GB1592255A - Method of continuous casting of metallic strips - Google Patents
Method of continuous casting of metallic strips Download PDFInfo
- Publication number
- GB1592255A GB1592255A GB4234977A GB4234977A GB1592255A GB 1592255 A GB1592255 A GB 1592255A GB 4234977 A GB4234977 A GB 4234977A GB 4234977 A GB4234977 A GB 4234977A GB 1592255 A GB1592255 A GB 1592255A
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- United Kingdom
- Prior art keywords
- chill
- molten metal
- nozzle
- strip
- metal
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- 238000009749 continuous casting Methods 0.000 title description 2
- 229910052751 metal Inorganic materials 0.000 claims abstract description 110
- 239000002184 metal Substances 0.000 claims abstract description 110
- 238000001816 cooling Methods 0.000 claims abstract description 16
- 239000005300 metallic glass Substances 0.000 claims abstract description 10
- 238000007711 solidification Methods 0.000 claims description 15
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- 229910045601 alloy Inorganic materials 0.000 claims description 10
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- 238000010791 quenching Methods 0.000 claims description 10
- 238000000151 deposition Methods 0.000 claims description 9
- 239000011261 inert gas Substances 0.000 claims description 8
- 239000007787 solid Substances 0.000 claims description 8
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- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
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- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 1
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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F1/00—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
- H01F1/01—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
- H01F1/03—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
- H01F1/12—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials
- H01F1/14—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of soft-magnetic materials metals or alloys
- H01F1/147—Alloys characterised by their composition
- H01F1/153—Amorphous metallic alloys, e.g. glassy metals
- H01F1/15341—Preparation processes therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/06—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
- B22D11/0611—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars formed by a single casting wheel, e.g. for casting amorphous metal strips or wires
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/06—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
- B22D11/0631—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars formed by a travelling straight surface, e.g. through-like moulds, a belt
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D11/00—Continuous casting of metals, i.e. casting in indefinite lengths
- B22D11/06—Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
- B22D11/0637—Accessories therefor
- B22D11/0697—Accessories therefor for casting in a protected atmosphere
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Chemical & Material Sciences (AREA)
- Dispersion Chemistry (AREA)
- Power Engineering (AREA)
- Continuous Casting (AREA)
Abstract
Molten metal is applied under pressure, through a slit nozzle (10), to a moving cooling body (7). The slit nozzle (10) is arranged directly adjacent to the surface of the cooling body (7). The cooling body (7) moves past the slit nozzle (10) at a surface velocity of 100 to 2000 m/min. The distance between the slit nozzle (10) and the surface of the cooling body (7) is 0.03 to 1 mm. These dimensions permit high-speed production of continuous polycrystalline metal strips and amorphous metal strips with hitherto unachieved dimensions of isotropic thickness and other isotropic properties, e.g. magnetisability. <IMAGE>
Description
(54) METHOD OF CONTINUOUS CASTING OF METALLIC STRIPS
(71) We, ALLIED CHEMICAL CORPORATION, a Corporation organised and existing under the laws of the State of New York, United States of America, of Columbia
Road and Park Avenue, Morris Township, Morris County, New Jersey, 07960, United
States of America, do hereby declare the invention for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly described in and by the following statement:
This invention relates to a method of making continuous metal strips, particularly metal strips with an amorphous molecular structure, by depositing molten metal onto the moving surface of a chill body by forcing the metal through a slotted nozzle located in close proximity to the surface of the chill body.
For purposes of the present invention, a strip is a slender body whose transverse dimensions are much less than its length and which may have a regular or irregular cross section.
There has long been recognized the need for processes which would permit manufacture of finished or semi-finished products such as wire, ribbon or sheet directly from the molten metal. Hubert et al. provided a review of such processes and classified then available technology into the "melt spin process" and the "melt drag process", [Zeitschrift fuer
Metallkunde 64, 835-843 (1973).
In the melt spin process, a jet of molten metal is cooled, either in free flight or by jetting it against a chill block, to obtain continuous filament. Both of these embodiments employ a pressurized orifice. There is also a melt spin process operating without an orifice, wherein molten metal is supplied to a jet-forming device, such as a grooved spinning disc, to be expelled therefrom. Hubert et al. stated that the key to success in the melt spin process is to stabilize the liquid jet until it solidifies. Jets of molten metal are inherently unstable since they have a strong tendency for droplet formation on account of the low viscosity and high surface tension of molten metal. Basic problems of jet stability have been discussed by
Butler et al., in Fiber Science and Technology 5 243-262 (1972).
In the melt drag process British Patent Specification No 1160934, molten metal is made to form a meniscus held on by surface tension, at the outlet of a nozzle. From this meniscus molten metal is then dragged onto a rotating continuous cooled drum or belt. This method avoids the difficulties of jet instability inherent in the melt spin process. Unfortunately, however, the speed of the moving chill surface in the melt drag process is severely restricted due to restriction in melt flow at the meniscus, or else only discontinuous filament is obtained. Also, it is believed that the melt drag process is not readily adaptable to provide sufficiently high rates of cooling of the molten metal to permit production of amorphous metal strips. Such strips require rapid quenching of certain molten alloys at a cooling rate of at least 104"C per second, more usually 106"C per second.
Continuous amorphous metal strips of narrow widths and thicknesses have heretofore been made by the melt spin process involving rapid quenching of a jet of molten metal directed against a moving chill surface, such as the inside or outside of a rotating roll, or a moving belt. The molten alloy jet which is to be quenched is stable due to its high velocity for a relative short distance, say 3 to about 6 millimeters. When it hits the rapidly moving chill substrate (velocity typically between about 1300 and about 2000 meters per minute) it wets it and forms a puddle. That puddle is essentially stationary in space as the moving substrate draws it out into a strip, which is travelling at the same speed as the substrate. In actual application, it has been found that, using a single jet, the maximum width of strip so obtained from a jet of substantially circular cross section is limited to about 5 to 6 millimeters. Attempts to provide wider strips of impinging a sheet-like jet against a moving chill surface met with little success, principally because the wide jet initially does not form a smooth line puddle as required to obtain a uniform, wide product, and consequently produces kinky, nonuniformly quenched strip.
