WO2005016579A1 - Flow system for pressure casting - Google Patents

Flow system for pressure casting Download PDF

Info

Publication number
WO2005016579A1
WO2005016579A1 PCT/AU2004/001096 AU2004001096W WO2005016579A1 WO 2005016579 A1 WO2005016579 A1 WO 2005016579A1 AU 2004001096 W AU2004001096 W AU 2004001096W WO 2005016579 A1 WO2005016579 A1 WO 2005016579A1
Authority
WO
WIPO (PCT)
Prior art keywords
alloy
runner
flow
outlet end
die cavity
Prior art date
Application number
PCT/AU2004/001096
Other languages
English (en)
French (fr)
Inventor
Barrie Robert Finnin
Original Assignee
Commonwealth Scientific And Industrial Research Organisation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Commonwealth Scientific And Industrial Research Organisation filed Critical Commonwealth Scientific And Industrial Research Organisation
Priority to AU2004264995A priority Critical patent/AU2004264995A1/en
Priority to EP04761133A priority patent/EP1670605A4/en
Priority to US10/568,011 priority patent/US20070187059A1/en
Priority to CA002535486A priority patent/CA2535486A1/en
Priority to JP2006523484A priority patent/JP4580930B2/ja
Priority to MXPA06001784A priority patent/MXPA06001784A/es
Publication of WO2005016579A1 publication Critical patent/WO2005016579A1/en

Links

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
    • B22D17/02Hot chamber machines, i.e. with heated press chamber in which metal is melted
    • B22D17/04Plunger machines
    • 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
    • B22D17/20Accessories: Details
    • B22D17/22Dies; Die plates; Die supports; Cooling equipment for dies; Accessories for loosening and ejecting castings from dies
    • B22D17/2272Sprue channels

