:
  • FIG. 1 is a perspective view of a first method.
  • the mold 20 is preheated and the molten alloy is superheated (hotter than melting point). This allows separation of the stainless steel fiber/powder before the solidification process starts.
  • the superheat applied to the metal matrix material required is approximately 250° C.
  • the poured metal matrix material is then allowed to cool. Once cooled to ambient conditions the cast reinforced part is removed from the mold 20 .
  • selective dispersion of fiber or powder material to predetermined portions of the metal matrix can be achieved using a variety of processes. These include separation processes wherein the fiber or powder is mixed with the host metal matrix alloy, and then moved to a desired location or concentration by use of magnetic force which causes the fiber or powder to move to the desired location(s) in the part.
  • FIG. 2 is a perspective view of a magnetic mold. Mold 20 is surrounded by an electromagnet 22 . Prior to pouring the host metal matrix material 10 is mixed with the reinforcing fiber or powder. The host metal matrix alloy is superheated and the mold 20 preheated to prevent premature solidification of the material 10 . The superheat and preheat are approximately 250° C. above the melting point of the host alloy. The fiber and powder are then migrated to a desired location in the casting by force of electromagnet or permanent magnet 22 .
  • FIG. 3 is a perspective view of the magnetic mold. After the molten metal matrix material is poured into the mold the magnet is turned on. While under the influence of the electromagnetic field the fibers or powder 11 are drawn toward the surface 21 of the mold 20 . This causes the concentration of fibers or powder to significantly increase in the outer regions of the part, for example, at an outer wear (tooth) surface where a belt would engage the sprocket.
  • FIG. 4 is a perspective view of the finished part. Fibers 11 are concentrated at an outer region of the part at the teeth 102 where enhanced strength and wear characteristics afforded by the fibers are desired. Where the enhanced wear and strength are not required, only the non-reinforce metal material 101 is present.
  • FIG. 12 is a perspective view of the magnetic mold with the fibers or powder applied before pouring.
  • the electromagnet 22 is turned on. Fibers or powder 11 are then sprayed on the mold 20 to the desired depth and concentration. The electromagnetic force aligns and holds the fibers or powder in the desired position in the mold.
  • the host alloy is then poured into the mold 20 . The host alloy flows around the fibers held in place by the electromagnet.
  • a static charge is applied to the mold 20 .
  • the static charge then holds the fibers or powder in place on the mold until the host alloy is poured and solidifies.
  • mold 20 is made of a conductive metal material.
  • FIG. 13 is a perspective view of the filled mold. In this alternate process there are no fibers or powder mixed into the host alloy 101 , the fibers are only combined with the molten metal once in the mold.
  • FIG. 14 is a perspective view of the finished part.
  • the reinforced portion 110 is disposed at the outer region of the part where the desired enhanced wear and strength is required.
  • FIG. 5 is a perspective view of the centrifugal mold.
  • Metal matrix material 10 containing fibers or powder are heated to a molten state and poured into a mold 10 . Again, during the process the host metal matrix alloy must be superheated and the mold preheated to prevent premature solidification.
  • a cover 23 is attached using fasteners 24 or clamps.
  • the assembly is then attached to an armature 30 .
  • FIG. 6 is a perspective view of an armature machine. The assembly is rotated at a speed sufficient to cause the fibers and/or powder to be moved radially outward to the outer region of the part. To achieve uniform separation around the part the speed is ramped up from one RPM to approximately 3000 RPM over a period of approximately 30 seconds and then kept at the top speed until the part solidifies.
  • FIG. 7 is a perspective view of a finished part.
  • the reinforcing material 11 is disposed in the area of the teeth 102 thereby enhancing the strength and durability of the part.
  • Non-reinforced material 101 is radially inwardly displaced by the radially outward movement of the reinforcing material.
  • FIG. 8 is a side view of a part formed using gravity separation.
  • a mixture of metal matrix material is prepared with the desired concentration of fibers or powder.
  • the host metal matrix material is superheated and the mold preheated to prevent premature solidification.
  • the denser powder or fibers 11 sink toward the bottom of the mold, thereby reinforcing the metal matrix material accordingly.
  • Non-reinforced or less densely reinforced material 101 develops as the fibers or powders sink in the mold through the molten metal.
  • Gravity separation cannot be used for symmetrical parts that require uniform strengthening on all sides, such as sprockets. It is suitable for applications such as pistons and shafts where one end requires higher wear resistance or higher strength.
  • the fiber or powder is placed in a mold using different means and then the host metal alloy is poured in the mold. This can be achieved by covering the mold with the powder and/or fiber and pouring the molten metal into the mold. The molten metal material will penetrate the fiber or powder coating, thereby enriching only on the surface of the finished part.
  • FIG. 9 is a perspective view showing application of powder or fiber to a mold.
  • Covering or coating of the mold 20 surface with the powder or fiber 11 can be accomplished by spraying, brushing, or any other suitable method using for example, a spray gun SP.
  • powder and fiber 11 can be mixed with a liquid suspension material such as water, solvents, or any suitably tacky material to make the fibers or powder temporarily adhere to the mold surface until the molten metal is poured.
  • the tacky material should be of a type that burns off easily with little or no gases generated when contacted by molten metal. Any fumes from the suspension and adhesive are vented from the mold.
  • the molten metal fills the porosity/cavity of the fiber or powder material on the mold surface to create a layer of very high concentration of durable material intermixed with host metal material on the part surface. It is important to note that for this method the alloy is not premixed with fibers or powder. It is only during casting that the alloy mixes with the fibers or powder already applied to the mold surface.
