[go: up one dir, main page]

US20030029526A1 - Quasicrystalline phase-reinforced Mg-based metallic alloy with high warm and hot formability and method of making the same - Google Patents

Quasicrystalline phase-reinforced Mg-based metallic alloy with high warm and hot formability and method of making the same Download PDF

Info

Publication number
US20030029526A1
US20030029526A1 US10/232,444 US23244402A US2003029526A1 US 20030029526 A1 US20030029526 A1 US 20030029526A1 US 23244402 A US23244402 A US 23244402A US 2003029526 A1 US2003029526 A1 US 2003029526A1
Authority
US
United States
Prior art keywords
phase
quasicrystalline
alloy
quasicrystalline phase
hot
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US10/232,444
Inventor
Do Kim
Won Kim
Dong Bae
Eun Park
Seong Yi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US10/232,444 priority Critical patent/US20030029526A1/en
Publication of US20030029526A1 publication Critical patent/US20030029526A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • C22C23/06Alloys based on magnesium with a rare earth metal as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • C22C23/04Alloys based on magnesium with zinc or cadmium as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C45/00Amorphous alloys
    • C22C45/005Amorphous alloys with Mg as the major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/002Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working by rapid cooling or quenching; cooling agents used therefor
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/06Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of magnesium or alloys based thereon

Definitions

  • the present invention relates, in general, to a quasicrystalline phase-reinforced Mg-based metallic alloy superior in warm and hot formability and, more particularly, to an Mg—Zn—Y alloy which has a two-phase region consisting of a quasicrystalline phase and a magnesium-based solid solution phase, in which the solid solution is formed as a primary phase constituting a matrix structure upon solidification, while the quasicrystalline phase serves as a second phase and forms, together with the solid solution phase, a eutectic phase, thereby reinforcing the matrix.
  • Casings for portable electronic appliances, such as mobile phones, or materials for automobile parts are required to be of light weight, high strength, high toughness, and high formability.
  • U.S. Pat. No. 5,851,317 discloses composite materials reinforced with quasicrystalline particles and a gas atomization process of making the same, in which aluminum or aluminum alloy particles and spherical Al—Cu—Fe quasicrystalline particles are mixed at an appropriate ratio and hot pressed or hot extruded to form a composite product of high strength with interfacial bonding between the quasicrystalline particles and the aluminum or aluminum alloy particles.
  • the composite materials of the cited reference have the advantage of being made to show versatile mechanical properties by controlling the amounts of components, but the disadvantage of being poor in bonding strength between component particles.
  • the oxide coatings deteriorate the bonding between the matrix metal particles and the reinforcement particles, giving rise to a decrease in mechanical properties, especially elongation and fracture toughness.
  • the composite materials are not advantageous in terms of product reliability and production cost owing to their complicated production procedure and many production parameters.
  • Al—Cu—Fe alloy is unsuitable as materials for use in casings for electronic appliances or materials for automobile parts, which require lightness, high strength, high toughness and high formability because the quasicrystalline phase region in Al—Cu—Fe alloy is surrounded by various brittle intermetallic phase regions.
  • the intensive and thorough research on metallic alloy, conducted by the present inventors resulted in the finding that, when Mg—Zn—Y alloy is solidified from a liquid state, the quasicrystalline phase particles in the matrix of the metal solid solution acts as a reinforcement, which brings about an improvement in the mechanical properties of quasicrystalline phase-reinforced materials and their production cost.
  • the Mg—Zn—Y alloy is defined as the composition range which allows hot molding processes to be applied to the alloy.
  • FIG. 1 is a phase diagram of Mg—Zn—Y alloy showing a two-phase region of an alpha magnesium phase and a quasicrystalline phase.
  • FIG. 2 is an optical photograph taken of a eutectic alloy, showing a solidification structure in which an alpha magnesium matrix is formed as a dentritic structure with interdentritic segregation of a eutectic phase (alpha magnesium and quasicrystalline phase).
  • FIG. 3 is a transmission electron microphotograph showing a structure of a hot-rolled plate made of the eutectic alloy of FIG. 2, in which the quasicrystalline phase of the hot-rolled plate forms a stable interface to the matrix, being broken down into microparticles.
  • FIG. 4 is an electron microscopic diffraction pattern identifying the crystal structure of the second phase of the alloy.