It is also possible to impinge a plurality of parallel, uniform jets properly spaced onto a moving substrate to form a relatively wide strip. This approach, however, has inherent difficulties inasmuch as it requires a close matching of the jet velocities and spacings with the substrate speed. The principal difficulty is that either the jets do not join together to form a puddle, or the jets run together to form a ridge, so that, from a practical standpoint, it is difficult to obtain strips with uniform cross sections. Moreover, since the molten metal puddle deposited by the jets onto the chill substrate tends to assume the equilibrium shape of a droplet, thick at the center and thin at the edges, it is very difficult, if not impossible, to maintain a puddle of sufficiently uniform thickness for "drawing out" strips having even approximately uniform cross section wider than about 7.5 mm.
In any event, it has not been possible to obtain wide metal strips, say wider than about 6 millimeters, having isotropic strengths, by single or multiple jet casting procedures that is to say having identical tensile strengths and elongation measured in the transverse as well as in the longitudinal direction, or in any direction therebetween, even though metal strips with amorphous structures should be isotropic at least with respect to their tensile properties, and those with cast polycrystalline structures should be approximately isotropic. Anisotropic tensile properties of wide strips of amorphous metal obtained by multiple jet casting procedure are believed to be caused by inherent imperfections in the strips obtained by that procedure. Significantly, however, strips made by jet casting procedures, regardless of width, lack uniformity of thickness, measured transversely, and they are prone to show significant variations in width along their length. They lack such uniformity of thickness because they are drawn out from a puddle of liquid metal, which puddle has a strong tendency to assume the equilibrium shape of a droplet on account of the high surface tension of molten metal; they are prone to variations in width because even slight unavoidable variations in the flow rate of the molten metal through the orifice to form the jet will cause variations in the diameter of the puddle with resultant variations in width of the strip drawn therefrom.
U. S. P. 3,862,658 to Bedell inter alia discloses a method for making amorphous strips (filaments) by ejecting molten alloy into the nip of two closely spaced counter-rotating steel rolls. This method provides for rapid, effective cooling of the melt, but involves rolling of the solidified strip between the steel rolls, as a result of which the product has anisotropic tensile properties. By that method Bedell obtained an amorphous ribbon of 0.012 centimeters thickness and 1.27 centimeters width (Example 4 of U. S. P. 3,862,658).
It has been found that, if a thin uniform layer of molten metal is mechanically supported on a chill surface by the method of our invention, it becomes possible to draw out thin metal strips in the form of ribbons and sheets with aspect ratios (width/thickness) ranging from unity to any desired value, as below described.
Accordingly, the present invention provides a method of forming continuous strip of metal from a molten metal comprising: forcing the molten metal under pressure through a nozzle having an outlet orifice in the form of a slot, the nozzle being positioned generally perpendicular to the direction of movement of a chill surface and located in close proximity thereto to provide a gap of from 0.03 to 1 millimeter between the nozzle and the chill surface; advancing the chill surface relative to the nozzle at a velocity of from 200 to 2000 meters per minute; and quenching the molten metal in contact with the chill surface at a rapid rate to effect solidification. Preferably the quenching is at a rate of at least 104"C per second to effect solidification into a continuous amorphous metal strip. The length of the slot (measured perpendicular to the direction of movement of the chill surface) will determine the width of the strip being cast and, as a practical consideration, should not be longer than the width of the chill surface.
According to another aspect of the invention there is provided a method of forming a continuous metal strip by depositing molten metal onto the surface of a moving chill body, which comprises: (a) moving the surface of a chill body in a longitudinal direction at a constant predetermined velocity of from 100 to 2000 meters per minute past the orifice slot of a nozzle defined by a pair of generally parallel lips located proximate to said surface such that the gap between the lips and the surface is from 0.03 to 1 millimeter, said orifice being arranged generally perpendicular to the direction of movement of the surface of said chill body; and (b) forcing a stream of molten metal through the orifice of the nozzle into contact with the surface of the moving chill body to permit the metal to solidify thereon to form a continuous strip.
Means for effecting expulsion of the molten metal contained in a reservoir through the nozzle for deposition onto the moving chill surface include pressurization of the reservoir, such as by an inert gas, or utilization of the hydrostatic head of molten metal if the level of metal in the reservoir is located in sufficiently elevated position.
In our copending Divisional Application No. 7935142 Serial No 1592257) we claim apparatus for making continuous metal strip from a melt comprising, in combination:
(a) a movable chill body providing a chill surface for deposition thereon of molten metal for solidification, means being provided for driving the chill body at a speed to provide longitudinal movement of said chill surface at a velocity of from 100 to 2000 metres per minute; and
(b) a reservoir for holding molten metal, said reservoir including heating means for maintaining the temperature of the metal above its melting point, said reservoir being in communication with
(c) a nozzle having an orifice slot for depositing molten metal onto said chill surface, located in close proximity to said chill surface, the orifice slot being arranged generally perpendicular to the direction of movement of the chill surface and being defined by a pair of parallel lips, a first lip and a second lip numbered in direction of movement of the chill surface, wherein said slot has a width of from 0.3 to about 1 millimetre, measured in direction of movement of the chill surface, wherein said first lip has a width at least equal to the width of said slot, and said second lip has a width of from 1.5 to 3 times the width of said slot, wherein the gap between the lips and the chill surface is between 0.03 and 1 millimetres and from 0.1 to 1 times the width of said slot;
(d) the apparatus being adapted to operate with means being provided for effecting expulsion of the molten metal contained in said reservoir through said nozzle for deposition onto the moving chill surface.
Strips made by the method of the present invention are specifically claimed in our copending Divisional Application No. 7935141, (Serial No 1592256) which claims a continuously cast strip of amorphous metal having a width of at least 7 millimeters, preferably at least 1 centimeter, and having isotropic tensile properties.
