EP0745694A1 - Procédé et dispositif pour mettre des métaux semi-solides en forme - Google Patents

Procédé et dispositif pour mettre des métaux semi-solides en forme Download PDF

Info

Publication number
EP0745694A1
EP0745694A1 EP96108499A EP96108499A EP0745694A1 EP 0745694 A1 EP0745694 A1 EP 0745694A1 EP 96108499 A EP96108499 A EP 96108499A EP 96108499 A EP96108499 A EP 96108499A EP 0745694 A1 EP0745694 A1 EP 0745694A1
Authority
EP
European Patent Office
Prior art keywords
vessel
temperature
alloy
metal
semisolid
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.)
Granted
Application number
EP96108499A
Other languages
German (de)
English (en)
Other versions
EP0745694B1 (fr
Inventor
Mitsuru c/o Ube Industries Ltd. Adachi
Hiroto c/o Ube Industries Ltd. Sasaki
Yasunori c/o Ube Industries Ltd. Harada
Tatsuo c/o Ube Industries Ltd. Sakamoto
Satoru c/o Ube Industries Ltd. Sato
Atsushi c/o Ube Industries Ltd. Yoshida
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.)
Ube Corp
Original Assignee
Ube Industries Ltd
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=27584868&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP0745694(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Priority claimed from JP13013495A external-priority patent/JP3246273B2/ja
Priority claimed from JP7160890A external-priority patent/JPH0910893A/ja
Priority claimed from JP7236501A external-priority patent/JPH0976051A/ja
Priority claimed from JP7244109A external-priority patent/JPH0987767A/ja
Priority claimed from JP7244111A external-priority patent/JPH0987768A/ja
Priority claimed from JP24789795A external-priority patent/JP3473214B2/ja
Priority claimed from JP7249482A external-priority patent/JPH0987770A/ja
Priority claimed from JP7252769A external-priority patent/JPH0987773A/ja
Priority claimed from JP25276895A external-priority patent/JP3473216B2/ja
Priority claimed from JP7252762A external-priority patent/JPH0987771A/ja
Priority claimed from JP29076095A external-priority patent/JP3246296B2/ja
Priority claimed from JP32065095A external-priority patent/JP3536491B2/ja
Priority claimed from JP33295595A external-priority patent/JP3669388B2/ja
Priority claimed from JP08784896A external-priority patent/JP3783275B2/ja
Application filed by Ube Industries Ltd filed Critical Ube Industries Ltd
Priority to EP02028272A priority Critical patent/EP1331279A3/fr
Publication of EP0745694A1 publication Critical patent/EP0745694A1/fr
Publication of EP0745694B1 publication Critical patent/EP0745694B1/fr
Application granted granted Critical
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D17/00Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
    • B22D17/007Semi-solid pressure die casting
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/12Making non-ferrous alloys by processing in a semi-solid state, e.g. holding the alloy in the solid-liquid phase

