Process for producing amorphous alloy materials having high toughness and high strength

Abstract: A process for producing amorphous alloy materials having high toughness and high strength from various alloy powders, thin ribbons or bulk materials consisting of an amorphous phase by heating them to a temperature at which intermetallic compounds or other compounds are not produced. In this heating, fine crystal grains consisting of a supersaturated solid solution made of a main alloying element and additive elements and having a mean grain diameter of 5 nm to 500 nm are precipitated and uniformly dispersed in a volume percentage of 5 to 50% throughout an amorphous matrix. In the process, when deformation, pressing or other working is simultaneously conducted with the heating, consolidation or combining of the resultant alloy materials can also be effected in the same production procedure. The amorphous alloy used in the production process preferably comprises Al, Mg or Ti as a main element and as additive elements, rare earth elements and/or other elements.

Description: BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a process for producing amorphous alloy materials having high mechanical strength and high toughness. 2. Description of the Prior Art The present inventors have already discovered aluminum-based alloys and Mg-based alloys having excellent strength, corrosion resistance, etc., as described in Japanese Patent Application Laid-open No. 64-47831 and 3-10041, respectively. The alloys described in these Japanese applications have been developed with the object of obtaining single-phase amorphous alloys. It is generally known that some amorphous alloys are crystallized when heated to a certain temperature (crystallization temperature) and become brittle. The present inventors have discovered that a high strength material can be obtained from a specific alloy whose composition is so controlled that fine crystal grains comprising additive elements dissolved in a main alloying element to form a supersaturated solution are dispersed throughout an amorphous matrix and made Japanese Patent Application No. 2-59139 which was laid open to public inspection under Laid-Open No. 3-260037. The process described in this patent application is carried out by controlling the cooling rate in the preparation of the alloys by liquid quenching. The resulting allov is not beyond alloy powders or thin ribbons ordinarily obtained. Further, US-A-4,512,826 discloses a method wherein α - Ti - alloys are subjected to a heat treatment to thereby precipitate intermetallic compounds. SUMMARY OF THE INVENTION The present inventors has found a process for effectively and stably producing amorphous bulk materials having high toughness and high strength and containing fine crystal grains consisting of a supersaturated solid solution therein. This invention has been reached on the basis of such a finding. The present invention provides a process for producing amorphous alloy materials containing fine crystal grains consisting of a supersaturated solid solution, comprising as a main element Al, Mg or Ti and having high toughness and high strength from various single phase amorphous alloy powders, thin-ribbons or bulk materials by heating them to a temperature which does not cause the formation of intermetallic compounds or other compounds, but cause the precipitation of supersaturated solid solution crystal grains. By this heating, fine crystal grains, which consist of a supersaturated solid solution made of a main alloying element and additive elements and have a mean diameter of 5 nm to 500 nm, are precipitated and uniformly dispersed in a volume percentage of 5 to 50% in an amorphous matrix. In the process of the present invention, when deformation, pressing or other working is simultaneously conducted with the heating or consolidation of the resultant alloy materials can also be effected in the same production procedure. The amorphous alloys used in the production process are preferably composed of Al, Mg or Ti as a main element and, as additive elements, rare earth elements, including Y and Mm (misch metal) consisting of a mixture of rare earth elements, and/or other elements. The Al-based amorphous alloy, Mg-based amorphous alloy and Ti-based amorphous alloy are heated at temperatures ranging from 100 to 200°C (373 to 573 K), 80 to 200°C (353 to 573 K) and 200 to 800°C (573 to 1073 K), respectively, and in these temperature ranges, fine crystal grains consisting of a supersaturated solid solution uniformly precipitate in their amorphous matrix without causing the formation of intermetallic compounds or other compounds. BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is stress-strain curves diagrammatically showing the results of tensile tests for the materials obtained in an example. FIG. 2 is a graph summarizing the results shown in FIG. 1. DETAILED DESCRIPTION of THE PREFERRED EMBODIMENTS When well-known amorphous alloys are crystallized by heating, intermetallic compounds and other compounds unavoidably precipitate out since the proportion of additive elements to the main alloying element is relatively high. Therefore, the resulting alloy material becomes considerably more brittle. In single-phase amorphous alloys prepared by reducing the amount of additive elements in order to prevent the problem of embrittlement, the abovementioned precipitation of intermetallic compounds and other compounds, which occurs during crystallization by heating, can be suppressed and only fine crystal grains including additive elements dissolved in crystals of the main element so as to form a supersaturated solid solution can be precipitated. When the main element is aluminum, the crystals have a face-centered cubic structure. In case of using magnesium or titanium as the main element, the crystal has a hexagonal close-packed structure. The thus precipitated crystal grains have a mean diameter ranging from several nanometers to several hundreds of nanometers and they are uniformly dispersed throughout the amorphous matrix. In such a multiphase state, the material is not embrittled and exhibits a better ductility than in an amorphous single-phase state. Therefore, the material can be bent to 180° even at