The invention will be further described by way of example, with reference to the accompanying drawings, wherein:
Figure 1 of the drawings provides a side view in partial cross-section illustrating formation of strip from molten metal deposited onto a moving chill surface from a nozzle having specific configuration and placement with relation to the chill surface, in accordance with the present invention;
Figures 2 and 3 of the drawings each provide a somewhat simplified perspective view of two embodiments of apparatus which may be used to practice the method of the present invention in operation. In Figure 2, formation of strip takes place on the surface of a chill roll mounted to rotate around its longitudinal axis. In Figure 3, formation of strip takes place on the surface of an endless moving belt;
Figure 4 provides a side view in cross-section of a nozzle in its relation to the surface of the chill substrate for discussion of relative dimensions of slot width, lip dimensions, and gap between lip and chill surface;
Figure 5 provides a cross-sectional view taken in a plane perpendicular to direction of movement of the chill surface illustrating a preferred embodiment of a nozzle employed in the practice of the present invention providing concave-shaped internal side walls; Figures 6 and 7 each provide a schematic view of the shape of the slot of a slotted nozzle in accordance with the present invention, seen from the surface of the chill substrate. Figure 6 illustrates a generally rectangular slot: Figure 7 illustrates a slot having enlarged (lobed) end sections.
The method of casting a continuous strip of the present invention may be termed "planar flow casting." Its principle of operation is explained in the following with reference to
Figure 1.
Figure 1 shows in partial cross section a side view illustrating the method of the present invention. As shown in Figure 1, a chill body 1, here illustrated as a belt, travels in the direction of the arrow in close proximity to a slotted nozzle defined by a first lip 3 and a second lip 4. Molten metal 2 is forced under pressure through the nozzle to be brought into contact with the moving surface of the chill body. As the metal is solidified in contact with the surface of the moving chill body, a solidification front, indicated by line 6, is formed.
Above the solidification front a body of molten metal is maintained. A shown in the illustrated method the solidification front barely misses the end of second lip 4. First lip 3 supports the molten metal essentially by the pumping action of the melt which results from constant removal of solidified strip 5. The surface of the moving chill body 1 travels at a velocity within the range of from 100 to 2000 meters per minute. The rate of flow of molten metal equals the rate of removal of metal in the form of solid strip and is self-controlled.
The rate of flow is pressure assisted, but controlled by the forming solidification front and the second lip 4 which mechanically defines the depth of the molten metal below it. Thus, the rate of flow of the molten metal is primarily controlled by the viscous flow between the second lip and the solid strip being formed, and is not primarily controlled by the slot width.
In order to obtain a sufficiently high quench-rate to make an amorphous ribbon, the surface of the chill body must ordinarily move at a velocity of at least 200 meters per minute. At lower velocities it is generally not possible to obtain quench rates, that its to say cooling rates at the solidification temperature, of at least 104"C. per second, as is required in order to obtain amorphous metal strips. Of course, lower velocities, as low as about 100 meters per minute, are usually operable, but result in polycrystalline strips. And, in any event, casting by the present process of metal alloys which do not form amorphous solids will result in polycrystalline strips, regardless of the velocity of travel of the chill surface. The velocity of movement of the chill surface should not be in excess of 2000 meters per minute because as the speed of the substrate increases, the height of the solidification front is depressed due to decreased time available for solidification. This leads to formation of thin strip (thickness less than 0.02 millimeter). Since the success of the process hinges on thorough wetting of the chill substrate by the molten metal, and since very thin layers of molten metal (e.g.
thinner than 0.02 millimeter) do not adequately wet the chill substrate, thin, porous strip is obtained which is not commercially acceptable. This is particularly pronounced if the casting operation is carried out other than in vacuum, since currents of the ambient gas, such as air, have substantial adverse influence on strip formation at higher substrate speeds.
As a general proposition, it can be stated that an increase in chill surface velocity results in production of thinner strip and, conversely, that a reduction of that velocity results in thicker strip. Preferably, velocities range from 300 to 1500, more preferably from 600 to 1000 meters per minute.
In order to obtain solid continuous strip of uniform cross section, certain dimensions concerning the nozzle and its interrelationship with the chill surface are critical. They are explained with reference to Figure 4 of the drawings. With reference to Figure 4, width a of the slot of the slotted nozzle, which slot is arranged perpendicular to the direction of movement of the chill surface, should be from 0.3 to about 1 millimeter, preferably from 0.6 to 0.9 millimeter. As previously stated, the width of the slot does not primarily control the rate of flow of molten metal therethrough, but it might become a limiting factor if it is too narrow. While, to some extent that may be compensated for by employing higher pressures to force the molten metal at the required rate through the narrower slot, it is more convenient to provide a slot of sufficient width, If, on the other hand, the slot is too wide, say wider than about 1 millimeter, then at any given velocity of movement of the chill surface, the solidification front formed by the metal as it solidifies on the chill surface will be correspondingly longer, resulting in a thicker strip which could not be cooled at a rate sufficient to obtain amorphous strip, if this were desired.
With further reference to Figure 4, width b of second lip 4 is from 1.5 to 3 times the width of the slot, preferably from 2 to 2.5 times the width of the slot. Optimum width can be determined by simple routine experimentation. If the second lip is too narrow, then it will fail to provide adequate support to the molten metal and only discontinuous strip is produced. If, on the other hand, the second lip is too wide, solid-to-solid rubbing between the lip and the strip will result, leading to rapid failure of the nozzle. With further reference to Figure 4, width c of first lip 3 must be at least substantially equal to the width of the slot, preferably at least 1.5 times the width of the slot. If the first lip is too narrow, then the molten metal will tend to ooze out, the molten metal will not uniformly wet the chill surface, and no strip, or only irregular strip will be formed. Preferred dimensions of the first lip are from 1.5 to 3, more preferably from 2 to 2.5 times the width of the slot.
Still with reference to Figure 4, the gaps 1 between the surface of the chill body 1 and first and second lips 3 and 4, respectively represented by d and e, and which may be of the same or different depths as illustrated, may be from 0.03 to 1 millimeter, preferably from 0.03 to 0.25 millimeter, more preferably yet from 0.08 to 0.15 millimeter. A gap in excess of 1 millimeter would cause flow of the molten metal to be limited by slot width rather than by the lips. Strips produced under this condition are thicker, but are of non-uniform thickness.
