A process and apparatus for continuous casting of amorphous alloy sheets having large sheet thickness using bulk solidifying amorphous alloys are provided. Thick continuous amorphous alloy sheets made of bulk solidifying amorphous alloys are also provided.

Patent
   RE45414
Priority
Apr 14 2004
Filed
Aug 29 2012
Issued
Mar 17 2015
Expiry
Apr 14 2024
Assg.orig
Entity
Large
0
98
all paid
0. 21. An apparatus comprising:
a closed reservoir comprising a nozzle and a plunger, the reservoir configured for stabilizing a bulk solidifying amorphous alloy at a casting temperature below a melting temperature (Tm) of the alloy and above a temperature at which crystallization occurs on the shortest time scale for the alloy (TNOSE) such that the alloy is in a viscosity regime of about 0.1 to 10,000 poise; and at least two quench substrates configured for quenching the alloy at sufficiently fast rate such that the alloy remains in a substantially amorphous phase, to form a solid continuous sheet of the alloy, wherein the at least two quench substrates sandwich the alloy therebetween, wherein the reservoir is positioned vertically to contain the alloy and the nozzle is configured to discharge the alloy in a horizontal direction; wherein the solid continuous sheet has a thickness of at least 0.1 mm and the solid continuous sheet is a bulk solidifying amorphous alloy sheet.
0. 36. An apparatus comprising:
a closed reservoir comprising a nozzle and a plunger, the reservoir configured for stabilizing a bulk solidifying amorphous alloy at a casting temperature below a melting temperature (Tm) of the alloy and above a temperature at which crystallization occurs on the shortest time scale for the alloy TNOSE) such that the alloy is in a viscosity regime of about 0.1 to 10,000 poise; and at least two quench substrates configured for quenching the alloy at sufficiently fast rate such that the alloy remains in a substantially amorphous phase, to form a solid continuous sheet of the alloy, wherein the at least two quench substrates sandwich the alloy therebetween, wherein the nozzle is positioned with respect to the at least two quench substrates in a manner so as to discharge the alloy in a horizontal direction and cause the alloy to traverse from the nozzle to the at least two quench substrates in a substantially straight line, wherein the solid continuous sheet has a thickness of at least 0.1 mm and the solid continuous sheet is a bulk solidifying amorphous alloy sheet.
0. 1. A method for the continuous casting of sheets of an amorphous material comprising:
providing a quantity of a bulk a solidifying amorphous alloy at a temperature above the melting temperature of the bulk solidifying amorphous alloy;
stabilizing the bulk solidifying amorphous alloy at a casting temperature below the melting temperature (Tm) of the alloy and above the temperature at which crystallization occurs on the shortest time scale for the alloy (TNOSE) such that the bulk solidifying amorphous alloy is in a viscosity regime of about 0.1 to 10,000 poise;
introducing the stabilized bulk solidifying amorphous alloy onto a moving casting body such that a continuous sheet of heated bulk solidifying amorphous alloy is formed thereon; and
quenching the heated bulk solidifying amorphous alloy at a quenching rate sufficiently fast such that the bulk solidifying amorphous alloy remains in a substantially amorphous phase to form a solid amorphous continuous sheet having a thickness of at least 0.1 mm.
0. 2. The method of claim 1, wherein the viscosity of the bulk solidifying amorphous alloy at the “melting temperature” Tm of the bulk solidifying amorphous alloy is from about 10 to 100 poise.
0. 3. The method of claim 1, wherein the viscosity of the bulk solidifying amorphous alloy at the “melting temperature” Tm of the bulk solidifying amorphous alloy is from about 1 to 1000 poise.
0. 4. The method of claim 1, wherein the critical cooling rate of the bulk solidifying amorphous alloy is less than 1,000° C./sec.
0. 5. The method of claim 1, wherein the critical cooling rate of the bulk solidifying amorphous alloy is less than 10° C./sec.
0. 6. The method of claim 1, wherein the quenching occurs on the casting body.
0. 7. The method of claim 1, wherein the casting body is selected from the group consisting of a wheel, a belt, double-roll wheels.
0. 8. The method of claim 1, wherein the casting body is formed from a material having a high thermal conductivity.
0. 9. The method of claim 1, wherein the casting body is formed of a material selected from the group consisting of copper, chromium copper, beryllium copper, dispersion hardening alloys, and oxygen-free copper.
0. 10. The method of claim 1, wherein the casting body is at least one of either highly polished or chrome-plated.
0. 11. The method of claim 1, wherein the casting body moves at a rate of 0.5 to 10 cm/sec.
0. 12. The method of claim 1, wherein the casting temperature is stabilized in a viscosity regime of 1 to 1,000 poise.