Definitions

  • This invention relates to a method of shaping semisolid metals. More particularly, the invention relates to a method of shaping semisolid metals, in which liquid alloy having crystal nuclei at a temperature not lower than the liquidus temperature or a partially solid, partially liquid alloy having crystal nuclei at a temperature not lower than a molding temperature is fed into an insulated vessel having heat insulateing effect, holding the alloy for a period from 5 seconds to 60 minutes as it is cooled to the molding temperature where a specified fraction liquid is established, thereby generating fine primary crystals in the alloy solution and the alloy is shaped under pressure.
  • the invention also relates to an apparatus for implementing this method.
  • the first two concern magnesium alloys that will easily produce an equiaxed microstructure and Zr is added to induce the formation of finer crystals [method (B)] or a carbonaceous refiner is added for the same purpose [method (C)];
  • the third approach concerns aluminum alloy and a master alloy comprising an Al-5% Ti-1% B system is added as a refiner in amounts ranging from 2 - 10 times the conventional amount [method (D)].
  • the raw materials prepared by these methods are heated to temperature ranges that produce semisolid metals and the resulting primary crystals are spheroidized before molding.
  • alloys within a solubility limit are heated fairly rapidly up to a temperature near the solidus line and, thereafter, in order to ensure a uniform temperature profile through the raw material while avoiding local melting, the alloy is slowly heated to an appropriate temperature beyond the solidus line so that the material becomes sufficiently soft to be molded [method (E)].
  • method (A) is cumbersome and the production cost is high irrespective of whether the agitation or recrystallization technique is utilized.
  • method (B) is economically disadvantageous since Zr is an expensive element and speaking of method (C), in order to ensure that carbonaceous refiners will exhibit their function to the fullest extent, the addition of Be as an oxidation control element has to be reduced to a level as low as about 7 ppm but then the alloy is prone to burn by oxidation during the heat treatment just prior to molding and this is inconvenient in operations.
  • Method (E) is a thixo-casting process which is characterized by heating the raw material slowly after the temperature has exceeded the solidus line such that the raw material is uniformly heated and spheroidized. In fact, however, an ordinary dendritic microstructure will not transform to a thixotropic structure (in which the primary dendrites have been spheroidized).
  • thixo-casting methods (A) - (E) have a common problem in that they are more costly than the existing casting methods because in order to perform molding in the semisolid state, the liquid phase must first be solidified to prepare a billet, which is heated again to a temperature range that produces a semisolid metal.
  • method (F) which continuously generates and supplies a molten metal containing spherical primary crystals is more advantageous than the thixocasting approach from the viewpoint of cost and energy but, on the other hand, the machine to be installed for producing a metal material consisting of a spherical structure and a liquid phase requires cumbersome procedures to assure effective operative association with the casting machine to yield the final product.
  • the present invention has been accomplished under these circumstances and has as an object providing a method that does not use billets or any cumbersome procedures but which ensures convenience and ease in the production of semisolid metals having fine primary crystals and shaping them under pressure.
  • Another object of the invention is to provide an apparatus that can implement this method.
  • the first object of the invention can be attained by the method of shaping a semisolid metal recited in claim 1, in which a liquid alloy having crystal nuclei at a temperature not lower than the liquidus temperature or a partially solid, partially liquid alloy having crystal nuclei at a temperature not lower than a molding temperature is fed into an insulated vessel having a heat insulating effect, held in said insulated vessel for a period from 5 seconds to 60 minutes as it is cooled to the molding temperature where a specified fraction liquid is established, thereby crystallizing primary crystals in the alloy solution, and the alloy is fed into a forming mold, where it is shaped under pressure.
  • the crystal nuclei mentioned in claim 1 are generated by contacting the molten alloy with a surface of a jig at a temperature lower than the melting point of said alloy which has been held superheated to less than 300°C above the liquidus temperature.
  • the jig mentioned in claim 2 is a metallic or nonmetallic jig, or a metallic jig having a surface coated with nonmetallic materials or semiconductors, or a metallic jig compounded of nonmetallic materials or semiconductor, with said jig being adapted to be coolable from either inside or outside.
  • the crystal nuclei mentioned in claim 1 or 2 are generated by applying vibrations to the molten metal in contact with either the jig or the insulated vessel or both.
  • the alloy mentioned in claim 1 or 2 is an aluminum alloy of a composition within a maximum solubility limit or a hypoeutectic aluminum alloy of a composition at or above a maximum solubility limit.
  • the alloy mentioned in claim 1 or 2 is a magnesium alloy of a composition within a maximum solubility limit.
  • the aluminum alloy mentioned in claim 5 has 0.001% - 0.01% B and 0.005% - 0.3% Ti added thereto.
  • the magnesium alloy mentioned in claim 6 is one having 0.005% - 0.1% Sr added thereto, or one having 0.01% - 1.5% Si and 0.005% - 0.1% Sr added thereto, or one having 0.05% - 0.30% Ca added thereto.
  • a molten aluminum alloy held superheated to less than 100°C above the liquidus temperature is directly poured into an insulated vessel without using a jig.
  • a molten magnesium alloy held superheated to less than 100°C above the liquidus temperature is directly poured into an insulated vessel without using a jig.
  • a partially solid, partially liquid alloy having crystal nuclei at a temperature not lower than a molding temperature is held within an insulated vessel for a period from 5 seconds to 60 minutes as it is cooled to the molding temperature where a specified fraction liquid is established,such that the period of cooling from the initial temperature at which said alloy is held in said insulated vessel to a temperature 5°C lower than its liquidus temperature is not longer than 15 minutes, whereby fine primary crystals are crystallized in the alloy solution, which is then fed into a forming mold, where it is shaped under pressure.
  • the crystal nuclei mentioned in claim 11 or 12 are generated by holding a molten alloy superheated to less than 300°C above the liquidus temperature and contacting the melt with a surface of a jig at a lower temperature than its melting point.
  • the second object of the invention can be attained by the apparatus recited in claim 14 which is for producing a semisolid forming metal having fine primary crystals dispersed in a liquid phase, said apparatus comprising a nucleus generating section that causes a molten metal to contact a cooling jig to generate crystal nuclei in the solution and a crystal generating section having an insulated vessel in which the metal obtained in said nucleus generating section is held as it is cooled to a molding temperature at which said metal is partially solid, partially liquid.
  • the cooling jig in the nucleus generating section mentioned in claim 14 is either an inclined flat plate that has an internal channel for a cooling medium and that has a pair of weirs provided on the top surface parallel to the flow of the melt, or a cylindrical or semicylindrical tube.
  • liquid alloy having crystal nuclei at a temperature not lower than the liquidus temperature or a partially solid, partially liquid having crystal nuclei at a temperature not lower than a molding temperature is poured into a vessel so that it is cooled to a temperature at which a fraction solid appropriate for shaping is established, said vessel being adapted to be heatable or coolable from either inside or outside, being made of a material having a thermal conductivity of at least 1.0 kcal/hr ⁇ m ⁇ °C (at room temperature) and being held at a temperature not higher than the liquidus temperature of said alloy prior to its pouring, and said alloy is poured into said vessel in such a manner that fine, nondendritic primary crystals are crystallized in said alloy solution and that said alloy is cooled rapidly enough to be provided with a uniform temperature profile in said vessel, and said alloy, after being cooled, is fed into a forming mold, where it is shaped under pressure.
  • the step of cooling the alloy mentioned in claim 16 is performed with the top and bottom portions of the vessel being heated by a greater degree than the middle portion or heat-retained with a heat-retaining material having a thermal conductivity of less than 1.0 kcal/hr ⁇ m ⁇ °C or with either the top or bottom portion of the vessel being heated while the remainder is heat-retained.
  • the step of cooling the alloy mentioned in claim 16 is performed with the vessel holding said alloy being accommodated in an outer vessel that is capable of accommodating said alloy holding vessel and that has a smaller thermal conductivity than said holding vessel, or that has a thermal conductivity equal to or greater than that of said holding vessel and which has a higher initial temperature than said holding vessel, or that is spaced from said holding vessel by a gas-filled gap, at a sufficiently rapid cooling rate to provide a uniform temperature profile through the alloy in said holding vessel no later than the start of the shaping step.
  • a method of managing the temperature of a semisolid metal slurry for use in molding equipment in which a molten metal containing a large number of crystal nuclei is poured into a vessel, where it is cooled to produce a semisolid metal slurry containing both a solid and a liquid phase in specified amounts, said slurry being subsequently fed into a molding machine for shaping under pressure, which method is characterized in that the vessel for holding said molten metal is temperature-managed such as to establish a preset desired temperature prior to the pouring of said molten metal and such that said molten metal is cooled at an intended rate after said molten metal is poured into said vessel.
  • an apparatus for managing the temperature of a semisolid metal slurry to be used in molding equipment in which a molten metal containing a large number of crystal nuclei is poured from a melt holding furnace into a vessel, where it is cooled to produce a semisolid metal slurry containing both a solid and a liquid phase in specified amounts and in which said slurry is directly fed into a molding machine for shaping under pressure
  • apparatus is further characterized by compriseing the vessel for holding said molten metal, a vessel temperature control section for managing the temperature of said vessel, a semisolid metal cooling section for managing the temperature of the as-poured molten metal such that it is cooled at an intended rate, and a vessel transport mechanism comprising basically a robot for gripping, moving and transporting said vessel and a conveyor for carrying, moving and transporting said vessel.
  • the vessel temperature control section mentioned in claim 20 comprises a vessel cooling furnace for cooling the vessel in an ambient temperature not higher than a target temperature for the vessel and a vessel heat-retaining furnace for holding the vessel at an ambient temperature equal to said target temperature.
  • the semisolid metal cooling section mentioned in claim 20 comprises a semisolid metal cooling furnace and a semisolid metal annealing furnace for managing the temperature in itself to be higher than the temperature in said semisolid metal cooling furnace.
  • the semisolid metal cooling furnace in the semisolid metal cooling section mentioned in claim 22 is such that the area around the vessel carried on the conveyor device moving to pass through said furnace is partitioned into three regions, the upper, middle and lower parts, by means of two pairs of heat insulating plate, one pair consisting of an upper right and an upper left plate and the other pair consisting of a lower right and a lower left plate, with a heater being installed in both said upper and lower parts for heating said two parts at a higher temperature than hot air to be supplied to said central part.
  • a preheating furnace is installed at a stage prior to the semisolid metal cooling furnace in claim 22 to ensure that both a plinth having a lower thermal conductivity than the vessel and which carries said vessel before it is directed to said semisolid metal cooling furnace and a lid having a lower thermal conductivity than said vessel and which is to be placed to cover it after it accommodates said molten metal are preheated by being moved to pass through said preheating furnace in advance.
  • the semisolid metal cooling furnace is equipped with a control unit with which the temperature or the velocity of hot air to be supplied into said semisolid metal cooling furnace is controlled to vary with the lapse of time.
  • the semisolid metal cooling furnace mentioned in claim 22 comprises an array of housings each accommodating the vessel as it contains the molten metal and being equipped with an openable cover and hot air feed/exhaust pipes, as well as a mechanism by which a receptacle for carrying said vessel is rotated about a vertical shaft.
  • a vibrator for vibrating the receptacle mentioned in claim 26 is provided for each housing.
  • the semisolid metal cooling furnace for treating the molten metal as poured into a vessel having a thermal conductivity of at least 1.0 kcal/hr ⁇ m ⁇ °C is supplied with hot air having a temperature in the range from 150°C to 350°C for aluminum alloys and from 200°C to 450°C for magnesium alloys.
  • the semisolid metal cooling furnace for treating the molten metal as poured into a vessel having a thermal conductivity of less than 1.0 kcal/hr ⁇ m ⁇ °C is supplied with hot air having a temperature in range from 50°C to 200°C for aluminum alloys and from 100°C to 250°C for magnesium alloys.
  • the molten metal as poured into the insulated vessel in claim 1 or 2 is isolated from the ambient atmosphere by closing the top surface of said vessel with an insulating lid having a heat insulating effect as long as said molten metal is held within said vessel until the molding temperature is reached.
  • the alloy in claim 1 or 2 is specified to a zinc alloy.
  • the alloy in claim 1 or 2 is specified to a hypereutectic Al-Si alloy having 0.005% - 0.03% P added thereto or a hypereutectic Al-Si alloy containing 0.005% - 0.03% P having either 0.005% - 0.03% Sr or 0.001% - 0.01% Na or both added thereto.
  • the alloy in claim 1 or 2 is specified to a hypoeutectic Al-Mg alloy containing Mg in an amount not exceeding a maximum solubility limit and which has 0.3% - 2.5% Si added thereto.
  • the pressure forming in claim 1 or 2 is accomplished with the alloy being inserted into a container on an extruding machine.
  • the extruding machine is of either a horizontal or a vertical type or of such a horizontal type in which the container changes position from being vertical to horizontal and the method of extrusion is either direct or indirect.
  • the crystal nuclei in claim 1 are generated by a method in which two or more liquid alloys having different melting points that are held superheated to less than 50°C above the liquidus temperature are mixed either directly within the insulated vessel having a heat insulating effect or along a trough in a path into the insulated vessel, such that the temperature of the metal as mixed is either just above or below the liquidus temperature.
  • the two or more metals to be mixed in claim 36 are preliminarily contacted with respective jigs each having a cooling zone such as to produce metals of different melting points that have crystal nuclei and which have attained temperatures just either above or below the liquidus temperature.
  • the top surface of the semisolid metal that is held within the insulated vessel and which is to be fed into the forming mold in claim 1 is removed by means of either a metallic or nonmetallic jig during a period from just after the pouring into said vessel but before the molding temperature is reached and, thereafter, said semisolid metal is inserted into an injection sleeve.
  • the outer vessel in claim 18 is heated either from inside or outside or by induction heating, with such heating being performed only or before or after the insertion of the holding vessel into the outer vessel or continued throughout the period not only before but also after the insertion.
  • the aluminum alloy in claim 9 is replaced by a zinc alloy.
  • liquid or partially solid, partially liquid alloys having crystal nuclei are charged into an insulated vessel having a heat insulating effect and held there for a period from 5 seconds to 60 minutes as they are cooled to a molding temperature, whereby fine and spherical primary crystals are generated in the solution and the resulting semisolid alloy is fed into a mold, where it is pressure formed to produce a shaped part having a homogeneous microstructure.
  • a liquid alloy having crystal nuclei at a temperature not lower than the liquidus line or a partially solid, partially liquid alloy having crystal nuclei at a temperature not lower than a molding temperature is fed into an insulated vessel having a heat insulating effected, and the alloys are held in that vessel for a period from 5 seconds to 60 minutes as they are cooled to the molding temperature, thereby generating fine and spheroidized primary crystals in the alloy solution and the resulting semisolid alloy is fed into a mold, where it is pressure formed into a shaped part having a homogeneous microstructure.
  • Fig. 1 is a diagram showing a process sequence for the semisolid forming of a hypoeutectic aluminum alloy having a composition at or above a maximum solubility limit
  • Fig. 2 is a diagram showing a process sequence for the semisolid forming of a magnesium or aluminum alloy having a composition within a maximum solubility limit
  • Fig. 3 shows a process flow starting with the generation of spherical primary crystals and ending with the molding step
  • Fig. 4 shows diagrammatically the metallographic structures obtained in the respective steps shown in Fig. 3;
  • Fig. 1 is a diagram showing a process sequence for the semisolid forming of a hypoeutectic aluminum alloy having a composition at or above a maximum solubility limit
  • Fig. 2 is a diagram showing a process sequence for the semisolid forming of a magnesium or aluminum alloy having a composition within a maximum solubility limit
  • Fig. 3 shows a process flow starting with the generation of spherical primary crystals and ending with the molding
  • Fig. 5 is an equilibrium phase diagram for an Al-Si alloy as a typical aluminum alloy system
  • Fig. 6 is an equilibrium phase diagram for a Mg-Al alloy as a typical magnesium alloy system
  • Fig. 7 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the invention
  • Fig. 8 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the prior art.
  • the first step of the process according to the invention comprises:
  • the cooled molten alloy prepared in (1) is poured into an insulated vessel having a heat insulating effect and, in the case of (2), the melt is directly poured into the insulated vessel without being cooled with a jig.
  • the melt is held within the insulated vessel for a period from 5 seconds to 60 minutes at a temperature not higher than the liquidus temperature but higher than the eutectic or solidus temperature, whereby a large number of fine spherical primary crystals are generated in the alloy, which is then shaped at a specified fraction liquid.
  • a specified fraction liquid means a relative proportion of the liquid phase which is suitable for pressure forming.
  • the fraction liquid ranges from 20% to 90%, preferably from 30% to 70%. If the fraction liquid is less than 30%, the formability of the raw material is poor; above 70%, the raw material is so soft that it is not only difficult to handle but also less likely to produce a homogeneous microstructure.
  • the fraction liquid ranges from 0.1% to 70%, preferably from 0.1% to 50%, beyond which an inhomogeneous structure can potentially occur.
  • the "insulated vessel” as used in the invention is a metallic or nonmetallic vessel, or a metallic vessel having a surface coated with nonmetallic materials or semiconductors, or a metallic vessel compounded of nonmetallic materials or semiconductor, which vessels are adapted to be either heatable or coolable from either inside or outside.
  • step (1) of the process shown in Figs. 3 and 4 a complete liquid form of metal M is contained in a ladle 10.
  • step (2) the metal is treated by either one of the following methods to produce an alloy having a large number of crystal nuclei which is of a composition just below the liquidus line: (a) the low-temperature melt (which may optionally contain an element that is added to promote the generation of crystal nuclei) is cooled with a jig 20 to generate crystal nuclei and the melt is then poured into a ceramic vessel 30 having a heat insulating effect; or (b) the low-temperature melt of a composition just above the melting point which contains an element to promote the generation of a fine structure is directly poured into the insulated vessel (or a ceramics-coated metallic vessel 30A) having a heat insulating effect.
  • step (3) the alloy is held partially molten within the insulated vessel 30 (or 30A).
  • step (3)-a very fine, isotropic dendritic primary crystals result from the introduced crystal nuclei [step (3)-a] and grow into spherical primary crystals as the fraction solid increases with the decreasing temperature of the melt [steps (3)-b and (3)-cl.
  • Metal M thus obtained at a specified fraction liquid is inserted into a die casting injection sleeve 40 [step (3)-d] and thereafter pressure formed within a mold cavity 50a on a die casting machine to produce a shaped part [step (4)].
  • the semisolid metal forming process of the invention shown in Figs. 1 - 4 has obvious differences from the conventional thixocasting and rheocasting methods.
  • the dendritic primary crystals that have been crystallized within a temperature range for the semisolid state are not ground into spherical grains by mechanical or electromagnetic agitation as in the prior art but the large number of primary crystals that have been crystallized and grown from the introduced crystal nuclei with the decreasing temperature in the range for the semisolid state are spheroidized continuously by the heat of the alloy itself (which may optionally be supplied with external heat and held at a desired temperature).
  • the semisolid metal forming method of the invention is very convenient since it does not involve the step of partially melting billets by reheating in the thixocasting process.
  • the casting temperature is at least 300°C higher than the melting point or if the surface temperature of jig 20 is not lower than the melting point, the following phenomena will occur; (1) only a few crystal nuclei are generated; (2) the temperature of the melt M as poured into the insulated vessel having a heat insulating effect is higher than the liquidus temperature and, hence, the proportion of the remaining crystal nuclei is low enough to produce large primary crystals.
  • the casting temperature to be employed in the invention is controlled to be such that the degree of superheating above the liquidus line is less than 300°C whereas the surface temperature of jig 20 is controlled to be lower than the melting point of alloy M.
  • Primary crystals of an even finer size can be produced by ensuring that the degree of superheating above the liquidus line is less than 100°C and by adjusting the surface temperature of jig 20 to be at least 50°C lower than the melting point of alloy M.
  • the melt M can be contacted with jig 20 by one of two methods: the melt M is moved on the surface of jig 20 (the melt is caused to flow down the inclined jig), or the jig moves through the melt.
  • the "jig" as used herein means any device that provides a cooling action on the melt as it flows down.
  • the jig may be replaced by the tubular pipe on a molten metal supply unit.
  • Insulated vessel 30 for holding the melt the temperature of which has dropped to just below the liquidus line shall have a heat insulating effect in order to ensure that the primary crystals generated will spheroidize and have the desired fraction liquid after the passage of a specified time.
  • the constituent material of the insulated vessel is in no way limited and those which have a heat-retaining property and which wet with the melt only poorly are preferred.
  • the exterior to the vessel is preferably filled with a specified atmosphere (e.g. an inert or vacuum atmosphere).
  • a specified atmosphere e.g. an inert or vacuum atmosphere.
  • Be or Ca is preliminarily added to the molten metal.
  • the shape of the insulated vessel 30 is by no means limited to a tubular form and any other shapes that are suitable for the subsequent forming process may be adopted.
  • the molten metal need not be poured into the insulated vessel but it may optionally be charged directly into a ceramic injection sleeve.
  • the holding time within the insulated vessel 30 is less than 5 seconds, it is not easy to attain the temperature for the desired fraction liquid and it is also difficult to generate spherical primary crystals. If the holding time exceeds 60 minutes, the spherical primary crystals and eutectic structure generated are so coarse that deterioration in mechanical properties will occur. Hence, the holding time within the insulated vessel is controlled to lie between 5 seconds and 60 minutes. If the fraction liquid in the alloy which is about to be shaped by high-pressure casting processes is less than 20%, the resistance to deformation during the shaping is so high that it is not easy to produce shaped parts of good quality. If the fraction liquid exceeds 90%, shaped parts having a homogeneous structure cannot be obtained.
  • the fraction liquid in the alloy to be shaped is preferably controlled to lie between 20% and 90%.
  • the effective fraction liquid By adjusting the effective fraction liquid to range from 30% to 70%, shaped parts having a more homogeneous structure and higher quality can be easily obtained by pressure forming.
  • Na or Sr may be added as an Si modifying element and this is advantageous for refining the eutectic Si grains, thereby providing improved ductility.
  • the means of pressure forming are in no way limited to high-pressure casting processes typified by squeeze casting and die casting and various other methods of pressure forming may be adopted, such as extruding and casting operations.
  • the constituent material of the jig 20 with which the melt M is to be contacted is not limited to any particular types as long as it is capable of lowering the temperature of the melt.
  • a jig 20 that is made of a highly heat-conductive metal such as copper, a copper alloy, aluminum or an aluminum alloy and which is controlled to provide a cooling effect for maintaining temperatures below a specified level is particularly preferred since it allows for the generation of many crystal nuclei.
  • coating the cooling surface of the jig 20 with a nonmetallic material is effective for the purpose of ensuring that solid lumps of metal will not adhere to the jig 20 when it is contacted by the melt M.
  • the coating method may be either mechanical or chemical or physical.
  • a semisolid alloy containing a large number of crystal nuclei and which has a temperature not higher than the liquidus line can be obtained by contacting the melt M with the jig 20. If desired, (1) in order to generate more crystal nuclei so as to produce a homogeneous structure comprising fine spherical grains or (2) to ensure that a semisolid alloy containing a large number of crystal nuclei and which has a temperature not higher than the liquidus line is produced from a melt that has been superheated to less than 100°C above the liquidus line and which is not contacted with any jig, various elements may be added to the melt, as exemplified by Ti and B for the case where the melt is an aluminum alloy, and Sr, Si and Ca for the case where the melt is a magnesium alloy.
  • the Ti addition is less than 0.005%, the intended refining effect is not attained; beyond 0.30%, a coarse Ti compound will form to cause deterioration in ductility. Hence, the Ti addition is controlled to lie between 0.005% and 0.30%.
  • Boron (B) cooperates with Ti to promote the refining of crystal grains but its refining effect is small if the addition is less than 0.001%; on the other hand, the effect of B is saturated at 0.02% and no further improvement is expected beyond 0.02%. Hence, the B addition is controlled to lie between 0.001% and 0.02%.
  • the Sr addition is less than 0.005%, the intended refining effect is not attained; on the other hand, the effect of Sr is saturated at 0.1% and no further improvement is expected beyond 0.1%. Hence, the Sr addition is controlled to lie between 0.005% and 0.1%. If 0.01% - 1.5% of Si is added in combination with 0.005% - 0.1% of Sr, even finer crystal grains will be formed than when Sr is added alone. If the Ca addition is less than 0.05%, the intended refining effect is not attained; on the other hand, the effect of Ca is saturated at 0.30% and no further improvement is expected beyond 0.30%. Hence, the Ca addition is controlled to lie between 0.05% and 0.30%.
  • the degree of superheating above the liquidus line is set to be less than 100°C and this is to ensure that the molten alloy poured into the insulated vessel 30 having a heat insulating effect is brought to either a liquid state having crystal nuclei or a partially solid, partially liquid state having crystal nuclei at a temperature not lower than the molding temperature. If the melt poured into the insulated vessel 30 is unduly hot, so much time will be taken for the temperature of the melt to decrease to establish a specified fraction liquid that the operating efficiency becomes low. Another inconvenience is that the poured melt M is oxidized or burnt at the surface.
  • Table 1 shows the conditions of various samples of semisolid metal to be shaped, as well as the qualities of shaped parts.
  • the shaping operation consisted of inserting the semisolid metal into an injection sleeve and subsequent forming on a squeeze casting machine.
  • the forming conditions were as follows: pressure, 950 kgf/cm 2 ; injection speed, 1.5 m/s; mold cavity dimensions, 100 x 150 x 10; mold temperature, 230°C.
  • Comparative Sample 1 the temperature of jig 20 with which the melt M was contacted was so high that the number of crystal nuclei generated was insufficient to produce fine spherical primary crystals; instead coarse unspherical primary crystals formed as shown in Fig. 7.
  • Comparative Sample 2 the casting temperature was so high that very few crystal nuclei remained within the ceramic vessel 30, yielding the same result as with Comparative Sample 1.
  • Comparative Sample 3 the holding time was so long that the fraction liquid in the metal to be shaped was low, yielding a shaped part of poor appearance. In addition, the size of primary crystals was undesirably large.
  • Comparative Sample 4 the holding time within the ceramic vessel 30 was short whereas the fraction liquid in the metal to be shaped was high; hence,only dendritic primary crystals formed. In addition, the high fraction liquid caused many segregations of components within the shaped part.
  • the insulated vessel 30 was a metallic container having a small heat insulating effect, so the dendritic solidified layer forming on the inner surface of the vessel 30 would enter the spherical primary crystals generated in the central part of the vessel, thus yielding an inhomogeneous structure involving segregations.
  • Comparative Sample 6 the fraction liquid in the metal to be shaped was so high that the result was the same as with Comparative Sample 4. With Comparative Sample 7, the jig 20 was not used; the starting alloy did not contain any grain refiners, so the number of crystal nuclei generated was small enough to yield the same result as with Comparative Sample 1.
  • X°C degree
  • a partially solid, partially liquid alloy (at a temperature not lower than a molding temperature higher than the eutectic or solidus temperature) is held within the insulated vessel for a period from 5 seconds to 60 minutes as it is cooled to the molding temperature where a specified fraction liquid is established, such that the period of cooling from the initial temperature at which said alloy is held within the insulated vessel to a temperature 5°C lower than the liquidus temperature of said alloy is not longer than 150 minutes, whereby fine spherical primary crystals are crystallized in the alloy solution, which is then fed into a forming mold, where it is shaped under pressure.