  • FIG. 10 is a perspective view of the mold with poured metal. Fibers or powder 11 are present at the mold surface. The poured metal material 101 (without fibers or powder) mixes among the fibers or powder and then cools in the mold.
  • FIG. 11 is a perspective view of a finished part.
  • Enriched metal matrix material 110 is present on the outer surface of the part.
  • Non-reinforced material 101 is present in the interior of the part. In this embodiment only the wear surface of the part is reinforced without the need to reinforce the entire part.
  • static electricity may be used to hold the sprayed powder or fiber on the mold surface.
  • the fiber or powder is charged in a manner known in the art and the mold is given a charge opposite that of the powder/fiber so the powder or fiber adheres to the mold surface as it is sprayed in.
  • FIG. 15 is a perspective view of the two step mold.
  • the mold comprises a mold 20 and a core 25 . Disposed between mold 20 and core 25 is a cavity 200 . Cavity 200 is where the highly reinforced metal matrix material is poured. Core 200 serves as a means of restricting the reinforced material to the portion of the finished part as needed.
  • reinforced metal matrix material containing fibers and/or powder is mixed. The mixed material is then superheated and poured into cavity 200 and allowed to cool, thereby forming reinforced layer 201 . Once cooled core 25 is removed.
  • FIG. 16 is a perspective view of the two step mold with the core removed. Layer 201 has solidified.
  • FIG. 17 is a perspective view of the two step mold. Superheated and non-reinforced alloy 101 is then poured into the volume created by the withdrawn core 25 and allowed to cool.
  • the second casting is performed at a higher temperature than a “normal” casting operation, that is the material for the second casting is super heated.
  • the super heating will be anywhere from 100 to 250 degrees Celsius above the melting point of the cast material.
  • the method comprises using the core wherein the bulk of the mold volume is closed to the flow of the molten metal during the first casting leaving only a relatively narrow layer 201 open at the desired finished part surfaces, in most cases these are usually outer surfaces.
  • the molten metal matrix material is poured into the mold, with a very high concentration of powder already in it.
  • concentration can be in the range of up to approximately 95% powder or fiber, or a combination of both, to approximately 5% alloy.
  • the core is removed and a non-reinforced, that is not containing fibers or powder, host metal alloy is poured in the cavity formerly occupied by the now removed core.
  • the second pour In order for the second pour to weld completely to the solidified high fiber/powder content outer layer, it is super heated to cause it to partially melt the surface of the first pour layer and thereby solidify the two pours together.
  • FIG. 18 is a perspective view of the dam mold.
  • the mold comprises an outer portion 301 and an inner portion 302 . Disposed between the inner and outer portion is a cavity 300 .
  • non-reinforced metal material 101 is poured into the cavity 300 and allowed to cool forming a dam 150 .
  • FIG. 19 is a perspective view of the mold with the dam. Dam 150 is placed within mold 20 . Dam 150 is advantageously sized to create a cavity 200 and cavity 202 .
  • FIG. 20 is a perspective view of the finished part. Dam 150 is completely subsumed into the reinforced material 201 and the non-reinforced material 101 .
  • parts with a heavy concentration of powder and/or fiber in a surface layer can be forged, spun, or worked mechanically with known metal working methods to compact the powder and/or fiber area further.
  • the reinforced fiber/powder layer can be briefly exposed to very high temperatures (1100° to 1250° Celsius) to sinter the fiber and/or powder particles together.
  • very high temperatures (1100° to 1250° Celsius)
  • the low melt temperature host metal material core cannot be exposed to the high sintering temperature, thus induction heating is an acceptable method to heat the outer layer rapidly.
  • the reinforced layer which is in the range of approximately 70% to 95% fiber and/or powder material with the reminder being host metal material will see a rapid sintering of the fiber and/or powder particles. Most of the host alloy in the reinforced layer (approximately 25% to 5% remainder) which is disposed in the interstitial cavities/porosities between the fiber and/or powder particles will melt and solidify rapidly.
  • a slight amount of the trapped host metal material may sweat out of the part in this stage without any problems.
  • the general categories described in this specification namely, mold coating and separation of the fiber/powder from the molten metal matrix, can also be combined to achieve higher concentrations of fiber/powder in the desired areas if needed.
  • the reinforcing process described herein does not have to be only applied symmetrically to a part, it can be localized on a specific portion of a part as well.
  • localized reinforcement or strengthening can be performed on shafts or other parts that have a limited area that needs to be stronger or have more wear resistance, but not otherwise required on the entire part. For instance where a particular area of a shaft is in oscillating contact with another part and as a result requires enhanced wear resistance.
  • a non symmetrical version is shown for only one process, namely, magnetic coating, localized reinforcement can be used for all of the processes explained in this specification.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
US11/652,305 2007-01-11 2007-01-11 Method of reinforcing low melting temperature cast metal parts Abandoned US20080169077A1 (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
US11/652,305 US20080169077A1 (en) 2007-01-11 2007-01-11 Method of reinforcing low melting temperature cast metal parts
CNA2008800020313A CN101578149A (zh) 2007-01-11 2008-01-03 强化低熔点铸造金属部件的方法
PCT/US2008/000027 WO2008085820A1 (en) 2007-01-11 2008-01-03 Method of reinforcing low melting temperature cast metal parts
EP08712937A EP2111315A1 (de) 2007-01-11 2008-01-03 Verfahren zur verstärkung von gussmetallteilen mit niedriger schmelztemperatur
JP2009545564A JP2010515582A (ja) 2007-01-11 2008-01-03 低融点鋳造金属を強化する方法
BRPI0806329-0A BRPI0806329A2 (pt) 2007-01-11 2008-01-03 método de reforço de partes metálicas fundidas a baixa temperatura de fusão
KR1020097015037A KR20090095652A (ko) 2007-01-11 2008-01-03 저융점 주조 금속 부품의 보강 방법