  • FIG. 5 shows curves in which stresses of the metallic alloys Mg 97.9 Zn 1.8 Y 0.3 ( ⁇ ) and Mg 95 Zn 4.3 Y 0.7 ( ⁇ ) are plotted versus temperature.
  • FIG. 6 shows curves in which the elongation of the metallic alloys of the present invention is plotted versus temperature.
  • FIG. 7 is an optical photograph showing the structure of a rolled plate made of an alloy of the present invention, in which the quasicrystalline phase is homogeneously distributed, in addition to forming a stable interface with the matrix metal.
  • a quasicrystalline phase-reinforced Mg-based metallic alloy superior in warm and hot formability which has a two-phase region consisting of a quasicrystalline phase and an Mg-based solid solution phase.
  • the Mg-based solid solution phase alpha magnesium
  • the quasicrystalline phase serves as a second phase and forms, together with the magnesium-based solid solution phase, a eutectic phase, thereby reinforcing the matrix structure.
  • the quasicrystalline phase-reinforced Mg-based metallic alloy has a composition of 1-10 at % Zn, and 0.1-3 at % Y, the remainder Mg.
  • a method of making a quasicrystalline phase-reinforced magnesium-based metallic alloy which comprises the steps of: casting a quasicrystalline phase-reinforced magnesium-based metallic alloy consisting of Mg-1 ⁇ 10 at % Zn-0.1 ⁇ 3 at % Y, into a mass, in which a two-phase region consisting of a quasicrystalline phase and a metal solid solution phase exists; and warm or hot forming the mass to separate and disperse the quasicrystalline phase throughout the matrix, so as to provide the quasicrystalline phase-reinforced magnesium-based metallic alloy with improved strength and elongation.
  • the quasicrystalline phase-reinforced Mg-based metallic alloy When being solidified from a liquid state, the quasicrystalline phase-reinforced Mg-based metallic alloy is required to have a two-phase region consisting of a quasicrystalline phase and a metal solid solution phase.
  • Mg—Zn—Y alloys are suitable because thermodynamically stable quasicrystalline phase exists therein.
  • a eutectic reaction occurs in which a magnesium-based solid solution phase and a quasicrystalline phase are formed during solidification from a liquid state.
  • Mg—Zn—Y alloys have a two-phase region of the magnesium-based solid solution phase and a quasicrystalline phase as seen in the phase diagram of FIG. 1.
  • the quasicrystalline phase-reinforced Mg-based metallic alloys of the present invention may be prepared into ingot or slab from a molten metal of Mg—Zn—Y alloys by a conventional casting method such as gravity die casting.
  • the interface between the matrix and the quasicrystalline phase is not destroyed, but the quasicrystalline phase is separated and dispersed throughout the matrix.
  • This hot forming process can be conducted on the eutectic alloy which has a quasicrystalline phase to a maximum of 30% of the alloy volume.
  • a hot rolling process is not successfully achieved in an alloy throughout which a quasicrystalline phase is distributed at a volume higher than 30% because the quasicrystalline phase is of high brittleness.
  • the quantity of the quasicrystalline phase is limited to 30% by volume in the alloy.
  • the magnesium-based metallic alloy which is superior in warm and hot formability and has such a dispersed quasicrystalline phase as to afford high strength and elongation can be obtained when they have a composition of Mg-1 ⁇ 10 at % Zn-0.1 ⁇ 3 at % Y.
  • the reason that the composition of the alloy is limited to such ranges is as follows.
  • a plate material can be successfully produced into final products only when it has an elongation of at least 50% at forming temperatures.
  • the plate At a temperature as high as or higher than one third of the melting point, which is the typical forming temperature for general metallic materials when using a warm or hot forming process, the plate is found to be of high formability as its elongation is measured to be 50% or higher. After undergoing this warm or hot forming process, the quasicrystalline phase is further dispersed and thus more homogeneously distributed throughout the matrix metal while stably maintaining the interface to the matrix metal, thereby bringing about a significant reinforcement effect attributed to the dispersion of the quasicrystalline phase.
  • alloy #1 the primary solid phase is a quasicrystalline phase in a solid structure.
  • alloys #2 to 11 showed the primary solid phase as a magnesium-base solid solution (alpha magnesium matrix) while having a quasicrystalline phase as a second phase.