room temperature or even in a thin ribbon form of 20 to 50 µm in thickness. The important feature for an amorphous alloy having a properly controlled composition is that it must have a plastic elongation of at least 20% at an appropriate working temperature for the precipitation of crystalline phases regardless of the type of the alloy. If such behavior can be effectively used, consolidation-forming or shaping of amorphous alloy materials containing a crystalline phase becomes possible using various powdered or thin-ribbon like amorphous alloys or amorphous alloy bulk materials obtained, for example, by casting, as starting materials. This is a principal subject contemplated by this invention. Alternatively, an amorphous alloy having a controlled composition as mentioned above can also be formed into a multiphase material consisting of an amorphous phase and a supersaturated solid solution phase by choosing an appropriate cooling rate in a rapid quenching process. However, the plastic elongation of the thus obtained material is less than 20% under the above-mentioned conditions. It can be construed from this fact that elongation observed in the crystallization process of a single-phase amorphous alloy is not simply due to the viscous flow of the amorphous phase, but due to the plastic flow (deformation) dynamically related to the precipitation of crystal grains. With an increase in the volume percentage of crystal grains dispersed in the amorphous matrix, the strength of the material tends to increase. However, when the volume percentage of the supersaturated solid solution crystal grains contained in the amorphous matrix exceeds 50%, the material is considerably more brittle and cannot be used in practical applications. When the volume percentage is less than 5%, the elongation is the same level as that of an amorphous single phase and no substantial improvement is revealed. Under such consideration, the volume percentage of the crystal grains is limited to the range of 5 to 50% in the present invention. When the strength and elongation are considered important, the optimum volume percentage of the fine crystal grains is from 15 to 35%. In general, the mixed phase structure of an amorphous phase and fine crystal grains can provide an improvement of 30 to 60% in strength as compared with an amorphous single-phase structure. In the amorphous alloy material of the present invention, the mean diameter of the fine crystal grains dispersed therein is limited within the range of 5 nm to 500 nm in order to achieve the desired high toughness and high strength. In general, the above properties are not limited only to specific alloy systems but may also be applied to any alloy system that can form an amorphous phase. The following amorphous alloys can be preferably used for the preparation of the amorphous alloy materials of the present invention and they may be in the form of powder, thin ribbon and bulk. Al-based amorphous alloys consisting of Al as a main element and rare earth elements and/or other elements, as additive elements. For example, there may be mentioned an Al-based amorphous alloy consisting of, in atomic percentages, 85 to 99.8% Al as the main element, 0.1 to 5% of at least one element selected from the group consisting of rare earth elements including Y and Mm as primary additive elements of the additive elements and up to 10% of at least one element selected from the group consisting of Ni, Fe, Co and Cu as secondary additive elements of the additive elements, with the proviso that the total content of the rare earth elements including Y and Mm is not more than the total content of the other additive elements. In the Al-based amorphous alloy, Al as the main element may be partially replaced in the range of 0.2 to 3 atomic % with at least one element selected from the group consisting of Ti, Mn, Mo, Cr, Zr, V, Nb and Ta. Mg-based amorphous alloys consisting of Mg as a main element and rare earth elements and/or other elements as additive elements. For example, there may be mentioned an Mg-based amorphous alloy consisting of, in atomic percentages, 80 to 91% Mg as the main element, 8 to 15% of at least one element selected from the group consisting of Cu, Ni, Sn and Zn as primary additive elements of the additive elements and 1 to 5% of at least one element selected from the group consisting of Al, Si and Ca as secondary elements of the additive elements; and an Mg-based amorphous alloy consisting of, in atomic percentages, 80 to 91% Mg as the main element, 8 to 15% of at least one element selected from the group consisting of Cu, Ni, Sn and Zn as primary additive elements of the additive elements and 1 to 5% of at least one element selected from the group consisting of rare earth elements including Y and Mm as secondary additive elements of the additive elements. Mg as the main element of the Mg-based amorphous alloy may be partially substituted in the range of 1 to 5 atomic % by at least one element selected from the group consisting of Al, Si and Ca, when these elements are not present as the additive elements. Ti-based amorphous alloy consisting of Ti as a main element and other elements as additive elements. Hereinafter, the present invention will be specifically described with reference to Examples. Example 1 A mother alloy having a composition of Al 88 Y 2 Ni 10 (atomic %) was prepared in an arc melting furnace. An amorphous thin ribbon (thickness: 30 µm, width: 1.5 mm) consisting of an amorphous single phase was prepared from the above alloy, using an ordinary single-roll liquid quenching apparatus. Whether the resultant thin ribbon was amorphous or not was examined by checking the presence of the characteristic halo pattern of an amorphous structure using an X-ray diffraction apparatus. It was confirmed that the thin ribbon was amorphous. Tensile tests were carried out on the thin ribbon at various temperatures. At each temperature, the holding time before measuring the tensile strength was 300 seconds. Stress-strain curves showing the test results are shown in FIG. 1 and the test results are summarized in FIG. 2. As shown in FIG. 2, the tensile strength (σ B ) was a constant strength of 300 MPa at temperatures of not higher than 127°C (400 K) (containing room temperature). At temperatures exceeding 127°C (400 K), the tensile strength abruptly dropped to about 700 MPa, then remained almost constant up to 227°C (500 K), and gradually increased. The elongation.