  • Example 2 The specific procedure of semisolid metal forming to be performed in Example 2 is essentially the same as described in Example 1.
  • the alloy to be held within the insulated vessel 30 is superheated such that its initial temperature is at least 10°C above the liquidus line, only unspherical primary crystals of a size of 300 ⁇ m and larger will form and fine, spherical primary crystals cannot be obtained no matter what conditions are used to cool the alloy to the molding temperature where a specified fraction liquid is established with a view to introducing crystal nuclei into the melt.
  • the initial temperature of the alloy held within the insulated vessel 30 is controlled to be less than 10°C above the liquidus line.
  • the cooling from the initial temperature to the temperature 5°C lower than the liquidus temperature must be completed within 15 minutes; otherwise, unspherical primary crystals of a size of 300 ⁇ m and larger will form or the size of spherical crystals to be obtained tends to be larger than 200 ⁇ m. Therefore, the period of cooling from the initial temperature to the temperature 5°C lower than the liquidus temperature should not be longer than 15 minutes.
  • Figs. 15 and 16 show how the holding time affects the crystal grain sizes of AZ91 and AC4CH which respectively are typical magnesium and aluminum alloys.
  • the "holding time” is the time for which the metal as poured into the insulated vessel is held until the molding temperature is reached.
  • the “molding temperature” is a typical value at which about 50% fraction liquid is established and it is 570°C for AZ91 and 585°C for AC4CH.
  • the dependency of the crystal grain size on the holding time differs with the alloy type but in both cases the grain size tends to be greater than 200 ⁇ m if the holding time exceeds 60 minutes.
  • primary crystals finer than 200 ⁇ m are prone to occur in the present invention.
  • Figs. 17 and 18 show how the degree by which the AZ91 and AC4CH within the holding vessel are superheated above the liquidus temperature and the holding time from the initial temperature within the insulated vessel to the liquidus temperature will affect the crystal grain sizes of the respective alloys.
  • Figs. 19 and 20 show how the holding time (from the initial temperature within the insulated vessel to the liquidus temperature minus 5°C) affects the crystal grain sizes of AZ91 and AC4CH, respectively.
  • the crystal grain size increases with the holding time and if the latter exceeds 15 minutes, there is a marked tendency for the crystal grain size to exceed 200 ⁇ m and coarse unspherical primary crystals occur.
  • the holding time is less than 15 minutes, there is a marked tendency for the primary crystals to be generated in small sizes less than 200 ⁇ m.
  • Fig. 21 is a side view of an apparatus 100 for producing a semisolid forming metal
  • Fig. 22 is a perspective view of a cooling jig 1 as part of the nucleus generating section 12 of the apparatus 100
  • Fig. 23 shows in cross section two other cooling jigs 1A and 1B
  • Fig. 24 is a sectional side view of another cooling jig 1C which is funnel-shaped
  • Fig. 25 is a plan view showing the general layout of another apparatus 100A for producing a semisolid forming metal
  • Fig. 26 is a longitudinal section A - A of Fig. 25; Fig. 27 is a longitudinal section B - B of Fig. 25; Fig. 28 is a longitudinal section of an insulated vessel 22; Fig. 3 shows a process flow illustrating the method of producing a semisolid forming metal; Fig. 7 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the invention; and Fig. 8 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part produced by a prior art process in which the molten metal is directly poured into the insulated vessel for cooling without passing through the nucleus generating section.
  • the apparatus 100 for producing semisolid forming metal consists of the nucleus generating section 12 and a crystal generating section 18.
  • the nucleus generating section 12 consists of the cooling jig 1 having a pair of weirs 2 provided to project from the right and left sides of the top surface of an inclined flat copper plate, stands 3 for supporting the jig 1 in an inclined position, and cooling pipes 4 (an inlet pipe 42 and a outlet pipe 4b) which are connected to a passage through which a cooling medium (usually water) is to be supplied into the cooling jig 1.
  • the crystal generating section 18 serves to generate fine crystals by ensuring that the molten metal obtained in the nucleus generating section 12 is held as it is cooled to a molding temperature where it becomes partially solid, partially liquid.
  • the crystal generating section 18 is constituted of the insulated vessel 22 which serves as a container of the molten metal M pouring down the cooling jig 1.
  • the insulated vessel 22 may optionally be accommodated within a metallic container 24 and equipped with a bolted cover plate 25 to ensure rigidity.
  • a pair of hooks 24a made of a round steel bar are provided to project from the lateral side of the metallic container 24 in order to assure convenience in transport.
  • a flat metallic (e.g. Cu) plate is to be used as the cooling jig 1
  • the molten metal can potentially stick to the cooling plate; to prevent this problem, it is desirable to reduce the wettability of the plate by applying a nonmetallic (e.g. BN) coating material onto its surface.
  • Weirs 2 are provided to control the flow of the molten metal as it descends the top surface of the cooling jig 1.
  • Fig. 23 shows the case where cooling jig 1A in the form of a cylindrical tube or cooling jig 1B in the form of a semicylindrical tube 1B is used as the cooling jig.
  • both cooling jigs 1A and 1B are equipped with a cooling medium channel 5 and cooling pipes 4 (inlet pipe 4a and outlet pipe 4b).
  • a funnel-shaped tube may be used as the cooling jig as shown in Fig. 24.
  • the cooling jig 1C may be stationary while the molten metal M is poured so that it drips into the underlying insulated vessel 22.
  • the cooling jig 1C may be rotationally journaled on a thrust bearing 1b on a pedestal 1a such that the molten metal is poured into the jig as it is rotated at slow speed by means of a reduction motor 1f which transmits the rotating power via spur gears 1e and 1d.
  • a molten alloy held superheated to less than 300°C above the liquidus temperature is poured on to the upper end of the cooling jig 1 (or 1A, 1B or 1C) in the nucleus generating section 12 so that the alloy flows down the jig.
  • the surface temperature of the cooling jig 1 is held to be lower than the melting point of the alloy.
  • the molten alloy which has flowed down the cooling jig 1 (or 1A, 1B or 1C) is gently received by the insulated vessel 22, in which it is held for a period from 5 seconds to 60 minutes in such a condition that its temperature is not higher than the liquidus temperature but higher than the eutectic or solidus temperature, whereby a large number of fine spherical primary crystals are generated to ensure that the alloy can be shaped at a specified fraction liquid.
  • Example 3 The specific procedure of semisolid metal forming to be performed in Example 3 is essentially the same as described in Example 1.
  • the holding time within the insulated vessel 22 varies widely from 5 seconds to 60 minutes depending on the time taken for the alloy to be cooled to the molding temperature. If the holding time is as long as 10 - 60 minutes, the productivity is very low on an apparatus in which one nucleus generating section 12 (cooling jig 1) is combined with one crystal generating section 18 (insulated vessel 22).
  • the apparatus comprises a turntable 60 that is capable of suspending a plurality of insulated vessels 22 on the circumference and which is free to rotate horizontally about a central shaft 62.
  • Each of the insulated vessels 22 is accommodated within a metallic container 24 which, as shown in Fig. 28, is fitted with a pair of hooks 24a that are each formed of a round steel bar and which are welded to project from the lateral side of the container 24.
  • the turntable 60 is provided with semicircular cutouts in the circumference that are spaced apart at generally equal intervals and which have a greater diameter than the metallic container 24; at the same time, the turntable 60 has as many hook receptacles 30a as the insulated vessels 22 and each receptacle 30a is in the form of a semicircular pipe that extends horizontally from the circumference of the turntable 60 so that the hooks 24a will rest on the receptacle to suspend the metallic container 24 which is integral with the insulated vessel 24 as shown in Fig. 28.
  • Each of the insulated vessels 22 suspended on the turntable 60 is charged with the molten metal via the cooling jig 1 on the left side (see Fig. 25) and carried by the slowly rotating turntable until it reaches the diametrically opposite position (as a result of 180° turn) after the passage of a predetermined cooling period.
  • a hydraulic cylinder or other means 26 for vertically moving the insulated vessel 22 is provided below the position where the insulated vessel is suspended (see Fig. 26).
  • the hydraulic cylinder 26 serves to push up the bottom of the insulated vessel 22 so that it is transferred to an injection sleeve 40 at the subsequent stage, which is then supplied with the partially solidified metal from within the insulated vessel.
  • a hydraulic cylinder or some other depressing means 28 is provided below the cooling jig 1; as shown, the hydraulic cylinder 28 has a piston rod 28a fitted at the terminal end with a rotatable depressing plate 28b supported on a pin.
  • the thus constructed apparatus 100A for producing semisolid forming metals is capable of feeding the molten metal into the injection sleeve by continuous treatment in a plurality of insulated vessels 22 and compared to the apparatus using a single unit of insulated vessels 22, the interval between successive cooling cycles is substantially reduced to ensure against the drop in productivity.
  • the apparatus 100 and 100A according to the invention are capable of producing semisolid metals that are suitable for use in semisolid forming, that have fine primary crystals dispersed within a liquid phase and that are free from the contamination by nonmetallic inclusions.
  • the semisolid metal obtained is difficult to be oxidized at the surface and has a very uniform temperature profile in its interior; hence, with almost all alloys, there is no need to use a high-frequency furnace for heating molding materials although this has been necessary in the conventional semisolid forming technology.
  • a robot or a dedicated machine may be used to grip the insulated vessel 22 and when the metal within the vessel has attained a specified molding temperature, it may be inserted into the injection sleeve 40 in a die casting machine (which may be a squeeze casting machine), with the top end directed to the side facing the injection tip, such as to accomplish semisolid forming.
  • a die casting machine which may be a squeeze casting machine
  • the top end directed to the side facing the injection tip, such as to accomplish semisolid forming.
  • a die casting machine which may be a squeeze casting machine
  • the semisolid metals produced with the apparatus of the invention may be shaped by pressure forming methods other than die casting; alternatively, they may be inserted into a sand or metallic mold gently without applying pressure.
  • the flat copper plate having internal cooling means is used as the nucleus generating means but this is not the sole case of the invention and any other means may be employed as long as it is capable of generating crystal nuclei that will not redissolve in the liquid phase.
  • nucleus generating means is described below.
  • the flat copper plate without weirs 2 may be replaced by the tubular cooling jig 1A or semicylindrical cooling jig 1B as shown in Fig. 23.
  • the molten metal may be poured into the conical cooling jig 1C as it is rotated by drive means and after crystal nuclei have been generated in the metal, the latter is withdrawn from the bottom the cooling jig 1C to be poured into the insulated vessel 22.
  • the constituent material of the cooling jig 1 is by no means limited to metals and it may be of any type as long as it is capable of cooling the molten alloy within a specified time while producing crystal nuclei in the alloy.
  • the insulated ceramic vessel is used as the crystal generating means and in a practical version of the example, the rotating turntable 60 which is capable of arranging a plurality of insulated vessels 22 is used.
  • this is not the sole method of arranging and fixing the insulated vessels 22 and they may be linearly or otherwise arranged.
  • To fix the insulated vessel 22, it may be positioned at a specified site as typically shown in Fig. 28, wherein the insulated vessel 22 is placed within the metallic container 24 having a slightly larger inside diameter and the bottom of the container 24 is pushed up by the hydraulic cylinder 26 as required.
  • the cooling jig consists of the nucleus generating section and the crystal generation section but, if desired, the two steps may be integrated.
  • the molten metal within the insulated vessel 22 may be treated with the cooling jig and/or a melt surface vibrating jig to ensure that both nuclei and crystals will be generated.
  • Fig. 1 is a diagram showing a process sequence for the semisolid forming of a hypoeutectic aluminum alloy having a composition at or above a maximum solubility limit
  • Fig. 2 is a diagram showing a process sequence for the semisolid forming of a magnesium or aluminum alloy having a composition within a maximum solubility limit
  • Fig. 29 shows a process flow starting with the generation of spherical primary crystals and ending with the molding step
  • Fig. 4 shows diagrammatically the metallographic structures obtained in the respective steps shown in Fig. 29; Fig.
  • Fig. 30 compares two graphs plotting the temperature changes in the metal being cooled within a vessel during step 3 shown in Fig. 29;
  • Fig. 31 illustrates four methods of managing the temperature within a vessel according to the invention;
  • Fig. 5 is an equilibrium phase diagram for an Al-Si alloy as a typical aluminum alloy system;
  • Fig. 6 is an equilibrium phase diagram for a Mg-Al alloy as a typical magnesium alloy system;
  • Fig. 7 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the invention;
  • Fig. 8 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the prior art.
  • the wall thickness of the vessel 30 is desirably such that after pouring of the molten metal, no dendritic primary crystals will result from the metal in contact with the inner surface of the vessel and yet no solidified layer will remain in the vessel at the stage where the semisolid metal has been discharged from within the vessel just before shaping.
  • the exact value of the wall thickness of the vessel is appropriately determined in consideration of the alloy type and the weight of the alloy in the vessel 30.
  • fraction solid appropriate for shaping means a relative proportion of the solid phase which is suitable for pressure forming.
  • the fraction solid ranges from 10% to 80%, preferably from 30% to 70%, If the fraction solid is more than 70%, the formability of the raw material is poor; below 30%, the raw material is so soft that it is not only difficult to handle but also less likely to produce a homogeneous structure.
  • the fraction solid ranges from 30% to 99.9%, preferably from 50% to 99.9%; if the fraction solid is less than 50%, an inhomogeneous structure can potentially occur.
  • the "temperature not higher than the liquidus temperature” means such a temperature that even if the temperature of the metal within the vessel is rapidly lowered to the level equal to the molding temperature, no dendritic primary crystals will result from the melt in contact with the inner surface of the vessel and yet no solidified layer will remain in the vessel at the stage where the semisolid metal is discharged from within the vessel just before shaping.
  • the exact value of the "temperature not higher than the liquidus temperature” varies with the alloy type and the weight of the alloy within the vessel.
  • the "vessel” as used in the invention is a metallic or nonmetallic vessel, or a metallic vessel having a surface coated with nonmetallic materials or semiconductors, or a metallic vessel compounded of nonmetallic materials or semiconductors. Coating the surface of the metallic vessel with a nonmetallic material is effective in preventing the sticking of the metal.
  • To heat the vessel its interior or exterior may be heated with an electric heater; alternatively, induction heating with high-frequency waves may be employed if the vessel is electrically conductive.
  • Example 4 The specific procedure of semisolid metal forming to be performed in Example 4 is essentially the same as described in Example 1.
  • Vessel 30 is used to hold the molten metal until it is cooled to a specified fraction solid after its temperature has dropped just below the liquidus line. If the thermal conductivity of the vessel 30 is less than 1.0 kcal/hr ⁇ m ⁇ °C at room temperature, it has such a good heat insulating effect that an unduly prolonged time will be required for the molten metal M in the vessel 30 to be cooled to the temperature where a specified fraction solid is established, thereby reducing the operational efficiency. In addition, the generated spherical primary crystals become coarse to deteriorate the formability of the alloy.
  • the holding time necessary to achieve the intended cooling becomes short even if the thermal conductivity of the vessel is less than 1.0 kcal/hr ⁇ m ⁇ °C at room temperature. If the temperature of the vessel 30 is higher than the liquidus temperature, the molten metal M as poured into the vessel is higher than the liquidus temperature, so that only a few crystal nuclei will remain in the liquid phase to produce large primary crystals.
  • dendritic primary crystals may occur at the site in the top or bottom portion of the vessel that is contacted by the metal M or a solidified layer will grow at that site, thereby creating a nonuniform temperature profile through the metal in the vessel which makes the subsequent shaping operation difficult to accomplish on account of the remaining solidified layer within the vessel.
  • top or bottom portion of the vessel by a greater degree than the middle portion while the bottom or top portion is heat-retained during the cooling process after the pouring of the metal; if necessary, the top or bottom portion of the vessel may be heated not only during the cooling process following the pouring of the metal but also prior to its pouring and this is another preferred practice in the invention.
  • the constituent material of the vessel 30 is in no way limited except on the thermal conductivity and those which are poorly wettable with the molten metal are preferred.
  • Table 2 shows the conditions of various samples of semisolid metal to be shaped, as well as the qualities of shaped parts.
  • the shaping operation consisted of inserting the semisolid metal into an injection sleeve and subsequent forming on a squeeze casting machine.
  • the forming conditions were as follows: pressure, 950 kgf/cm 2 ; injection speed, 1.0 m/s; casting weight (including biscuits), 30 kg; mold temperature, 230°C.
  • Comparative Sample 1 the thermal conductivity of the holding vessel was small and, in addition, the vessel was heated or heat-retained inappropriately after the pouring of the metal so that the holding time to the shaping temperature was unduly long; what is more, the formation of a solidified layer within the vessel prevented the discharge of the semisolid metal, thus making it impossible to perform shaping.
  • Comparative Sample 2 the thermal conductivity of the holding vessel was so small that the holding time to the shaping temperature was unduly prolonged.
  • Comparative Sample 3 the holding vessel was heated or heat-retained inappropriately after the pouring of the metal so that a solidified layer formed within the vessel to prevent the discharge of the semisolid metal, thus making it impossible to start the shaping step.
  • Comparative Sample 4 the wall thickness of the holding vessel was unduly great and, in addition, the vessel was heated or heat-retained inappropriately after the pouring of the metal so that unspherical primary crystals were generated; what is more, the formation of a solidified layer within the vessel prevented the discharge of the semisolid metal, thus making it impossible to perform shaping.
  • the casting temperature was so high that very few crystal nuclei remained within the vessel to yield only coarse unspherical primary crystals as shown in Fig. 8.
  • the cooling jig had such a high temperature that the number of crystal nuclei formed was insufficient to produce fine spherical primary crystals and, instead, only coarse unspherical primary grains formed as in Comparative Sample 5.
  • Comparative Sample 7 the fraction solid in the metal was so small that many segregations occurred within the shaped part.
  • Fig. 9 is a diagram showing a process sequence for the semisolid forming of hypoeutectic aluminum alloys having a composition at or above a maximum solubility limit
  • Fig. 10 is a diagram showing a process sequence for the semisolid forming of magnesium or aluminum alloys having a composition within a maximum solubility limit
  • Fig. 32 shows a process flow starting with the generation of spherical primary crystals and ending with the molding step
  • Fig. 4 shows diagrammatically the metallographic structures obtained in the respective steps shown in Fig. 32; Fig.
  • Fig. 34 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the prior art
  • Fig. 35 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the invention.
  • the invention recited in claim 18 is such that the melt of a hypoeutectic aluminum alloy of a composition at or above a maximum solubility limit or the melt of a magnesium or aluminum alloy of a composition within a maximum solubility limit is held superheated to less than 300°C above the liquidus temperature, contacted with a surface of the jig 20 at a lower temperature than the melting point of either alloy, and poured into a holding vessel 29 of a specified wall thickness that is made of a material having a thermal conductivity of at least 1.0 kcal/hr ⁇ m ⁇ °C (at room temperature) and that is preliminarily held at a temperature not higher than the liquidus temperature of either alloy, and the melt is subsequently cooled, with a heat insulating lid 32 placed on top of the holding vessel, down to a temperature at which a fraction solid appropriate for shaping is established, characterized in that during the cooling of the alloy, the outer surface of said holding vessel is heated or heat-retained
  • the wall thickness of the holding vessel 29 is desirably such that after pouring of the molten metal, no dendritic primary crystals will result from the metal in contact with the inner surface of the vessel and yet no solidified layer will remain in the vessel at the stage where the semisolid metal has been discharged from within the vessel just before shaping.
  • the exact value of the wall thickness of the vessel is appropriately determined in consideration of the alloy type and the weight of the alloy in the holding vessel 29.
  • fraction solid appropriate for shaping means a relative proportion of the solid phase which is suitable for pressure forming.
  • the fraction solid ranges from 10% to 80%, preferably from 30% to 70%. If the fraction solid is more than 70%, the formability of the raw material is poor; below 30%, the raw material is so soft that it is not only difficult to handle but also less likely to produce a homogeneous structure.
  • the fraction solid ranges from 30% to 99.9%, preferably from 50% to 99.9%; if the fraction solid is less than 50%, an inhomogeneous structure can potentially occur.
  • the "temperature not higher than the liquidus temperature” means such a temperature that even if the temperature of the alloy within the holding vessel is rapidly lowered to the level equal to the molding temperature, no dendritic primary crystals will result from the melt in contact with the inner surface of the holding vessel and yet no solidified layer will remain in the vessel at the stage where the semisolid alloy has been discharged from within the vessel just before shaping.
  • the "temperature not higher than the liquidus temperature” is also such that the alloy containing crystal nuclei can be poured into the holding vessel 29 without losing the crystal nuclei. The exact value of this temperature differs with the alloy type and the weight of the alloy within the holding vessel.
  • the "holding vessel” as used in the invention is a metallic or nonmetallic vessel, or a metallic vessel having a surface coated with nonmetallic materials or semiconductors, or a metallic vessel compounded of nonmetallic materials or semiconductors. Coating the surface of the metallic vessel with a nonmetallic material is effective in preventing the sticking of the metal.
  • the "outer vessel” as used in the invention serves to ensure that the alloy in the holding vessel will be cooled within a specified time.
  • the outer vessel must have the ability to cool the, holding vessel 29 rapidly in addition to a capability for heat-retaining or heating said vessel.
  • the temperature of the outer vessel 31 should be lowered to the level equal to the molding temperature within a specified time.
  • the outer vessel 31 may be provided with a temperature profile by, for example, heating the top and bottom portions of the outer vessel 31 in a high-frequency heating furnace by a greater degree than the middle portion.
  • the heating of the outer vessel 31 may be interrupted temporarily if it is necessary for adjusting the temperature of the alloy within the holding vessel 29.
  • the inside diameter of the outer vessel 31 is made sufficiently larger than the outside diameter of the holding vessel 29 to provide a clearance between the outer vessel 31 and the holding vessel 29 accommodated in it.
  • a plurality of projections are provided along the outer circumference of the holding vessel 29 and/or the inner circumference of the outer vessel 31.
  • the clearance may be insured by replacing the projections with recesses formed in either the outer circumference of the holding vessel or the inner circumference of the outer vessel.
  • the gap between the holding vessel 29 and the outer vessel 31 is typically filled with air but various other gases may be substituted such as inert gases, carbon dioxide and SF 6 .
  • step (1) of the process shown n Figs. 32 and 4 a complete liquid form of metal M is contained in a ladle 10.
  • step (2) the low-temperature melt (which may optionally contain an element that is added to promote the generation of crystal nuclei) is cooled with a jig 20 to generate crystal nuclei; in step (3)-0, the melt is poured into a vessel 30 that is preliminarily held at a specified temperature not higher than the liquidus temperature, thereby yielding an alloy containing a large number of crystal nuclei at a temperature either just below or above the liquidus line.
  • the cooling jig 20 may be dispensed with and the low-temperature melt of a composition just above the melting point and which contains an element added to promote the generation of a fine structure may be directly poured into the holding vessel 29 which is preliminarily maintained at a temperature not higher than the liquidus temperature.
  • the holding vessel 29 is accommodated within the outer vessel 31 lined with a heat insulator 33 on the bottom and then fitted with a lid. Thereafter, the alloy in the holding vessel is held in a semisolid condition with its temperature being lowered, whereby fine particulate (nondendritic) primary crystals are generated from the introduced crystal nuclei.
  • the outer vessel 31 is temperature managed such as by internal or external heating or by induction heating, with the heating being performed only before or after the insertion of the holding vessel 29 or for a continued period starting prior to the insertion of the holding vessel and ending after its insertion.
  • Metal M thus obtained at a specified fraction solid is inserted into a die casting injection sleeve 70 and thereafter pressure formed within a mold cavity 50a on a die casting machine to produce a shaped part.
  • the holding vessel 29 is used to hold the molten metal until it is cooled to a specified fraction solid after its temperature has dropped just below the liquidus line. If the thermal conductivity of the vessel 29 is less than 1.0 kcal/hr ⁇ m ⁇ °C (at room temperature), it has such a good heat insulating effect that an unduly prolonged time is required for the molten metal M in the holding vessel 29 to be cooled to the temperature where a specified fraction solid is established, thereby reducing the operational efficiency. In addition, the generated spherical primary crystals become coarse to deteriorate the formability of the alloy.
  • the holding vessel contains a comparatively small quantity of the melt, the holding time necessary to achieve the intended cooling becomes short even if the thermal conductivity of the vessel is less than 1.0 kcal/hr ⁇ m ⁇ °C at room temperature. If the temperature of the holding vessel 29 is higher than the liquidus temperature, the molten metal M as poured into the vessel is higher than the liquidus line, so that only a few crystal nuclei will remain in the liquid phase to produce large primary crystals.
  • the top of the holding vessel 29 should be fitted with a lid; an adequate clearance should be provided between the holding vessel 29 and the outer vessel 31; a heat insulator should be provided in the area where the bottom of the holding vessel 29 contacts the outer vessel 31; or projections or recesses should be provided on either the holding vessel 29 or the outer vessel 31.
  • Table 3 shows the conditions of the holding vessel, the alloy within the holding vessel, and the outer vessel, as well as the qualities of shaped parts.
  • the shaping operation consisted of inserting the semisolid metal into an injection sleeve and subsequent forming on a squeeze casting machine.
  • the forming conditions were as follows: pressure, 950 kgf/cm 2 ; injection speed; 1.0m/s; casting weight (including biscuits), 2 kg; mold temperature, 250°C.
  • Fig. 36 is a plan view showing the general layout of molding equipment (its first embodiment) according to an example of the invention
  • Fig. 37 is a plan view of a temperature management unit (its first embodiment) according to the example of the invention
  • Fig. 38 is a graph showing the specific positions of temperature measurement within a vessel according to an example of the invention
  • Figs. 39, 40 and 41 are graphs showing the temperature history of cooling within the vessel under different conditions
  • Fig. 42 is a longitudinal section of a semisolid metal cooling furnace according to another example of the invention
  • FIG. 43 is a plan view of a temperature management unit (its second embodiment) according to yet another example of the invention
  • Fig.44 is a longitudinal section A - A of Fig.43
  • Fig. 45 shows the temperature profiles in the vessel fitted with heat insulators according to an example of the invention
  • Fig. 46 is a plan view of a temperature management unit (its third embodiment) according to another example of the invention
  • Fig. 47 shows schematically the composition of a temperature controller for a semisolid metal cooling furnace (its first embodiment) according to an example of the invention
  • Fig. 48 shows schematically the composition of a temperature controller (its second embodiment) for a semisolid metal cooling furnace according to another example of the invention
  • Fig.49 is a longitudinal section of a vessel rotating unit according to an example of the invention
  • Fig. 53 is a longitudinal section of a semisolid metal cooling furnace as it is equipped with a vessel vibrator according to another example of the invention.
  • the molding equipment generally indicated by 300 consists of a melt holding furnace 14 for feeding the molten metal as a molding material (containing a large number of crystal nuclei), a molding machine 200, and a temperature management unit 104 for managing the temperature of the melt until it is fed to the molding machine 200.
  • the molten metal held within the furnace 14 contains a large number of crystal nuclei.
  • the temperature management unit 104 consists of a semisolid metal cooling section 110 and a vessel temperature control section 140; the semisolid metal cooling section 110 is composed of a semisolid metal cooling furnace 120 and a semisolid metal slowly cooling furnace 130 which are connected in a generally rectangular arrangement by means of a transport mechanism such as a conveyor 170 whereas the vessel temperature control section 140 is composed of a vessel cooling furnace 150 and a vessel heat-retaining furnace 160.