0. 13. The method of claim 1, wherein the casting temperature is stabilized in a viscosity regime of 10 to 100 poise.
0. 14. The method of claim 1, wherein the solid amorphous alloy sheet has a thickness of 0.1 to 10 mm.
0. 15. The method of claim 1, wherein the solid amorphous alloy sheet has a thickness of 0.5 to 3 mm.
0. 16. The method of claim 1, wherein the heated alloy is introduced onto the casting body under pressure.
0. 17. The method of claim 1, wherein the bulk solidifying amorphous alloy can be described as (Zr,Ti)a(Ni,Cu,Fe)b(Be,Al,Si,B)c, where a is in the range of from 30 to 75, b is in the range of from 5 to 60, and c in the range of from 0 to 50 in atomic percentages.
0. 18. The method of claim 17, wherein the bulk solidifying amorphous alloy further comprises up to 20% atomic of at least one additional transition metal selected from the group consisting of Hf, Ta, Mo, Nb, Cr, V, Co.
0. 19. The method of claim 1, wherein the bulk solidifying amorphous alloy ferrous metal based.
0. 20. The method of claim 1 wherein the bulk solidifying amorphous alloy further comprises ductile crystalline phase precipitates.
0. 22. The apparatus of claim 21, wherein the viscosity of the alloy at the melting temperature Tm of the alloy is from about 10 to 100 poise.
0. 23. The apparatus of claim 21, wherein the viscosity of the alloy at the melting temperature Tm of the alloy is from about 1 to 1000 poise.
0. 24. The apparatus of claim 21, wherein the critical cooling rate of the alloy is less than 1,000° C./sec.
0. 25. The apparatus of claim 21, further comprising a casting body.
0. 26. The apparatus of claim 25, wherein the casting body comprises a material selected from the group consisting of copper, chromium copper, beryllium copper, dispersion hardening alloys, and oxygen-free copper.
0. 27. The apparatus of claim 25, wherein the casting body moves at a rate of 0.5 to 10 cm/sec.
0. 28. The apparatus of claim 21, wherein the bulk solidifying amorphous alloy is stabilized at a casting temperature such that the alloy is in a viscosity regime of 1 to 1,000 poise.
0. 29. The apparatus of claim 21, wherein the bulk solidifying amorphous alloy is stabilized at a casting temperature such that the alloy is in a viscosity regime of 10 to 100 poise.
0. 30. The apparatus of claim 21, wherein the solid amorphous alloy sheet has a thickness of 0.1 to 10 mm.
0. 31. The apparatus of claim 21, wherein the solid amorphous alloy sheet has a thickness of 0.5 to 3 mm.
0. 32. The apparatus of claim 25, wherein the alloy is introduced onto the casting body under pressure.
0. 33. The apparatus of claim 21, wherein the alloy can be described as (Zr,Ti)a(Ni,Cu,Fe)b(Be,Al,Si,B)c, where a is in the range of from 30 to 75, b is in the range of from 5 to 60, and c in the range of from 0 to 50 in atomic percentages.
0. 34. The apparatus of claim 21, wherein the alloy is ferrous metal based.
0. 35. The apparatus of claim 21 wherein the alloy further comprises ductile crystalline phase precipitates.
0. 37. The apparatus of claim 36, wherein the viscosity of the alloy at the melting temperature Tm of the alloy is from about 10 to 100 poise.
0. 38. The apparatus of claim 36, wherein the viscosity of the alloy at the melting temperature Tm of the alloy is from about 1 to 1000 poise.
0. 39. The apparatus of claim 36, wherein the critical cooling rate of the alloy is less than 1,000° C./sec.
0. 40. The apparatus of claim 36, further comprising a casting body.
0. 41. The apparatus of claim 40, wherein the casting body comprises a material selected from the group consisting of copper, chromium copper, beryllium copper, dispersion hardening alloys, and oxygen-free copper.
0. 42. The apparatus of claim 40, wherein the casting body moves at a rate of 0.5 to 10 cm/sec.
0. 43. The apparatus of claim 36, wherein the bulk solidifying amorphous alloy is stabilized at a casting temperature such that the alloy is in a viscosity regime of 1 to 1,000 poise.
0. 44. The apparatus of claim 36, wherein the bulk solidifying amorphous alloy is stabilized at a casting temperature such that the alloy is in a viscosity regime of 10 to 100 poise.
0. 45. The apparatus of claim 36, wherein the solid amorphous alloy sheet has a thickness of 0.1 to 10 mm.
0. 46. The apparatus of claim 36, wherein the solid amorphous alloy sheet has a thickness of 0.5 to 3 mm.
0. 47. The apparatus of claim 40, wherein the alloy is introduced onto the casting body under pressure.
0. 48. The apparatus of claim 36, wherein the alloy can be described as (Zr,Ti)a(Ni,Cu,Fe)b(Be,Al,Si,B)c, where a is in the range of from 30 to 75, b is in the range of from 5 to 60, and c in the range of from 0 to 50 in atomic percentages.
0. 49. The apparatus of claim 36, wherein the alloy is ferrous metal based.
0. 50. The apparatus of claim 36 wherein the alloy further comprises ductile crystalline phase precipitates.