Definitions

  • the reduction in flow velocity from that attained at the inlet end to that at the outlet end is such that the state of the alloy changes from the molten state at the inlet end to a semi-solid or thixotropic state at the outlet end.
  • the alloy In its flow beyond the outlet end, and substantially throughout a die cavity with which the flow path communicates, the alloy most preferably is retained in the semi-solid or thixotropic state.
  • a resultant casting produced is able to be characterised by a microstructure having fine, spheroidal or rounded primary particles of degenerate dendritic form in a matrix of secondary phase.
  • PCT/AU03/00195 there is disclosed a metal flow system for high pressure die casting, and a method of producing alloy castings using a high pressure die casting machine.
  • the system and method of that application utilises a flow path including a CEP, but also including a CEP exit module, referred to as a CEM, through which alloy from the outlet of the CEP passes in its flow to a die cavity.
  • the alloy undergoes a change of state, from a molten state to a semi-solid state, as a consequence of being subjected to a sufficient reduction of flow velocity in the CEP from a suitable flow velocity at the inlet end of the CEP.
  • the CEM has a form which controls the alloy flow whereby the alloy flow velocity decreases progressively from the level at the outlet end of the CEP, such that, at the location at which the flow path communicates with the die cavity, the alloy flow velocity is at a level significantly below the level at the outlet end of the CEP, the change in state generated in the CEP is maintained substantially throughout filling of the die cavity, and the alloy is able to undergo rapid solidification in the die cavity and back along the flow path towards the CEP.
  • CEM represents an exit module for a CEP. That terminology is not appropriate for the present invention in that a CEP is not used. Rather, the invention utilises a flow path which has an exit module through which alloy flows from a runner to a die cavity. While the exit module of the invention has a form suitable for a CEM, it is distinguished herein as a flow- path exit module or "FEM”.
  • the invention provides a metal flow device for high pressure die casting of alloys using a machine having, or operable to provide, a pressurised source of molten alloy and a mould defining at least one die cavity, wherein the device defines a metal flow path by which alloy received from the pressurised source is able to flow into the die cavity, wherein: (a) a first part of the length of the flow path includes a runner; and (b) a second part of the length of the flow path from an outlet end of the runner includes a flow-path exit module (FEM); and wherein the FEM has a form which controls the alloy flow whereby the alloy flow velocity decreases progressively from the level at the outlet end of the runner whereby, at a location at which the flow path communicates with the die cavity, the alloy flow velocity is at a level significantly below the level at the outlet end of the runner and such that, on filling of the die cavity, the alloy is able to undergo solidification in the die cavity and back along the flow path towards the runner.
  • the invention provides a pressure casting machine for high pressure die casting of alloys, wherein the machine has, or operable to provide, a pressurised source of molten alloy, a mould defining at least one die cavity, and a metal flow device which defines a metal flow path by which alloy received from the pressurised source is able to flow into the die cavity, wherein: (a) a first part of the length of the flow path includes or comprises a runner; and (b) a second part of the length of the flow path from an outlet end of the runner includes a flow-path exit module (FEM); and wherein the FEM has a form which controls the alloy flow whereby the alloy flow velocity decreases progressively from the level at the outlet end of the runner whereby, at a location at which the flow path communicates with the die cavity, the alloy flow velocity is at a level significantly below the level at the outlet end of the runner and such that, on filling of the die cavity, the alloy is able to undergo solidification in the die cavity and back along the flow path towards
  • the invention also provides a method of producing alloy castings using a high pressure die casting machine having, or operable to provide, a pressurised source of molten alloy and a mould defining at least one die cavity, in which the alloy flows from the source to the die cavity along a flow path, wherein: (a) the alloy, in a first part of the flow path, is caused to flow along a runner; and (b) in a second part of the flow path, between the first part and the die cavity, the alloy flow is controlled whereby the flow velocity progressively decreases from the level at an outlet end of the runner to a flow velocity where the flow path communicates with the die cavity which is at a level significantly below the level at the outlet of the runner.
  • the second part of the flow path decreases the alloy flow velocity below the flow velocity level at the outlet end of the runner.
  • the second part of the flow path is herein more briefly referred to as the "flow-path exit module" or "FEM".
  • FEM flow-path exit module
  • the runner has a cross-sectional area at least at its outlet end such that, at an alloy mass flow rate able to be generated by the machine, the runner will result in an alloy flow velocity at the outlet end of the runner in excess of about 60 m/s up to about 180 m/s for a magnesium alloy and in excess of about 40 m/s up to about 120 m/s for alloys other than magnesium alloys.
  • the FEM increases in transverse cross-sectional area in a direction extending beyond the outlet end of the runner, whereby the decrease in alloy flow velocity is able to preclude a change of state of the alloy from a molten state to a semi-solid state exhibiting thixotropic properties.
  • the increase in cross-sectional area is such that the decrease in the flow velocity is able to prevent the alloy from undergoing a change of state to enable die cavity fill by molten alloy.
  • a gate defined at the outlet end of the flow path may provide a constriction to alloy flow therethrough, although it need not provide such a constriction. In one form, the gate is at the outlet end of the FEM.
  • the outlet end of the FEM is spaced from the gate by a secondary runner which has a cross-sectional area at least equal to the cross-sectional area at the outlet end of the FEM.
  • the die cavity fill is able to be achieved with molten metal. That is, the alloy is able to be received into the flow path in its molten state, from the pressurised source, and is able to remain in that state until it solidifies in the die cavity.
  • the invention may be similar to conventional high pressure die casting practice.
  • the resultant semi- solid alloy typically has a solids content such that it is able to exhibit thixotropic properties.
  • the alloy has in excess of about 25 wt% solids, usually at least about 30 wt% solids, such as up to about 60 to 65 wt%.
  • the present invention enables die cavity fill with molten metal, there are circumstances in which alloy received into the die cavity can have a low solids content.
  • the low solids content obtainable with the present invention is insufficient to enable the alloy to exhibit thixotropic properties.
  • primary dendritic particles can form in the shot sleeve.
  • the present invention can range in size up to about 60 ⁇ m or larger and can be detrimental in a casting.
  • the particles in a modified form comprise or contribute to a solids content in alloy flowing into the die cavity.
  • a low level of solids can be formed as a consequence of flow of the alloy along the flow path.
  • the weight percentage of these solids is insufficient to confer on the alloy the properties of alloy in a fully thixotropic condition.
  • the solids content is at a level below about 25 wt%, such as below about 20 or 22 wt% and, more usually, less than about 17 wt%.
  • the solids have a very small particle size. This is able to be established by the microstructure of a sufficiently rapidly solidified casting produced with use of the invention.
  • the castings are able to exhibit microstructures having rounded primary dendritic particles of not more than about 50 ⁇ m in size, indicative of solids produced in flow of alloy along the flow path comprising particles of about that size or less.
  • the solids having a small particle size are indicative of the alloy being subjected to very intense shear forces in flow along the flow path. Those forces result from the significant reduction in flow velocity for the alloy, as it passes through the FEM, from the flow velocity in the runner. The intensity of the forces is evidently from flow modelling determinations. The intense shear forces also is indicated by principal characteristics of the microstructure able to be achieved in a casting produced with use of the present invention.
  • a first microstructure characteristic is the above-mentioned rounded primary dendrite particles, and the fine particle size and uniform distribution of those particles.