Moreover, they usually are insufficiently quenched and consequently have non-uniform properties. Such product lacks commercial acceptability. On the other hand, a gap of less than 0.03 millimeter would lead to solid-to-solid contact between the solidification front and the nozzle when the slot width is in excess of 0.3 millimeter, leading to rapid failure of the nozzle. Within the above parameters, the gaps 1 between the surface of the chill body and the lips may vary. A larger gap may, for example, be provided on one side than on the other, so that a strip of varying thickness across its width is obtained.
When the chill surface is a flat surface, such as a belt, the gaps between the surface of the chill surface and the first and second lips represented by dimensions d and e in Figure 4 may be equal. If however, the movable chill body furnishing the chill surface is an annular chill roll then these gaps may not be equal, or else the strip formed will not separate from the chill roll, but it will be carried around the perimeter of the roll and will hit and destroy the nozzle. We have surprisingly found that this can be avoided by making gap d smaller than gap e, that is to say, by providing a smaller gap between the first lip and the chill surface than between the second lip and the chill surface. We have further surprisingly found that the larger the difference in the sizes 1 of the gaps 1 between the first and the second lip and the chill surface, the closer to the nozzle the strip will separate from the chill surface so that, by controlling the difference between these gaps, the point of separation of the strip from the annular chill roll can be controlled. Such difference in gaps can be established by slight tilting or off-centre mounting of the nozzle so that its exit points in the direction of rotation of the chill roll. We have further noted that residence time of the strip on an annular chill roll tends to increase with increasing gap between the nozzle and the chill surface.
Within the above parameters, when, for example, the chill surface may be moved at a velocity of 700 meters per minute, the width of the slot may be between 0.5 to 0.8 millimeter. The second lip should be between 1.5 to 2 times the width of the slot, and the first lip should be 1 to 1.5 times the width of the slot. The metal in the reservoir should be pressurized to between 0.5 to 2 psig. The gap between the second lip and the substrate may be between 0.05 and 0.2 millimeter. If an annular chill roll is employed, the gap between the first lip and the surface of the chill body must be less than the gap between the second lip and the surface of the chill body, as above discussed. This can, for example, be accomplished by off-center mounting of the nozzle. Increasing the gap and/or the gas pressure increases the strip thickness when the velocity of movement chill surface remains unchanged.
With reference to Figure 2 of the drawings, which provides a perspective view of apparatus for carrying out the method of the present invention, there is shown an annular chill roll 7 rotably mounted around its longitudinal axis, and reservoir 8 for holding molten metal equipped with induction heating coils 9. Reservoir 8 is in communication with slotted nozzle 10, which, as above described, is mounted in close proximity to the surface of annular chill roll 7. Annular chill roll 7 may optionally be provided with cooling means (not shown), as means for circulating a cooling liquid, such as water, through its interior.
Reservoir 8 is further equipped with means (no shown) for pressurizing the molten metal contained therein to effect expulsion thereof through nozzle 10. In operation, molten metal maintained under pressure in reservoir 8 is ejected through nozzle 10 onto the surface of the rotating chill roll 1, whereon it immediately solidifies to form strip 11. Due to unequal gaps between the first and second lips of the nozzle and the chill roll surface, as above discussed, strip 11 separates form the chill roll and is flung away therefrom to be collected by a suitable collection device (not shown). In Figure 2 there is further shown nozzle 11a adapted to direct a stream of inert gas, such as helium, argon or nitrogen, against the surface of the chill roll before it reaches the slotted nozzle 10, for purposes described further below.
The embodiment illustrated in Figure 3 of the drawings employs as chill body an endless belt 12 which is placed over rolls 13 and 13a which are caused to rotate by external means (not shown). Molten metal is provided from reservoir 14, equipped with means for pressurizing the molten metal therein (not shown). Molten metal in reservoir 14 is heated by electrical induction heating coil 15. Reservoir 14 is in communication with nozzle 16 equipped with a slotted orifice. In operation, belt 10 is moved at a longitudinal velocity of at least about 600 meters per minute. Molten metal from reservoir 14 is pressurized to force it through nozzle 16 into contact with belt 12, whereon it is solidified into a solid strip 17 which is separated from belt 12 by means not shown.
The surface of the chill body which provides the actual chill surface can be any metal having relatively high thermal conductivity, such as copper. This requirement is particularly applicable if it is desired to make amorphous or metastable strips. Preferred materials of construction include beryllium copper and oxygen free copper. If desired, the chill surface may be highly polished or may be provided with a highly uniform surface, such as chrome plate, to obtain filament having smooth surface characteristics. To provide protection against erosion, corrosion, or thermal fatigue, the surface of the chill body may be coated with a suitable resistant or high melting coating, for example, a ceramic coating, or with a coating of corrosion resistant high melting metal, which may be applied by known procedures provided that in each case the wettability of the molten metal on the chill substrate is adequate.
In short run operation it will not ordinarily be necessary to provide cooling for the chill body provided it has relatively large mass so that it can act as a heat sink and absorb considerable amount of heat. However, for longer runs, and especially if the chill body is a belt which has relatively little mass, cooling of the chill body is desirably provided. This may be conveniently accomplished by contacting it with cooling media which may be liquids or gases. If the chill body is a chill roll, water or other liquid cooling media may be circulated through it,or air or other gases may be blown over it. Alternatively, evaporative cooling may be employed, as by externally contacting the chill body with water or any other liquid medium which through evaporation provides cooling. Even though one might expect considerable variations in thickness along the length of the strip due to thermal expansion of the chill surface as the casting process progresses, we have in our experiments surprisingly found that equilibrium conditions apparently are established very rapidly, within production of a few meters of strip, and that thereafter the strip is of remarkably uniform thickness from end to end. For example, thickness along the length of the strip has been found to vary as little as about +5 percent. This is particularly remarkable since ordinarily unavoidable runout of the chill roll will be of larger magnitude than the variation in thickness. In a way, the process is self-compensating for wear-generated variations in gap between lips and chill surface. Furthermore, strip made by the process is of remarkably uniform width, with variations in width along the length having been measured as small as about to0.0004 centimeter. Such uniformity of width is believed to be unobtainable employing conventional melt spin procedures; strip of such uniform width would ordinarily only be obtained employing cutting procedures.
The slotted nozzle employed for depositing molten metal onto the chill surface may be constructed of any suitable material. Desirably, a material is chosen which is not wetted by the molten metal. A convenient material of construction is fused silica, which may be blown into desired shape and then be provided with a slotted orifice by machining. For the sake of convenience, the reservoir and the nozzle may be shaped from a single piece of material. A suitable form of nozzle employing concave lower walls terminating in a slot is illustrated in
Figure 5. Nozzles of that configuration have been found very effective. The shape of the slot may be substantially rectangular as illustrated by Figure 6. Preferably, the ends of the slot are lobed, as in generally rounded form as illustrated in Figure 7 to provide adequate flow of molten metal at the marginal portions. The velocity of flow of metal near the nozzle walls is always lower than the velocity near the center. Therefore, when a rectangular slot such as illustrated by Figure 6 is employed, the amount of molten metal available at the marginal portions is less than at the center, resulting in a filament having tapered or serrated edges.
If, on the other hand, the slot is formed with lobed ends, as shown in Figure 7, adequate flow of molten metal at the end of the slot is provided and a smooth-edged filament is obtained.
The molten metal which is to be formed into a strip is heated, preferably in an inert atmosphere, to a temperature approximately 50 to 100"C. above its melting point or higher. A slight vacuum may be applied to the vessel holding the molten metal to prevent premature flow of the molten metal through the nozzle. Ejection of the molten metal through the nozzle is required and may be effected by the pressure of the static head of the molten metal in the reservoir, or prefe impingement methods of the prior art. Furthermore, jet impingement methods of the prior art are not capable of making strips having width in excess of about 6 millimeters and having isotropic tensile properties. The described method provides for uniformity of quench due to reduced momentum transfer, inter alia, which appears to be an important factor for obtainment of high quality product strip.
Furthermore, the method provides ready means for casting of metal in an inert atmosphere. Such inert atmosphere may be readily provided by the simple expedient of directing a stream of inert gas such as nitrogen, argon or helium against the moving chill surface ahead of the nozzle, as illustrated in Figure 2. By this simple expedient, it is possible to cast reactive alloys such as Fe70Mo10cl8B2 which burn readily when exposed to air in molten form and which cannot be cast in air by conventional jet impingement methods.
The process may be carried out in air, in a partial or high vacuum, or in any desired atmosphere which may be provided by an inert gas such as nitrogen, argon helium. When it is conducted in vacuum, it is desirably conducted under vacuum within the range of from about 100 up to about 3000 microns. We have made the surprising discovery that in the process use of vacuum below about 100 or 50 microns has unexpectedly adverse influence on adhesion of the metal strip to the chill surface, with resultant tendency to form imperfect, insufficiently quenched strip. An amorphous quenching alloy may lack ductility and be brittle instead. We have no explanation for this phenomenon at present. In the present process the benefits of operation under vacuum, viz. improved uniformity of the strip product and elimination of oxidative attack, are obtained by operation under vacuum within the above stated range, preferably by operation under vacuum within the range of from about 200 micron to about 2000 micron. The benefit of operation in an inert atmosphere is obtained by merely directing a stream of the inert gas against the surface of the moving chill body ahead of the nozzle as above described. Alternatively, the apparatus can be enclosed in a suitable housing which is then evacuated, or the air in the housing may be replaced with the desired inert gas. While the method of the present invention is particularly suited for making amorphous metal strips because of the improved quench rate which it provides, as above discussed, it is also eminently suited for making strips of polycrystalline metals and of nonductile or brittle alloys which are not readily formable into strip using conventional procedures.
The preferred product of the present invention is a strip of metal with an amorphous molecular structure having width of at least 7 millimeters, preferably at least 1 centimeter, and, more preferably yet, having width of at least 3 centimeters. The strip is at least 0.02 millimeter thick, but may be as thick as 0.14 millimeter, or thicker, depending on the melting point, solidification and crystallization characteristics of the alloy employed. The product has isotropic tensile properties, as above described. These tensile properties are conveniently determine on tensile specimens cut from the strip in various directions, viz.
longitudinal, transverse, and at angles therebetween, employing standard tensile testing methods and apparatus. The product is further characterized by smooth, even surfaces, and uniformity of cross section as well as of thickness and width along its length. It has all of the advantageous properties of known amorphous metal strips, so that it is suitable for use in applications in which such strips have been previously employed, e.g. in cutting implements and magnetic shielding devices. In these applications its greater width is a decided advantage. Additionally, because of its greater width coupled with its isotropic tensile properties, it is eminently suited for use as reinforcement material, particularly in composite structures.
The following examples illustrate the present invention and set forth the best mode presently contemplated for its practice.
Example 1
Apparatus employed is similar to that depicted in Figure 2. The chill roll employed has a diameter of 16 inches and it is 5 inches wide. It is rotated at a speed of about 700 rpm, corresponding to a linear velocity of the peripheral surface of the chill roll of about 895 meters per minute. A nozzle having a slotted orifice of 0.9 millimeter width and 51 millimeter length defined by a first lip of 1.8 millimeters width and a second lip of 2.4 millimeters width (lips numbered in direction of rotation of the chill roll) is mounted perpendicular to the direction of movement of the peripheral surface of the chill roll, such that the gap between the second lip and the surface of the chill roll is 0.05 millimeter, and the gap between the first lip and the surface of the chill roll is 0.06 millimeter. Metal having composition Fe4nNi40P14B6 with a melting point of about 950"C. is employed. It is supplied to the nozzle from a pressurized crucible wherein it is maintained under pressure of about 0.7 psig at temperature of 1000"C. Pressure is supplied by means of an argon blanket. The molten metal is expelled through the slotted orifice at the rate of 14 kilograms per minute.