This is a divisional reissue application of its parent reissue application Ser. No. 13/212,410, filed Aug. 18, 2011, which is the reissue of U.S. Pat. No. 7,575,040 (application Ser. No. 10/552,667, filed Jun. 21, 2006), which is a National Stage Entry of PCT/US04/11559, filed Apr. 14, 2004, all of which are incorporated herein by reference in their entireties.

This invention relates to continuous sheet casting of bulk-solidifying amorphous alloys, and, more particularly, to a method of continuous sheet casting amorphous alloy sheets having a large thickness.

Amorphous alloys have non-crystalline (amorphous) atomic structures generally formed by fast cooling the alloy from the molten liquid state to a solid state without the nucleation and growth of crystalline phases. As a result of the unique atomic structure produced during this process, amorphous alloys have high mechanical strength and good elasticity, while also exhibiting good corrosion resistance. Therefore, there is strong motivation in the materials field to find new applications for these materials in a variety of industries. However, because amorphous alloys require rapid cooling rates as they are solidified from temperatures above the melting state, it typically has only been possible to produce very thin ribbons or sheets of the alloys on a commercial scale, usually by a melt spin process wherein a stream of molten metal is rapidly quenched.

FIGS. 1a and 1b show partial cross sectional schematic side views of a conventional continuous sheet casting apparatus. In a conventional continuous sheet casting process and apparatus 1, as shown in FIG. 1a, there is an orifice 3 through which molten alloy from a reservoir 5 is injected onto a chilled rotating wheel 7 to form a solidified sheet 9. To provide a steady state flow of melt through the orifice, there are some complex relations that need to be satisfied between the applied pressure (or gravitational pull-down), the orifice slit size, the surface tension of the melt, the viscosity of the melt, and the pull-out speed of the solidification front. In the apparatus shown in FIG. 1a, the pull-out speed of the solidification front is primarily determined by the speed 11 of rotating wheel 7.

As shown, in the detailed view in FIG. 1b, the chill body wheel 7 travels in a clockwise direction in close proximity to a slotted nozzle 3 defined by a left side lip 13 and a right side lip 15. As the metal flows onto the chill body 7 it solidifies forming a solidification front 17. Above the solidification front 17 a body of molten metal 19 is maintained. The left side lip 13 supports the molten metal essentially by a pumping action which results from the constant removal of the solidified sheet 9. The rate of flow of the molten metal is primarily controlled by the viscous flow between the right side lip 15 and solidified sheet 9. In order to obtain a sufficiently high quench-rate to ensure that the formed sheet is amorphous, the surface of the chill body 7 must move at a velocity of at least about 200 meters per minute. This speed of rotation in turn limits the thickness of the sheets formed by the conventional process to less than about 0.02 millimeter.

Although it is possible to obtain quench rates at lower velocities, there are many difficulties that are encountered. For example, at typical melt viscosities and low wheel rotational speeds it is not possible to reliably sustain a continuous process. As a result, the melt may flow too fast through the orifice slit and spill over the wheel, precluding a stable melt puddle and a steady state moving solidification front. Although, some remedies can be implemented, such as reducing the orifice slit size, generally this is not a practical solution because the molten metal would erode the opening of such a small orifice very quickly. Despite these problems, an amorphous metal sheet having a sheet thickness ranging from 50 to 75 μm, and also retaining the mechanical properties of the amorphous alloys is disclosed in U.S. Pat. No. 6,103,396; however, the thickness range available for the disclosed process still leads to limitations in the types of applications in which such materials may be used.

Accordingly a need exists for a continuous process to cast thick sheets of bulk solidifying amorphous alloys.

The present invention is directed to a process and apparatus for continuous casting of amorphous alloy sheets having large sheet thickness using bulk solidifying amorphous alloys.

In one embodiment of the invention, the sheet is formed using conventional single roll, double roll, or other chill-body forms.

In another embodiment of the invention, the amorphous alloy sheets have sheet thicknesses of from 0.1 mm to 10 mm.

In one embodiment of the invention, the casting temperature is stabilized in a viscosity regime of 0.1 to 10,000 poise, preferably 1 to 1,000 poise, and more preferably 10 to 100 poise.

In one embodiment of the invention, the extraction of continuous sheet is preferably done at speeds of 0.1 to 50 cm/sec, and preferably 0.5 to 10 cm/sec, and more preferably of 1 to 5 cm/sec.

These and other features and advantages of the present invention will be better understood by reference to the following detailed description when considered in conjunction with the accompanying drawings wherein:

FIG. 1a is a side view in partial cross section of an exemplary conventional prior art apparatus for forming sheets of a molten metal.

FIG. 1b is a close-up of the formation of the sheet of molten metal shown in FIG. 1a.

FIG. 2 is a side view in partial cross section of an exemplary apparatus for forming sheets of a bulk solidifying amorphous alloy in accordance with the current invention.

FIG. 3 is block flow diagram of an exemplary method for continuous casting bulk solidifying amorphous alloys in accordance with the current invention.

FIG. 4 is a temperature-viscosity of an exemplary bulk solidifying amorphous alloy in accordance with the current invention.

FIG. 5 is a time-temperature transformation diagram for an exemplary continuous casting sequence in accordance with the current invention.

The present invention is directed to a continuous casting process and apparatus for forming an amorphous alloy sheet having a large sheet thickness using a bulk solidifying amorphous alloy. The invention recognizes that it is possible to form a sheet of large thickness using bulk-solidifying amorphous alloys at high viscosity regimes.

For the purposes of this invention, the term amorphous means at least 50% by volume of the alloy is in amorphous atomic structure, and preferably at least 90% by volume of the alloy is in amorphous atomic structure, and most preferably at least 99% by volume of the alloy is in amorphous atomic structure.

Bulk solidifying amorphous alloys are a recently discovered family of amorphous alloys, which can be cooled at substantially lower cooling rates, of about 500 K/sec or less, and substantially retain their amorphous atomic structure. As such, they can be produced in thicknesses of 1.0 mm or more, substantially thicker than conventional amorphous alloys, which are typically limited to thicknesses of 0.020 mm, and which require cooling rates of 105 K/sec or more. U.S. Pat. Nos. 5,288,344; 5,368,659; 5,618,359; and 5,735,975, the disclosures of which are incorporated herein by reference in their entirety, disclose such bulk solidifying amorphous alloys.

One exemplary family of bulk solidifying amorphous alloys can be described as (Zr,Ti)a(Ni,Cu,Fe)b(Be,Al,Si,B)c, where a is in the range of from 30 to 75, b is in the range of from 5 to 60, and c in the range of from 0 to 50 in atomic percentages. Furthermore, these basic alloys can accommodate substantial amounts (up to 20% atomic, and more) of other transition metals, such as Hf, Ta, Mo, Nb, Cr, V, Co. A preferable alloy family is (Zr,Ti)a(Ni,Cu)b(Be)c, where a is in the range of from 40 to 75, b is in the range of from 5 to 50, and c in the range of from 5 to 50 in atomic percentages. Still, a more preferable composition is (Zr,Ti)a(Ni,Cu)b(Be)c, where a is in the range of from 45 to 65, b is in the range of from 7.5 to 35, and c in the range of from 10 to 37.5 in atomic percentages. Another preferable alloy family is (Zr)a(Nb,Ti)b(Ni,Cu)c(Al)d, where a is in the range of from 45 to 65, b is in the range of from 0 to 10, c is in the range of from 20 to 40 and d in the range of from 7.5 to 15 in atomic percentages.

Another set of bulk-solidifying amorphous alloys are ferrous metals (Fe, Ni, Co) based compositions, where the ferrous metal content is more than 50% by weight. Examples of such compositions are disclosed in U.S. Pat. No. 6,325,868 and in publications to (A. Inoue et. al., Appl. Phys. Lett., Volume 71, p 464 (1997)), (Shen et. al., Mater. Trans., JIM, Volume 42, p 2136 (2001)), and Japanese patent application 2000126277 (Publ. # 2001303218 A), all of which are incorporated herein by reference. One exemplary composition of such alloys is Fe72Al5Ga2P11C6B4. Another exemplary composition of such alloys is Fe72Al7Zr10Mo5W2B15. Although, these alloy compositions are not processable to the degree of the Zr-base alloy systems, they can still be processed in thicknesses of 1.0 mm or more, sufficient enough to be utilized in the current invention.

In general, crystalline precipitates in bulk amorphous alloys are highly detrimental to the properties of amorphous alloys, especially to the toughness and strength of these alloys, and as such it is generally preferred to minimize the volume fraction of these precipitates. However, there are cases in which, ductile crystalline phases precipitate in-situ during the processing of bulk amorphous alloys, which are indeed beneficial to the properties of bulk amorphous alloys, especially to the toughness and ductility of the alloys. Such bulk amorphous alloys comprising such beneficial precipitates are also included in the current invention. One exemplary case is disclosed in (C. C. Hays et. al, Physical Review Letters, Vol. 84, p 2901, 2000), the disclosure of which is incorporated herein by reference.

As discussed above, in one embodiment the present invention is directed to an apparatus for forming amorphous alloy sheets having large thicknesses of from 0.1 mm to 10 mm and having good ductility. In such an embodiment the sheet may be formed using a conventional single roll, double roll or other chill-body forms. Schematic diagrams of such conventional single roll apparatus are provided in FIGS. 1a and 1b.

As shown in these diagrams, the continuous casting apparatus has a chill body 7 which moves relative to a injection orifice 3, through which the melt 19 is introduced. In this specification, the apparatus is described with reference to the section of a casting wheel 7 which is located at the wheel's periphery and serves as a quench substrate as used in the prior art. It will be appreciated that the principles of the invention are also applicable, as well, to other conventional quench substrate configurations such as a belt, double-roll wheels, wheels having shape and structure different from those of a wheel, or to casting wheel configurations in which the section that serves as a quench substrate is located on the face of the wheel or another portion of the wheel other than the wheel's periphery. In addition, it should be understood that the invention is also directed to apparatuses that quench the molten alloy by other mechanisms, such as by providing a flow of coolant fluid through axial conduits lying near the quench substrate.

In FIG. 2, there is shown generally an apparatus for continuous casting of metallic sheet in accordance with an exemplary embodiment of the current invention. The apparatus has an annular casting wheel 20 rotatably mounted on its longitudinal axis, a reservoir 21 for holding molten metal 23. The reservoir 21 is in communication with a slotted nozzle 25, which is mounted in proximity to the substrate 27 of the annular casting wheel 20. The reservoir 21 is further equipped with means for pressurizing the molten metal contained therein to effect expulsion thereof through the nozzle 25. In operation, molten metal maintained under pressure in the reservoir 21 is ejected through nozzle 25 onto the rapidly moving casting wheel substrate 27, whereon it solidifies to form a continuous sheet 29. After solidification, the sheet 29 separates from the casting wheel 20 and is flung away therefrom to be collected by a winder or other suitable collection device (not shown).

The casting wheel quench substrate 27 may be comprised of copper or any other metal or alloy having relatively high thermal conductivity. Preferred materials of construction for the substrate 27 include fine, uniform grain-sized precipitation hardening copper alloys such as chromium copper or beryllium copper, dispersion hardening alloys, and oxygen-free copper. If desired, the substrate 27 may be highly polished or chrome-plated, or the like to obtain a sheet having smooth surface characteristics.

To provide additional protection against erosion, corrosion or thermal fatigue, the surface of the casting wheel may be coated in a conventional way using a suitably resistant or high-melt coating. For example, a ceramic coating or a coating of a corrosion-resistant, high-melting temperature metal may be applied provided that the wettability of the molten metal or alloy being cast on the chill surface is adequate.

The present invention is also directed to a processing method for making continuous amorphous alloy sheets with large thickness from bulk-solidifying amorphous alloys. A flow chart of this general process is shown in FIG. 3, and the process comprises the following general steps:

As described above, in a first processing step a charge of the bulk solidifying amorphous alloy is provided. Viscosity and temperature processing parameters for an exemplary bulk solidifying amorphous alloy are provided in FIGS. 4 and 5. Such alloys can be cooled from the above the casting temperatures at relatively low cooling rates, on the order of about 1000° C. per second or less, yet retain a substantially amorphous structure after cooling.

FIG. 5 shows the time-temperature cooling curve of an exemplary bulk solidifying amorphous alloy, or TTT diagram. Bulk-solidifying amorphous metals do not experience a liquid/solid crystallization transformation upon cooling, as with conventional metals. Instead, the highly fluid, non crystalline form of the metal found at high temperatures becomes more viscous as the temperature is reduced, eventually taking on the outward physical properties of a conventional solid. This ability to retain an amorphous structure even at a relatively slow cooling rate is to be contrasted with the behavior of other types of amorphous metals that require cooling rates of at least about 104˜106° C. per second to retain their amorphous structure upon cooling. As discussed previously, because of these high cooling rates such metals can only be fabricated in the amorphous form as very thin sheets of about 0.020 mm. As a result, such a metal has limited usefulness because it cannot be prepared in the thicker sections require for most applications.

Even though there is no liquid/crystallization transformation for a bulk solidifying amorphous metal, a “melting temperature” Tm may be defined as the thermodynamic liquidus temperature of the corresponding crystalline phase. Under this regime, the viscosity of bulk-solidifying amorphous alloys at the melting temperature lay in the range of about 0.1 poise to about 10,000 poise, which is to be contrasted with the behavior of other types of amorphous metals that have the viscosities at the melting temperature under 0.01 poise. In addition, higher values of viscosity can be obtained for bulk solidifying amorphous alloys by undercooling the alloy below the melting temperature, whereas ordinary amorphous alloys will tend to crystallize rather rapidly when undercooled.

FIG. 4 shows a viscosity-temperature graph of an exemplary bulk solidifying amorphous alloy, from the VIT-001 series of Zr—Ti—Ni—Cu—Be family manufactured by Liquidmetal Technology. It should be noted that there is no clear liquid/solid transformation for a bulk solidifying amorphous metal during the formation of an amorphous solid. The molten alloy becomes more and more viscous with increasing undercooling until it approaches solid form around the glass transition temperature. Accordingly, the temperature of solidification front for bulk solidifying amorphous alloys can be around glass transition temperature, where the alloy will practically act as a solid for the purposes of pulling out the quenched amorphous sheet product.

In accordance with FIG. 3, in the next steps of the process the charge is first heated above Tm, and then stabilized at the casting temperature in the reservoir such that the viscosity of the melt is around about 0.1 to 10,000 poise. The charge is then ejected from the reservoir through the nozzle onto the moving surface of the chill body. Throughout these steps the viscosity of the alloy is about 0.1 to about 10,000 poise, as shown in FIG. 4. Since the viscosity of the alloy increases with decreasing temperature, the step of ejecting the molten amorphous alloy is preferably carried out below the Tm to ensure increased viscosity and thickness. For larger thicknesses of amorphous alloy sheet a higher viscosity is preferred, and accordingly, greater undercooling below Tm is employed. However, it should be noted that the viscosity stabilization should be done at temperatures above Tnose as shown in the TTT diagram of FIG. 5.

Using the TTT and viscosity-temperature measurements shown in FIGS. 5 and 4, respectively for the alloys to be cast, the ejection temperature can be chosen to provide a specified thickness of cast sheet. Regardless of the cast temperature, the extraction of a continuous sheet is preferably done at speeds of 0.1 to 50 cm/sec, and preferably 0.5 to 10 cm/sec, and more preferably of 1 to 5 cm/sec.

After the alloy is ejected onto the chill body, the charge of amorphous alloy on the surface of chill body is cooled to temperatures below the glass transition temperature at a rate such that the amorphous alloy retains the amorphous state upon cooling. Preferably, the cooling rate is less than 1000° C. per second, but is sufficiently high to retain the amorphous state in the bulk solidifying amorphous alloy upon cooling. Once the lowest cooling rate that will achieve the desired amorphous structure in the article is chosen it can be engineered using the design of the chill body and the cooling channels. It should be understood that although several exemplary cooling rates are disclosed herein, the value of the cooling rate for any specific alloy cannot be specified herein as a fixed numerical value, because that value varies depending on the metal compositions, materials, and the shape and thickness of the sheet being formed. However, the value can be determined for each case using conventional heat flow calculations.

Accordingly, for bulk solidifying amorphous alloys, it is possible to reliably continue to process sheets even at low wheel rotational speeds by employing a high viscosity regime, so that the melt does not spill over the wheel, allowing for the formation of sheets with thicknesses up to about 10 mm.

Although specific embodiments are disclosed herein, it is expected that persons skilled in the art can and will design alternative continuous sheet casting apparatuses and methods to produce continuous amorphous alloy sheets that are within the scope of the following claims either literally or under the Doctrine of Equivalents.

Johnson, William L.