  • a second microstructure characteristic in the case of use of a cold chamber machine, is the substantial absence of larger, branched dendritic particles able to be formed in the shot sleeve.
  • the form of an FEM, in causing a decrease in alloy flow velocity is such that it necessarily increases in cross-sectional area in the direction of alloy flow. Alloy flow is able to be at a substantially fixed mass flow rate.
  • the alloy undergoes a progressive, but substantial reduction in flow velocity from the level at the outlet end of the runner to the location at which the alloy enters the die cavity.
  • an FEM achieves a result similar to that achieved in a CEP.
  • the reduction is not such as to cause the alloy to change from its molten state to a semi-solid state to an extent resulting in thixotropic properties, even if the alloy flow velocity in the runner is similar to that required at the inlet end of a CEP for that change of state. That is, the reduction in flow velocity in an FEM is such as to preclude the change of state, at least to that extent.
  • a flow device Due to its FEM increasing in cross-sectional area in the flow direction, a flow device according to the present invention is different from a flow system used in conventional die casting practice.
  • a substantially constant flow velocity usually is maintained, except at the location at which the flow path communicates with the die cavity.
  • a constriction provided at that location referred to as a gate, causes the alloy to undergo a sharp increase in flow velocity such that the alloy flows into the die cavity as a thin, high velocity jet.
  • a gate constriction need not be provided and the alloy may flow into the die cavity as a relatively wide stream.
  • the flow path may have a cross-section at the location at which the flow path communicates with the die cavity which is larger than the cross-sectional area of the runner.
  • the area of the gate is smaller than the cross-sectional area of its runner.
  • the flow path according to the invention need not have a gate constriction, this is not essential and a constricting gate can be provided in at least some instances. In any event, whether or not a constricting gate is provided, the flow path of the invention differs from conventional practice.
  • the first part of the flow path which includes a runner is significantly smaller in cross-sectional area than a conventional runner.
  • the second part of the flow path increases in cross- sectional area in the flow direction to thereby cause a required reduction in alloy flow velocity through the FEM.
  • the flow path is somewhat similar to that of PCT/AU03/00195, although there are necessary and important differences.
  • a runner flow velocity which is high relative to that used in conventional pressure die casting is required in use of the present invention.
  • the runner required for the invention necessarily has a smaller cross-sectional area relative to a conventional runner in order to achieve the higher flow velocity at that mass flow rate.
  • the FEM in the arrangement of PCT/AU03/00195 is to facilitate maintenance of semi-solid alloy generated in the CEP and having thixotropic properties.
  • the outlet end of the FEM may be at the location at which the flow path communicates with the die cavity. While this is preferred, the outlet end of the FEM may be spaced from the location by a secondary runner which does not provide a significant restriction to alloy flow. Thus, the cross-sectional area of the secondary runner may be substantially the same as the area of the outlet of the FEM.
  • a secondary runner in the system of the invention will have a larger cross-sectional area than the runner of the first part of the flow path, and this is the converse of the relationship between a secondary and primary runner of conventional pressure casting practice.
  • the FEM in the device of the invention can take a variety of forms.
  • the FEM defines or comprises a channel which has a width which is substantially in excess of its depth and a transverse cross-sectional area greater than the area of the outlet of a runner from which it is able to receive molten alloy.
  • the width of the channel which may exceed its depth by at least an order of magnitude, preferably is disposed in a plane extending transversely with respect to the runner.
  • the channel is such that it enables alloy flowing into it from the runner to spread in a radial fashion and thereby undergo a reduction in flow velocity.
  • the cross-sectional area of the channel may increase in the direction of alloy flow to thereby cause a further decrease in alloy flow velocity.
  • the channel may be substantially flat or, if appropriate for the die cavity for a given casting, it may be curved across its width. However, it alternatively can have a saw-toothed or corrugated configuration, to define peaks and troughs across its width, somewhat similar to some forms of chill vent.
  • the channel may increase in cross-sectional area due to one of the width and depth of the channel may be constant along its length, with the other progressively increasing, preferably uniformly.
  • each of the width and depth may increase in the direction of alloy flow.
  • a saw-tooth or corrugated form it generally is more convenient for only the width to increase, although this form has the benefit of maximising flow length for a given spacing between the runner outlet end and the location at which the flow path communicates with the die cavity.
  • the arrangement With the first form, in which the FEM defines a channel having a width substantially in excess of its depth, the arrangement generally is such that the alloy flow path communicates with the die cavity through an opening having a width substantially in excess of its depth. This is well suited to die cavity fill by indirect or edge feed, particularly when the die cavity is for producing a thin casting.
  • the FEM of a device defines or comprises a channel having a width and depth which have dimensions of the same order, and a transverse cross-section which progressively increases in the direction of alloy flow.
  • This form in having a progressively increasing cross- section, also provides a required low flow velocity at the location at which the flow path communicates with the die cavity.
  • the channel of the second form of the FEM may be open at its end remote from the runner from which it is able to receive molten alloy, with the open end defining that location.
  • the location is defined by an elongate opening extending along a side of the channel.
  • each channel remote from the runner may terminate a short distance from each other, such that their side openings are longitudinally spaced along the common edge of the die cavity.
  • the two channels may merge at those ends to thereby form respective arms of closed loop, in which case the openings again may be so spaced, or they may form a single elongate opening common to each arm.
  • the progressive decrease in alloy flow velocity in the FEM of the metal flow system of the invention, and the progressive increase in cross-sectional area of that second part which causes that decrease may be continuous. Also, the progressive decrease in velocity and increase in area may be substantially uniform, or it may be step-wise, along at least a section of the second part.
  • the first and second forms for the FEM described above are well suited to providing a continuous decrease in velocity, produced by a continuous increase in cross- sectional area, such as along at least a major part of the length of the second part.
  • the FEM includes a chamber into which alloy received from the runner flows, with the chamber achieving a step-wise reduction in the alloy flow velocity.
  • the FEM includes channel means which provides communication between the chamber and the die cavity and which has a form at least substantially maintaining the flow velocity level attained in the chamber. That communicating channel means may be of a form similar to that of the first form of FEM described, while it may have a substantially uniform or slightly increasing cross- section.
  • the channel means may comprise at least one channel, but preferably at least two channels, similar to the second form of the FEM described above except that, if required, such channel or each such channel may have a substantially uniform cross-section.
  • the chamber of the third form can have a variety of suitable shapes. In one convenient arrangement, it may have the form of an annular disc. That arrangement is suitable for use where the communicating means is at least one channel. Where, in that arrangement, the communicating means comprises at least two channels, the channels may communicate with a common die cavity, or with a respective die cavity.
  • the at least one channel of the communicating means of the third form of FEM may open to its die cavity at an end opening of the channel, or at an elongate side opening as described with reference to the second form.
  • the FEM most preferably is disposed parallel to the parting plane of a mould defining the die cavity.
  • the first part of the flow path may be similarly located, such that its runner also is parallel to that plane, with alloy received from a sprue or runner portion extending through one mould part to that plane.