  • alloy compositions provided to the alloys #2-11 fall within the range suitable in the present invention when their solidification structures are taken into account.
  • FIG. 2 there is an optical photograph taken of the alloy #10, showing a solidification structure in which an alpha magnesium matrix is formed as a dentritic structure with interdentritic segregation of a eutectic phase (alpha magnesium and quasicrystalline phase).
  • the fraction of the quasicrystalline phase was found to be, by volume, about 33% for the alloy #8, about 20% for the alloy #9, about 15% for the alloy #10, and about 4% for the alloy #11 as measured by an image analyzer.
  • the alloys #8 to 11 was hot rolled according to a hot rolling process that is usually used for general wrought metallic materials. That is, the hot rolling was conducted in multiple passes at a temperature of 400° C. using 10% thickness reduction per pass to reduce the original body thickness to a final hot rolled thickness of 1.7 mm; i.e. a total reduction in thickness of 80%.
  • the alloy #8 was not hot rolled successfully. Success was achieved in hot rolling the alloys #9, 10 and 11.
  • the structure of the hot-rolled plate is shown in FIG. 3.
  • the quasicrystalline phase of the hot-rolled plate forms a stable interface to the matrix as shown in the transmission electron micrograph of FIG. 3.
  • the quasicrystalline phase was identified to be broken down into micro-scale fine particles during the hot rolling and dispersed throughout the matrix through thermal energy-induced mass flow, forming a stable interface to the matrix without destroying the matrix nor separating from the matrix.
  • the Mg-based alloy with superior hot formability and a dispersed quasicrystalline phase can be obtained from a composition of Mg-1 ⁇ 10 at % Zn-0.1 ⁇ 3 at % Y.
  • magnesium alloys are generally of hexagonal close-packed structure, they are unlikely to be formed into plates at room temperature. Thus, hot rolling is used to form magnesium alloys into plates.
  • Representative of convertional wrought magnesium-based alloys are AZ31 and ZM21.
  • the alloys of the present invention are described with regard to the tested properties in Table 2, below. TABLE 2 Yield Strength Max. Tensile Strength Elongation (MPa) (MPa) (%) Alloy #10 225 370 20 Alloy #11 150 330 28 AZ31B-H24 220 290 15 ZM21-O 120 240 11 ZM21-H24 165 250 6
  • the alloys of the present invention are superior in yield strength, max tensile strength, and elongation.
  • conventional magnesium alloys listed in Table 2 which are capable of being hot-rolled, form solid solutions, so that only a small quantity of other elements can be permitted in the matrix, resulting in a decrease in their strength.
  • the alloys of the present invention as seen in Table 1, have a quasicrystalline phase which is added at large amounts as a second phase.
  • the quasicrystalline phase forms a stable interface with the matrix metal, serving to increase the strength of the alloys.
  • FIG. 5 shows curves in which the fracture stress and yield stress of the metallic alloys Mg 97.9 Zn 1.8 Y 0.3 ( ⁇ ) and Mg 95 Zn 4.3 Y 0.7 ( ⁇ ) are plotted versus temperature.
  • FIG. 6 shows curves in which the elongation of the metallic alloys of the present invention is plotted versus temperature. As seen in these curves, the yield stress does show only a little change up to 100° C., but decreases with increasing of temperature above 100° C. The elongation increases in an almost linear pattern with increasing temperature.
  • FIG. 7 there is an optical photograph showing the structure of a rolled plate made of the alloy #10. As seen in FIG. 7, the quasicrystalline phase is homogeneously distributed in addition to maintaining a stable interface with the matrix metal. In this case, a dispersion-induced reinforcement effect comes out more effectively, leading to an increase in strength.
  • the alloy of the present invention retains not only the excellent mechanical properties that the metallic materials made by conventional various methods show, but also is superior in warm and hot formability.
  • the alloy of the present invention can be prepared into various, final metallic products of high quality on a mass scale.
  • the alloy of the present invention is characterized in warm and hot formability because conventional Mg-based alloys are poor in formability.
  • the alloy of the present invention is used where superior mechanical properties are needed.
  • the materials obtained through the hot rolling or extrusion of the quasicrystalline phase-reinforced Mg-based metallic alloy of the present invention have an increased volume % of the second phase and thus show significantly increased strength.
  • the materials warm- or hot-rolled or extruded from the alloy of the present invention have much more stable interface between the particles and the matrix and are remarkably improved in elongation upon warm and hot rolling compared to composite metallic materials made by conventional powder metallurgy.
  • the alloy of the present invention is useful as a material for high-quality metallic products which are required to be of light weight, high strength, high toughness and high formability.
  • the alloy of the present invention is suitable for use in casings for portable electronic appliances such as mobile phones, and automobile parts, which require light weight, high strength, high toughness and high formability. Also, the alloy of the ID present invention can be used where wear-resistance is needed because the quasicrystalline phase has a friction coefficient of as low as 0.1-0.2.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Powder Metallurgy (AREA)

Abstract

Disclosed is a quasicrystalline phase-reinforced Mg-based metallic alloy with high warm and hot formability, and making method thereof. The metallic alloy comprises a composition of Mg-1˜10 at % Zn-0.1˜3 at % Y, in which a two-phase region consisting of a quasicrystalline phase and a magnesium-based solid solution phase exists. Constituting a matrix structure, the Mg-based solid solution phase (α-Mg) is formed as a primary solid phase upon solidification. The quasicrystalline phase serves as a second phase and forms, together with the Mg-based solid solution phase, a eutectic phase, thereby reinforcing the matrix. The materials obtained through the hot rolling or extrusion of the cast alloy have an increased volume % of the second phase and thus show significantly increased strength.

Description

    BACKGROUND OF THE INVENTION
  • 1. Field of the Invention [0001]
  • The present invention relates, in general, to a quasicrystalline phase-reinforced Mg-based metallic alloy superior in warm and hot formability and, more particularly, to an Mg—Zn—Y alloy which has a two-phase region consisting of a quasicrystalline phase and a magnesium-based solid solution phase, in which the solid solution is formed as a primary phase constituting a matrix structure upon solidification, while the quasicrystalline phase serves as a second phase and forms, together with the solid solution phase, a eutectic phase, thereby reinforcing the matrix. [0002]
  • 2. Description of the Prior Art [0003]
  • Casings for portable electronic appliances, such as mobile phones, or materials for automobile parts are required to be of light weight, high strength, high toughness, and high formability. [0004]
  • While crystals generally have one-, two-, three-, and six-fold rotational axes of symmetry only, quasicrystals have five-, eight-, ten- and twelve-fold rotational axes of symmetry, which are not formed in crystals. Since their first finding in Al-Mn alloy, quasicrystals have been disclosed to exist in many alloys. For instance, Al—Cu—Fe, Mg—Zn—Y, and Al—Pd—Mn alloys have been reported to have thermodynamically stable quasicrystalline structures. Superior as they are in hardness as compared to crystals of similar compositions, quasicrystals are unsuitable for use as sole structural materials owing to their high brittleness. Recently, reinforced composite materials which comprise metal matrices having reinforcement particles dispersed in the matrix have been developed through powder metallurgy route. [0005]
  • U.S. Pat. No. 5,851,317 discloses composite materials reinforced with quasicrystalline particles and a gas atomization process of making the same, in which aluminum or aluminum alloy particles and spherical Al—Cu—Fe quasicrystalline particles are mixed at an appropriate ratio and hot pressed or hot extruded to form a composite product of high strength with interfacial bonding between the quasicrystalline particles and the aluminum or aluminum alloy particles. [0006]
  • The composite materials of the cited reference have the advantage of being made to show versatile mechanical properties by controlling the amounts of components, but the disadvantage of being poor in bonding strength between component particles. In case particles that are likely to be coated with oxides, such as aluminum or aluminum alloy particles, are used as starting materials, the oxide coatings deteriorate the bonding between the matrix metal particles and the reinforcement particles, giving rise to a decrease in mechanical properties, especially elongation and fracture toughness. Additionally, the composite materials are not advantageous in terms of product reliability and production cost owing to their complicated production procedure and many production parameters. [0007]
  • Further, Al—Cu—Fe alloy is unsuitable as materials for use in casings for electronic appliances or materials for automobile parts, which require lightness, high strength, high toughness and high formability because the quasicrystalline phase region in Al—Cu—Fe alloy is surrounded by various brittle intermetallic phase regions. [0008]
  • Therefore, there remains a need for the alloy that has a quasicrystalline phase as a second phase dispersed in the metal solution so that it is provided with all of the above mechanical properties in addition to being of high formability. [0009]
  • SUMMARY OF THE INVENTION
  • Leading to the present invention, the intensive and thorough research on metallic alloy, conducted by the present inventors, resulted in the finding that, when Mg—Zn—Y alloy is solidified from a liquid state, the quasicrystalline phase particles in the matrix of the metal solid solution acts as a reinforcement, which brings about an improvement in the mechanical properties of quasicrystalline phase-reinforced materials and their production cost. In the present invention, the Mg—Zn—Y alloy is defined as the composition range which allows hot molding processes to be applied to the alloy. [0010]
  • Therefore, it is an object of the present invention to overcome the above problems encountered in prior arts and to provide a quasicrystalline phase-reinforced magnesium-based metallic alloy with excellent warm and hot formability, in which a two-phase region consisting of a quasicrystalline phase and a magnesium-based solid solution phase exists, said magnesium-based solid solution phase (alpha magnesium) being formed as a primary solid phase, constituting a matrix structure upon being solidified, said quasicrystalline phase serving as a second phase and forming, together with the magnesium-based solid solution phase, a eutectic phase, thereby reinforcing the matrix. [0011]
  • It is another object of the present invention to provide a method of making such an quasicrystalline phase-reinforced magnesium-based metallic alloy by subjecting a magnesium-based metallic alloy composition to hot forming to separate and disperse a quasicrystalline phase of micro particles throughout the metallic matrix, so as to bring about an improvement in room temperature mechanical properties as well as high-temperature elongation.[0012]
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a phase diagram of Mg—Zn—Y alloy showing a two-phase region of an alpha magnesium phase and a quasicrystalline phase. [0013]
  • FIG. 2 is an optical photograph taken of a eutectic alloy, showing a solidification structure in which an alpha magnesium matrix is formed as a dentritic structure with interdentritic segregation of a eutectic phase (alpha magnesium and quasicrystalline phase). [0014]
  • FIG. 3 is a transmission electron microphotograph showing a structure of a hot-rolled plate made of the eutectic alloy of FIG. 2, in which the quasicrystalline phase of the hot-rolled plate forms a stable interface to the matrix, being broken down into microparticles. [0015]
  • FIG. 4 is an electron microscopic diffraction pattern identifying the crystal structure of the second phase of the alloy. [0016]
  • FIG. 5 shows curves in which stresses of the metallic alloys Mg[0017] 97.9Zn1.8Y0.3 (□) and Mg95Zn4.3Y0.7 (±) are plotted versus temperature.
  • FIG. 6 shows curves in which the elongation of the metallic alloys of the present invention is plotted versus temperature. [0018]
  • FIG. 7 is an optical photograph showing the structure of a rolled plate made of an alloy of the present invention, in which the quasicrystalline phase is homogeneously distributed, in addition to forming a stable interface with the matrix metal.[0019]
  • DETAILED DESCRIPTION OF THE PRESENT INVENTION
  • In an aspect of the present invention, there is provided a quasicrystalline phase-reinforced Mg-based metallic alloy superior in warm and hot formability, which has a two-phase region consisting of a quasicrystalline phase and an Mg-based solid solution phase. When being solidified, the Mg-based solid solution phase (alpha magnesium) is formed as a primary solid phase, constituting a matrix structure. Meanwhile, the quasicrystalline phase serves as a second phase and forms, together with the magnesium-based solid solution phase, a eutectic phase, thereby reinforcing the matrix structure. [0020]
  • In an embodiment, the quasicrystalline phase-reinforced Mg-based metallic alloy has a composition of 1-10 at % Zn, and 0.1-3 at % Y, the remainder Mg. [0021]
  • In another aspect of the present invention, there is provided a method of making a quasicrystalline phase-reinforced magnesium-based metallic alloy, which comprises the steps of: casting a quasicrystalline phase-reinforced magnesium-based metallic alloy consisting of Mg-1˜10 at % Zn-0.1˜3 at % Y, into a mass, in which a two-phase region consisting of a quasicrystalline phase and a metal solid solution phase exists; and warm or hot forming the mass to separate and disperse the quasicrystalline phase throughout the matrix, so as to provide the quasicrystalline phase-reinforced magnesium-based metallic alloy with improved strength and elongation. [0022]
  • When being solidified from a liquid state, the quasicrystalline phase-reinforced Mg-based metallic alloy is required to have a two-phase region consisting of a quasicrystalline phase and a metal solid solution phase. To this end, Mg—Zn—Y alloys are suitable because thermodynamically stable quasicrystalline phase exists therein. During solidification of Mg—Zn—Y alloys, a eutectic reaction occurs in which a magnesium-based solid solution phase and a quasicrystalline phase are formed during solidification from a liquid state. Mg—Zn—Y alloys have a two-phase region of the magnesium-based solid solution phase and a quasicrystalline phase as seen in the phase diagram of FIG. 1. [0023]