It solidifies on the surface of the chill roll into a strip of 0.05 millimeter thickness having width of 5 centimeters. Upon examination using X-ray diffractometry, the strip is found to be amorphous in structure. Tensile specimens cut from the strip in longitudinal and transverse direction exhibit equal tensile strength and elongation. The strip has isotropic tensile properties.
Examples 2 to 6
The procedure of Example 1 was repeated, employing the equipment, process conditions, metal and alloys summarized in the Table, below, to obtain the products described in the Table.
TABLE
Example 2 3 4 5 6
Metal (alloy) Cu Cu+1 CU+8 Al+3 Pd80Si20
wt% Zn wt% Al wt% Cu (atomic %)
Chill roll diameter
(inch) 16 16 16 16 7 1/2
Chill roll width (inch) 4 5 4 4 11/2
Chill Roll rpm 714 714 714 600 1600
Nozzle orifice width
(mm) 0.635 0.635 0.635 0.762 1.01
Nozzle orifice length
(mm) 3 6 10 12 12
Width first lip (mm) 1.15 1.15 1.15 1.6 1.6
Width second lip (mm) 2 2 2 2 1.8
Gas-second lip to chill
roll (mm) 0.12 0.12 0.12 0.12 0.25
Gap-first lip to chill
roll (mm) 0.15 0.15 0.15 0.15 0.28
Melting point of metal ( C) 1083 1075 1060 655 950 Pressure applied to
crucible (psig) 0.7 0.7 0.7 0.5 0.5
Temp. of metal in
crucible approx. ("C) 1150 1150 1150 680 1000
Thickness of strip
(0.001 in.) 2 2 2 2 8
Width of strip (mm) 3 6 10 12 12
Structure of strip + polycrystalline > amorphous
Claims (15)
1. A method of forming continuous strip of metal from a molten metal comprising: forcing the molten metal under pressure through a nozzle having an outlet orifice in the form of a slot, the nozzle being positioned generally perpendicular to the direction of movement of a chill surface and located in close proximity thereto to provide a gap of from 0.03 to 1 millimeter between the nozzle and chill surface; advancing the chill surface relative to the nozzle at a velocity of from 200 to 2000 meters per minute; and quenching the molten metal in contact with the chill surface at a rapid rate to effect solidification.
2. A method according to claim 1, wherein the molten metal is quenched at a rate of at least 104"C per second to effect solidification into a continuous amorphous metal strip.
3. A metal according to claim 1 or 2, wherein the nozzle orifice has a width of from 0.03 to about 1 millimeter, measured in direction of movement of the chill surface.
4. A method according to claim 3, wherein the step of forcing the molten metal through the nozzle orifice is conducted under vacuum up from 100 to 3000 microns.
5. A method according to any preceding claim, wherein the step of forcing the molten metal through nozzle orifice is conducted in an inert atosphere.
6. A method according to any preceding claim, wherein the chill surface is provided by rotating chill roll, and the molten metal is deposited onto its peripheral surface.
7. A method according to claim 6, wherein a stream of inert gas is directed against the surface of the chill roll before the chill surface is contacted by the molten metal.
8. A method according to any one of claims 1 to 5, wherein the chill surface is provided by a moving belt.
9. A method according to claim 8, wherein the belt is a moving endless belt.
10. A method of forming a continuous metal strip by depositing molten metal onto the surface of a moving chill body, which comprises: (a) moving the surface of a chill body in a longitudinal direction at a constant predetermined velocity of from 100 to 2000 meters per minute past the orifice slot of a nozzle defined by a pair of generally parallel lips located proximate to said surface such that the gap between the lips and the surface is from 0.03 to 1 millimeter, said orifice being arranged generally perpendicular to the direction of movement of the surface of said chill body; and (b) forcing a stream of molten metal through the orifice of the nozzle into contact with the surface of the moving chill body to permit the metal to solidify thereon to form a continuous strip.
11. A method according to claim 10, wherein the molten metal is an alloy which upon cooling from the melt and quenching at a rate of at least about 104"C/sec. forms an amorphous solid; the surface of the chill body having a velocity of at least 200 meters per minute.
12. A method according to claim 10 or 11, wherein the molten metal is forced through a nozzle having a width of from 0.3 to about 1 millimeter, measured in direction of movement of the chill body and the molten metal is deposited under vacuum of from 100 to 3000 microns.
13. A method according to claim 10 or 11, wherein the molten metal is forced through the orifice of the nozzle into contact with the surface of a moving chill roll and wherein a stream of inert gas is directed against the surface of the moving chill roll before it is contacted by the molten metal.
14. A method of forming a continuous metal strip by depositing molten metal onto the surface of a moving chill body, such method being substantially as hereinbefore described with reference to the accompanying drawings.