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/652,305 US20080169077A1 (en) 2007-01-11 2007-01-11 Method of reinforcing low melting temperature cast metal parts

Publications (1)

Publication Number Publication Date
US20080169077A1 true US20080169077A1 (en) 2008-07-17

Family

ID=39313140

Family Applications (1)

Application Number Title Priority Date Filing Date
US11/652,305 Abandoned US20080169077A1 (en) 2007-01-11 2007-01-11 Method of reinforcing low melting temperature cast metal parts

Country Status (7)

Country Link
US (1) US20080169077A1 (de)
EP (1) EP2111315A1 (de)
JP (1) JP2010515582A (de)
KR (1) KR20090095652A (de)
CN (1) CN101578149A (de)
BR (1) BRPI0806329A2 (de)
WO (1) WO2008085820A1 (de)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130266470A1 (en) * 2010-11-25 2013-10-10 Rolls Royce Deutschland Ltd & Co Kg Method for the manufacturing high-temperature resistant engine components
CN113664185A (zh) * 2021-07-06 2021-11-19 惠州学院 一种采用电磁铸造制备铝合金双金属复合材料的制备方法

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103111601B (zh) * 2012-10-15 2015-02-25 柳州市双铠工业技术有限公司 复合耐磨衬板制造工艺方法
CN103111600B (zh) * 2012-10-15 2015-05-20 柳州市双铠工业技术有限公司 复合耐磨管道制造工艺方法
CN103084564B (zh) * 2012-10-15 2015-02-25 柳州市双铠工业技术有限公司 复合耐磨件制造工艺方法
CN109746420B (zh) * 2019-03-15 2024-02-02 河北欧瑞特铝合金有限公司 镶铸在铝合金零件的钢套及铝合金零件内镶铸钢套的工艺
CN110666138B (zh) * 2019-10-28 2023-10-20 吉林大学 一种高耐磨活塞制备装置及方法

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6250364B1 (en) * 1998-12-29 2001-06-26 International Business Machines Corporation Semi-solid processing to form disk drive components