  • The quasicrystalline phase-reinforced Mg-based metallic alloys of the present invention may be prepared into ingot or slab from a molten metal of Mg—Zn—Y alloys by a conventional casting method such as gravity die casting. [0024]
  • In addition, when the alloys are fabricated into plates by hot rolling or extrusion at a temperature ranging from half the melting point to the melting point at which common wrought materials are produced, the interface between the matrix and the quasicrystalline phase is not destroyed, but the quasicrystalline phase is separated and dispersed throughout the matrix. This hot forming process can be conducted on the eutectic alloy which has a quasicrystalline phase to a maximum of 30% of the alloy volume. In this connection, a hot rolling process is not successfully achieved in an alloy throughout which a quasicrystalline phase is distributed at a volume higher than 30% because the quasicrystalline phase is of high brittleness. Thus, the quantity of the quasicrystalline phase is limited to 30% by volume in the alloy. [0025]
  • The magnesium-based metallic alloy which is superior in warm and hot formability and has such a dispersed quasicrystalline phase as to afford high strength and elongation can be obtained when they have a composition of Mg-1˜10 at % Zn-0.1˜3 at % Y. The reason that the composition of the alloy is limited to such ranges is as follows. [0026]
  • When the content of Zn is below 1 at %, the resulting quasicrystalline phase is too low in volume to achieve the desired effects. On the other hand, when Zn is used at an amount larger than 3 at %, the quasicrystalline phase is too high in volume, so that the material is increased in brittleness. [0027]
  • Less than 0.1 at % of Y results in too low a volume of the quasicrystalline phase, making it difficult to achieve desired effects. On the other hand, an excess quasicrystalline phase results when using Y at an amount larger than 3 at %, so that the brittleness of the material is increased. [0028]
  • Generally, a plate material can be successfully produced into final products only when it has an elongation of at least 50% at forming temperatures. [0029]
  • At a temperature as high as or higher than one third of the melting point, which is the typical forming temperature for general metallic materials when using a warm or hot forming process, the plate is found to be of high formability as its elongation is measured to be 50% or higher. After undergoing this warm or hot forming process, the quasicrystalline phase is further dispersed and thus more homogeneously distributed throughout the matrix metal while stably maintaining the interface to the matrix metal, thereby bringing about a significant reinforcement effect attributed to the dispersion of the quasicrystalline phase. [0030]
  • A better understanding of the present invention may be obtained in light of the following examples which are set forth to illustrate, but are not to be construed to limit the present invention. [0031]
  • EXAMPLE
  • Molten metal of Mg—Zn—Y was prepared according to the compositions listed in Table 1 below, and cast into ingots. [0032]
    TABLE 1
    Quasicry-
    Alloy Eutectic Phase stalline
    Composition (at %) at Fraction Rolling
    Alloy = Mg Zn Y Solidification (vol %) Possibilities
     1 68 28 4 Quasicrystalline
     2 70 25.7 4.3 Alpha Mg
     3 71.8 25.2 3 Alpha Mg
     4 73.2 23 3.8 Alpha Mg
     5 73.8 22.5 3.7 Alpha Mg
     6 74.7 21.7 3.6 Alpha Mg
     7 80 17.1 2.9 Alpha Mg
     8 86 12 2 Alpha Mg 33 X
     9 90 8.6 1.4 Alpha Mg 20
    10 95 4.3 0.7 Alpha Mg 15
    11 97.8 2 0.2 Alpha Mg 4
  • In the case of alloy #1, the primary solid phase is a quasicrystalline phase in a solid structure. On the other hand, during solidification, alloys #2 to 11 showed the primary solid phase as a magnesium-base solid solution (alpha magnesium matrix) while having a quasicrystalline phase as a second phase. Thus, alloy compositions provided to the alloys #2-11 fall within the range suitable in the present invention when their solidification structures are taken into account. [0033]
  • With reference to FIG. 2, there is an optical photograph taken of the alloy #10, showing a solidification structure in which an alpha magnesium matrix is formed as a dentritic structure with interdentritic segregation of a eutectic phase (alpha magnesium and quasicrystalline phase). In each alloy composition shown in Table 1, the fraction of the quasicrystalline phase was found to be, by volume, about 33% for the alloy #8, about 20% for the alloy #9, about 15% for the alloy #10, and about 4% for the alloy #11 as measured by an image analyzer. [0034]
  • After being preheated for 20 min in a furnace at half the melting point or higher than the melting temperature at which general metallic materials are formed, e.g., in a furnace of 400° C., the alloys #8 to 11 was hot rolled according to a hot rolling process that is usually used for general wrought metallic materials. That is, the hot rolling was conducted in multiple passes at a temperature of 400° C. using 10% thickness reduction per pass to reduce the original body thickness to a final hot rolled thickness of 1.7 mm; i.e. a total reduction in thickness of 80%. [0035]
  • Owing to the existence of an excessive amount of quasicrystalline phase, the alloy #8 was not hot rolled successfully. Success was achieved in hot rolling the alloys #9, 10 and 11. The structure of the hot-rolled plate is shown in FIG. 3. The quasicrystalline phase of the hot-rolled plate forms a stable interface to the matrix as shown in the transmission electron micrograph of FIG. 3. In detail, the quasicrystalline phase was identified to be broken down into micro-scale fine particles during the hot rolling and dispersed throughout the matrix through thermal energy-induced mass flow, forming a stable interface to the matrix without destroying the matrix nor separating from the matrix. [0036]
  • In addition, in order to determine the crystal structure of the second phase, a diffraction pattern of the second phase existing in the alloy was observed under an electron microscope. The result is given in FIG. 4. As shown in the diffraction pattern, the crystal structure of the second phase present in the alloy of the present invention is found to have a five-fold rotational axis of symmetry, which is typical of a quasicrystal. [0037]
  • Therefore, the Mg-based alloy with superior hot formability and a dispersed quasicrystalline phase can be obtained from a composition of Mg-1˜10 at % Zn-0.1˜3 at % Y. [0038]
  • After being treated at 400° C. for 30 min to be homogenized, the plates (alloys #10 and 11) were prepared into tensile test specimens which were then tested for yield strength, maximum tensile strength, and elongation. The results are given in Table 2, below. [0039]
  • As a rule, since magnesium alloys are generally of hexagonal close-packed structure, they are unlikely to be formed into plates at room temperature. Thus, hot rolling is used to form magnesium alloys into plates. Representative of convertional wrought magnesium-based alloys are AZ31 and ZM21. Along with these representative conventional magnesium alloys, the alloys of the present invention are described with regard to the tested properties in Table 2, below. [0040]
    TABLE 2
    Yield Strength Max. Tensile Strength Elongation
    (MPa) (MPa) (%)
    Alloy #10 225 370 20
    Alloy #11 150 330 28
    AZ31B-H24 220 290 15
    ZM21-O 120 240 11
    ZM21-H24 165 250  6
  • As apparent from the data of Table 2, the alloys of the present invention are superior in yield strength, max tensile strength, and elongation. On the whole, conventional magnesium alloys listed in Table 2, which are capable of being hot-rolled, form solid solutions, so that only a small quantity of other elements can be permitted in the matrix, resulting in a decrease in their strength. In contrast, the alloys of the present invention, as seen in Table 1, have a quasicrystalline phase which is added at large amounts as a second phase. In addition, the quasicrystalline phase forms a stable interface with the matrix metal, serving to increase the strength of the alloys. [0041]
  • As a rule, an increase in the volume of the second phase in an alloy enlarges the total area of the interface between the particles and the matrix and thus causes a higher probability of interface problems such as interface debonding, finally reducing the elongation of the alloy. However, high elongation percentages were detected in the alloys of the present invention. These results indicate that the stable interface did not act as a source of destruction while the instability of the matrix metal is a fatal weakness. Plates made of magnesium alloys are prepared into final products through a hot sheet forming process. In this case, an elongation of 50% or higher at the temperature higher than one third of the melting temperature is required to fabricate the final products. Another requirement of the hot forming process is a low flow stress at the forming temperature in view of reduced energy consumption. [0042]
  • With reference to FIG. 5, there are curves in which the fracture stress and yield stress of the metallic alloys Mg[0043] 97.9Zn1.8Y0.3 (□) and Mg95Zn4.3Y0.7 (±) are plotted versus temperature. FIG. 6 shows curves in which the elongation of the metallic alloys of the present invention is plotted versus temperature. As seen in these curves, the yield stress does show only a little change up to 100° C., but decreases with increasing of temperature above 100° C. The elongation increases in an almost linear pattern with increasing temperature. Turning now to FIG. 7, there is an optical photograph showing the structure of a rolled plate made of the alloy #10. As seen in FIG. 7, the quasicrystalline phase is homogeneously distributed in addition to maintaining a stable interface with the matrix metal. In this case, a dispersion-induced reinforcement effect comes out more effectively, leading to an increase in strength.