  • the first part of the flow path may extend through such mould part, with the outlet of the runner at or closely adjacent to the parting plane.
  • the flow velocity at the inlet end of the CEP generally is in excess of about 60 m/s, preferably at about 140 to 165 m/s.
  • the inlet end flow velocity generally is in excess of 40 m/s, such as about 80 to 120 m/s.
  • the CEP inlet end flow velocity generally is similar to that for aluminium alloys, but can vary with the unique properties of individual alloys.
  • the reduction in flow velocity to be achieved in the CEP generally is such as to achieve a flow velocity at the CEP outlet end which is from about 50 to 80%, such as from 65 to 75% of the flow velocity at the inlet end.
  • a CEP is not used.
  • the alloy may remain molten in its flow to the die cavity but, even where some solids are formed, the alloy does not undergo a change of state to an extent resulting in thixotropic properties.
  • runner flow velocities, at least at the runner outlet end can be similar to those required with use of a CEP.
  • a flow velocity at the outlet end of the runner or the inlet end of the FEM can be in excess of about 60 m/s, and preferably is from about 130 m/s to 160 m/s, but can range up to about 180 m/s.
  • a flow velocity at the outlet end of the runner or inlet end of the FEM can be as detailed above for use of a CEP.
  • the reduction in flow velocity to be achieved in an FEM usually is very substantial. Indeed, the reduction can exceed that obtained in use of a CEP.
  • an FEM can achieve a greater reduction in flow velocity.
  • Practical considerations favour an FEM having an effective flow length which is as short as possible.
  • the length of an FEM varies with its average cross- sectional area, but may be from about 15 to 35 mm.
  • an FEM preferably has an overall length which is less than its effective flow length, due to it having an undulating, corrugated or saw-toothed configuration which increases backpressure in the flow system.
  • the length of an FEM varies with the cross-sectional area at the outlet end of the runner from which it receives a flow of alloy.
  • a CEP is to result in a change in the state of the alloy, from a molten state to a semi- solid state exhibiting thixotropic properties, it is to be expected that an FEM would have a shorter length than a CEP, for a given runner outlet end cross- sectional area.
  • a longer length, providing a more gradual increase in cross- sectional area for a FEM from the runner inlet, would seem to be necessary for providing the conditions appropriate for avoiding a change of state at all, or at least to the extent required for a CEP. However, we have found that this is not the case.
  • an FEM needs to have a shorter length than would be required for a CEP provided for such runner.
  • the preceding description of the invention makes reference to a die cavity or the die cavity.
  • the FEM defined by the system of the invention may divide or extend to provide separate flow to a common die cavity or to each of at least two die cavities. Indeed, as illustrated herein by reference to the drawings, providing such separate flow from a common FEM generally facilitates attainment of the required reduction in alloy flow velocity.
  • Figure 1 is a schematic representation of a two cavity mould arrangement, taken on the parting plane between fixed and movable mould parts, illustrating a first embodiment of the invention
  • Figure 2 is a sectional view taken on line II of Figure 1 and shown on an enlarged scale
  • Figure 3 is a schematic representation, similar to Figure 1 , but illustrating a second embodiment of the invention having a single die cavity
  • Figure 4 is a side elevation of the arrangement of Figure 3
  • Figure 5 is similar to Figure 4, but shows a first variant of the second embodiment
  • Figure 6 is similar to Figure 4 but shows a second variant of the second embodiment
  • Figure 7 is similar to Figure 3, but illustrates a third embodiment of the invention
  • Figure 8 is a side elevation of the arrangement of Figure 7
  • Figure 9 is a schematic representation, similar to Figure 1 , but illustrating a fourth embodiment of the invention
  • Figure 10 is a part sectional view taken on line X-X of Figure 9
  • Figure 1 1 is similar to Figure 3, but illustrate
  • Figure 11 shows a first variant of the fifth embodiment of the invention
  • Figure 14 is similar to Figure 1 1 , but shows a second variant of the fifth embodiment
  • Figure 15 is a part sectional view taken on line XV-XV of Figure 14
  • Figure 16 is similar to Figure 3, but illustrates a sixth embodiment of the invention
  • Figure 17 is a side elevation of the arrangement of Figure 16
  • Figure 18 is similar to Figure 17, but illustrates a variant on the sixth embodiment
  • Figure 19 is a plan view of a casting produced using a seventh embodiment of the present invention
  • Figure 20 is a schematic representation of part of the seventh embodiment in plan view
  • Figure 21 is a side elevation of the arrangement shown in Figure 20.
  • die cavities 10 and 1 1 there is represented therein two die cavities 10 and 1 1 , defined by fixed mould half 12 and movable mould half 13 and each for use in producing a respective casting in a high pressure casting machine (not shown).
  • Each of die cavities 10 and 1 1 is arranged to receive alloy from a pressurised supply of molten alloy of the machine, with alloy passing to each cavity by a common alloy feed device 14 according to a first embodiment of the present invention.
  • the embodiment is one in accordance with the first form of the invention as described above.
  • the alloy feed device 14 defines a flow path for molten alloy which has a first part defined by nozzle 16, shown in more detail in Figure 2, and a second part 18, referred to as an FEM as identified earlier herein, which extends between each cavity and across the outlet end of nozzle 16.
  • nozzle 16 includes an elongate annular housing 20 by which the first part of the metal flow path defines a bore comprising a runner 22.
  • Housing 20 has its outlet end neatly received in an insert 26 of fixed mould half 12, while its inlet end abuts against a fitting 28 of platen 29.
  • Around housing 20 there is an electric resistance coil 30 and, outside coil 30, a layer of insulation 32.
  • an insulating gap 34 is provided between insulation 32 and insert 26, except for a short distance at the outlet end of housing 20 where the latter is in metal to metal contact with insert 26. Additionally, gap 34 extends between insulation 32 and fitting 28. Coil 30 and insulation 32 provide for control of heat energy level of housing 20 and the temperature of alloy flowing through runner 22.
  • runner 22 is of constant cross-section throughout its length, except for a short distance at its outlet end at which it tapers down to the cross-section of the outlet end 22a of runner 22. From the outlet end 22a of runner 22, the bore of housing 20 flares over a very short end portion 35.
  • Channel 36 provides alloy flow to each of the die cavities 10 and 11 in which the alloy flow velocity decreases below the level prevailing at outlet end 22a of runner 22. This is achieved by the alloy spreading radially outwardly in channel 36, from end 22a, as represented by the broken circles shown in Figure 1.
  • the molten alloy is able to progress on an expanding front in channel 36 which is tangential to radial directions from end 22a.
  • the expanding flow of alloy is constrained on reaching the opposite sides of channel 36, but is divided to continue to flow at a reduced flow velocity to each of open ends 36a and 36b of channel 36 by which channel 36 communicates with die cavities 10 and 1 1 , respectively.
  • the opposite sides of channel 36 are substantially parallel, such that required, reduced flow velocity for cavity 10 may be attained a short distance before open end 36a. However, for the portion of channel 36 leading to cavity 1 1 , the opposite sides diverge in the flow direction, such that the flow velocity is able to continue to decrease to obtain a different required, reduced flow velocity at open end 36b for cavity 1 1 . Alloy flow continues to achieve filling of each die cavity 10,1 1. Alloy flow throughout each of cavities 10,1 1 is able to be at a sufficiently low flow velocity, below the flow velocity at end 22a of runner 22, that back pressure against alloy flow is able to be maintained at a suitable level.
  • mould halves 12,13 The arrangement of mould halves 12,13 is such that heat energy extraction from alloy in each die cavity 10,11 , on completion of cavity fill, provides rapid solidification of alloy in each cavity 10,11 and back along channel 36 to the outlet end 22a of runner 22.
  • the thin cross-section of channel 36 facilitates this.
  • heat energy extraction, principally by die half 12 and its insert 26, enables that cooling to progress back into the end 22a, despite heating by coil 30, due to the metal to metal contact between housing 20 and insert 26, around end 22a.
  • Figures 3 and 4 show a second embodiment of an arrangement for producing a casting, in this case using a single cavity mould of a high pressure casting machine.