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5319926A (en) * 1976-08-09 1978-02-23 Toshiba Machine Co Ltd Method of die casting
JPS58116970A (ja) * 1981-12-30 1983-07-12 Kubota Ltd 耐摩耗鋳物の竪型遠心鋳造法
JPS609570A (ja) * 1983-06-29 1985-01-18 Aisin Seiki Co Ltd 補強材よりなるピストンの製造方法
DE3404092C1 (de) * 1984-02-07 1985-06-13 Daimler-Benz Ag, 7000 Stuttgart Verfahren zur Herstellung faserverstaerkter Leichtmetallgussstuecke durch Druckgiessen
JPS6127164A (ja) * 1984-07-13 1986-02-06 Kubota Ltd 圧延用ロ−ルの竪型遠心力鋳造方法
JPS62259660A (ja) * 1986-05-07 1987-11-12 Aisin Seiki Co Ltd 遠心分散成形による摺動材料の製造方法
EP0280830A1 (de) * 1987-03-02 1988-09-07 Battelle Memorial Institute Verfahren zur Herstellung von faser- oder teilchenverstärkten, gegossenen Metallverbundwerkstoffen oder Metallegierungsverbundwerkstoffen
JPS63290676A (ja) * 1987-05-22 1988-11-28 Ishikawajima Harima Heavy Ind Co Ltd セラミック短繊維強化体の製造方法及びその製造装置
JPH01154861A (ja) * 1987-12-14 1989-06-16 Toshiba Corp 歯車の製造方法
JPH02155559A (ja) * 1988-12-07 1990-06-14 Yasuyoshi Fukui 比重の差に起因する遠心力の差を利用した傾斜機能材料の管製造法
JPH03158435A (ja) * 1989-11-17 1991-07-08 Suzuki Motor Corp 傾斜機能複合材料と、その製造方法
JPH067915A (ja) * 1992-06-26 1994-01-18 Mitsubishi Heavy Ind Ltd 耐摩耗性アルミニウム合金鋳物及びその製法
JPH08218129A (ja) * 1995-02-13 1996-08-27 Showa Alum Corp 耐摩耗性過共晶Ａｌ−Ｓｉ合金材の製造方法
US5980792A (en) * 1996-09-04 1999-11-09 Chamlee; Thomas C. Particulate field distributions in centrifugally cast composites
JP2001115224A (ja) * 1999-10-15 2001-04-24 Ueda Seni Kagaku Shinkokai 配向度傾斜型傾斜機能材料及びその製造方法
JP2004034084A (ja) * 2002-07-03 2004-02-05 J-Tec Inc 部分強化型金属基複合材料の製造方法

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6250364B1 (en) * 1998-12-29 2001-06-26 International Business Machines Corporation Semi-solid processing to form disk drive components

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130266470A1 (en) * 2010-11-25 2013-10-10 Rolls Royce Deutschland Ltd & Co Kg Method for the manufacturing high-temperature resistant engine components
CN113664185A (zh) * 2021-07-06 2021-11-19 惠州学院 一种采用电磁铸造制备铝合金双金属复合材料的制备方法

Also Published As

Publication number Publication date
JP2010515582A (ja) 2010-05-13
EP2111315A1 (de) 2009-10-28
BRPI0806329A2 (pt) 2011-09-06
KR20090095652A (ko) 2009-09-09
WO2008085820A1 (en) 2008-07-17
CN101578149A (zh) 2009-11-11
WO2008085820A8 (en) 2009-08-13

Similar Documents

Publication Publication Date Title
US20080169077A1 (en) Method of reinforcing low melting temperature cast metal parts
AU732289B2 (en) Particulate field distributions in centrifugally cast metal matrix composites
KR20050058404A (ko) 주조 공정 및 이를 수행하기 위한 물품
CS103891A2 (en) Method of composites manufacture by means of casting
CN105008068A (zh) 形成包含由金属基复合材料形成的套管构件的部件的方法
CN103352978A (zh) Al3Ti/Al3Ni颗粒协同增强硅铝基复合活塞及制备方法
US20110162521A1 (en) Mmc cylinder liner and method for producing the same
US3752212A (en) Method of forming castings of different metals
CN116804418A (zh) 用替代材料制成曲轴的系统和方法
US5803153A (en) Nonferrous cast metal matrix composites
CN1038314C (zh) 金属基复合材料的电磁搅拌铸造工艺
JP2004034084A (ja) 部分強化型金属基複合材料の製造方法
WO2004101197A3 (de) Verfahren zum schleudergiessen
JPS61281848A (ja) 機械部品用鋳型
US11745256B2 (en) Casting parts cycle life improvement using localized gradient material
JPS6411384B2 (de)
FR2675063A1 (fr) Procede d'elaboration de pieces metalliques composites a renforts metalliques.
JP3077084B2 (ja) 複合鋳造法
JP2000317616A (ja) 耐摩耗性クラッド板の製造方法
Barbosa New Approaches to Reinforce Cast Aluminum
JP6735025B2 (ja) 精密鋳造用消失性模型の製造方法および精密鋳造用消失性模型
Mao et al. Research on the composite slurry preparation and rheocasting of aluminum alloy
JPS5827023B2 (ja) 繊維強化複合部材の製造方法
JPH08300137A (ja) 複合部材の製造方法
Mahadevan et al. Development of Selectively Reinforced Squeeze Cast Pistons

Legal Events

Date Code Title Description
AS Assignment

Owner name: GATES CORPORATION, THE, COLORADO

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:HODJAT, YAHYA;REEL/FRAME:018794/0633

Effective date: 20070108

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION