US3886994A - Device for making a casting of a directionally solidified alloy - Google Patents
Device for making a casting of a directionally solidified alloy Download PDFInfo
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- US3886994A US3886994A US473365A US47336574A US3886994A US 3886994 A US3886994 A US 3886994A US 473365 A US473365 A US 473365A US 47336574 A US47336574 A US 47336574A US 3886994 A US3886994 A US 3886994A
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- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 39
- 239000000956 alloy Substances 0.000 title claims abstract description 39
- 238000005266 casting Methods 0.000 title claims abstract description 23
- 238000007711 solidification Methods 0.000 claims abstract description 28
- 230000008023 solidification Effects 0.000 claims abstract description 28
- 238000010438 heat treatment Methods 0.000 claims abstract description 21
- 239000007788 liquid Substances 0.000 claims abstract description 13
- 239000007791 liquid phase Substances 0.000 claims abstract description 12
- 229910001092 metal group alloy Inorganic materials 0.000 claims abstract description 5
- 230000000750 progressive effect Effects 0.000 claims abstract description 5
- 238000001816 cooling Methods 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 5
- 239000000203 mixture Substances 0.000 claims description 3
- 238000003860 storage Methods 0.000 claims description 3
- 238000000034 method Methods 0.000 abstract description 10
- 229910001338 liquidmetal Inorganic materials 0.000 description 9
- 239000007790 solid phase Substances 0.000 description 8
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 7
- 238000004519 manufacturing process Methods 0.000 description 6
- 239000012071 phase Substances 0.000 description 6
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 5
- 229910000753 refractory alloy Inorganic materials 0.000 description 4
- 230000003014 reinforcing effect Effects 0.000 description 4
- 230000007423 decrease Effects 0.000 description 3
- 239000000835 fiber Substances 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 229910052750 molybdenum Inorganic materials 0.000 description 3
- 239000011733 molybdenum Substances 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- 229910052721 tungsten Inorganic materials 0.000 description 3
- 239000010937 tungsten Substances 0.000 description 3
- 239000000498 cooling water Substances 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- FRWYFWZENXDZMU-UHFFFAOYSA-N 2-iodoquinoline Chemical compound C1=CC=CC2=NC(I)=CC=C21 FRWYFWZENXDZMU-UHFFFAOYSA-N 0.000 description 1
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 235000007319 Avena orientalis Nutrition 0.000 description 1
- 241000209763 Avena sativa Species 0.000 description 1
- 235000007558 Avena sp Nutrition 0.000 description 1
- 229910001018 Cast iron Inorganic materials 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- FNYLWPVRPXGIIP-UHFFFAOYSA-N Triamterene Chemical compound NC1=NC2=NC(N)=NC(N)=C2N=C1C1=CC=CC=C1 FNYLWPVRPXGIIP-UHFFFAOYSA-N 0.000 description 1
- LTPBRCUWZOMYOC-UHFFFAOYSA-N beryllium oxide Inorganic materials O=[Be] LTPBRCUWZOMYOC-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000012938 design process Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000003467 diminishing effect Effects 0.000 description 1
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- 239000011810 insulating material Substances 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- NFFIWVVINABMKP-UHFFFAOYSA-N methylidynetantalum Chemical compound [Ta]#C NFFIWVVINABMKP-UHFFFAOYSA-N 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000013021 overheating Methods 0.000 description 1
- 238000004382 potting Methods 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 239000011819 refractory material Substances 0.000 description 1
- 239000003870 refractory metal Substances 0.000 description 1
- 239000012783 reinforcing fiber Substances 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 229910003468 tantalcarbide Inorganic materials 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D27/00—Treating the metal in the mould while it is molten or ductile ; Pressure or vacuum casting
- B22D27/04—Influencing the temperature of the metal, e.g. by heating or cooling the mould
- B22D27/045—Directionally solidified castings
Definitions
- the present invention concerns a process and a device for casting parts and ingots. in particular, it enables the obtention of high strength alloy ingots intended to be cut for machining of parts which structure must be fine, homogeneous and free from micro-flaws such as microscopic voids and microscopic shrinkages.
- the art of the founder-moulder consists in judiciously disposing in the moulds sources of heat (deadheads that are metal reserves as well) and cold sources (coolers in sand moulds, cooled zones in cast iron moulds) in order to control the isotherm distribution and the temperature gradients.
- the isothermal areas, and consequently the interfaces of solidification remain approximately plane (an essential requirement for obtaining parallel fibers) only if the moulds and parts have small lateral dimensions.
- care must be taken to maintain within very restricted limits, the rate at which the solidification interface progresses, for example of the order of cm per hour. Consequently, using said processes, it is possible to produce only castings with small transverse dimensions at a very slow rate of production.
- FIGS. 1, 2 and 3 each representing a diagrammatic cross-section view of different embodiments.
- FIG. 1 illustrates the simplest form of embodiment of the moulding device according to the invention.
- the mould 1 is of a refractory material which is a good heat conductor, for example a molybdenum sheet covered by an appropriate potting, or else alumina externally reinforced with a molybdenum ring. lt rests on an alumina block 2, itself disposed on a copper plate 3 which is provided with circular channels through which passes a flow of cooling water supplied by autonomous circuits.
- a heat shield 4 of polished refractory metal for example molybdenum to decrease lateral loss of radiated heat.
- an molybdenum functioning as a heat shield, itself attached to a molybdenum ring insulating wall 5 increasing the efficiency of the shield.
- Resistances 6 in crown formation for example of tungsten strip are suspended by means of tubes 7 of refractory insulating material from a plate 8 of polished molybdenum ring 9 bearing against the wall 5.
- the resistances 6 are supplied by independant electrical power sources.
- the crucible which is of molybdenum, is vertically moveable. It is moved by a device not represented in the figure.
- the bottom of the crucible is connected to a calibrated central nozzle 11.
- the device of FIG. 1 is used as follows
- Crucible 10 is arranged in its lowest position so that the lower end of nozzle 11 is only a few millimeters from the bottom of mould l.
- the resistances 6 and the cooling channels of the cold source 3 are powered.
- crucible 10 is filled with liquid metal which flows at a slow, constant rate through calibrated nozzle 11.
- crucible 10 is raised progressively so that the nozzle 11 is always flush with the free surface I of the liquid metal within a few millimeters.
- the combination of the heat source constituted by the resistances 6 and of the cold source constituted by block 2 cooled by plate 3 causes a marked vertical heat flow while the lateral flow is very small owing to the insulating effect of shield 4 and wall 5.
- the electrical power supplied to resistances 6, the water flow rate of cold source 3 channels and the raising speed of crucible 10 and nozzle 11 are regulated in such a way that the solidification interface f of the casted metal progresses at the same speed as level I of the liquid metal.
- the thickness of the liquid phase is a few millimeters, and the temperature gradient across the solidification interface is uniform over its entire surface and is vertically oriented whatever the transverse dimensions of the mould.
- the method device according to the invention thus combine the required conditions for obtaining a casting having a fine, ordered structure free from micro-flaws.
- the device in FIG. 1 does not, however, enable a constant temperature gradient to be obtained in the vicinity of the solidification interface throughout the entire duration of the operation, since the distance between the interface and the heat source constituted by the resistances 6 decreases as casting progresses, whle the impedance or heat resistance imposed by the solidified metal to the heat flow going towards the cold source increases at the same time.
- the device of FIG. 2 enables the obtention of a sharper and more constant temperature gradient than that of FIG. 1. It comprises almost all the elements of FIG. 2, but shield 8 and support 9 are discarded.
- Crucible l and nozzle 11 are integral with a refractory plate 12 which, in addition supports tubes 7 and resistances 6. This arrangement enables the same distance to be maintained between resistances 6, the free surface I of the liquid metal and the interface f of solidification throughout casting by means of the upward movement of plate 12.
- the device of FIG. 2 does, however, enable aluminium alloy ingots having an ordered structure and a height of about cm to be obtained.
- FIG. 3 represents a device according to the invention which enables obtention of ingots of an even greater height and production of refractory alloys with ordered reinforcing phase.
- the invention enables a constant temperature gradient at the solidification interface to be obtained throughout the entire casting operation, despite the increasing resistance of the solid phase to the heat flow, by providing means to impose to the lower and of said solid phase a variable temperature according to a law of the following kind.
- the invention thus allows for the fact that the temperature T, of the lower end of the solid phase must vary in inverse proportion to the height H to preserve a constant gradient G.
- the invention provides different constructive solutions meeting this requirement while ensuring evacuation of the heat flow through this liquid and solid phases, for example a. applying an auxiliary, diminishing heat flow to the lower end of the solid phase, using an auxiliary source of heat in contact with the bottom of the mould (solution adopted in FIG. 3)
- variable heat resistance for example a liquid layer of variable thickness
- the device in FIG. 3 shows different embodiments in the system supplying the bath, and in the system heating the bath, which is an inductor 18.
- the alloy is supplied in the form of a strip or wire 13 driven and guided by rollers 14 integral with plate 12 and it is fed by a storage real not represented in the figure. It is pushed towards the bath through a nozzle 15 and, on passing through, is progressively heated by resistances 16 which bring it close to the melting point temperature. Melting is induced by the radiation of surface I of the bath.
- the water circulation channels are here made by machining the upper surface of the plate 3 on which block 2 is brazed.
- Tungsten strip heating resistances 17 are set in the upper face of block 2 and are in contact with mould 1.
- a refractory wall 18 in which are set tungsten strip resistances 19.
- the device in FIG. 3 allows the obtention of a temperature gradient in the vicinity of the solidification interface that is substantially constant and uniform throughout the entire duration of the cast ing operation.
- lateral heat losses may be completely eliminated by judiciously adjusting heating of wall 19 b.
- the increased heat resistance of the solid portion s of the alloy may be compensated for by reducing the temperature of resistances 17 as solidification progresses,
- the block 2 is 99.5 alumina and is 25 mm thick.
- the cooling water is at a temperature of C.
- the temperature of the heat source resistances 6 is adjusted so that they are brought to 2,250C and calculation shows that the heat flow through the bath is about 30 W/cm.
- the temperature of resistances 17 will be decreased progressively from 1,350C to 350C.
- the device in FIG. 3 enables the production of castings or ingots of refractory alloys, with an ordered reinforcing phase, the size of which may reach 1501mm and the diameter 200 mm or more.
- the invention may comprise arrangements other than those illustrated in the given examples.
- the alloy may be brought to the surface of the bath not only in a liquid form or in the form of a wire or strip, but also as a powder.
- the bath may be heated not only by radiant resistantes, but also by induction or electron flow.
- the material with a variable heat transmission coefficient constituting block 2 of FIG. 3 may be made of alumina but also, for example, of beryllium oxide.
- the alloy may be supplied to the mould by means of several lines 11 or nozzles 15 judiciously distributed.
- the heating means are constituted by elements radiating the heating energy and facing said free surface
- the lateral walls of the mould are surrounded by heat insulating walls.
- heating device further comprises means for maintaining constant the distance between the radiating elements and the free surface of the liquid bath.
- the alloy introducing means comprise a device for feeding the alloy in the form of a wire or strip.
- the heat shield is constituted by a plate of a material which heat conductivity varies in inverse proportion to its own temperature.
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Abstract
A method and device are disclosed for casting parts and ingots of a metallic alloy with an ordered structure obtained by the progressive solidification of a liquid alloy. The device comprises a thin walled mould means for introducing the alloy into the mould having at least one duct and means for maintaining the lower end of the duct at a constant distance from the free surface of the liquid phase, heating means constituted by elements radiating heating energy and facing said free surface, and heat insulating means around the lateral walls of the mould.
Description
United States Patent Daigne et a1. June 3, 1975 [54] DEVICE FOR MAKING A CASTING ()F A 1,042,092 10/1912 Custer 164/133 3,405,220 10/1968 Barrow et al. 13/27 DIRECTIONALLY SOLIDIFIED ALLOY 3,620,288 1 H1971 Barrow et a1. 164/52 [75] Inventors: Bernard Daigne, Chatillon; Francois Girard, Paris, both of France [73] Assignee: Office National dEtudes et de 'f Exami'ferFranci5 Husar Recherches Aerospafiales Assistant ExammerJohn E. Roethel Attorney, Agent, or FirmMorse, Altman, Oates & Chatillon-sous-Bagneux, France B6110 [221 Filed: May 28, 1974 21 A l. N .2 473,365 I 1 W o 57 ABSTRACT Related US. Application Data 1 1 Division Of 301,633, 06L 1972. A method and device are disclosed for casting parts 3333-729 and ingots of a metallic alloy with an ordered struc- 0 ture obtained by the progressive solidification of a liq- 1 1 Foreign pp Priority Data uid alloy. The device comprises a thin walled mould Nov. 5, 1971 France 71.39703 means for introducing the alloy into the mould having at least one duct and means for maintaining the lower [52] US. Cl 164/250; 164/338 end of the duct at a constant distance from the free [51] Int. Cl B2211 27/02 surface of the liquid phase, heating means constituted [58] Field 01' Search 164/50, 51', 60, 122, 124, by elements radiating heating energy and facing said 5 25, 127. 133, 136, 250, 338 H, 348, 371 free surface, and heat insulating means around the lateral walls of the mould. [56] References Cited UNITED STATES PATENTS 11 Claims, 3 Drawing Figures 901,361 10/1908 McCarty [64/136 DEVICE FOR MAKING A CASTING OF A DIRECTIONALLY SOLIDIFIED ALLOY This is a division, of application Ser. No. 30l,638, filed on Oct. 27, I972, now U.S. Pat. No. 3,838,729.
The present invention concerns a process and a device for casting parts and ingots. in particular, it enables the obtention of high strength alloy ingots intended to be cut for machining of parts which structure must be fine, homogeneous and free from micro-flaws such as microscopic voids and microscopic shrinkages.
It is particularly suitable for the manufacture of refractory alloy ingots or parts having an ordered or directional structure and eventually comprising a reinforcement phase of metallic compounds fibers.
It is known that, in order to obtain fine ingots or fine castings, care must be taken to ensure that the zones in the process of solidification are supplied with liquid metal as the solidification areas or interfaces are in movement, in order to espacially compensate the decreases in volume resulting from the shrinkage accompanying solidification. This precaution consists in making the isotherm and isobar surfaces coincide as much as possible in the zones that are in the process of solidification. It is also known that the solidification structure is all the finer and sounder as the greater the temperature gradients are in the vicinity of the solidification interfaces. The art of the founder-moulder consists in judiciously disposing in the moulds sources of heat (deadheads that are metal reserves as well) and cold sources (coolers in sand moulds, cooled zones in cast iron moulds) in order to control the isotherm distribution and the temperature gradients.
While it is enough for the majority of castings, to approximately observe the above conditions, this is not the case when castings or ingots of refractory alloys with a very fine and compact structure and with an ordered reinforcing phase have to be produced. The reinforcing fibers appear during solidification and their orientation corresponds precisely to that of the temperature gradients and their continuity may be seriously affected if the values of said gradients are not sufficient in certain zones.
We have thus been led to design processes and devices for controlled solidification such as those described in US. Pat. N 3,124,452 and the C.l.P. Application Ser. No. 268,751 in which are described devices comprising a heat source surrounding the upper portion of the mould and shifting at the same rate as the interface of solidification and a cold source located at the lower portion of the mould. While providing advantageous results, these devices and processes may be industrially exploited on a small scale only.
On the one hand, the isothermal areas, and consequently the interfaces of solidification, remain approximately plane (an essential requirement for obtaining parallel fibers) only if the moulds and parts have small lateral dimensions. On the other hand, in order to obtain sharp temperature gradients without excessive overheating of the liquid metal, care must be taken to maintain within very restricted limits, the rate at which the solidification interface progresses, for example of the order of cm per hour. Consequently, using said processes, it is possible to produce only castings with small transverse dimensions at a very slow rate of production.
By using the method and the device according to the invention, it is possible to obtain ingots or castings made of high strength alloys and, in particular, ingots having an ordered structure, with relatively large lateral dimensions and from which a great number of parts may be cut, thus considerably increasing the production rate.
Reference is now made, to provide non-limitative examples of the embodiment of the invention, to FIGS. 1, 2 and 3, each representing a diagrammatic cross-section view of different embodiments.
FIG. 1 illustrates the simplest form of embodiment of the moulding device according to the invention.
The mould 1 is of a refractory material which is a good heat conductor, for example a molybdenum sheet covered by an appropriate potting, or else alumina externally reinforced with a molybdenum ring. lt rests on an alumina block 2, itself disposed on a copper plate 3 which is provided with circular channels through which passes a flow of cooling water supplied by autonomous circuits.
Surrounding the crucible l, are found successively a heat shield 4 of polished refractory metal, for example molybdenum to decrease lateral loss of radiated heat. and an molybdenum, functioning as a heat shield, itself attached to a molybdenum ring insulating wall 5 increasing the efficiency of the shield.
The crucible, which is of molybdenum, is vertically moveable. It is moved by a device not represented in the figure. The bottom of the crucible is connected to a calibrated central nozzle 11.
The device of FIG. 1 is used as follows Crucible 10 is arranged in its lowest position so that the lower end of nozzle 11 is only a few millimeters from the bottom of mould l. The resistances 6 and the cooling channels of the cold source 3 are powered. When thermal equilibrium is attained, crucible 10 is filled with liquid metal which flows at a slow, constant rate through calibrated nozzle 11. As the level of liquid metal rises in the mould, crucible 10 is raised progressively so that the nozzle 11 is always flush with the free surface I of the liquid metal within a few millimeters.
It is noteworthy that the combination of the heat source constituted by the resistances 6 and of the cold source constituted by block 2 cooled by plate 3 causes a marked vertical heat flow while the lateral flow is very small owing to the insulating effect of shield 4 and wall 5. By means of preliminary adjustment trials, the electrical power supplied to resistances 6, the water flow rate of cold source 3 channels and the raising speed of crucible 10 and nozzle 11 are regulated in such a way that the solidification interface f of the casted metal progresses at the same speed as level I of the liquid metal. Since the free surface of the bath is not disturbed by the casting, since the height of fall of the liquid metal is almost zero, the thickness of the liquid phase is a few millimeters, and the temperature gradient across the solidification interface is uniform over its entire surface and is vertically oriented whatever the transverse dimensions of the mould.
There is no disadvantage in the capacity of crucible 10 to be less than that of the mould. Since nozzle 11 regulates the casting rate, it is always possible, during the operation, to add liquid metal to the crucible.
The method device according to the invention thus combine the required conditions for obtaining a casting having a fine, ordered structure free from micro-flaws.
The device in FIG. 1 does not, however, enable a constant temperature gradient to be obtained in the vicinity of the solidification interface throughout the entire duration of the operation, since the distance between the interface and the heat source constituted by the resistances 6 decreases as casting progresses, whle the impedance or heat resistance imposed by the solidified metal to the heat flow going towards the cold source increases at the same time.
Now, the production of alloys having a directional reinforcement phase such as those of US. C.l.P. Application Ser. No. 268,751 not only requires the solidification interface to progress at a constant speed, but also requires the temperature gradients to remain constantly greater than a critical value below which cristallization degenerates.
The device of FIG. 2 enables the obtention of a sharper and more constant temperature gradient than that of FIG. 1. It comprises almost all the elements of FIG. 2, but shield 8 and support 9 are discarded. Crucible l and nozzle 11 are integral with a refractory plate 12 which, in addition supports tubes 7 and resistances 6. This arrangement enables the same distance to be maintained between resistances 6, the free surface I of the liquid metal and the interface f of solidification throughout casting by means of the upward movement of plate 12.
Although the heat impedance opposed by the solid phase s to the heat flow travelling between interface f and the cold source remains variable, since it increases as casting progresses, the device of FIG. 2 does, however, enable aluminium alloy ingots having an ordered structure and a height of about cm to be obtained.
FIG. 3 represents a device according to the invention which enables obtention of ingots of an even greater height and production of refractory alloys with ordered reinforcing phase.
Before going on to describe it, it should be noted that, at this stage of development, the invention enables a constant temperature gradient at the solidification interface to be obtained throughout the entire casting operation, despite the increasing resistance of the solid phase to the heat flow, by providing means to impose to the lower and of said solid phase a variable temperature according to a law of the following kind.
s j C(T) d T G C ll 1 T, being the temperature of the lower end of the in- T the alloy solidification temperature,
C (T) the heat conductivity of the solid phase at temperature T,
C the heat conductivity of the liquid phase in the vicinity of the solidification interface,
G the temperature gradient in the liquid phase in the vicinity of the interface,
H the height of the solid phase.
According to this equation, the invention thus allows for the fact that the temperature T, of the lower end of the solid phase must vary in inverse proportion to the height H to preserve a constant gradient G.
The invention provides different constructive solutions meeting this requirement while ensuring evacuation of the heat flow through this liquid and solid phases, for example a. applying an auxiliary, diminishing heat flow to the lower end of the solid phase, using an auxiliary source of heat in contact with the bottom of the mould (solution adopted in FIG. 3)
b. placing a decreasing thermal resistance under said lower end,
either, for example, by using a material having a heat conductivity varying in inverse proportion to its own temperature to make the support block of the mould (solution adopted in FIG. 3) or the lower wall of the mould,
or, for example, by inserting into the support a variable heat resistance, for example a liquid layer of variable thickness.
These different arrangements may be employed independantly.
It will be noted that the device in FIG. 3 shows different embodiments in the system supplying the bath, and in the system heating the bath, which is an inductor 18. The alloy is supplied in the form of a strip or wire 13 driven and guided by rollers 14 integral with plate 12 and it is fed by a storage real not represented in the figure. It is pushed towards the bath through a nozzle 15 and, on passing through, is progressively heated by resistances 16 which bring it close to the melting point temperature. Melting is induced by the radiation of surface I of the bath.
The water circulation channels are here made by machining the upper surface of the plate 3 on which block 2 is brazed. Tungsten strip heating resistances 17 are set in the upper face of block 2 and are in contact with mould 1.
Finally, between the lateral wall of mould l and shield 4 is inserted a refractory wall 18 in which are set tungsten strip resistances 19.
By judiciously dimensioning the different elements, by regulating the heating voltages and the other functional parameters, the device in FIG. 3 allows the obtention of a temperature gradient in the vicinity of the solidification interface that is substantially constant and uniform throughout the entire duration of the cast ing operation.
In fact,
a. lateral heat losses may be completely eliminated by judiciously adjusting heating of wall 19 b. the increased heat resistance of the solid portion s of the alloy may be compensated for by reducing the temperature of resistances 17 as solidification progresses,
c. finally, a very interesting property, in this respect, of certain materials'such as alumina, which has a heat conductivity coefficient varying in inverse proportion to the temperature, is exploited in order to compensate even more efficiently for said increase in heat resistance.
The above will now be illustrated using a numerical example.
it is desired to obtain a mm high alloy ingot with an ordered reinforcing phase, in a cobalt/nickelchrome matrix reinforced by tantalum carbide fibers.
The block 2 is 99.5 alumina and is 25 mm thick. The cooling water is at a temperature of C. The temperature of the heat source resistances 6 is adjusted so that they are brought to 2,250C and calculation shows that the heat flow through the bath is about 30 W/cm. During solidification, the temperature of resistances 17 will be decreased progressively from 1,350C to 350C.
Calculation will show that, under these conditions, the thickness of the liquid bath will be of the order of 15 mm and that, during the entire process of solidification, the thermal gradient in the bath will be of the order of 100C/cm, a suitable value for the chosen alloy. As a certain thermal gradient fluctuation is admissible in many cases, the device in FIG. 3 enables the production of castings or ingots of refractory alloys, with an ordered reinforcing phase, the size of which may reach 1501mm and the diameter 200 mm or more.
The invention may comprise arrangements other than those illustrated in the given examples. Thus, the alloy may be brought to the surface of the bath not only in a liquid form or in the form of a wire or strip, but also as a powder.
The bath may be heated not only by radiant resistantes, but also by induction or electron flow.
The material with a variable heat transmission coefficient constituting block 2 of FIG. 3 may be made of alumina but also, for example, of beryllium oxide.
The alloy may be supplied to the mould by means of several lines 11 or nozzles 15 judiciously distributed.
We claim:
1. Device for casting parts and ingots of a metallic alloy with an ordered structure obtained by the progressive solidification of a liquid alloy and comprising a thin walled mould, means for introducing into the mould an alloy with suitable initial composition, means for heating the liquid phase of the alloy introduced into the mould and means for cooling the lower portion of the mould, wherein a. the means for introducing the alloy comprise at least one duct and means for maintaining the lower end of the duct at a constant distance from the free surface of the liquid phase,
b. the heating means are constituted by elements radiating the heating energy and facing said free surface,
c. the lateral walls of the mould are surrounded by heat insulating walls.
2. Device according to claim 1, wherein the radiating elements are electrical resistances.
3. Device according to claim 2, wherein the radiating elements are inductors.
4. Device according to claim 1, wherein the heating device further comprises means for maintaining constant the distance between the radiating elements and the free surface of the liquid bath.
5. Device according to claim 1, wherein the means for introducing the alloy into the mould comprise a liquid alloy storage device and the duct is a nozzle through which the liquid alloy flows.
6. Device according to claim 1, wherein the alloy introducing means comprise a device for feeding the alloy in the form of a wire or strip.
7. Device according to claim 6, wherein the supply means further comprise a wire or strip heating device.
8. Device according to claim 1, further comprising a heat shield inserted between the lower wall of the mould and the cooling means of said lower wall.
9. Device according to claim 8, wherein the heat shield is constituted by electrical resistances.
10. Device according to claim 8, wherein the heat shield is constituted by a plate of a material which heat conductivity varies in inverse proportion to its own temperature.
11. Device according to claim 1, wherein the heat insulating walls surrounding the lateral walls of the mould comprise a wall in which are set electrical resistances. l
Claims (11)
1. Device for casting parts and ingots of a metallic alloy with an ordered structure obtained by the progressive solidification of a liquid alloy and comprising a thin walled mould, means for introducing into the mould an alloy with suitable initial composition, means for heating the liquid phase of the alloy introduced into the mould and means for cooling the lower portion of the mould, wherein : a. the means for introducing the alloy comprise at least one duct and means for maintaining the lower end of the duct at a constant distance from the free surface of the liquid phase, b. the heating means are constituted by elements radiating the heating energy and facing said free surface, c. the lateral walls of the mould are surrounded by heat insulating walls.