  • the temperature management unit 104 is also equipped with a robot 180 which grips the vessel 102 and transports it to one of the specified positions A - F (to be described below).
  • the temperature management unit 104 is operated as follows. An empty vessel 102 is first located in the heating vessel pickup position A. The robot 180 then transfers the vessel 102 to the position B, where the vessel is charged with a prescribed amount of the molten metal from the melt holding furnace 14. Thereafter, the robot 180 transports the vessel 102 to the filled vessel rest position C; subsequently, the vessel is cooled as it is carried by the conveyor 170 to pass through the semisolid metal cooling furnace 120 in a specified period of time.
  • the vessel 102 leaving the furnace 120 reaches the slurry vessel rest position D, from which it is immediately transferred to the sleeve position E by the robot 180 if the injection sleeve 202 in the molding machine 200 is ready to accept the molten metal; at position E, the slurry ofsemisolid metal in the vessel is poured into the injection sleeve 202. If the injection sleeve 202 is not ready to acceptthe molten metal when the vessel 102 has reached the slurry vessel rest position D (i.
  • the slurry of semisolid metal within the vessel will progressively solidify upon cooling while it is waiting for acceptance in the position D, thereby making it impossible for all the slurry to be discharged from the vessel or the crystal nuclei in the slurry will disappear to cause deterioration in the quality of the shaped part.
  • the vessel 102 is forwarded to the semisolid metal slowly cooling furnace 130,where it waits for the molding machine 200 to become completely ready for the acceptance of the molten metal while ensuring against its rapid cooling.
  • the vessel 102 from which the slurry of semisolid metal having satisfactory properties has been emptied into the injection sleeve 202 is then transferred to the empty vessel rest position F by means of the robot 180, carried by the conveyor 170 into the vessel cooling furnace 150, where it is cooled for a specified time, passed through the vessel heat-retaining furnace 160 as it is held at a suitable temperature, and is thereafter returned to the heating vessel pick up position A.
  • FIG.37 A specific embodiment of the temperature management unit 104 is shown in Fig.37.
  • the system configuration is such that the molding cycle on the molding machine 200 is about 75 seconds and the time of passage through the semisolid metal cooling furnace 120 and the vessel temperature controller 140 (i. e., consisting of the vessel cooling furnace 150 and the vessel heat-retaining furnace 160) is 600 seconds in total. If the total passage time is longer than 600 seconds, the overall equipment becomes impractically bulky and the volume of the slurry in process which results from machine troubles and which has to be discarded is increased and these are by no means preferred or the purpose of constructing commercial production facilities.
  • the vessel 102 is made of an Al 2 O 3 ⁇ SiO 2 composite having a small thermal conductivity (0.3 kcal/hr ⁇ m ⁇ °C).
  • a slurry of semisolid metal having satisfactory properties can be obtained if only the temperature of the vessel 102 is retained by circulation of hot air the temperature of which is set at a constant value of 120°C.
  • the system shown in Fig. 37 has the following differences from the system of Fig.36. Since the vessel 102 is made of the Al 2 O 3 ⁇ SiO 2 composite, it has a sufficiently small thermal conductivity that one only need supply the interior of the semisolid metal cooling furnace 120 (which is set at a temperature of 200°C) with a circulating hot air flow of a constant temperature from a hot air generating furnace 122.
  • the temperature in the vessel 102 can be managed correctly to ensure that slurries of semisolid metal having satisfactory properties can be produced in a short time while assuring farily consistent temperature management.
  • the temperature in the vessel is optimally at 70 °C; to ensure that the temperature in the vessel is consistently managed at the optimal 70°C, adequate heat removal must be effected in the vessel cooling furnace 150; otherwise, the temperature in the vessel 102 becomes undesirably high.
  • the vessel cooling furnace 150 is fitted with a blower 152 and a blow nozzle 152a such that a fast air flow is blown at room temperature to achieve forced cooling.
  • a sheathed thermocouple was set up in the vessel and temperature data were taken under various conditions.
  • Fig. 38 shows five different positions (A) - (E) of temperature measurement in the vessel 102, into which the 1.0- mm thick sheathed thermocouple was inserted.
  • Fig.39 shows the temperature history of cooling under condition I, i. e., the vessel temperature control section 140 was not divided into the vessel cooling furnace 150 and the vessel heat-retaining furnace 160 and a hot air flow having the target temperature of 70°C was circulated within the monolithic vessel temperature control section 140 at a velocity of about 5 m/sec. With this approach, the temperature in the vessel dropped to only about 200 °C which was far from the target value.
  • Fig.40 shows the temperature history of cooling under condition II, i. e., a hot air flow having a temperature of 70°C was circulated at a higher velocity of about 30 m/sec. This approach was effective in further reducing the temperature inthe vessel but not to the desired level of 70°C.
  • Fig.41 shows the temperature history of cooling under condition III, i. e., the vessel temperature control section 140 was divided into the vessel cooling furnace 150 and the vessel heat-retaining furnace 160, with an air flow at ordinary temperature being circulated within the cooling furnace 150 at a velocity of 30 m/sec whereas the atmosphere in the vessel heat-retaining furnace 160 had its temperature raised to 70°C by means of an electric heater. It was only with this system that the temperature in the vessel could be managed to be stable at the intended 70°C.
  • the vessel 102 is made of ceramics having thermal conductivities of no more than 1 kcal/m ⁇ hr ⁇ °C, the time to cool the slurry of semisolid metal becomes impractically long. Therefore, in the second embodiment of the temperature management unit 104 which is adapted for handling comparatively large volumes of aluminum alloys such that the molten alloy is poured in an amount of 20 kg or more, the vessel 102 is made of SUS304 (see Fig.43) rather than the ceramics which are used with the first embodiment shown in Fig.37 and which require a prolonged cooling time.
  • the resulting differences between the first embodiment of the temperature management unit 104 (Fig.37) and the second embodiment are as follows.
  • a water-soluble (which is desirable for ensuring against gas evolution) spray of a lubricant In order to ensure smooth recovery of the slurry from the vessel 102, its inner surfaces have to be coated with a water-soluble (which is desirable for ensuring against gas evolution) spray of a lubricant and, to this end, a spray position (spray equipment) is provided between the vessel cooling furnace 150 and the vessel heat-retaining furnace 160. Accordingly, the vessel 102 emerging from the vessel cooling furnace 150 must be kept at a sufficient temperature (200 °C)to allow for the deposition of the spray solution; to meet this requirement, hot air at 200°C is applied against the vessel through a blow nozzle. As the result of the application of the water-soluble spray, the vessel 102 experiences a local temperature drop.
  • a hot air flow at 200 °C is circulated within the vessel heat-retaining furnace 160 while it is agitated by a rotating fan to ensure uniformity in the temperature of the vessel 102.
  • the vessel 102 which is made of SUS304 allows thermal diffusion through it, so even if the semisolid metal cooling furnace 120 is of the design shown in Fig.42, no sharp border line can be drawn between the high-temperature range of the vessel (consisting of its top and bottom portions) and the low-temperature range (the middle portion of the vessel).
  • a preheating furnace 190 is provided as accessory equipment on a lateral side of the semisolid metal cooling furnace 120 and, as shown in Fig.44, a lid 102a made of a ceramic material (Al 2 O 3 ⁇ SiO 2 composite) and a plinth 102b are used to heat-retain the top and bottom of the vessel 102 while it is heated in the preheating furnace 190 before it is charged into the semisolid metal cooling furnace 120.
  • a lid 102a made of a ceramic material (Al 2 O 3 ⁇ SiO 2 composite) and a plinth 102b are used to heat-retain the top and bottom of the vessel 102 while it is heated in the preheating furnace 190 before it is charged into the semisolid metal cooling furnace 120.
  • the interior of the semisolid metal cooling furnace 120 is supplied with hot air from the hot air generating furnace via two sets of blow nozzles 124, one being in the upper position and the other in the lower position.
  • the supplied hot air is circulated within the cooling furnace 120 with its temperatureand velocity being 220°C and 5 m/sec at the entrance and 180 °C and 20 m/sec at the exit, whereby the semisolid metal is cooled comparatively slowly in the initial cooling period but cooled rapidly in the latter period.
  • the present invention provides a method of temperature management in which the step of managing the temperature in the vessel 102 at an appropriate level before it is supplied with the molten metal is distinctly separated from the step of managing the temperature in the vessel 102 in such a way that the as poured molten metal can be cooled at a desired appropriate rate; the invention also provides the apparatus for temperature management 104 which is capable of automatic performance of these steps in an efficient and continuous manner. Also proposed by the invention is a system configuration that implements the respective steps by means of the vessel temperature control section 140 and the semisolid metal cooling section 110.
  • the vessel temperature control section 140 is composed of the vessel cooling furnace 150 capable of forced cooling with a circulating hot air flow that provides an appropriate cooling capacity by controlling the temperature and velocity of the air passing through the furnace and the vessel heat-retaining furnace 160 which controls the temperature of the atmosphere to lie at the target value in the vessel 102 and which maintains the vessel 102 at said temperature of the atmosphere. It should be noted here that the temperature to which the vessel cooling furnace 150 and the vessel heat-retaining furnace 160 should be controlled differs between aluminum and magnesium alloys.
  • the interior of the vessel cooling furnace 150 is controlled to lie between room temperature and 300 °C whereas the interior of the vessel heat-retaining furnace 160 is controlled to lie between 50 °C and 350 °C; in the case of magnesium alloys, the interior of the vessel cooling furnace 150 is controlled to lie between room temperature and 350°C whereas the interior of the vessel heat-retaining furnace 160 is controlled to lie between 200 °C and 450 °C.
  • the semisolid metal cooling section 110 is composed of the semisolid metal cooling furnace 120 which is adapted to circulate hot air at an appropriate temperature such as to accomplish cooling within the shortest possible time that produces the slurry of semisolid metal with satisfactory properties and the semisolid metal slowly cooling furnace 130 which is designed to maintain the slurry of semisolid metal for 2 - 5 minutes in a temperature range appropriate for shaping such as to be adaptive for the specific molding cycle on the molding machine 200.
  • the temperature to which the semisolid metal cooling furnace 120 should be controlled differs between aluminum and magnesium alloys. In the case of aluminum alloys, the temperature should be controlled to lie between 150 °C and 350 °C and in the case of magnesium alloys, the temperature should be controlled to lie between 200 °C and 450 °C.
  • the interior of the semisolid metal slowly cooling furnace 130 should be controlled to be at 500 °C and above in both cases.
  • the injection sleeve 202 on the molding machine 200 is ready to accept the molten metal just at time when the vessel 102 holding the metal has left the semisolid metal cooling furnace 120, the metal is immediately fed (poured) into the molding machine 200 without being directed into the semisolid metal slowly cooling furnace 130. Conversely, if the injection sleeve 202 is not ready to accept the molten metal since the molding machine 200 is operating, the vessel 102 leaving the semisolid metal cooling furnace 120 is transferred to the semisolid metal slowly cooling furnace 130.
  • the semisolid metal cooling furnace 120 has the vessel 102 carried on the conveyor 170 via a heat insulating plate 120c and the inner surfaces on the sidewall of the furnace 120 is partitioned by an upper and a lower heat insulating plate 120b in the middle portion of its height, with hot air (set at an appropriate temperature of 120°C) being circulated through the partitioned area to establish a low-temperature region; at the same time, the inner surfaces of both top and bottom portions of the furnace 120 are heated with electric heaters 120a (set at a temperature of 500°C) to establish a high-temperature (ca. 500 °C) region, thereby ensuring that a uniform temperature is provided throughout the molten metal in the vessel 102.
  • a first version of the heating system in the semisolid metal cooling furnace 120 according to the invention is such that either the temperature or the velocity of the circulating hot air is controlled to vary appropriately with the lapse of time or, alternatively, both the temperature and the velocity of the hot air are controlled to vary simultaneously with the lapse of time.
  • the first specific embodiment of the heating system is as shown in Fig.47 and comprises a hot air line for supplying a hot air flow into the semisolid metal cooling furnace 120, an air line from which an air flow at ordinary temperature emerges to combine with the hot air to lower its temperature, a damper for controlling the quantity of the air flowing through the air line, and a damper opening controller.
  • the second specific embodiment of the heating system is as shown in Fig.48 and comprises a temperature sensor installed within the semisolid metal cooling furnace 120, a hot air line for supplying a hot air flow into the furnace, an air line that combines with the hot air line, an automatic damper installed on the air line, and a damper opening controller that performs feed back control on the damper opening on the basis of the data obtained by measurement with the temperature sensor.
  • the opening of the automatic damper is controlled on the basis of the data for the temperature in the furnace and the hot air is mixed with an appropriate amount of air and fed into the furnace, whereby the temperature and the velocity of the circulating hot air are controlled such that the molten metal will be cooled at a desired rate.
  • Fig.50 is a plan view showing the general layout of molding equipment
  • Fig. 43 is a plan view of the temperature management unit (its first embodiment)
  • Fig.51 is a longitudinal sectional view showing in detail the position of temperature measurement within the holding vessel
  • Fig. 52 is a graph showing the temperature history of cooling within the holding vessel
  • Fig. 44 is a longitudinal section A - A of Fig.43
  • Fig.46 is a plan view of the temperature management unit (its second embodiment) according to another example of the invention
  • Fig. 50 is a plan view showing the general layout of molding equipment
  • Fig. 43 is a plan view of the temperature management unit (its first embodiment)
  • Fig.51 is a longitudinal sectional view showing in detail the position of temperature measurement within the holding vessel
  • Fig. 52 is a graph showing the temperature history of cooling within the holding vessel
  • Fig. 44 is a longitudinal section A - A of Fig.43
  • Fig.46 is a plan view of the temperature management unit (its second embodiment
  • Fig. 45 shows the temperature profiles in the vessel fitted with heat insulators as compared with the temperature profile in the absence of such heat insulators;
  • Fig.47 shows schematically the composition of the temperature control unit (its first embodiment) for a semisolid metal cooling furnace;
  • Fig.48 shows schematically the composition of the temperature control unit (its second embodiment) for a semisolid metal cooling furnace according to another example of the invention;
  • Fig.49 is a longitudinal section of the semisolid metal cooling furnace according to the second embodiment in which it is equipped with a vessel rotating mechanism;
  • Fig.53 is a longitudinal section of the semisolid metal cooling furnace according to the third embodiment in which it is equipped with a vessel vibrating mechanism.
  • the molding equipment generally indicated by 104 consists of a melt holding furnace 10 for feeding the molten metal as a molding material, a molding machine 200 and a temperature management unit 100 for managing the temperature of the melt until it is fed to the molding machine 200.
  • the temperature management unit generally indicated by 104 consists of a semisolid metal cooling section 110 and a vessel temperature control section 140;
  • the semisolid metal cooling section 110 is composed of a semisolid metal cooling furnace 120 and a semisolid metal slowly cooling furnace 130 which are connected in a generally rectangular arrangement by means of a transport mechanism such as a conveyor 170 whereas the vessel temperature control section 140 is composed of a vessel cooling furnace 150 and a vessel heat-retaining vessel 160.
  • the temperature management unit 100 is also equipped with a robot 180 which grips the vessel 102 and transports it to one of the specified positions A - F (to be described below). The vessel 102 moves in the direction of arrows.
  • the preheating furnace 190 is provided near and parallel to the semisolid metal cooling furnace as shown in Figs.43 and 44.
  • the purpose of the preheating furnace 190 is to ensure that both the plinth 102b placed under the melt containing vessel 102 and the lid 102a placed on top of the vessel 102 are preliminarily heated to a higher temperature than the hot air to be passed through the semisolid metal cooling furnace 120 such that uniformity will be assured for the temperature of the melt within the vessel as it is cooled in the semisolid metal cooling furnace 120.
  • both the lid 102a and the plinth 102b which are carried on the conveyor 170 will be heated by the hot air being injected through the blow nozzle 192 as they move together with the conveyor 170 (see Fig. 44).
  • the temperature management unit 104 is operated as follows. An empty vessel 102 is first located in the heating vessel pickup position A. The robot 180 then transfers the vessel 102 to the position B, where the vessel is charged with a prescribed amount of the molten metal from the melt holding furnace 10 (which holds the molten metal containing a large number of crystal nuclei). Thereafter, the robot 180 transports the vessel 102 to the filled vessel rest position C, where it is placed on the plinth 102b and has its top covered with the lid 102a (both the lid 102a and the plinth 102b are preliminarily heated with the preheater 190); subsequently, the vessel is cooled as it is carried by the conveyor 170 to pass through the semisolid metal cooling furnace 120 in a specified period of time.
  • the vessel 102 leaving the furnace 120 reaches the slurry vessel rest position D, from which it is immediately transferred to the sleeve position E by the robot 180 if the injection sleeve 202 in the molding machine 200 is ready to accept the molten metal; at position E, the slurry of semisolid metal in the vessel is poured into the injection sleeve 202. If the injection sleeve 202 is not ready to accept the molten metal when the vessel 202 has reached the slurry vessel rest position D (i.
  • the slurry of semisolid metal within the vessel will progressively solidify upon cooling while it is waiting for acceptance in position D, thereby making it impossible for all the slurry to be discharged from the vesselor the crystal nuclei in the slurry will disappear to cause deterioration in the quality of the shaped part.
  • the vessel 102 is forwarded to the semisolid metal slowly cooling furnace 130, where it waits for the molding machine 200 to become completely ready for the acceptance of the molten metal while ensuring against its rapid cooling.
  • the vessel 102 from which the slurry of semisolid metal having satisfactory properties has been emptied into the injection sleeve 202 is then transferred to the empty vessel rest position F by means of the robot 180, carried by the conveyor 170 into the vessel cooling furnace 150, where it is cooled for a specified time, passed through the vessel heat-retaining furnace 160 as it is held at a suitable temperature, and is thereafter returned to the heating vessel pickup position A.
  • FIG.43 A specific embodiment of the temperature management unit 104 is shown in Fig.43.
  • the system configuration is such that the molding cycle on the molding machine 200 is about 150 seconds and the time of passage through the semisolid metal cooling furnace 120 and the vessel temperature control section 140 (i. e. consisting of the vessel cooling furnace 150 and the vessel heat-retaining furnace 160) is 600 seconds in total. If the total passage time is longer than 600 seconds, the overall equipment becomes impractically bulky and the volume of the slurry in process which results from machine troubles and which has to be discarded is increased and these are by no means preferred for the purpose of constructing commercial production facilities.
  • SUS304 was adopted as the constituent material of the vessel (in the case of a comparatively small-scale operation with the molten metal being poured in an amount of no more than 10 kg, materials of small thermal conductivity provide comparative ease in temperature management; however, in a large-scale operation like the case under discussion, the use of ceramics and other materials of small thermal conductivity as the constituent material of the vessel requires an unduly prolonged time to cool the slurry, resulting in the failure to satisfy the cycle time requirementset forth above).
  • the vessel 102 experienced a local temperature drop.
  • the vessel 102 was heated in the vessel heat-retaining furnace 160 in which a hot air flow at 190 °C was circulated by means of a fan.
  • preheating furnace 190 was installed as an accessory and the plinth 102b and lid 102a which were each made of a heat insulator (Al 2 O 3 ⁇ SiO 2 composite) were heated at 350 °C before they were set up on the vessel 102; this arrangement allowed the vessel 102 to be inserted into the semisolid metal cooling furnace 120 together with the lid 102a and plinth 102b.
  • a heat insulator Al 2 O 3 ⁇ SiO 2 composite
  • the interior of the semisolid metal cooling furnace 120 was equipped with two sets each of hot air generating furnaces and blow nozzles, through which hot air was supplied to circulate within the furnace 120, with its temperature and velocity being 220°C and 5 m/sec at the entrance and 180 °C and 20 m/sec at the exit, whereby the semisolid metal was cooled comparatively slowly in the initial cooling period but cooled rapidly in the latter period.
  • thermocouple For management of the temperature in the vessel 102, a sheathed thermocouple was set in the vessel to take data on the temperature. Detailed discussion will follow based on the thus taken temperature data.
  • Fig.51 shows the position of temperature measurement in the vessel 102. As shown enlarged on the right-hand illustration, a hole was made in the outer surface of the sidewall of the vessel to a depth at one half the wall thickness and thermocouple was inserted into the hole and spotwelded.
  • Fig.52 shows the temperature history of cooling of the vessel 102.
  • the vessel temperature control section 140 was divided into the vessel cooling furnace 150 and the vessel heat-retaining furnace 160 and, as already mentioned above, the vessel cooling furnace 150 was so adapted that "hot air at 100 °C was applied against the vessel through the blow nozzles" whereas the vessel heat-retaining vessel 160 was designed to "permit circulation of hot air at 190 °C.”
  • the system under discussion requires that the " spray should be deposited" within a limited time period while "a uniform temperature (180°C - 190 °C) should be established throughout the vessel 102".
  • the vessel temperature control section 140 was divided into the vessel cooling furnace 150 and the vessel heat-retaining furnace 160 and optimal temperature management was performed in each furnace.
  • the temperature management unit 100 shown in Fig. 46 was chiefly intended for the treatment of magnesium alloys.
  • the temperature management unit 100 comprises a plurality of linearly arranged housings 120A in a generally cubic shape, each being fitted with a top cover 120B that could be opened or closed by means of an air cylinder 120C. Hot air could be forced into the housings 120A. With the cover 120B open, the melt containing vessel 102 was placed on the plinth 102b at the bottom of each housing 120A and a lid 102a fixed to the inside surface of the cover 120B was fitted over the top of the vessel 102 so that it would ensure a heat insulating effect during the cooling of the vessel 102.
  • the vessel was adapted for transfer into or out of the housing 120A by manipulation of the robot 180.
  • the semisolid metal cooling furnace 120 according to the first embodiment shown in Fig.44 is of a continuous type in which the vessel 102 is carried by the conveyor 170 while the furnace is operating and, in contrast, the semisolid metal cooling furnace 120 according to the second embodiment shown in Fig.46 is of a batch system.
  • the plinth 102b seated on the bottom of the housing 120A is coupled to a rotational drive mechanism consisting of a motor 121a, a chain 121b, a sprocket121c, a bearing 121d, etc. and this drive mechanism allows the vessel 102 to rotate freely during its cooling operation.
  • FIG.53 Another embodiment of the semisolid metal cooling furnace 120 is shown in Fig.53; it is fitted with not only a vibrator 121f that is actuated with an ultrasonic oscillator 121e but also a water-cooled booster 121g and this arrangementwill provide effective vibrations to the vessel 102.
  • Fig.45 shows the temperature profiles obtained by fitting the top and bottom of the vessel with the lid 102a and the plinth 102b which were each made of a heat insulator (Al 2 O 3 ⁇ SiO 2 composite). Obviously, the use of the heat insulator produced uniform temperature profiles as compared with the case of using no such heat insulators. The uniformity in temperature profile was further improved by preheating the insulator.
  • the alloy to be treated in the case at issue is AC4C which has a eutectic temperature of 577 °C. Within a narrow temperature range centered at this eutectic point, the fraction solid increases sharply from 56 % to 100 % and the viscosity will inturn rises noticeably. Hence, the region of 56 % to 100 % fraction solid may well be considered as the "high-density region". When no heat insulator was used, both the top and bottom portions of the vessel were entirely covered with the "high-density region" and in a case like this, the desired slurry would not form smoothly.
  • the semisolid metal cooling furnace 120 according to the second embodiment shown in Fig. 46 have the following differences from the first embodiment shown in Fig.43.
  • the semisolid metal cooling furnace 120 for handling vessels having a diameter of more than 100 mm had to be equipped with a vessel rotating mechanism as indicated by 120X in Fig.49 or a vessel vibrator as indicated by 120Y in Fig.53.
  • a vessel rotating mechanism as indicated by 120X in Fig.49 or a vessel vibrator as indicated by 120Y in Fig.53.
  • vessels having diameters ranging from 50 mm to less than 100 mm neither the vessel rotating mechanism nor the vessel vibrator had to be installed.
  • vessel diameters of 100 mm - 200 mm a vessel vibrator as indicated by 120Y in Fig. 53 was necessary and with vessel diameters of more than 200 mm, a vessel rotating mechanism capable of more vigorous agitation as indicated by 120X in Fig. 49 had to be employed.
  • a furnace temperature controller as indicated by 120Z in Fig. 47 or 48 was installed. (With vessel diametersof less than 100 mm, the rate of cooling the slurry was so sensitive to the variations in the temperature within the furnace that it was necessary to control the temperature in the furnace by the mechanism shown in Fig.47. With vessel diameters of less than 70 mm, not only the furnace temperature controller but also a feedback control system as shown in Fig. 48 was necessary.)
  • the semisolid metal cooling furnace 120 was designed as a batch system of the type shown in Fig.46 and the timing for the transfer of the vessel into and out of the furnace 120 was controlled by the robot 180.
  • the present invention provides a method of temperature management in which the step of managing the temperature in the vessel 102 at an appropriate level before it is supplied with the molten metal is distinctly separated from the step of managing the temperature in the vessel 102 in such a way that the as poured molten metal can be cooled at a desired appropriate rate; the invention also provides the apparatus for temperature management 104 which is capable of automatic performance of these steps in an efficient and continuous manner. Also proposed by the invention is a system configuration that implements the respective steps by means of the vessel temperature control section 140 and the semisolid metal cooling section 110.
  • the vessel temperature control section 140 is composed of the vessel cooling furnace 150 capable of forced cooling with a circulating hot air flow that provides an appropriate cooling capacity by controlling the temperature and velocity of the air passing through the furnace and the vessel heat-retaining furnace 160 which controls the temperature of the atmosphere to lie at the target value in the vessel 102 and which maintains the vessel 102 at said temperature of the atmosphere. It should be noted here that the temperature to which the vessel cooling furnace 150 and the vessel heat-retaining furnace 160 should be controlled differs between aluminum and magnesium alloys.
  • the interior of the vessel cooling furnace 150 is controlled to lie between room temperature and 300 °C whereas the interior of the vessel heat-retaining furnace 160 is controlled to lie between 50 °C and 350 °C; in the case of magnesium alloys, the interior of the vessel cooling furnace 150 is controlled to lie between room temperature and 350°C whereas the interior of the vessel heat-retaining vessel 160 is controlled to lie between 200 °C and 450 °C.
  • the semisolid metal cooling section 110 is composed of the semisolid metal cooling furnace 120 which is adapted to circulate hot air at an appropriate temperature such as to accomplish cooling within the shortest possible time that produces the slurry of semisolid metal with satisfactory properties and the semisolid metal slowly cooling furnace 130 which is designed to maintain the slurry of semisolid metal for 2 - 5 minutes in a temperature range appropriate for shaping such as to be adaptive for the specific molding cycle on the molding machine 200.
  • the temperature to which the semisolid metal cooling furnace 120 should be controlled differs between aluminum and magnesium alloys. In the case ofaluminum alloys, the temperature should be controlled to lie between 150 °C and 350 °C and in the case of magnesium alloys, the temperature should be controlled to lie between 200 °C and 450 °C.
  • the interior of the semisolid metal slowly cooling furnace 130 should be controlled to be at 500 °C and above in both cases.
  • the injection sleeve 202 on the molding machine 200 is ready to accept the molten metal just at the time when the vessel 102 holding the metal has left the semisolid metal cooling furnace 120, the metal is immediately fed (poured) into the molding machine 200 without being directed into the semisolid metal slowly cooling furnace 130. Conversely, if the injection sleeve 202 is not ready to accept the molten metal since the molding machine 200 is operating, the vessel 102 leaving the semisolid metal cooling 120 is transferred to the semisolid metal annealing furnace 130.
  • a first version of the heating system in the semisolid metal cooling furnace 120 according to the invention is such that either the temperature or the velocity of the circulating hot air is controlled to vary appropriately with the lapse of time or, alternatively, both the temperature and the velocity of the hot air are controlled to vary simultaneously with the lapse of time.
  • the first specific embodiment of the heating system (furnace temperature control unit 120Z) is as shown in Fig.47 and comprises a hot air line for supplying a hot air flow into the semisolid metal cooling furnace 120, an air line from which an air flow at ordinary temperature emerges to combine with the hot air to lower its temperature, a damper for controlling the quantity of the air flowing through the air line, and a damper opening controller.