(ε f ) at temperatures up to 127°C (400 K) was a low value of about 2%. However, at temperatures exceeding 127°C (400 K), the elongation sharply increased and reached 30% at 177°C (450 K) and decreased to 20% at 227°C (500 K). Further, after reaching a temperature of 277°C (550 K), the elongation again increased. On the other hand, no substantial elongation was measured in the yield strength (σ y ) at a temperature lower than 127°C (400 K) (not greater than 0.2%). The ductility was examined by a bending test after standing each test sample, which had been subjected to the above tests, at room temperature. When the test sample could be bond-bent to 180° without cracking or other fracturing, it was judged as "ductile". When the test sample was subjected to cracking or fracturing, it was judged as "brittle". The test samples subjecte to the tensile tests at temperatures not higher than 177°C (450 K) exhibited ductility and the samples tested at temperatures of 202°C (475 K) or higher showed embrittlement. Further, the test samples after the tensile tests were observed by a transmission electron microscope (TEM). The TEM observation revealed that, in the sample after the tensile test at temperature of 177°C (450 K), crystal grains of supersaturated solid solution having a face-centered cubic structure (fcc-Al) and having a diameter of 5 to 20 nm were uniformly dispersed in an amorphous matrix and the volume percentages of the crystal grains were about 30%. It was observed that the crystal grains dispersed in the samples tested at 227°C (500 K) had almost the same diameter but their volume percentage was 60%. It can be seen from the above test results that crystallization induced by heating at a temperature of 127 to 177°C (400 to 450 K) provides an elongation sufficient for consolidation-forming or shaping and the material has ductility after the above working. Therefore, it is clear that the production process of the present invention is very useful as a process for producing amorphous alloy materials having high toughness and high strength. Example 2 An amorphous thin ribbon having a composition of Al 88 Ce 2 Ni 9 Fe 1 (atomic %) was prepared in the same manner as set forth in Example 1 and the same tests as set forth in Example 1 were conducted. The test results showed that fine crystal grains having a face-centered cubic structure (fcc-Al) precipitated at 182°C (455 K). The precipitated crystal grains consisted of a supersaturated solid solution and were uniformly dispersed with a mean diameter of 5 to 20 nm in a volume percentage of 20% throughout an amorphous matrix. At a deformation temperature of 182°C (455 K), the thin ribbon showed a plastic elongation of 40%. Further, after standing this tested sample at room temperature, it was subjected to a 180° bond-bending test. As a result, the sample was found to be ductile. Example 3 An amorphous thin ribbon having a composition of Al 88 Mm 2 Ni 9 Mn 1 (atomic %) was prepared in the same manner as set forth in Example 1 and the same tests as set forth in Example 1 were conducted. The test results showed that fine crystal grains having a face-centered cubic structure (fcc-Al) precipitated at 177°C (450 K). The precipitated crystal grains consisted of a supersaturated solid solution and were uniformly dispersed with a mean diameter of 5 to 20 nm in a volume percentage of 20% throughout an amorphous matrix. When the thin ribbon was subjected to deformation at 177°C (450 K), it showed a plastic elongation of 38%. Further, after standing the tested sample at room temperature, it was subjected to a 180° bond-bending test. As a result, the sample was found to be ductile. Example 4 An amorphous thin ribbon having a composition of Mg 85 Zn 12 Ce 3 (atomic %) was prepared in the same manner as set forth in Example 1 and the same tests as set forth in Example 1 were conducted. The test results showed that fine crystal grains having a hexagonal close-packed structure (hcp-Mg) precipitated at 87°C (360 K). The precipitated crystal grains consisted of a supersaturated solid solution and were uniformly dispersed with a mean diameter of 5 to 30 nm in a volume percentage of 25% throughout an amorphous matrix. When the thin ribbon was subjected to deformation at 87°C (360 K), it showed a plastic elongation of 35%. Further, after standing the tested sample at room temperature, it was subjected to a 180° bond-bending test. As a result, the sample was found to be ductile. Example 5 An amorphous thin ribbon having a composition of Ti 87 Si 10 Fe 3 (atomic %) was prepared in the same manner as set forth in Example 1 and the same tests as set forth in Example 1 were conducted. The test results showed that β-Ti fine crystal grains precipitated at 377°C (650 K). The precipitated crystal grains consisted of a supersaturated solid solution and were uniformly dispersed with a mean diameter of 5 to 15 nm in a volume percentage of 25% throughout an amorphous matrix. When the thin ribbon was subjected to deformation at this temperature, i.e., 377°C (650K), it showed a plastic elongation of 40%. Further, after standing the tested sample at room temperature, it was subjected to a 180° bond-bending test. As a result, the sample was found to be ductile. In the above tensile tests at various temperatures, when the thin ribbons were heated to temperatures which caused precipitation of fine crystal grains consisting of a supersaturated solid solution but did not cause formation of intermetallic compounds or the like, the resulting fine crystal grains were uniformly dispersed within the ranges of volume percentages (5 to 50%) and mean diameters (5 to 500 nm) specified in the present invention in the amorphous matrix. Further, the heated thin ribbons exhibited high strength, good elongation and good ductility. As set forth above, according to the production process of the present invention, amorphous alloy bulk materials containing fine crystal grains consisting of a supersaturated solid solution can be effectively and stably produced with high toughness and strength.