15. A strip of polycrystalline metal when made by the method of claim 1 or 10.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US73477676A | 1976-10-22 | 1976-10-22 | |
US05/821,110 US4142571A (en) | 1976-10-22 | 1977-08-02 | Continuous casting method for metallic strips |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1592255A true GB1592255A (en) | 1981-07-01 |
Family
ID=27112782
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3514279A Expired GB1592257A (en) | 1976-10-22 | 1977-10-11 | Apparatus for making continuously cast metallic strip |
GB3514179A Expired GB1592256A (en) | 1976-10-22 | 1977-10-11 | Continuously cast amorphous metal strip |
GB4234977A Expired GB1592255A (en) | 1976-10-22 | 1977-10-11 | Method of continuous casting of metallic strips |
Family Applications Before (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3514279A Expired GB1592257A (en) | 1976-10-22 | 1977-10-11 | Apparatus for making continuously cast metallic strip |
GB3514179A Expired GB1592256A (en) | 1976-10-22 | 1977-10-11 | Continuously cast amorphous metal strip |
Country Status (10)
Country | Link |
---|---|
JP (1) | JPS5942586B2 (en) |
AU (1) | AU503857B2 (en) |
CA (1) | CA1078111A (en) |
CH (1) | CH625438A5 (en) |
DE (1) | DE2746238C2 (en) |
FR (2) | FR2368324A1 (en) |
GB (3) | GB1592257A (en) |
IT (1) | IT1116337B (en) |
NL (1) | NL176150C (en) |
SE (2) | SE433712B (en) |
Families Citing this family (49)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU503857B2 (en) * | 1976-10-22 | 1979-09-20 | Allied Chemical Corp. | Continuous casting of metal strip |
US4142571A (en) * | 1976-10-22 | 1979-03-06 | Allied Chemical Corporation | Continuous casting method for metallic strips |
DE2856795C2 (en) * | 1977-12-30 | 1984-12-06 | Noboru Prof. Sendai Tsuya | Use of molten steel for a method of continuously casting a thin strip |
JPH029900B2 (en) * | 1978-05-11 | 1990-03-05 | Allied Signal Inc | |
DE2830522A1 (en) * | 1978-07-12 | 1980-01-31 | Licentia Gmbh | Silicon strip foil or sheet for solar cells - made by pouring molten stream of silicon onto rotating plate or wheel so continuous cast prod. is obtd. |
JPS5528357A (en) * | 1978-08-19 | 1980-02-28 | Sumitomo Special Metals Co Ltd | Manufacture of fine crystalline, thin continuous body- shaped liquid quenched metal |
SE448381B (en) * | 1978-09-19 | 1987-02-16 | Tsuya Noboru | SET TO MAKE A THIN BAND OF SILICONE, THIN BAND AND APPLICATION |
EP0009603B1 (en) * | 1978-09-29 | 1982-05-26 | Vacuumschmelze GmbH | Method and apparatus for the production of metallic strips |
JPS5558935A (en) * | 1978-10-27 | 1980-05-02 | Matsushita Electric Ind Co Ltd | Edge tool and electric razor |
US4212343A (en) * | 1979-03-16 | 1980-07-15 | Allied Chemical Corporation | Continuous casting method and apparatus for structurally defined metallic strips |
US4285386A (en) * | 1979-03-16 | 1981-08-25 | Allied Chemical Corporation | Continuous casting method and apparatus for making defined shapes of thin sheet |
JPS55165261A (en) * | 1979-06-13 | 1980-12-23 | Hitachi Ltd | Roll device for rapid cooling of molten metal |
US4258756A (en) * | 1979-08-27 | 1981-03-31 | Allied Chemical Corporation | Composite shell |
DE2938709A1 (en) * | 1979-09-25 | 1981-04-02 | Vacuumschmelze Gmbh, 6450 Hanau | METHOD AND DEVICE FOR PRODUCING AMORPHOUS METAL BANDS |
JPS5662660A (en) * | 1979-10-29 | 1981-05-28 | Hitachi Ltd | Producing equipment of thin metal strip |
JPS5669344A (en) * | 1979-11-07 | 1981-06-10 | Showa Alum Ind Kk | Aluminum alloy for forging and its manufacture |
JPS5667905A (en) * | 1979-11-07 | 1981-06-08 | Hitachi Metals Ltd | Improvement method of magnetic characteristic |
DE2950406C2 (en) * | 1979-12-14 | 1986-12-04 | Hitachi Metals, Ltd., Tokyo | Device for the continuous casting of a metal strip |
FR2471824A1 (en) * | 1979-12-20 | 1981-06-26 | Hitachi Ltd | Casting wheel for mfg. metal strip - where gas jet produces smooth cast surface, esp. on amorphous metal strip made of iron-nickel-boron-silicon alloys |
DE3000889C2 (en) * | 1980-01-11 | 1984-07-26 | Siemens AG, 1000 Berlin und 8000 München | Use of a metal foil rotating around two rolls for continuous casting of amorphous silicon |
US4658885A (en) * | 1980-05-09 | 1987-04-21 | Battelle Development Corporation | Method of repetitiously marking continuously cast metallic strip material |
JPS6043221B2 (en) * | 1980-06-27 | 1985-09-27 | 株式会社日立製作所 | Thin plate manufacturing equipment |
US4330025A (en) * | 1980-09-11 | 1982-05-18 | Allegheny Ludlum Steel Corporation | Nozzle in a strip casting apparatus |
YU96781A (en) * | 1980-10-06 | 1983-12-31 | Allegheny Ludlum Steel | Device for casting bands |
US6296948B1 (en) * | 1981-02-17 | 2001-10-02 | Ati Properties, Inc. | Amorphous metal alloy strip and method of making such strip |
JPS58157245U (en) * | 1982-04-14 | 1983-10-20 | 古河電気工業株式会社 | Molten metal spout nozzle for manufacturing metal ribbon |
DE3364158D1 (en) * | 1982-04-15 | 1986-07-24 | Allied Corp | Apparatus for the production of magnetic powder |
EP0111728A3 (en) * | 1982-11-12 | 1985-04-03 | Concast Standard Ag | Method of and device for producing products in the shape of strips or foils |
JPS59183957A (en) * | 1983-03-31 | 1984-10-19 | Hitachi Metals Ltd | Production of thin metallic strip |