  • the second embodiment also is in accordance with the first form of the invention as described above, but utilises a saw-toothed like channel form, rather than a flat channel as in Figures 1 and 2. Parts corresponding to those of Figures 1 and 2 have the same reference numeral, plus 100. However, the mould halves are not shown, while only part of housing 120 of a nozzle 1 16 is illustrated. In Figures 3 and 4, the end of channel 136 of FEM 1 18 has a round- ended flat portion 40 with which the runner 122 communicates.
  • the variant of Figure 6 is the same in overall form as Figures 3 and 4, except that portion 42 of the channel 136 of the FEM 118 is of an undulating or corrugated configuration, rather than saw-toothed. However, that configuration of Figure 6 again provides suitable back-pressure.
  • the third embodiment of Figures 7 and 8 also is in accordance with the first form of the invention as described above. In the arrangement of Figures 7 and 8, parts corresponding to those of Figures 1 and 2 have the same reference numeral, plus 200. As with the embodiment of Figures 3 and 4, the third embodiment of Figures 7 and 8 is for producing a casting using a single cavity mould. However, in this case, channel 236 of the FEM 1 18 does not include a portion of saw-toothed configuration.
  • channel 236 has flat top and bottom main surfaces. Also, while those surfaces converge slightly in the direction of alloy flow therethrough, to outlet end 236a and cavity 210, the opposite sides of channel 236 diverge in that direction.
  • the arrangement is such that, in the flow direction, channel 236 increases in transverse cross-sectional area towards the elongate, thin open end 236a, such that alloy flow velocity progressively decreases to a suitable level at end 236a which is significantly below that at outlet end 222a of runner 222.
  • runner 222 extends parallel to the parting plane P-P between mould halves 212,213, and provides communication with the end of channel 236 remote from die cavity 210.
  • the runner 222 is defined by the halves 212,213, rather than by a nozzle, while runner 222 is aligned with a centre-line of channel 236 of the FEM 218 and cavity 210.
  • the supply of alloy to the inlet end of runner 222 may be via a main runner or the bore of a nozzle, with such main runner or nozzle bore extending through fixed mould half 212, such as perpendicularly with respect to plane P-P.
  • the machine has a mould which defines two die cavities 310,311 between its mould halves 312,313.
  • the die halves also define an elongate channel 336 which extends between cavities 310,311 , parallel to the parting plane P-P.
  • the channel 336 forms the FEM 318 of a molten alloy flow path of which the first part is provided by a runner 322.
  • the runner 322 is defined by the housing 320 of a nozzle mounted in the fixed mould half 312 at right angles to plane P-P.
  • the runner 322 communicates with channel 336 mid-way between cavities 310,311 , such that the alloy is divided to flow in opposite directions to each cavity 310,311.
  • the alloy spreads in end portion 335 of the bore of housing 320 and then enters a central region 54 of channel 336.
  • the depth of channel 336 is increased such that region 54 provides a circular recess which can assist in stabilising alloy flow.
  • the alloy is divided so as to flow in opposite directions to each open end 336a and 336b of channel 336, and then into the respective die cavity 310,311. Alloy received into runner 322, from a pressurised source of the machine, is caused to undergo a decrease in flow velocity in the FEM 318.
  • the alloy flow path is such that the flow velocity is decreased in end portion 335 from the value at the outlet end 322a of runner 322, and then further decreased through to respective open ends 336a,336b of channel 336. This further decrease results from the alloy spreading radially from the outlet end of housing 320, in region 54, to the extent permitted by the opposite sides of channel 336. The alloy then flows along channel 336, to each of the opposite ends 336a and 336b, in which the flow velocity continues to decrease due to the opposite sides diverging slightly from region 54 to the opposite ends 336a, 336b.
  • channel 336 is inclined at an angle to the end of each die cavity 310,311 at which open ends 336a and 336b, respectively, provide communication
  • the ends 336a and 336b have a greater area than transverse cross-sections normal to the longitudinal extent of channel 336, thereby enabling a further reduction in alloy flow velocity at ends 336a and 336b.
  • the arrangement is such that alloy passing through open ends 336a and 336b has a flow velocity which is substantially lower than the flow velocity at the outlet end 322a of runner 322.
  • the substantially lower flow velocity is such as to facilitate maintenance of a sufficient back pressure on the alloy during filling of die cavities 310,311.
  • each open end 336a,336b has an area less than that at runner end 322a, each open end 336a,336b accommodated approximately half of the total alloy flow (as in the case of ends 36a,36b of the arrangement of Figures 1 and 2).
  • the open ends 336a,336b can have a width of 30mm and a depth of 0.9mm.
  • the arrangement is suitable for a die cavity 310 having a 2mm depth dimension normal to the plane P-P, with the cavity 311 having a corresponding dimension of 1 mm.
  • the alloy is able to flow on a front, to achieve die cavity fill, which spreads as it moved away from the respective open end 336a, 336b.
  • the alloy flow device shown has an alloy flow path which extends parallel to the parting plane P-P between fix mould half 60 and movable mould half 61 , to die cavity 62.
  • the flow path includes a runner 63 which defines a first part of the flow path.
  • the second part of the flow path comprises an FEM in the form of a channel 66 which has oppositely facing C-shaped arms 67,68. Only part of arm 67 is shown, although it is of the same form as arm 68, but oppositely facing.
  • Each arm 67,68 of FEM channel 66 has a respective first portion 67a,68a which extends laterally outwardly from an enlargement 69 at the outlet end 63a of runner 63.
  • arm 68 From the outer end of portion 68a, arm 68 has a second portion 68b which extends in the same direction as, but away from, runner 63. Beyond portion 68b, arm 68 has a third portion 68c which extends laterally inwardly towards a continuation of the line of runner 63. While not shown, arm 67 also has respective second and third portions, beyond portion 67a, which correspond to portions 68b and 68c of arm 68. Each arm 67,68 provides communication with the die cavity 62, within a U-shaped recess 72 at an end of cavity 62. Runner 63 and FEM channel 66 are of bi-laterally symmetrical trapezoidal form in transverse cross-section, as shown for portion 67a of arm 67 in Figure 12.
  • Runner 63 is of uniform cross-sectional area over the major part of its length but, adjacent to its outlet end, it tapers down to the area at the outlet end 63a of runner 63. From the enlargement 69 of the flow path, each arm 67,68 of channel 66 increases in cross-sectional area to a maximum adjacent to its remote end.
  • An example was based on Figures 11 and 12, and suitable for production of magnesium alloy castings on a hot chamber pressure die casting machine with a single die cavity mould, could have an arrangement such that molten magnesium alloy from the machine source was supplied under pressure to the inlet end of runner 63 in which the flow velocity was 50 m/sec.
  • the molten alloy flow velocity was increased to attain 112.5 m/s. From enlargement 69, the alloy divided equally for flow along each arm. Relative to the locations A to E shown for arm 68, the alloy flow velocity could decrease progressively to 90 m/sec at A, 80 m/sec at B, 70 m/sec at C, 60 m/sec at D, and 50 m/sec at E. Each arm was provided with an elongate opening by which it was in communication with the die cavity 62.
  • the opening for arm 68 could have an average width of 0.5mm from C to D, of 0.6mm from D to E and of 0.8mm from E to the end.
  • the overall length of each slot therefore would be 35.85mm, with the overall alloy flow velocity therethrough decreasing from 70 m/sec at C to less than 50 m/s at the end of each arm beyond E.
  • Figure 13 shows a variant on the arrangement of Figures 1 1 and 12, and corresponding parts have the same reference numerals, plus 100.
  • Figure 13 shows a main runner 70 by which alloy is supplied to runner 163.
  • arms 167,168 of FEM channel 166 each communicate with the die cavity along a straight end of the cavity.
  • the arrangement, for use with a magnesium alloy, could provide for a molten alloy flow velocity of 150 m/sec at outlet end 163a of runner 163. In each arm of channel 166, the alloy flow velocity could decrease to 125 m/sec at A, 1 10 m/sec at B, 95 m/sec at C and
  • FIG. 13 are as follows: Location Area (mm 2 ) 163a 8.5 A 6.0 B 6.8 C 8.0 D 9.6. As will be appreciated, the areas shown for locations A to D are for one arm of FEM channel 166. However, relating these to the areas for outlet end 163a of runner 163 needs to take into account the fact that each arm provides for the flow of only half of the alloy flowing through the runner.
  • Figure 16 shows part of the flow device for a further embodiment of the present invention, viewed perpendicularly of a parting plane.
  • Figures 17 and 18 show alternatives for the arrangement of Figure 16. In Figures 16 to 18, the runner by which molten alloy flows is shown only at a terminal portion 80 defining outlet end 80a.
  • runner 80 forms the first part of the flow path of the flow system, while channel 82, chamber 84 and channels 86 form the second part or FEM of the flow system.
  • Molten alloy flows from runner 80 to channel 82, into chamber 84, and the alloy then flows through each channel 86 to a single or respective die cavity (not shown).
  • Channel 82 has a larger cross-sectional area than the outlet end of runner 80, and the cross-sectional may be constant or it may increase to chamber 84. In either case, it provides a lower alloy flow velocity than that attained at the outlet end of runner 80. In chamber 84, the alloy flow is able to spread, resulting in a further reduction in flow velocity.
  • the casting comprises a pair of laterally adjacent tensile bars 91 joined in series at adjacent ends by a tie 92 of metal which solidified in a channel providing for metal flow between respective die cavities in which the bars 91 were cast.
  • the casting 90 is illustrated in an as cast condition and it accordingly includes metal 93 solidified along part of the metal flow path by which alloy was supplied to the die cavities.
  • the metal 93 includes metal section 94 solidified in the FEM, and metal section 95 solidified in the runner, of the metal flow path.
  • the casting 90 would be cut along the junction between each end of tie 92 and the respective side of each bar 91 while metal 93 would be severed from the side of the tensile bar 91 to which it is attached.
  • the shape of the severed metal 93 is shown in more detail in Figures 20 and 21.
  • the metal 93 of course has the same form as a corresponding section 96 of a metal flow device according to the present invention and further description of metal 93 in Figures 20 and 21 is with reference to metal 93 as if representing that corresponding section 96.
  • Metal sections 94 and 95 thus are taken as respectively representing the FEM 97 and the runner 98 of the corresponding metal flow system.
  • the shading depicts respective mould halves 101 and 102 which are separable on parting line P-P and which define the die cavities and metal flow system.
  • the FEM 97 has an overall rectangular form, with the runner 98 longitudinally in-line.
  • the outlet end 98a of the runner 98 communicates with the FEM 97 at the middle of one end of the FEM.
  • the molten alloy flows along runner 98 and, from runner 98, the alloy flows through the FEM 97 towards its end remote from the runner outlet 98a.
  • the FEM 97 opens laterally to a short secondary runner 100 through which alloy is able to pass to the first of in-series die cavities in which tensile bars 91 are cast.
  • the FEM 97 is of a form which generates resistance to alloy flow therethrough.
  • ribs 101a and 102a defined by the respective mould parts, which extend laterally with respect to alloy flow through the FEM 97, and which protrude into the general rectangular form of the FEM.
  • the width of the FEM 97 and the minimum distance A between successive ribs is calculated so that a required flow velocity for a given alloy is achieved.
  • a molten magnesium alloy may be reduced in flow velocity from 150 m/s at inlet 98a of runner 98 in its flow through FEM 97.
  • the molten alloy flow velocity in the runner preferably is very substantial, as detailed earlier herein.
  • the reduction in flow velocity to be achieved in an FEM usually is in excess of 20%, but preferably is in excess of 30%, and can be in excess of 50% of the runner flow velocity. It usually is necessary to achieve higher levels of flow velocity reduction with use of higher runner flow velocities. In any event, the reduction in flow velocity is to be sufficiently gradual as to avoid substantially a change in the alloy from a molten state to a semi-solid state in which it exhibits thixotropic properties, at least during its flow to the inlet to the die cavity. As detailed herein, the FEM achieves a reduction in flow velocity by increasing the cross-sectional area of the flow path, from the area at the outlet end of the runner. The reduction in flow velocity can be to a level used in conventional die casting.
  • the increase in cross-sectional area along the FEM can be to an area at its outlet end which is similar to the cross-sectional area of a conventional runner.
  • the volume of the FEM is substantially less than the volume of a corresponding length of a conventional runner.
  • each metal flow device of the embodiments of Figures 1 to 21 will vary with the machine with which it is to be used.
  • the device needs to be operable in the required manner at an alloy mass flow rate at which the machine is operable.
  • the runner of the first part of the flow path of the device needs to have a cross-sectional area which generates a required alloy flow velocity therein at that mass flow rate. That cross-sectional area need not prevail throughout the length of the runner, and may for example, be provided only at an outlet end portion of the runner.
  • the runner may step down from a larger cross-sectional area so that the required flow velocity is attained in the outlet end portion.
  • the FEM is to have a length, and is to increase in cross-sectional area along that length in the flow direction, such that shear forces generated in the alloy are not such as to change the state of the alloy to a semi-solid state having thixotropic properties. If the shear generates any solids in the alloy, this should be to an extent of less than 25%, preferably less than about 20 to 22%, such as less than about 17 wt%. However, it is not necessary that any solids be generated at all, since even in this case, a superior microstructure as detailed above is found to be achieved.
  • a respective magnesium alloy casting for each of the products detailed in Table 1 was produced under the conventional casting conditions detailed in Table 2, and under the conditions in accordance with the present invention detailed in Table 3.
  • a metal flow device corresponding to the embodiment illustrated in Figures 14 and 15.
  • Each of the castings for which details are provided in Table 2 or Table 3 was found to be sound.
  • those produced in accordance with the invention exhibited a superior microstructure. This superiority was in terms of greater uniformity of microstructure throughout the castings and the form of the constituents of the microstructure.
  • the castings produced under conventional conditions exhibited larger individual grains of a normal, branched dendritic pattern and, in several instances, regions of porosity to levels of 1.5% or greater resulting from air entrapment.
  • microstructures were essentially as detailed above in respect of the magnesium alloy castings.
  • the microstructures for the brackets of castings A8 and A9 appeared clearly to have resulted from die cavity fill with molten alloy having negligible if any solids content.
  • the situation was less clear with the microstructures of castings A1 to A7, although it appeared that each of these resulted from die cavity fill with only a very minor solids content.
  • None of the microstructures for castings A1 to A9 exhibited large isolated grains resulting from primary phase solidification in the shot sleeve. In each case, it appeared that if any such large grains were formed in the shot sleeve, they were broken down, increasing the number of finer grains, under the intense shear forces prevailing in the FEM.
  • the above-mentioned experimental metal flow device used for Trials A4 and each of A6 to A10 was formed in a respective face of each mould part which defines the parting plane between those parts. That is, both the runner and the FEM extended along the parting plane. Viewed perpendicularly to that plane, the FEM has side edges which diverged from each other in a direction away from the outlet end of the runner to an elongate gate which extended laterally with respect to the length of the runner. The runner thus ended at the apex of a FEM which, in that view, was of a delta or triangular form.
  • the FEM was curved or arched between the outlet end of the runner and the gate, due to the face of one mould part being convex and the face of the other mould part being concave.
  • the arrangement was such that convex surface portion curved across the end of the runner so that alloy flowing from the outlet of the runner was deflected by that surface portion to cause the alloy to fill the triangular volume of the FEM in passing to the elongate gate.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
PCT/AU2004/001096 2003-08-15 2004-08-16 Flow system for pressure casting WO2005016579A1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
AU2004264995A AU2004264995A1 (en) 2003-08-15 2004-08-16 Flow system for pressure casting
EP04761133A EP1670605A4 (en) 2003-08-15 2004-08-16 FLOW SYSTEM FOR PRESSURE MOLDING
US10/568,011 US20070187059A1 (en) 2003-08-15 2004-08-16 Flow system for pressure casting
CA002535486A CA2535486A1 (en) 2003-08-15 2004-08-16 Flow system for pressure casting
JP2006523484A JP4580930B2 (ja) 2003-08-15 2004-08-16 圧力鋳造流れシステム
MXPA06001784A MXPA06001784A (es) 2003-08-15 2004-08-16 Sistema de flujo para colado bajo presion.

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AU2003904394A AU2003904394A0 (en) 2003-08-15 2003-08-15 Flow system for pressure casting
AU2003904394 2003-08-15

Publications (1)

Publication Number Publication Date
WO2005016579A1 true WO2005016579A1 (en) 2005-02-24

Family

ID=32476665

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/AU2004/001096 WO2005016579A1 (en) 2003-08-15 2004-08-16 Flow system for pressure casting

Country Status (12)

Country Link
US (1) US20070187059A1 (zh)
EP (1) EP1670605A4 (zh)
JP (1) JP4580930B2 (zh)
KR (1) KR20060058718A (zh)
CN (1) CN100381229C (zh)
AU (1) AU2003904394A0 (zh)
CA (1) CA2535486A1 (zh)
MX (1) MXPA06001784A (zh)
RU (1) RU2006107982A (zh)
TW (1) TW200520875A (zh)
WO (1) WO2005016579A1 (zh)
ZA (1) ZA200601511B (zh)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20160115471A (ko) 2015-03-27 2016-10-06 이은선 사전 경품 행사를 통한 상품 판매 방법 및 장치

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999028065A1 (en) * 1997-11-28 1999-06-10 Commonwealth Scientific And Industrial Research Organisation Magnesium pressure casting
WO2001019552A1 (en) * 1999-09-16 2001-03-22 Hotflo Diecasting Pty Ltd Hot sprue system for diecasting