Claims: A process for producing an amorphous alloy material containing fine crystal grains consisting of a supersaturated solid solution, comprising as a main element Al, Mg or Ti and having high toughness and high strength, which process comprises heating a single phase Al-based amorphous alloy, Mg-based amorphous alloy or Ti-based amorphous alloy, used as a starting material, at temperatures ranging from 100 to 200 °C (373 to 573 K), 80 to 200 °C (353 to 573 K) and 200 to 800 °C (573 to 1073 K), respectively, and thereby causing precipitation and uniform dispersion of crystal grains consisting of a supersaturated solid solution made of said main element and additive elements and having a mean diameter of 5 nm to 500 nm in a volume percentage of 5 to 50% throughout an amorphous matrix. A process according to claim 1, wherein the starting material is present in the form of powders, thin ribbons or bulk shapes and is subjected to deformation-forming, pressing or other working while being heated to thereby cause said precipitation and uniform dispersion of said crystal grains consisting of a supersaturated solid solution made of said main element and said additive elements and having a means diameter of 5 nm to 500 nm in a volume percentage of 5 to 50% throughout said amorphous matrix, and for simultaneously effecting consolidation-forming. A process as claimed in claim 1 or 2 in which the starting material is an Al-based amorphous alloy comprising Al as a main element and rare earth elements as additive elements. A process as claimed in claim 3 in which the Al-based amorphous alloy consists of, in atomic percentages, 85 to 99.8% Al as the main element, optionally being partially substituted in the range of 0.2 to 3 atomic % by at least one element selected from the group consisting of Ti, Mn, Mo, Cr, Zr, V, Nb and Ta, 0.1 to 5% of at least one element selected from the group consisting of rare earth elements including Y and Mm (misch metal) consisting of a mixture of rare earth elements as primary additive elements and up to 10% of at least one element selected from the group consisting of Ni, Fe, Co and Cu as secondary additive elements, with the proviso that the total content of the rare earth elements including Y and Mm is not more than the total content of the other additive elements. A process as claimed in claim 1 or 2 in which the starting material is an Mg-based amorphous alloy comprising Mg as a main element and rare earth elements as additive elements. A process as claimed in claim 5 in which the Mg-based amorphous alloy consists of, in atomic percentages, 80 to 91% Mg as the main element, 8 to 15% of at least one element selected from the group consisting of Cu, Ni, Sn and Zn as primary additive elements of the additive elements and 1 to 5% of at least one element selected from the group consisting of Al, Si and Ca as secondary elements of the additive elements. A process as claimed in claim 5 in which the Mg-based amorphous alloy consists of, in atomic percentages, 80 to 91% Mg as the main element optionally being at least partially substituted in the range of 1 to 5 atomic % by at least one element selected from the group consisting of Al, Si and Ca, 8 to 15% of at least one element selected from the group consisting of Cu, Ni, Sn and Zn as primary additive elements and 1 to 5% of at least one element selected from the group consisting of rare earth elements including Y and Mm (misch metal) consisting of a mixture of rare earth elements as secondary additive elements.

Inventors: INOUE AKIHISA, MASUMOTO TSUYOSHI, INOUE, AKIHISA, MASUMOTO, TSUYOSHI
Applicants: INOE AKIHISA, MASUMOTO TSUYOSHI, YKK CORP, INOUE, AKIHISA, MASUMOTO, TSUYOSHI, YKK CORPORATION
Application year: 1992
Main classification: C22F1
IPC codes: C22F1, C22C14, C22C45, C22C23, C22C21