Patent Priority Assignee Title
Patent Priority Assignee Title
2190611,
3989517, Oct 30 1974 Allied Chemical Corporation Titanium-beryllium base amorphous alloys
4050931, Oct 30 1974 Allied Chemical Corporation Amorphous metal alloys in the beryllium-titanium-zirconium system
4064757, Oct 18 1976 Allied Chemical Corporation Glassy metal alloy temperature sensing elements for resistance thermometers
4067732, Jun 26 1975 Allied Chemical Corporation Amorphous alloys which include iron group elements and boron
4099961, Dec 21 1976 The United States of America as represented by the United States Closed cell metal foam method
4113478, Aug 09 1977 Allied Chemical Corporation Zirconium alloys containing transition metal elements
4116682, Dec 27 1976 Amorphous metal alloys and products thereof
4116687, Dec 13 1976 Allied Chemical Corporation Glassy superconducting metal alloys in the beryllium-niobium-zirconium system
4126449, Aug 09 1977 Allied Chemical Corporation Zirconium-titanium alloys containing transition metal elements
4135924, Aug 09 1977 Allied Chemical Corporation Filaments of zirconium-copper glassy alloys containing transition metal elements
4148669, Aug 09 1977 Allied Chemical Corporation Zirconium-titanium alloys containing transition metal elements
4157327, Dec 27 1977 United Technologies Corporation Thermally conductive caulk
4289009, Jun 02 1978 Swiss Aluminium Ltd. Process and device for the manufacture of blisters with high barrier properties
4472955, Apr 20 1982 Amino Iron Works Co., Ltd. Metal sheet forming process with hydraulic counterpressure
4478918, Dec 25 1981 International Fuel Cells Corporation Fuel cell stack
4621031, Nov 16 1984 Dresser Industries, Inc. Composite material bonded by an amorphous metal, and preparation thereof
4623387, Apr 11 1979 Shin-Gijutsu Kaihatsu Jigyodan Amorphous alloys containing iron group elements and zirconium and articles made of said alloys
4648437, Jan 12 1984 Olin Corporation Method for producing a metal alloy strip
4648609, Jan 22 1985 CONSTRUCTION ROBOTICS, INC AUST PTY LTD Driver tool
4710235, Mar 05 1984 Dresser Industries, Inc. Process for preparation of liquid phase bonded amorphous materials
4721154, Mar 14 1986 Sulzer-Escher Wyss AG; SULZER-ESCHER WYSS AG, A CORP OF SWITZERLAND Method of, and apparatus for, the continuous casting of rapidly solidifying material
4743513, Jun 10 1983 Dresser Industries, Inc. Wear-resistant amorphous materials and articles, and process for preparation thereof
4768458, Dec 11 1985 Hitachi, Metals Inc. Method of producing thin metal ribbon
4791979, Dec 17 1984 Metglas, Inc Gas assisted nozzle for casting metallic strip directly from the melt
4854370, Jan 20 1986 Toshiba Kikai Kabushiki Kaisha Die casting apparatus
4976417, Aug 14 1989 General Motors Corporation Wrap spring end attachment assembly for a twisted rope torsion bar
4978590, Sep 11 1989 UNITED STATES OF AMERICA, THE, AS REPRESENTED BY THE DEPARTMENT OF ENERGY Dry compliant seal for phosphoric acid fuel cell
4987033, Dec 20 1988 Dynamet Technology, Inc. Impact resistant clad composite armor and method for forming such armor
4990198, Sep 05 1988 YKK Corporation High strength magnesium-based amorphous alloy
5032196, Nov 17 1989 YKK Corporation Amorphous alloys having superior processability
5053084, Aug 12 1987 YKK Corporation High strength, heat resistant aluminum alloys and method of preparing wrought article therefrom
5053085, Apr 28 1988 YKK Corporation High strength, heat-resistant aluminum-based alloys
5074935, Jul 04 1989 MASUMOTO, TSUYOSHI; TEIKOKU PISTON RING CO , LTD ; YKK Corporation; Honda Giken Kogyo Kabushiki Kaisha Amorphous alloys superior in mechanical strength, corrosion resistance and formability
5117894, Apr 23 1990 Die casting method and die casting machine
5131279, May 19 1990 ENDRESS + HAUSER FLOWTEC AG A SWISS CORPORATION Sensing element for an ultrasonic volumetric flowmeter
5144999, Aug 31 1989 ALPS Electric Co., Ltd. Apparatus for making amorphous metal strips
5169282, Dec 02 1988 Mitsubishi Jukogyo Kabushiki Kaisha; Watakyu Shingu Co., Ltd. Method for spreading sheets
5213148, Mar 02 1990 YKK Corporation Production process of solidified amorphous alloy material
5225004, Aug 15 1985 Massachusetts Institute of Technology Bulk rapidly solifidied magnetic materials
5250124, Mar 14 1991 YKK Corporation Amorphous magnesium alloy and method for producing the same
5279349, Dec 29 1989 Honda Giken Kogyo Kabushiki Kaisha Process for casting amorphous alloy member
5288344, Apr 07 1993 California Institute of Technology Berylllium bearing amorphous metallic alloys formed by low cooling rates
5296059, Sep 13 1991 YKK Corporation Process for producing amorphous alloy material
5302471, Apr 08 1991 SANYO ELECTRIC CO LTD Compact phosphoric acid fuel cell system and operating method thereof