  • the second specific embodiment of the heating system is as shown in Fig.48 and comprises a temperature sensor installed within the semisolid metal cooling furnace 120, a hot air line for supplying a hot air flow into the furnace, an air line that combines with the hot air line, an automatic damper installed on the air line, and a damper opening controller that performs feedback control on the damper opening on the basis of the data obtained by measurement with the temperature sensor.
  • the opening of the automatic damper is controlled on the basis of the data for the temperature in the furnace and the hot air is mixed with an appropriate amount of air and fed into the furnace, whereby the temperature and the velocity of the circulating hot air are controlled such that the molten metal will be cooled at a desired rate.
  • Figs.1, 2, 54 and 4 - 7 concern Example 8, in which: Fig.1 is a diagram showing a process sequence for the semisolid forming of a hypoeutectic aluminum alloy having a composition at or above a maximum solubility limit; Fig.2 is adiagram showing a process sequence for the semisolid forming of a magnesium or aluminum alloy having a composition within amaximum solubility limit; Fig.
  • Fig.4 shows diagrammatically the metallographic structures obtained in the respective steps shown in Fig.54;
  • Fig.5 is an equilibrium phase diagram for an Al-Si alloy as a typical aluminum alloy system;
  • Fig.6 is an equilibrium phase diagram for a Mg-Al alloy as a typical magnesium alloy system;
  • Fig.7 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the invention;
  • Fig.8 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped according to the prior art.
  • the insulated vessel 30 for holding the molten metal the temperature of which has dropped to just below the liquidus line shall have a heat insulating effect in order to ensure that the primary crystals generated will spheroidize and have the desired fraction liquid after the passage of a specified time. Problems, however, will occur in certain cases, such as where near-eutectic Al-Si alloys and others that are prone to form skins are to be held, or where the molten metal is so heavy that it has to be held in a semisolid condition for more than 10 minutes, or where the height to diameter ratio of the insulated vessel 30 exceeds 1:2.
  • the top of the insulated vessel 30 is fitted with the heat insulating lid 42 in order to ensure against solidification from the surface of the molten metal which is being held within the insulated vessel 30, thereby enabling the metal to be cooled while providing uniformity in temperature throughout the metal.
  • the constituent material of the insulated vessel 30 and the heat-insulating lid 42 is in no way limited to metals and those which have a heat-retaining property and which yet wet with the melt only poorly are preferred. If a gas-permeable ceramic vessel is to be used as the insulated vessel 30 and the heat-insulating lid 42 for holding magnesium alloys which are easy to oxidize and burn, the exterior to the vessel is preferably filled with a specified atmosphere (e. g. an inert or vacuum atmosphere). For preventing oxidation, it is desired that Be or Ca is preliminarily added to the molten metal.
  • the shape of the insulated vessel 30 and the heat-insulating lid 42 is by no means limited to a tubular or cylindrical form and any other shapes that are suitable for the subsequent forming process maybe adopted. The molten metal need not be poured into the insulated vessel 30 but it may optionally be charged directly into the ceramic injection sleeve 40.
  • Comparative Samples 19 - 22 refer to the case of holding the molten metal without the insulating lid.
  • the insulated vessel 30 held the melt of an alloy that was prone to form a skin and, hence, a solidified layer formed over the semisolid metal, making it impossible to recover the metal from the vessel 30.
  • Comparative Sample 20 it was attempted to have the semisolid metal inserted into the injection sleeve with the molding temperature lowered; in Comparative Sample 22, the metal was unduly heavy.
  • Comparative Sample 21 the height-to-diameter ratio of the insulated vessel 30 was greater than 1:2 and, hence, the temperature profile through the semisolid metal was so poor that the result was substantially the same as with Comparative Sample 1 shown in Table 1.
  • Invention Samples 23 - 26 refer to the case of using the insulated vessel 30 fitted with the heat-insulating lid 42; they showed better results than Comparative Samples 19 - 22 in the recovery of the semisolid metal.
  • Fig. 55 is a diagram showing a process sequence for the semisolid forming of a zinc alloy of a hypoeutectic composition
  • Fig.3 shows a process flow starting with the generation of spherical primary crystals and ending with the molding step
  • Fig.4 shows diagrammatically the metallographic structures obtained in the respective steps shown in Fig.3
  • Fig. 56 is an equilibrium phase diagram for a binary Zn-Al alloy as a typical zinc alloy system
  • Fig.57 is adiagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the invention
  • Fig.58 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the prior art.
  • the first step of the process according to the invention comprises:
  • the cooled molten alloy prepared in (1) is poured into an insulated vessel having a heat insulating effect and, in the case of (2), the melt is directly poured into the insulated vessel without being cooled with a jig.
  • the melt is held within the insulated vessel for a period from 5 seconds to 60 minutes at a temperature not higher than the liquidus temperature but higher than the eutectic or solidus temperature, whereby a large number of fine spherical primary crystals are generated in the alloy, which is then shaped at aspecified liquid fraction.
  • a specified fraction liquid means a relative proportion of the liquid phase which is suitable for pressure forming.
  • the fraction liquid ranges from 20 % to 90 %, preferably from 30 % to 70 %. If the fraction liquid is less than 30 %, the formability of the raw material is poor; above 70 %, the raw material is so soft that it is not only difficult to handle but also less likely to produce a homogeneous micro-structure.
  • the fraction liquid ranges from 0.1 % to 70 %, preferably from 0.1 % to 50 %, beyond which an inhomogeneous structure can potentially occur.
  • the "insulated vessel” as used in the invention is a metallic or nonmetallic vessel, or a metallic vessel having a surface coated with a nonmetallic material or a semiconductor, or a metallic vessel compounded of a nonmetallic material or semiconductor, which vessels are adapted to be either heatable or coolable from either inside or outside.
  • Example 9 The specific procedure of semisolid metal forming to be erformed in Example 9 is essentially the same as described in Example 1.
  • the degree of superheating is adjusted to less than 100 °C above the liquidus line in order to ensure that the alloy poured into the insulated vessel 30 having a heat-insulating effect is rendered either liquid to have crystal nuclei or partially solid, partially liquid to have crystal nuclei at a temperature equal to or higher than the molding temperature. If the temperature of the melt as poured into the insulated vessel 30 is unduly high, the crystal nuclei once generated will dissolve again or coarse primary crystals will form and, in either case, it is impossible to produce the desired semisolid structure. In addition, so much time will be taken for the temperature of the melt to decrease to establish a specified fraction liquid that the operating efficiency becomes low. Another inconvenience is that the poured melt M is oxidized or burnt at the surface.
  • Table 5 shows the conditions of various samples of semisolid metal to be shaped, as well as the qualities of shaped parts.
  • the shaping operation consisted of inserting the semisolid metal into an injection sleeve and subsequent forming on a squeeze casting machine.
  • the forming conditions were as follows: pressure, 950 kgf/cm 2 ; injection speed, 1.0 m/s; mold temperature, 200 °C.
  • the product shaped parts were flat plates 100 mm wide and 200 mm long, with the thickness varying at 2 mm, 5 mm and 10 mm in the longitudinal direction.
  • Comparative Sample 9 the temperature of jig 20 with which the melt M was contacted was so high that the number of crystal nuclei generated was insufficient to produce fine spherical primary crystals; instead, coarse unspherical primary crystals formed.
  • the casting temperature was so high that very few crystal nuclei remained within the ceramic vessel 30, yielding the same result as with Comparative Sample 9.
  • the holding time was so long that the fraction liquid in the metal to be shaped was low, yielding a shaped part of poor appearance.
  • the size of primary crystals was undesirably large.
  • Comparative Sample 12 the holding time within the ceramic vessel 30 was short whereas the fraction liquid in the metal to be shaped was high; hence, many segregations of components occurred within the shaped part as shown in Fig.58.
  • the insulated vessel 30 was a metallic container having a very small heat insulating effect, so the dendritic solidified layer forming on the inner surface of the vessel 30 would enter the spherical primary crystals generated in the central part of the vessel, yielding an inhomogeneous structure involving segregations.
  • Fig. 59 is a diagram showing a processsequence for the semisolid forming of a hypereutectic Al-Si alloy starting with the preparation of a semisolid metal and ending with the molding step
  • Fig.60 is a diagram showing a process flow starting with the generation of very fine primary Si crystals and ending with the molding step
  • Fig.61 shows diagrammatically the metallographic structures obtained in the respective steps shown in Fig.60
  • Fig.62 is an equilibrium phase diagram for a binary Al-Si alloy
  • Fig. 59 is a diagram showing a processsequence for the semisolid forming of a hypereutectic Al-Si alloy starting with the preparation of a semisolid metal and ending with the molding step
  • Fig.60 is a diagram showing a process flow starting with the generation of very fine primary Si crystals and ending with the molding step
  • Fig.61 shows diagrammatically the metallographic structures obtained in the respective steps shown in Fig.60
  • Fig.62 is an equilibrium phase diagram for
  • Fig.64 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the prior art.
  • the process of the invention starts with superheating the melt of a hypereutectic Al-Si alloy to less than 300°C above the liquidus line.
  • the thus superheated alloy is contacted with a jig at lower temperaturethan its melting point so as to generate crystal nuclei within the alloy solution; the alloy is then cooled in an insulated vessel until a specified fraction liquid is established, with it being held either at a temperature between the liquidus and eutectic temperatures or at the eutectic temperature for a period from 5 seconds to 60 minutes, thereby generating a large number of fine primary crystals.
  • the hypereutectic Al-Si alloy permits only a small amount of primary crystals to be crystallized and, hence, it has high fraction liquid in a semisolid condition at temperatures exceeding the eutectic point. Therefore, if the desired fraction liquid is low, the alloy which has been heated to its eutectic temperature has to be held at that temperature for a sufficient time to allow for the progress of solidification (eutectic reaction).
  • step (1) of the process shown in Figs. 60 and 61 a complete liquid form of metal M is contained in a ladle 10.
  • step (2) the metalis cooled with a jig 20 to generate crystal nuclei and the melt is then poured into a ceramic vessel 30 (or ceramics-coated vessel 30A) having a heat insulating effect so as to produce an alloy having a large number of crystal nuclei which is of a composition just below the liquidus line.
  • step (3) the alloy is held partially molten within the insulated vessel 30 (or 30A).
  • very-fine primary Si crystals result from the introduced crystal nuclei [step (3)-a] and grow into granules together with the surrounding primary ⁇ as the fraction solid increases.
  • Metal M thus obtained at a specified fraction liquid maybe inserted into a die casting injection sleeve 40 [step (3)-b] and thereafter pressure formed within a mold cavity 50a in a die casting machine to produce a shaped part (step (4)].
  • the semisolid metal forming process of the invention shown in Figs. 59, 60 and 61 has obvious differences from the conventional thixocasting and rheocasting methods.
  • the primary crystals that have been crystallized within a temperature range for the semisolid state are not ground into spherical grains by mechanical or electromagnetic agitation as in the prior art but the large number of primary crystals that have been crystallized and grown from the introduced crystal nuclei with the decreasing temperature in the range for the semisolid state and with the lapse of the time of holding at the eutectic point are continuously rendered granular by the heat of the alloy itself (which may optionally be supplied with external heat and held at a desired temperature).
  • the semisolid metal forming method of the invention is very convenient since it does not involve the step of partially melting billets by reheating in the thixocasting process.
  • the casting temperature is at least 300 °C higher than the melting point or if the surface temperature of jig 20 is not lower than the melting point, the following phenomena will occur:
  • the casting temperature to be employed in the invention is controlled to be such that the degree of superheating above the liquidus line is less than 300 °C whereas the surface temperature of jig 20 is controlled to be lower than the melting point of alloy M.
  • Primary crystals of an even finer size can be produced by ensuring that the degree of superheating above the liquidus line is less than 100 °C and by adjusting the surface temperature of jig 20 to be at least 50 °C lower than the melting point of alloy M.
  • the molten metal should be superheated to at least 30 °C above the liquidus line; if the temperature of the melt is unduly low, the grains of AlP serving as a refiner will agglomerate to become no longer effective.
  • either Sr or Na or both are added. If the P addition is less than 0.005 %, it is not very effective in refining the primary Si crystals; the effect of P is saturated at 0.03 % and no further improvement is expected beyond 0.03 %. Hence, the P addition is controlled to lie between 0.005 % and 0.03 %. If the Sr addition is less than 0.005 %, it is not very effective in modifying the eutectic Si structures; beyond 0.03 %, an Al-Si-Sr compound will crystalize out to cause deterioration in the mechanical properties of the alloy.
  • the Sr addition is controlled to lie between 0.005 % and 0.03%. If the Na addition is less than 0.001 %, it is not very effective in modifying the eutectic Si structures; beyond 0.01 %, coarse eutectic Si grains will form. Hence, the Na addition is controlled to lie between 0.001 % and 0.01 %.
  • Table 6 sets forth the conditions for the preparation of semisolid metal samples and the results of evaluation of their metallographic structures by microscopic examination.
  • Comparative Sample 7 the temperature of jig 20 with which the melt M was contacted was so high that the number of crystal nuclei generated was insufficient to produce fine primary crystals; instead, coarse primary crystals formed.
  • Comparative Sample 8 the casting temperature was so high that very few crystal nuclei remained within the ceramic vessel 30, yielding the same result as with Comparative Sample 7.
  • Comparative Sample 9 the holding time was so long that the fraction liquid in the metal to be shaped was low, making the alloy unsuitable for shaping. In addition, the size of primary crystals was undesirably large.
  • Comparative Sample 10 the holding time within the ceramic vessel 30 was short whereas the fraction liquid in the metal to be shaped was high; hence, many segregations of components occurred within the shaped part.
  • Comparative Sample 11 solidification occurred within the insulated vessel and many coarse primary crystals were generated in the form of a rectangular rod (see Fig. 64).
  • Fig.1 is a diagram showing a process sequence for the semisolid forming of an Al-Mg alloy
  • Fig.3 shows a process flow starting with the generation of granular primary crystals and ending with the molding step
  • Fig.4 shows diagrammatically the metallogrphic structures obtained in the respective steps shown in Fig.3
  • Fig.65 is an equilibrium phase diagram for a binary Al-Mg alloy
  • Fig.66 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the invention
  • Fig.67 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the prior art.
  • the poured metal is held within the insulated vessel at a temperature not higher than the liquidus temperature but higher than the eutectic or solidus temperature for a period from 5 seconds to 60 minutes until a specified liquid fractionis established, whereby a large number of fine granular primary crystals are generated to produce a semisolid Al-Mg alloy at the specified fraction liquid.
  • Example 11 The specific procedure of semisolid metal forming to be performed in Example 11 is essentially the same as described in Example 1.
  • Si Silicon
  • Si is added in order to promote the spheroidization of the generated granular primary crystals. If the Si addition is less than 0.3 %, the intended effect in promoting the spheroidization is not expected; adding more than 2.5 % of Si will merely result in deteriorated properties of the alloy and no further improvement in spheroidization is expected. Hence, the Si addition is controlled to lie between0.3 % and 2.5 %.
  • the Al-Mg alloy of the invention may incorporate up to 1 % of Mn or up to 0.5 % of Cu with a view to improving its strength.
  • Table 7 sets forth the conditions for the preparation of semisolid metal samples and the results of evaluation of their metallorgraphic structures by microscopic examination.
  • Comparative Sample 9 the temperature of jig 20 with which the melt M was contacted was so high that the number of crystal nuclei generated was insufficient to produce fine primary crystals; instead, coarse primary crystals formed.
  • Comparative Sample 10 the casting temperature was so high that very few crystal nuclei remained within the ceramic vessel 30, yielding the same result as with Comparative Sample 9.
  • Comparative Sample 11 the holding time was so long that the fraction liquid in the metal to be shaped was low, making the alloy unsuitable for shaping. In addition, the size of primary crystals was undesirably large.
  • Comparative Sample 12 the holding time within the ceramic vessel 30 was short whereas the fraction liquid in the metal to be shaped was high; hence, only coarse primary crystals formed.
  • Fig.1 is a diagram showing a process for the semisolid forming of a hypoeutectic aluminum alloy having a composition at or above a maximum solubility limit
  • Fig.2 is a diagram showing a process sequence for the semisolid forming of a magnesium or aluminum alloy having a composition within a maximum solubility limit
  • Fig.68 shows a process flow starting with the generation of spherical primary crystals and ending with the molding step
  • Fig.4 shows diagrammatically the metallographic structures obtained in the respective steps shown in Fig.68
  • Fig.5 is an equilibrium phase diagram for an Al-Si alloy as a typical aluminum alloy system
  • Fig.6 is an equilibrium phase diagram for a Mg-Al alloy as a typical magnesium alloy system
  • Fig.7 is a diagrammatic representation of a micrograph showing the metallographic structure of a
  • the invention recited in claims 34 and 35 comprises the following: the melt of a hypoeutectic aluminum alloy having a composition at or above a maximum solubility limit or the melt of a magnesium or aluminum alloy having a composition within a maximum solubility limit is held superheated to less than 300 °C above the liquidus temperature; either melt is contacted with a surface of a jig at a lower temperature than its melting point, thereby generating crystal nuclei in the alloy solution; the melt is then poured into an insulated vessel having a heat insulating effect, in which vessel the melt is held at a temperature not higher than the liquidus line but higher than the eutectic or solidus temperature for a period from 5 seconds to 60 minutes, whereby a large number of fine spherical primary crystals are generated in the melt, which is subsequently shaped at a specified fraction liquid.
  • the "specified fraction liquid” ranges from 0.1 % to 70 %, preferably from 10 % to 70 %.
  • insulated vessel refers to either a metallic or nonmetallic vessel or a metallic vessel either composited or coated with a nonmetallic material, which vessels are adapted to be heatable or coolable from either inside or outside.
  • step (1) of the process shown in Figs.68 and 4 a complete liquid form of metal M is contained in a ladle 10.
  • step (2) the metal is cooled with a jig 20 to generate crystal nuclei from the low-temperature melt (which may optionally contain an element that is added to promote the generation of crystal nuclei) and the metal is then poured into a ceramic vessel 30 having a heat insulating effect, thereby producing an alloy of a composition just below the liquidus line which has a large number of crystal nuclei.
  • step (3) the alloy is held partially molten within the insulated vessel 30 (or 30A).
  • the semisolid metal M in the insulated vessel 30 maybe inserted into the container 82 on the extruding machine 80 by accommodating it into the container 82 in such a way that the part of it which faces the bottom of the insulated vessel 30 and which has a comparatively small portion of the impurities is directed toward the die 84; upon extrusion through the die, one can obtain a shaped part of high quality which has only a small impurity content.
  • the surface (top surface) of the semisolid metal M may be freed of the oxide before it is recovered from the insulated vessel 30 and the thus cleaned semisolid metal is charged into the container 82 on the extruding machine 80.
  • the casting, spheroidizing and molding conditions that are respectively set for the steps shown in Fig. 68, namely, the step of pouring the molten metal on to the cooling jig 20,the step of generating and spheroidizing primary crystals and the forming step are the same as set forth in Example 1.
  • Table 8 sets forth the conditions for the preparation of semisolid metal samples and the qualities of shaped parts.
  • the forming step consisted of inserting the semisolid metal into the container and extruding the same.
  • the extruding conditions were as follows: extruding machine, 800 t; extruding rate, 80 m/min; billet diameter,75 mm; extrustion ratio, 20.
  • Comparative Sample 2 the casting temperature was so high that very few crystal nuclei remained within the ceramic vessel 30, yielding the same result as with Comparative Sample 1.
  • Comparative Sample 3 the holding time was so long that the fraction liquid in the metal to be shaped was low, yielding a shaped part of poor appearance. In addition, the size of primary crystals was undesirably large.
  • Comparative Sample 4 the holding time within the ceramic vessel 30 was short whereas the fraction liquid in the metal to be shaped was high; hence, only dendritic primary crystals formed. In addition, the high fraction liquid caused many segregations of components within the shaped part.
  • the insulated vessel 30 was a metallic container having a small heat insulating effect, so the dendritic solidified layer forming on the inner surface of the vessel 30 would enter the spherical primary crystals generated in the central part of the vessel, yielding an inhomogeneous structure involving segregations.
  • Comparative Sample 6 the fraction liquid in the metal to be shaped was so high that result was the same as with Comparative Sample 4.
  • Comparative Sample 7 the jig 20 was not used; the starting alloy did not contain any grain refiners, so the number of crystal nuclei generated was small enough to yield the same result as with Comparative Sample 1.
  • Fig. 69 shows two process sequences for the semisolid forming of a hypoeutectic aluminum alloy
  • Fig.70 shows a process flow starting with the generation of spherical primary crystals and ending with the molding step
  • Fig.71 shows diagrammatically the metallographic structures obtained in the respective steps shown in Fig.70
  • Fig.72 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the invention
  • Fig.73 is a diagrammatic representation of a micrograph showing the metallographic structure of a shaped part according to the prior art.
  • the invention concerns a process which starts with either one of the following steps:
  • Either of the metals thus obtained is held within the insulated vessel for a period from 5 seconds to 60 minutes as it is cooled to a molding temperature where a specified fraction liquid is established, whereby the fine grains that have formed within the alloy solution are crystallized out as no dendrites, and the metal is then fed into a mold, where it is subjected to pressure forming.
  • semisolid metal forming will proceed by the following specific procedure.
  • step (1) of the process shown in Figs.70 and 71 two complete liquid forms of metals MA and MB are contained in ladles 10 and poured into a ceramic container 30 (or ceramic-coated metal container30A) which is an insulated vessel having a heat insulating effect.
  • a ceramic container 30 or ceramic-coated metal container30A
  • an alloy having a large number of crystal nuclei is obtained at a temperature either just below or above the liquidus line.
  • Molten metals MA and MB may be poured either simultaneously or successively with one coming after the other.
  • molten metals MA and MB may be poured into partitioned compartments in the insulated vessel 30 and the partition is removed all of a sudden so as to achieve mutual contact between the two metals.
  • either molten metal MA or MB or both may be preliminarily contacted with a cooling jig 20 so as to have a number of crystal nuclei generated in the metal or metals and this is effective for the purpose of producing a large number of crystals [step (1A) in Fig.70].
  • step (2) the alloy mixture MC is held partially molten within the insulated vessel 30.
  • step (2)-a extremely fine primary crystals result from the introduced crystal nuclei [step (2)-a] and grow into spherical primary crystals as the fraction solid increases with the decreasing temperature of the alloy mixture MC [steps (2)-b and (2)-c].
  • Alloy mixture MC thus obtained at a specified fraction liquid is inserted into an injection sleeve 40 [step (2)-d] and, thereafter, pressure formed within a mold cavity 50a on a die casting machine to produce a shaped part [step (3)].
  • the semisolid metal forming process of the invention shown in Figs.69, 70 and 71 has obvious differences from the conventional thixocasting and rheocasting methods.
  • the temperature of either metal just after the mixing will neither be just above or below the liquidus temperature of the alloy mixture MC to be eventually formed. If the mixed metals are held within the insulated vessel 30, amicrostructure consisting of coarse dendrites will form rather than a structure of uniform, near-spherical nondendritic crystals. To avoid these problems, the temperatures of, molten (liquid) metals MA and MB to be mixed need be superheated to no more than 50 °C above the liquidus temperature.
  • the "temperature either just above or below the liquidus temperature of the metal mixture to be eventually formed” means a temperature within the liquidus temperature ⁇ 15°C.
  • the liquid metals to be mixed shall include alloys.
  • the insulated vessel 30 for holding the metals the temperature of which have dropped to be within the defined range after the mixing shall have a heat insulating effect in order to ensure that the crystal nuclei generated will grow into nondendritic (near-spherical) primary crystals and have the desired fraction liquid after a specified time.
  • the constituent material of the insulated vessel is in no way limited to metals and those which have a heat-retaining property and which yet wet with the melt only poorly are preferred.
  • the exterior to the vessel is preferably filled with a specified atmosphere (e. g. an inert or vacuum atmosphere).
  • a specified atmosphere e. g. an inert or vacuum atmosphere
  • the holding time within the insulated vessel is less than 5 seconds, it is not easy to attain the temperature for the desired fraction liquid and it is also difficult to generate spherical primary crystals. What is more, semisolid metals of a uniform temperature profile cannot be attained. If the holding time exceeds 60 minutes, coarse spherical primary crystals will be generated.
  • the fraction liquid in the alloy which is about to be shaped by high-pressure casting is less than 20 %, the resistance to deformation during the shaping is so high that it is not easy to produce shaped parts of good quality. If the fraction liquid exceeds 90 %, shaped parts having a homogeneous structure cannot be obtained. Therefore, as already mentioned, the fraction liquid in the alloy to be shaped is preferably controlled to lie between 20 % and 90 %. More preferably, the fraction liquid should be adjusted to range between 30 % and 70 % in order to ensure that shaped parts of high quality can easily be produced by pressure forming.
  • the means of pressure forming are in no way limited to high-pressure casting processes typified by squeeze casting and die casting and various other method of pressure forming may be adopted, such as extruding and casting operations.
  • the Ti and B may be added to the alloys. If the Ti content of the alloy mixture is less than 0.003 %, the intended refining effect of Ti is not attained; beyond 0.30 %, a coarse Ti compound will form to cause deterioration in ductility. Hence, the Ti addition is controlled to lie between 0.003 % and 0.30 %.
  • Boron (B) in the mixed metal MC cooperates with Ti to promote the refining of crystal grains but its refining effect is small if the addition is less than 0.0005 %; on the other hand, the effect of B is saturated at 0.01 % and no further improvement is expected beyond 0.01 %. Hence, the B addition is controlled to lie between 0.0005 % and 0.01 %.
  • the constituent material of the jig 20 having the cooling zone with which the molten metals MA and MB are to be contacted before they are mixed is not limited to any particular types as long as it is capable of lowering the temperatures of the melts.
  • a jig that is made of a highly heat-conductive metal such as copper, a copper alloy, aluminum or an aluminum alloy and which is controlled to provide a cooling effect for maintaining temperatures below a specified level is particularly preferred since it allows for the generation of many crystal nuclei.
  • the molten alloys held superheated to less than 300°C above the solidus temperatures are desirably contacted with a surface of the jig at a lower temperature than the melting points of said alloys.
  • the degree of superheating above the liquidus temperatures lie less than 100°C, more preferably less than 50°C.
  • Table 9 sets forth the conditions for the preparation of semisolid samples and the qualities of shaped parts.
  • the shaping operation consisted of inserting the semisolid metal into an injection sleeve and subsequent forming on a squeeze casting machine.
  • the forming conditions were as follows: pressure, 950 kgf/cm 2 ; injection speed, 1.5m/s; mold cavity dimensions, 100 x 150 x 10; mold temperature, 230 °C.
  • Comparative Sample 9 the holding time was so long that undesirably large primary crystals formed.
  • Comparative Sample 10 the temperatures of the alloys to be mixed were high and so was the temperature of the resulting mixture; hence, the number of the crystal nuclei generated was small enough to produce only dendritic primary crystals.
  • Comparative Sample 11 the holding time was short whereas the liquid fraction in the alloy mixture was high and this caused extensive segregations in the interior of the sharped part.
  • the shaping operation consisted of inserting the semisolid metal into an injection sleeve and subsequent forming on a squeeze casting machine.
  • the forming conditions were as follows: pressure, 950 kgf/cm 2 ; injection speed, 1.5 m/s; mold cavity dimensions, 100 x 150 x 10; mold temperature, 230°C.
  • Table 10 shows how the quality of shaped parts was affected by the presence or absence of the oxide. Obviously, Invention Samples 23 - 26 had better results than Comparative Samples 21 and 22.
EP96108499A 1995-05-29 1996-05-29 Procédé et dispositif pour mettre des métaux semi-solides en forme Expired - Lifetime EP0745694B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP02028272A EP1331279A3 (fr) 1995-05-29 1996-05-29 Procédé et dispositif pour mettre des métaux semi-solides en forme