JPS6021160A (en) * | 1983-07-13 | 1985-02-02 | Matsushita Electric Ind Co Ltd | Production of ultraquickly cooled light-gage metallic strip |
JPS60108144A (en) * | 1983-11-18 | 1985-06-13 | Nippon Steel Corp | Production of thin metallic strip |
DE3442009A1 (en) * | 1983-11-18 | 1985-06-05 | Nippon Steel Corp., Tokio/Tokyo | AMORPHOUS ALLOY TAPE WITH LARGE THICKNESS AND METHOD FOR THE PRODUCTION THEREOF |
JPS60177936A (en) * | 1984-02-25 | 1985-09-11 | Nippon Steel Corp | Thin strip consisting of fe-base amorphous alloy having large thickness |
FR2558085B1 (en) * | 1984-01-18 | 1987-05-15 | Usinor | PROCESS AND DEVICE FOR THE ELABORATION OF LOW THICKNESS METAL AND SEMI-METAL TAPES |
JPS60194779U (en) * | 1984-06-04 | 1985-12-25 | ソニー株式会社 | tape cassette |
JPS619947A (en) * | 1984-06-25 | 1986-01-17 | Kawasaki Steel Corp | Production of thin amorphous alloy strip |
JPS6163346A (en) * | 1984-09-06 | 1986-04-01 | Nippon Steel Corp | Production of thin amorphous metallic strip having large thickness |
JPS61147950A (en) * | 1984-12-20 | 1986-07-05 | Nippon Steel Corp | Production of thin porous metallic strip |
JPS61159246A (en) * | 1984-12-28 | 1986-07-18 | Hitachi Metals Ltd | Production of amorphous metallic ribbon |
JPS61182982U (en) * | 1985-05-02 | 1986-11-14 | ||
FR2583133B1 (en) * | 1985-06-11 | 1988-02-05 | Inst Francais Du Petrole | PIPING FOR USE IN PARTICULAR FOR TRANSPORTING FLUIDS AND FOR LIMITING PERMEABILITY TO TRANSPORTED FLUIDS |
EP0225901B1 (en) * | 1985-06-11 | 1989-12-20 | Institut Français du Pétrole | Conduit usable particularly for transporting fluids and enabling to limit the permeability to transported fluids |
FR2587783B2 (en) * | 1985-09-20 | 1988-05-20 | Inst Francais Du Petrole | PIPING FOR USE IN PARTICULAR FOR TRANSPORTING FLUIDS AND FOR LIMITING PERMEABILITY TO TRANSPORTED FLUIDS |
JPS62106090U (en) * | 1985-12-25 | 1987-07-07 | ||
JPS62199244U (en) * | 1986-06-10 | 1987-12-18 | ||
JPH0615099B2 (en) * | 1986-12-23 | 1994-03-02 | 東北金属工業株式会社 | Amorphous metal ribbon manufacturing method |
BR8807555A (en) * | 1987-07-21 | 1990-04-17 | Gomelsk Polt Inst | METAL FILM PRODUCTION PROCESS AND APPLIANCE FOR THE MATERIALIZATION OF Said Process |
DE3909091A1 (en) * | 1988-04-18 | 1989-10-26 | Lonza Ag | SCHLITZDUESENVORRICHTUNG |
JPH07102434B2 (en) * | 1989-10-19 | 1995-11-08 | 川崎製鉄株式会社 | Amorphous alloy ribbon manufacturing method |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US905758A (en) | 1908-03-14 | 1908-12-01 | Edward Halford Strange | Process of manufacturing thin sheets, foil, strips, or ribbons of zinc, lead, or other metal or alloy. |
CH461715A (en) | 1966-07-06 | 1968-08-31 | Battelle Development Corp | Process for manufacturing a continuous product from a molten material |
US3605863A (en) * | 1966-07-06 | 1971-09-20 | Battelle Development Corp | Apparatus for manufacturing wire and the like |
US3522830A (en) * | 1968-05-08 | 1970-08-04 | Standard Pressed Steel Co | Lock nut |
US3862658A (en) | 1973-05-16 | 1975-01-28 | Allied Chem | Extended retention of melt spun ribbon on quenching wheel |
CH604970A5 (en) * | 1974-11-01 | 1978-09-15 | Erik Allan Olsson | |
CA1068470A (en) | 1975-02-24 | 1979-12-25 | Allied Chemical Corporation | Production of improved metal alloy filaments |
AU503857B2 (en) * | 1976-10-22 | 1979-09-20 | Allied Chemical Corp. | Continuous casting of metal strip |
-
1977
- 1977-09-22 AU AU29048/77A patent/AU503857B2/en not_active Expired
- 1977-10-04 IT IT6919477A patent/IT1116337B/en active
- 1977-10-06 CA CA288,248A patent/CA1078111A/en not_active Expired
- 1977-10-10 NL NL7711091A patent/NL176150C/en not_active IP Right Cessation
- 1977-10-11 GB GB3514279A patent/GB1592257A/en not_active Expired
- 1977-10-11 GB GB3514179A patent/GB1592256A/en not_active Expired
- 1977-10-11 GB GB4234977A patent/GB1592255A/en not_active Expired
- 1977-10-12 SE SE7711476A patent/SE433712B/en not_active IP Right Cessation
- 1977-10-14 DE DE19772746238 patent/DE2746238C2/en not_active Expired
- 1977-10-18 CH CH1270877A patent/CH625438A5/en not_active IP Right Cessation
- 1977-10-20 FR FR7731659A patent/FR2368324A1/en active Granted
- 1977-10-21 JP JP12668577A patent/JPS5942586B2/en not_active Expired
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1978
- 1978-05-03 FR FR7813219A patent/FR2381581A1/en active Granted
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1983
- 1983-03-25 SE SE8301648A patent/SE460291B/en not_active IP Right Cessation
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SE7711476L (en) | 1978-04-23 |
FR2381581A1 (en) | 1978-09-22 |
DE2746238C2 (en) | 1982-12-02 |
DE2746238A1 (en) | 1978-04-27 |
SE8301648L (en) | 1983-03-25 |
CH625438A5 (en) | 1981-09-30 |
AU2904877A (en) | 1979-03-29 |
FR2368324A1 (en) | 1978-05-19 |
SE433712B (en) | 1984-06-12 |
GB1592256A (en) | 1981-07-01 |
JPS5942586B2 (en) | 1984-10-16 |
SE8301648D0 (en) | 1983-03-25 |
AU503857B2 (en) | 1979-09-20 |
JPS5353525A (en) | 1978-05-16 |
CA1078111A (en) | 1980-05-27 |
FR2368324B1 (en) | 1983-07-29 |
NL176150B (en) | 1984-10-01 |
NL7711091A (en) | 1978-04-25 |
GB1592257A (en) | 1981-07-01 |
SE460291B (en) | 1989-09-25 |
FR2381581B1 (en) | 1983-12-16 |
NL176150C (en) | 1985-03-01 |
IT1116337B (en) | 1986-02-10 |
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Effective date: 19971010 |