5306463, Apr 19 1990 HONDA GIKEN KOGYO KABUSHIKI KAISHA A CORPORATION OF JAPAN Process for producing structural member of amorphous alloy
5312495, May 15 1991 Tsuyoshi Masumoto; Akihisa Inoue; YKK Corporation Process for producing high strength alloy wire
5324368, May 31 1991 YKK Corporation Forming process of amorphous alloy material
5368659, Apr 07 1993 California Institute of Technology Method of forming berryllium bearing metallic glass
5380375, Apr 07 1992 YKK Corporation Amorphous alloys resistant against hot corrosion
5384203, Feb 05 1993 APFEL, ROBERT E Foam metallic glass
5390724, Jun 17 1992 Ryobi Ltd. Low pressure die-casting machine and low pressure die-casting method
5449425, Jul 31 1992 SALOMON S A Method for manufacturing a ski
5482580, Jun 13 1994 Liquidmetal Technologies Joining of metals using a bulk amorphous intermediate layer
5567251, Aug 01 1994 Liquidmetal Technologies Amorphous metal/reinforcement composite material
5589012, Feb 22 1995 SYSTEMS INTEGRATION AND RESEARCH, INC Bearing systems
5618359, Feb 08 1995 California Institute of Technology Metallic glass alloys of Zr, Ti, Cu and Ni
5634989, May 07 1987 Mitsubishi Materials Corporation; Koji Hashimoto Amorphous nickel alloy having high corrosion resistance
5647921, Aug 23 1993 Mitsui Chemicals, Inc Process for producing and amorphous alloy resin
5711363, Feb 16 1996 Liquidmetal Technologies Die casting of bulk-solidifying amorphous alloys
5735975, Feb 21 1996 California Institute of Technology Quinary metallic glass alloys
5797443, Sep 30 1996 Liquidmetal Technologies Method of casting articles of a bulk-solidifying amorphous alloy
5886254, Mar 30 1998 Tire valve pressure-indicating cover utilizing colors to indicate tire pressure
5950704, Jul 18 1996 Liquidmetal Technologies Replication of surface features from a master model to an amorphous metallic article
6021840, Jan 23 1998 ARCONIC INC Vacuum die casting of amorphous alloys
6027586, May 31 1991 YKK Corporation Forming process of amorphous alloy material
6044893, May 01 1997 Namiki Seimitsu Houseki Kabushiki Kaisha Method and apparatus for production of amorphous alloy article formed by metal mold casting under pressure
6200685, Mar 27 1997 Titanium molybdenum hafnium alloy
6203936, Mar 03 1999 Lynntech, Inc Lightweight metal bipolar plates and methods for making the same
6258183, Aug 08 1997 SRI Sports Limited Molded product of amorphous metal and manufacturing method for the same
6306228, Jul 08 1998 Japan Science and Technology Agency Method of producing amorphous alloy excellent in flexural strength and impact strength
6325868, Apr 19 2000 SAMSUNG ELECTRONICS CO , LTD Nickel-based amorphous alloy compositions
6371195, Aug 08 1997 SRI Sports Limited Molded product of amorphous metal and manufacturing method for the same
6376091, Aug 29 2000 LIQUIDMETAL COATINGS, LLC Article including a composite of unstabilized zirconium oxide particles in a metallic matrix, and its preparation
6408734, Apr 14 1998 Composite armor panel
6446558, Feb 27 2001 LIQUIDMETAL TECNNOLOGIES, INC Shaped-charge projectile having an amorphous-matrix composite shaped-charge liner
6491592, Nov 01 1999 Callaway Golf Company Multiple material golf club head
6585033, Feb 19 2001 Fukuda Metal Foil & Powder Co., Ltd. Process for producing vanadium alloy foil
6771490, Jun 07 2001 Liquidmetal Technologies; LIQUID METAL TECHNOLOGIES Metal frame for electronic hardware and flat panel displays
6843496, Mar 07 2001 Liquidmetal Technologies; LIQUID METAL TECHNOLOGIES Amorphous alloy gliding boards
6887586, Mar 07 2001 LIQUID METAL TECHNOLOGIES Sharp-edged cutting tools
20010052406,
20020036034,
20020050310,
20020153123,
20020187379,
20030024616,
20030222122,
20050006046,
GB2236325,
JP2000256811,
JP2000277127,
JP2001303218,
JP200256811,
JP359013056,
JP59013056,
JP61238423,
JP6264200,
/
Executed onAssignorAssigneeConveyanceFrameReelDoc
Aug 29 2012Crucible Intellectual Property, LLC(assignment on the face of the patent)
Date Maintenance Fee Events
Jan 26 2015ASPN: Payor Number Assigned.
Feb 09 2017M1552: Payment of Maintenance Fee, 8th Year, Large Entity.
Sep 29 2020M1553: Payment of Maintenance Fee, 12th Year, Large Entity.


Date Maintenance Schedule
Mar 17 20184 years fee payment window open
Sep 17 20186 months grace period start (w surcharge)
Mar 17 2019patent expiry (for year 4)
Mar 17 20212 years to revive unintentionally abandoned end. (for year 4)
Mar 17 20228 years fee payment window open
Sep 17 20226 months grace period start (w surcharge)
Mar 17 2023patent expiry (for year 8)
Mar 17 20252 years to revive unintentionally abandoned end. (for year 8)
Mar 17 202612 years fee payment window open
Sep 17 20266 months grace period start (w surcharge)
Mar 17 2027patent expiry (for year 12)
Mar 17 20292 years to revive unintentionally abandoned end. (for year 12)