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS54151513A (en) * 1978-04-27 1979-11-28 Leibfried Dieter Low pressure dieecasting of metal* particularly of ne metal and apparatus therefor
DE19618882A1 (de) * 1996-05-10 1997-11-13 Webasto Karosseriesysteme Schaltungsanordnung zur Stromversorgung eines Verbrauchers durch einen Solargenerator
JP3494020B2 (ja) * 1998-07-03 2004-02-03 マツダ株式会社 金属の半溶融射出成形方法及びその装置
KR100369919B1 (ko) * 1999-03-03 2003-01-29 미쓰비시덴키 가부시키가이샤 팬, 팬의 용융금속 성형방법 및 팬의 용융금속 성형장치
JP3427060B2 (ja) * 2000-04-28 2003-07-14 株式会社東芝 筐体部品の製造方法
AUPQ780400A0 (en) * 2000-05-29 2000-06-22 Commonwealth Scientific And Industrial Research Organisation Die casting sprue system
AUPQ967800A0 (en) * 2000-08-25 2000-09-21 Commonwealth Scientific And Industrial Research Organisation Aluminium pressure casting
AUPR076300A0 (en) * 2000-10-13 2000-11-09 Commonwealth Scientific And Industrial Research Organisation Device for high pressure casting
CN1193845C (zh) * 2001-05-22 2005-03-23 鸿富锦精密工业(深圳)有限公司 镁合金薄壁铸造的压铸方法
AU2930702A (en) * 2001-08-23 2003-02-27 Commonwealth Scientific And Industrial Research Organisation Metal flow system
AU2930502A (en) * 2001-08-23 2003-02-27 Commonwealth Scientific And Industrial Research Organisation Improved magnesium alloy castings
AUPR721501A0 (en) * 2001-08-23 2001-09-13 Commonwealth Scientific And Industrial Research Organisation Process and apparatus for producing shaped metal parts
AU2930302A (en) * 2001-08-23 2003-02-27 Commonwealth Scientific And Industrial Research Organisation Apparatus for pressure casting
AU2930002A (en) * 2001-08-23 2003-02-27 Commonwealth Scientific And Industrial Research Organisation improved alloy castings

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1999028065A1 (en) * 1997-11-28 1999-06-10 Commonwealth Scientific And Industrial Research Organisation Magnesium pressure casting
WO2001019552A1 (en) * 1999-09-16 2001-03-22 Hotflo Diecasting Pty Ltd Hot sprue system for diecasting

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP1670605A4 *

Also Published As

Publication number Publication date
JP4580930B2 (ja) 2010-11-17
EP1670605A4 (en) 2006-12-06
EP1670605A1 (en) 2006-06-21
ZA200601511B (en) 2007-05-30
MXPA06001784A (es) 2006-05-17
US20070187059A1 (en) 2007-08-16
CN1856378A (zh) 2006-11-01
TW200520875A (en) 2005-07-01
KR20060058718A (ko) 2006-05-30
CA2535486A1 (en) 2005-02-24
JP2007502212A (ja) 2007-02-08
RU2006107982A (ru) 2006-07-27
CN100381229C (zh) 2008-04-16
AU2003904394A0 (en) 2003-08-28

Similar Documents

Publication Publication Date Title
US7121319B2 (en) Magnesium pressure casting
US7234505B2 (en) Aluminium pressure casting
JP2004505785A5 (zh)
US7111663B2 (en) Pressure casting flow system
EP1670605A1 (en) Flow system for pressure casting
WO2002030596A1 (en) Device for high pressure casting
AU2004264995A1 (en) Flow system for pressure casting
AU2003203059B2 (en) Pressure casting flow system
EP1289693A1 (en) Die casting sprue system
AU2001281596C1 (en) Aluminium pressure casting
WO2003018235A1 (en) Metal flow system
AU754591B2 (en) Magnesium pressure casting
AU2001281596A1 (en) Aluminium pressure casting
AU2001258067A1 (en) Die casting sprue system

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 200480027495.1

Country of ref document: CN

AK Designated states

Kind code of ref document: A1

Designated state(s): AE AG AL AM AT AU AZ BA BB BG BR BW BY BZ CA CH CN CO CR CU CZ DE DK DM DZ EC EE EG ES FI GB GD GE GH GM HR HU ID IL IN IS JP KE KG KP KR KZ LC LK LR LS LT LU LV MA MD MG MK MN MW MX MZ NA NI NO NZ OM PG PH PL PT RO RU SC SD SE SG SK SL SY TJ TM TN TR TT TZ UA UG US UZ VC VN YU ZA ZM ZW

AL Designated countries for regional patents

Kind code of ref document: A1

Designated state(s): BW GH GM KE LS MW MZ NA SD SL SZ TZ UG ZM ZW AM AZ BY KG KZ MD RU TJ TM AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LU MC NL PL PT RO SE SI SK TR BF BJ CF CG CI CM GA GN GQ GW ML MR NE SN TD TG

121 Ep: the epo has been informed by wipo that ep was designated in this application
WWE Wipo information: entry into national phase

Ref document number: 2535486

Country of ref document: CA

WWE Wipo information: entry into national phase

Ref document number: 2004264995

Country of ref document: AU

WWE Wipo information: entry into national phase

Ref document number: 2006523484

Country of ref document: JP

Ref document number: 1020067003184

Country of ref document: KR

Ref document number: PA/a/2006/001784

Country of ref document: MX

WWE Wipo information: entry into national phase

Ref document number: 2006/01511

Country of ref document: ZA

Ref document number: 200601511

Country of ref document: ZA

ENP Entry into the national phase

Ref document number: 2004264995

Country of ref document: AU

Date of ref document: 20040816

Kind code of ref document: A

WWP Wipo information: published in national office

Ref document number: 2004264995

Country of ref document: AU

WWE Wipo information: entry into national phase

Ref document number: 869/CHENP/2006

Country of ref document: IN

WWE Wipo information: entry into national phase

Ref document number: 2004761133

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2006107982

Country of ref document: RU

DPEN Request for preliminary examination filed prior to expiration of 19th month from priority date (pct application filed from 20040101)
WWP Wipo information: published in national office

Ref document number: 1020067003184

Country of ref document: KR

WWP Wipo information: published in national office

Ref document number: 2004761133

Country of ref document: EP

WWE Wipo information: entry into national phase

Ref document number: 2007187059

Country of ref document: US

Ref document number: 10568011

Country of ref document: US

WWP Wipo information: published in national office

Ref document number: 10568011

Country of ref document: US