Applications Claiming Priority (42)

Application Number Priority Date Filing Date Title
JP13013495A JP3246273B2 (ja) 1995-05-29 1995-05-29 半溶融金属の成形方法
JP13013495 1995-05-29
JP130134/95 1995-05-29
JP160890/95 1995-06-27
JP16089095 1995-06-27
JP7160890A JPH0910893A (ja) 1995-06-27 1995-06-27 半溶融成形用金属の製造装置
JP23650195 1995-09-14
JP236501/95 1995-09-14
JP7236501A JPH0976051A (ja) 1995-09-14 1995-09-14 半溶融金属の成形方法
JP24410995 1995-09-22
JP24411195 1995-09-22
JP244109/95 1995-09-22
JP7244111A JPH0987768A (ja) 1995-09-22 1995-09-22 半溶融過共晶Al−Si合金の製造方法
JP7244109A JPH0987767A (ja) 1995-09-22 1995-09-22 半溶融亜鉛合金の成形方法
JP244111/95 1995-09-22
JP24789795 1995-09-26
JP247897/95 1995-09-26
JP24789795A JP3473214B2 (ja) 1995-09-26 1995-09-26 半溶融金属の成形方法
JP7249482A JPH0987770A (ja) 1995-09-27 1995-09-27 半溶融金属の成形方法
JP249482/95 1995-09-27
JP24948295 1995-09-27
JP25276295 1995-09-29
JP252768/95 1995-09-29
JP252762/95 1995-09-29
JP7252769A JPH0987773A (ja) 1995-09-29 1995-09-29 半溶融金属の成形方法
JP7252762A JPH0987771A (ja) 1995-09-29 1995-09-29 半溶融Al−Mg合金の製造方法
JP252769/95 1995-09-29
JP25276895A JP3473216B2 (ja) 1995-09-29 1995-09-29 半溶融金属の成形方法
JP25276895 1995-09-29
JP29076095 1995-11-09
JP29076095A JP3246296B2 (ja) 1995-11-09 1995-11-09 半溶融金属の成形方法
JP290760/95 1995-11-09
JP32065095A JP3536491B2 (ja) 1995-12-08 1995-12-08 半溶融金属スラリの温度管理方法および温度管理装置
JP320650/95 1995-12-08
JP32065095 1995-12-08
JP33295595A JP3669388B2 (ja) 1995-12-21 1995-12-21 半溶融金属スラリの温度管理装置
JP33295595 1995-12-21
JP332955/95 1995-12-21
JP25276995 1996-04-10
JP8784896 1996-04-10
JP08784896A JP3783275B2 (ja) 1996-04-10 1996-04-10 半溶融金属の成形方法
JP87848/96 1996-04-10