1. Device for casting parts and ingots of a metallic alloy with an ordered structure obtained by the progressive solidification of a liquid alloy and comprising a thin walled mould, means for introducing into the mould an alloy with suitable initial composition, means for heating the liquid phase of the alloy introduced into the mould and means for cooling the lower portion of the mould, wherein : a. the means for introducing the alloy comprise at least one duct and means for maintaining the lower end of the duct at a constant distance from the free surface of the liquid phase, b. the heating means are constituted by elements radiating the heating energy and facing said free surface, c. the lateral walls of the mould are surrounded by heat insulating walls.
2. Device according to claim 1, wherein the radiating elements are electrical resistances.
3. Device according to claim 2, wherein the radiating elements are inductors.
4. Device according to claim 1, wherein the heating device further comprises means for maintaining constant the distance between the radiating elements and the free surface of the liquid bath.
5. Device according to claim 1, wherein the means for introducing the alloy into the mould comprise a liquid alloy storage device and the duct is a nozzle through which the liquid alloy flows.
6. Device according to claim 1, wherein the alloy introducing means comprise a device for feeding the alloy in the form of a wire or strip.
7. Device according to claim 6, wherein the supply means further comprise a wire or strip heating device.
8. Device according to claim 1, further comprising a heat shield inserted between the lower wall of the mould and the cooling means of said lower wall.
9. Device according to claim 8, wherein the heat shield is constituted by electrical resistances.
10. Device according to claim 8, wherein the heat shield is constituted by a plate of a material which heat conductivity varies in inverse proportion to its own temperature.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US473365A US3886994A (en) | 1971-11-05 | 1974-05-28 | Device for making a casting of a directionally solidified alloy |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR7139703A FR2158138B1 (en) | 1971-11-05 | 1971-11-05 | |
| US00301638A US3838729A (en) | 1971-11-05 | 1972-10-27 | Method for making a casting of a directionally solidified alloy |
| US473365A US3886994A (en) | 1971-11-05 | 1974-05-28 | Device for making a casting of a directionally solidified alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3886994A true US3886994A (en) | 1975-06-03 |
Family
ID=27249690
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US473365A Expired - Lifetime US3886994A (en) | 1971-11-05 | 1974-05-28 | Device for making a casting of a directionally solidified alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3886994A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0218087A3 (en) * | 1985-09-10 | 1988-02-10 | Bayer Ag | Method for the melting and directional solidification of metals |
| EP0218088A3 (en) * | 1985-09-10 | 1988-02-10 | Bayer Ag | Method for the directional solidification of metal melts |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US901361A (en) * | 1907-08-02 | 1908-10-20 | George O Eaton | Molding process. |
| US1042092A (en) * | 1910-06-03 | 1912-10-22 | Custer Sandless Casting Company | Art of casting steel. |
| US3405220A (en) * | 1965-07-16 | 1968-10-08 | United Aircraft Corp | Induction electric mold heater |
| US3620288A (en) * | 1969-06-27 | 1971-11-16 | United Aircraft Corp | Directionally solidified castings |
-
1974
- 1974-05-28 US US473365A patent/US3886994A/en not_active Expired - Lifetime
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US901361A (en) * | 1907-08-02 | 1908-10-20 | George O Eaton | Molding process. |
| US1042092A (en) * | 1910-06-03 | 1912-10-22 | Custer Sandless Casting Company | Art of casting steel. |
| US3405220A (en) * | 1965-07-16 | 1968-10-08 | United Aircraft Corp | Induction electric mold heater |
| US3620288A (en) * | 1969-06-27 | 1971-11-16 | United Aircraft Corp | Directionally solidified castings |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0218087A3 (en) * | 1985-09-10 | 1988-02-10 | Bayer Ag | Method for the melting and directional solidification of metals |
| EP0218088A3 (en) * | 1985-09-10 | 1988-02-10 | Bayer Ag | Method for the directional solidification of metal melts |
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