Related Child Applications (1)

Application Number Title Priority Date Filing Date
EP02028272.9 Division-Into 2002-12-16

Publications (2)

Publication Number Publication Date
EP0745694A1 true EP0745694A1 (fr) 1996-12-04
EP0745694B1 EP0745694B1 (fr) 2004-12-08

Family

ID=27584868

Family Applications (2)

Application Number Title Priority Date Filing Date
EP96108499A Expired - Lifetime EP0745694B1 (fr) 1995-05-29 1996-05-29 Procédé et dispositif pour mettre des métaux semi-solides en forme
EP02028272A Withdrawn EP1331279A3 (fr) 1995-05-29 1996-05-29 Procédé et dispositif pour mettre des métaux semi-solides en forme

Family Applications After (1)

Application Number Title Priority Date Filing Date
EP02028272A Withdrawn EP1331279A3 (fr) 1995-05-29 1996-05-29 Procédé et dispositif pour mettre des métaux semi-solides en forme

Country Status (2)

Country Link
EP (2) EP0745694B1 (fr)
CA (1) CA2177455C (fr)

Cited By (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0841406A1 (fr) * 1996-11-08 1998-05-13 Ube Industries, Ltd. Procédé pour mettre des métaux semi-solides en forme
EP0908527A1 (fr) * 1997-10-08 1999-04-14 ALUMINIUM RHEINFELDEN GmbH Alliage de coulée à base d'aluminium
EP0911420A1 (fr) * 1997-10-08 1999-04-28 ALUMINIUM RHEINFELDEN GmbH Alliage de coulée à base d'aluminium
EP0931607A1 (fr) * 1997-12-20 1999-07-28 Ahresty Corporation Procédé de production d'un métal en phase pâteuse
EP1132162A1 (fr) * 2000-03-08 2001-09-12 Tetsuichi Motegi Procédé et dispositif pour la coulée de métal
DE10043717A1 (de) * 2000-09-04 2002-03-14 Buehler Druckguss Ag Uzwil Verfahren und Vorrichtung zum Druckumformen von metallischen Werkstoffen
DE10044630A1 (de) * 2000-09-09 2002-03-21 Alu Menziken Ind Ag Menziken Verfahren zum Herstellen von Metall mit thixotropem Verhalten und Vorrichtung zur Durchführung des Verfahrens
US6399017B1 (en) 2000-06-01 2002-06-04 Aemp Corporation Method and apparatus for containing and ejecting a thixotropic metal slurry
US6402367B1 (en) 2000-06-01 2002-06-11 Aemp Corporation Method and apparatus for magnetically stirring a thixotropic metal slurry
DE10100632A1 (de) * 2001-01-09 2002-07-11 Rauch Fertigungstech Gmbh Verfahren zum Bereitstellen einer teilerstarrten Legierungssuspension und Verrichtungen
US6428636B2 (en) 1999-07-26 2002-08-06 Alcan International, Ltd. Semi-solid concentration processing of metallic alloys
US6432160B1 (en) 2000-06-01 2002-08-13 Aemp Corporation Method and apparatus for making a thixotropic metal slurry
WO2003015959A1 (fr) * 2001-08-17 2003-02-27 Innovative Products Group, Llc Appareil et procede de production d'une boue sans brassage pour une application dans le formage semi-solide
US6544469B2 (en) 1999-12-16 2003-04-08 Honda Giken Kogyo Kabushiki Kaisha Apparatus and method for producing metal formed product
US6547896B2 (en) 1999-07-28 2003-04-15 Ruag Munition Process for the production of a material made of a metal alloy
US6611736B1 (en) 2000-07-01 2003-08-26 Aemp Corporation Equal order method for fluid flow simulation
EP1358956A1 (fr) * 2002-04-24 2003-11-05 Alcan Technology & Management Ltd. Procédé de traitement d'un alliage métallique pour l'obtention d'un article semi solide
EP1405684A2 (fr) * 2002-09-25 2004-04-07 Chunpyo Hong Matériaux métalliques pour la coulée d'après le procédé Rheocast ou le thixoformage et procédé pour leur fabrication
WO2004031423A2 (fr) * 2002-09-23 2004-04-15 Worcester Polytechnic Institute Alliage sensiblement exempt de dendrites et procede permettant de former cet alliage
US6796362B2 (en) 2000-06-01 2004-09-28 Brunswick Corporation Apparatus for producing a metallic slurry material for use in semi-solid forming of shaped parts
US6845809B1 (en) 1999-02-17 2005-01-25 Aemp Corporation Apparatus for and method of producing on-demand semi-solid material for castings
US6918427B2 (en) 2003-03-04 2005-07-19 Idraprince, Inc. Process and apparatus for preparing a metal alloy
US7024342B1 (en) 2000-07-01 2006-04-04 Mercury Marine Thermal flow simulation for casting/molding processes
US7051784B2 (en) * 1997-07-24 2006-05-30 Ahresty Corp. Method of producing semi-solid metal slurries
CN100346904C (zh) * 2003-03-04 2007-11-07 伊德拉王子公司 由液态金属合金成分生产金属部件的方法
CN102069158A (zh) * 2011-01-11 2011-05-25 大连理工大学 半固态浆料制备所用斜槽的涂层及其喷涂方法
WO2011097479A2 (fr) * 2010-02-05 2011-08-11 Thixomat, Inc. Procédé et appareil permettant de former un matériau forgé doté d'une fine structure des grains
CN103302265A (zh) * 2013-06-17 2013-09-18 昆明理工大学 一种过共晶铝硅合金管材的制备方法
CN104550888A (zh) * 2015-01-30 2015-04-29 林荣英 一种可连续生产金属半固态浆体的方法
CN107214311A (zh) * 2016-03-22 2017-09-29 焦作市合鑫机械有限公司 一种振动结晶器
CN107457373A (zh) * 2017-08-28 2017-12-12 广东工业大学 一种制备半固态浆料的装置及其实现方法
EP3360623A4 (fr) * 2016-04-08 2019-03-27 Zhuhai Runxingtai Electrical Co., Ltd Procédé et système de production semi-solide utilisant une technique de coulée sous pression continue

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2590432C2 (ru) * 2014-11-18 2016-07-10 Российская Федерация от имени которой выступает Министерство промышленности и торговли Российской Федерации Способ и устройство для изготовления тиксозаготовок
CN105149869B (zh) * 2015-07-30 2017-07-14 西安交通大学 内燃机用高压共轨管的楔横轧式应变诱发半固态模锻工艺
CN108015255B (zh) * 2017-12-08 2020-04-28 东北大学 一种高速工具钢的制备方法

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61235047A (ja) * 1985-04-11 1986-10-20 Nippon Kokan Kk <Nkk> 微細な結晶粒を有する金属の鋳造法
EP0392998A1 (fr) * 1989-04-14 1990-10-17 Giovanni Crosti Procédé pour la fabrication d'alliages d'aluminium, coulés à l'état semi-liquide
WO1992013662A1 (fr) * 1991-01-30 1992-08-20 Transvalor S.A. Procede de moulage d'un lingot d'alliage a structure dendritique fine et machine de moulage suivant ce procede
JPH05169227A (ja) * 1991-12-17 1993-07-09 Ube Ind Ltd 高圧鋳造製品の製造方法
EP0701002A1 (fr) * 1994-09-09 1996-03-13 Ube Industries, Ltd. Procédé de fabrication d'alliages d'aluminium ou de magnésium à l'état semi-solide
EP0719606A1 (fr) * 1994-12-28 1996-07-03 Ahresty Corporation Procédé de production d'un métal en phase pâteuse pour couler

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61235047A (ja) * 1985-04-11 1986-10-20 Nippon Kokan Kk <Nkk> 微細な結晶粒を有する金属の鋳造法
EP0392998A1 (fr) * 1989-04-14 1990-10-17 Giovanni Crosti Procédé pour la fabrication d'alliages d'aluminium, coulés à l'état semi-liquide
WO1992013662A1 (fr) * 1991-01-30 1992-08-20 Transvalor S.A. Procede de moulage d'un lingot d'alliage a structure dendritique fine et machine de moulage suivant ce procede
JPH05169227A (ja) * 1991-12-17 1993-07-09 Ube Ind Ltd 高圧鋳造製品の製造方法
EP0701002A1 (fr) * 1994-09-09 1996-03-13 Ube Industries, Ltd. Procédé de fabrication d'alliages d'aluminium ou de magnésium à l'état semi-solide
EP0719606A1 (fr) * 1994-12-28 1996-07-03 Ahresty Corporation Procédé de production d'un métal en phase pâteuse pour couler

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
PATENT ABSTRACTS OF JAPAN vol. 011, no. 078 (M - 570) 10 March 1987 (1987-03-10) *
PATENT ABSTRACTS OF JAPAN vol. 017, no. 574 (M - 1498) 19 October 1993 (1993-10-19) *

Cited By (52)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0841406A1 (fr) * 1996-11-08 1998-05-13 Ube Industries, Ltd. Procédé pour mettre des métaux semi-solides en forme
US7051784B2 (en) * 1997-07-24 2006-05-30 Ahresty Corp. Method of producing semi-solid metal slurries
EP0908527A1 (fr) * 1997-10-08 1999-04-14 ALUMINIUM RHEINFELDEN GmbH Alliage de coulée à base d'aluminium
EP0911420A1 (fr) * 1997-10-08 1999-04-28 ALUMINIUM RHEINFELDEN GmbH Alliage de coulée à base d'aluminium
US6309481B1 (en) 1997-10-08 2001-10-30 Aluminium Rheinfelden, Gmbh Aluminum casting alloy
EP0931607A1 (fr) * 1997-12-20 1999-07-28 Ahresty Corporation Procédé de production d'un métal en phase pâteuse
US6845809B1 (en) 1999-02-17 2005-01-25 Aemp Corporation Apparatus for and method of producing on-demand semi-solid material for castings
US6428636B2 (en) 1999-07-26 2002-08-06 Alcan International, Ltd. Semi-solid concentration processing of metallic alloys
US7140419B2 (en) 1999-07-26 2006-11-28 Alcan Internatinoal Limited Semi-solid concentration processing of metallic alloys
US6547896B2 (en) 1999-07-28 2003-04-15 Ruag Munition Process for the production of a material made of a metal alloy
US6544469B2 (en) 1999-12-16 2003-04-08 Honda Giken Kogyo Kabushiki Kaisha Apparatus and method for producing metal formed product
DE10062248B4 (de) * 1999-12-16 2005-06-16 Honda Giken Kogyo K.K. Vorrichtung und Verfahren zum Erzeugen eines Metallformteils
EP1132162A1 (fr) * 2000-03-08 2001-09-12 Tetsuichi Motegi Procédé et dispositif pour la coulée de métal
US6399017B1 (en) 2000-06-01 2002-06-04 Aemp Corporation Method and apparatus for containing and ejecting a thixotropic metal slurry
US6991670B2 (en) 2000-06-01 2006-01-31 Brunswick Corporation Method and apparatus for making a thixotropic metal slurry
US6796362B2 (en) 2000-06-01 2004-09-28 Brunswick Corporation Apparatus for producing a metallic slurry material for use in semi-solid forming of shaped parts
US6637927B2 (en) 2000-06-01 2003-10-28 Innovative Products Group, Llc Method and apparatus for magnetically stirring a thixotropic metal slurry
US6932938B2 (en) 2000-06-01 2005-08-23 Mercury Marine Method and apparatus for containing and ejecting a thixotropic metal slurry
US6432160B1 (en) 2000-06-01 2002-08-13 Aemp Corporation Method and apparatus for making a thixotropic metal slurry
US6402367B1 (en) 2000-06-01 2002-06-11 Aemp Corporation Method and apparatus for magnetically stirring a thixotropic metal slurry
US6611736B1 (en) 2000-07-01 2003-08-26 Aemp Corporation Equal order method for fluid flow simulation
US7024342B1 (en) 2000-07-01 2006-04-04 Mercury Marine Thermal flow simulation for casting/molding processes
DE10043717A1 (de) * 2000-09-04 2002-03-14 Buehler Druckguss Ag Uzwil Verfahren und Vorrichtung zum Druckumformen von metallischen Werkstoffen
DE10044630A1 (de) * 2000-09-09 2002-03-21 Alu Menziken Ind Ag Menziken Verfahren zum Herstellen von Metall mit thixotropem Verhalten und Vorrichtung zur Durchführung des Verfahrens
DE10100632A1 (de) * 2001-01-09 2002-07-11 Rauch Fertigungstech Gmbh Verfahren zum Bereitstellen einer teilerstarrten Legierungssuspension und Verrichtungen
US6742567B2 (en) 2001-08-17 2004-06-01 Brunswick Corporation Apparatus for and method of producing slurry material without stirring for application in semi-solid forming
WO2003015959A1 (fr) * 2001-08-17 2003-02-27 Innovative Products Group, Llc Appareil et procede de production d'une boue sans brassage pour une application dans le formage semi-solide
EP1358956A1 (fr) * 2002-04-24 2003-11-05 Alcan Technology &amp; Management Ltd. Procédé de traitement d'un alliage métallique pour l'obtention d'un article semi solide
WO2004031423A3 (fr) * 2002-09-23 2004-07-01 Worcester Polytech Inst Alliage sensiblement exempt de dendrites et procede permettant de former cet alliage
WO2004031423A2 (fr) * 2002-09-23 2004-04-15 Worcester Polytechnic Institute Alliage sensiblement exempt de dendrites et procede permettant de former cet alliage
US7513962B2 (en) 2002-09-23 2009-04-07 Worcester Polytechnic Institute Alloy substantially free of dendrites and method of forming the same
EP1405684A3 (fr) * 2002-09-25 2005-06-22 Chunpyo Hong Matériaux métalliques pour la coulée d'après le procédé Rheocast ou le thixoformage et procédé pour leur fabrication
EP1405684A2 (fr) * 2002-09-25 2004-04-07 Chunpyo Hong Matériaux métalliques pour la coulée d'après le procédé Rheocast ou le thixoformage et procédé pour leur fabrication
US6918427B2 (en) 2003-03-04 2005-07-19 Idraprince, Inc. Process and apparatus for preparing a metal alloy
CN100346904C (zh) * 2003-03-04 2007-11-07 伊德拉王子公司 由液态金属合金成分生产金属部件的方法
GB2490467B (en) * 2010-02-05 2014-11-12 Thixomat Inc Method and apparatus of forming a wrought material having a refined grain structure
CN102791402B (zh) * 2010-02-05 2015-04-15 西克索马特公司 具备细晶粒结构的锻造材料的制造方法及制造设备
WO2011097479A3 (fr) * 2010-02-05 2011-09-29 Thixomat, Inc. Procédé et appareil permettant de former un matériau forgé doté d'une fine structure des grains
GB2490467A (en) * 2010-02-05 2012-10-31 Thixomat Inc Method and apparatus of forming a wrought material having a refined grain structure
CN102791402A (zh) * 2010-02-05 2012-11-21 西克索马特公司 具备细晶粒结构的锻造材料的制造方法及制造设备
WO2011097479A2 (fr) * 2010-02-05 2011-08-11 Thixomat, Inc. Procédé et appareil permettant de former un matériau forgé doté d'une fine structure des grains
US9017602B2 (en) 2010-02-05 2015-04-28 Thixomat, Inc. Method and apparatus of forming a wrought material having a refined grain structure
CN102069158B (zh) * 2011-01-11 2013-01-02 大连理工大学 半固态浆料制备所用斜槽的涂层及其喷涂方法
CN102069158A (zh) * 2011-01-11 2011-05-25 大连理工大学 半固态浆料制备所用斜槽的涂层及其喷涂方法
CN103302265A (zh) * 2013-06-17 2013-09-18 昆明理工大学 一种过共晶铝硅合金管材的制备方法
CN104550888A (zh) * 2015-01-30 2015-04-29 林荣英 一种可连续生产金属半固态浆体的方法
WO2016119579A1 (fr) * 2015-01-30 2016-08-04 林荣英 Procédé de production de manière continue d'une suspension métallique semi-solide
CN104550888B (zh) * 2015-01-30 2016-08-31 林荣英 一种可连续生产金属半固态浆体的方法
CN107214311A (zh) * 2016-03-22 2017-09-29 焦作市合鑫机械有限公司 一种振动结晶器
EP3360623A4 (fr) * 2016-04-08 2019-03-27 Zhuhai Runxingtai Electrical Co., Ltd Procédé et système de production semi-solide utilisant une technique de coulée sous pression continue
US10682693B2 (en) 2016-04-08 2020-06-16 Zhuhai Runxingtai Electrical Co., Ltd. Method and apparatus for continuous semisolid die casting
CN107457373A (zh) * 2017-08-28 2017-12-12 广东工业大学 一种制备半固态浆料的装置及其实现方法

Also Published As

Publication number Publication date
EP1331279A3 (fr) 2004-01-02
EP1331279A2 (fr) 2003-07-30
EP0745694B1 (fr) 2004-12-08
CA2177455C (fr) 2007-07-03
CA2177455A1 (fr) 1996-11-30

Similar Documents

Publication Publication Date Title
EP0745694A1 (fr) Procédé et dispositif pour mettre des métaux semi-solides en forme
US6769473B1 (en) Method of shaping semisolid metals
JP3211754B2 (ja) 半溶融成形用金属の製造装置
US7051784B2 (en) Method of producing semi-solid metal slurries
EP0841406B1 (fr) Procédé pour mettre des métaux semi-solides en forme
JP2003535695A (ja) チキソトロピ金属スラリを製造する方法及び装置
EP0120584A1 (fr) Coulée de matériaux métalliques
EP1292411B1 (fr) Production de materiau semi-solide a la demande pour pieces de fonderie
EP1445044A2 (fr) Procédé et dispositif de production d&#39;un métal en phase pâteuse
EP1498196A1 (fr) Dispositif de production d&#39;un métal à l&#39;état d&#39;un mélange liquide-solide
EP0931607B1 (fr) Procédé pour préparer un tronçon de mètal à l&#39;état pâteux
JP2004538153A (ja) 半固体成形時に使用し得るよう攪拌せずにスラリー材料を製造する装置及び方法
EP1470874A1 (fr) Appareil pour la fabrication d&#39;une masse métallique semi-solide thixotrope
JP3920378B2 (ja) レオキャスト鋳造法及びレオキャスト鋳造装置
US6942009B2 (en) Apparatus for manufacturing billet for thixocasting
US20020011321A1 (en) Method of producing semi-solid metal slurries
JPH09137239A (ja) 半溶融金属の成形方法
JP3246358B2 (ja) 半溶融金属の成形方法
US6938672B2 (en) Rheoforming apparatus
JP3783275B2 (ja) 半溶融金属の成形方法
RU2782769C2 (ru) Ультразвуковое измельчение зерна
Bernard The Continuous Rheoconversion Process: Scale-up and Optimization
JPH02147147A (ja) 高固相率半凝固金属を連続的に製造する装置
JP2002522633A (ja) 複合材料の製造法

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 19960613

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE FR GB IT

17Q First examination report despatched

Effective date: 19991227

TPAC Observations filed by third parties

Free format text: ORIGINAL CODE: EPIDOSNTIPA

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB IT

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REF Corresponds to:

Ref document number: 69633988

Country of ref document: DE

Date of ref document: 20050113

Kind code of ref document: P

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED.

Effective date: 20050529

PLBI Opposition filed

Free format text: ORIGINAL CODE: 0009260

PLAX Notice of opposition and request to file observation + time limit sent

Free format text: ORIGINAL CODE: EPIDOSNOBS2

26 Opposition filed

Opponent name: ALCAN INTERNATIONAL LIMITED

Effective date: 20050907

ET Fr: translation filed
PLAF Information modified related to communication of a notice of opposition and request to file observations + time limit

Free format text: ORIGINAL CODE: EPIDOSCOBS2

PLBB Reply of patent proprietor to notice(s) of opposition received

Free format text: ORIGINAL CODE: EPIDOSNOBS3

PLBP Opposition withdrawn

Free format text: ORIGINAL CODE: 0009264

PLBD Termination of opposition procedure: decision despatched

Free format text: ORIGINAL CODE: EPIDOSNOPC1

PLBM Termination of opposition procedure: date of legal effect published

Free format text: ORIGINAL CODE: 0009276

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: OPPOSITION PROCEDURE CLOSED

PLAB Opposition data, opponent's data or that of the opponent's representative modified

Free format text: ORIGINAL CODE: 0009299OPPO

27C Opposition proceedings terminated

Effective date: 20080329

PGRI Patent reinstated in contracting state [announced from national office to epo]

Ref country code: IT

Effective date: 20090501

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 20

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20150527

Year of fee payment: 20

Ref country code: GB

Payment date: 20150527

Year of fee payment: 20

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20150508

Year of fee payment: 20

Ref country code: IT

Payment date: 20150515

Year of fee payment: 20

REG Reference to a national code

Ref country code: DE

Ref legal event code: R071

Ref document number: 69633988

Country of ref document: DE

REG Reference to a national code

Ref country code: GB

Ref legal event code: PE20

Expiry date: 20160528

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20160528