  • As described hereinbefore, a quasicrystalline phase is formed in a metal solid solution upon solidification and dispersed throughout the matrix through hot forming, thus functioning as a reinforcement in the alloy of the present invention. Therefore, the alloy of the present invention retains not only the excellent mechanical properties that the metallic materials made by conventional various methods show, but also is superior in warm and hot formability. With these advantages, the alloy of the present invention can be prepared into various, final metallic products of high quality on a mass scale. Particularly, the alloy of the present invention is characterized in warm and hot formability because conventional Mg-based alloys are poor in formability. In addition, the alloy of the present invention is used where superior mechanical properties are needed. [0044]
  • Compared to materials formed from conventional Mg-based alloys, the materials obtained through the hot rolling or extrusion of the quasicrystalline phase-reinforced Mg-based metallic alloy of the present invention have an increased volume % of the second phase and thus show significantly increased strength. Particularly, the materials warm- or hot-rolled or extruded from the alloy of the present invention have much more stable interface between the particles and the matrix and are remarkably improved in elongation upon warm and hot rolling compared to composite metallic materials made by conventional powder metallurgy. [0045]
  • Thanks to excellent warm and hot formability, quasicrystalline microparticles are further homogeneously distributed in the alloy of the present invention during warm and hot forming, thus bringing about a significant improvement in the strength and fracture toughness of final products. Accordingly, the alloy of the present invention is useful as a material for high-quality metallic products which are required to be of light weight, high strength, high toughness and high formability. [0046]
  • Consequently, the alloy of the present invention is suitable for use in casings for portable electronic appliances such as mobile phones, and automobile parts, which require light weight, high strength, high toughness and high formability. Also, the alloy of the ID present invention can be used where wear-resistance is needed because the quasicrystalline phase has a friction coefficient of as low as 0.1-0.2. [0047]
  • The present invention has been described in an illustrative manner, and it is to be understood that the terminology used is intended to be in the nature of description rather than of limitation. Many modifications and variations of the present invention are possible in light of the above teachings. Therefore, it is to be understood that within the scope of the appended claims, the invention may be practiced otherwise than as specifically described. [0048]

Claims (5)

What is claimed is:
1. A quasicrystalline phase-reinforced magnesium-based metallic alloy with warm and hot formability, comprising a composition of 1-10 at % Zn, 0.1-3 at % Y and the remainder Mg, in which a two-phase region consisting of a quasicrystalline phase and a metal solid solution phase exists.
2. The quasicrystalline phase-reinforced magnesium-based metallic alloy as set forth in claim 1, wherein the amount of the quasicrystalline phase is 30% by volume or less.
3. A method of making a quasicrystalline phase-reinforced magnesium-based metallic alloy, comprising the steps of:
casting a quasicrystalline phase-reinforced magnesium-based metallic alloy consisting of 1-10 at % Zn, 0.1-3 at % Y, and the remainder Mg into a mass, in which a two-phase region consisting of a quasicrystalline phase and a metal solid solution phase exists; and
warm or hot forming the mass to separate and disperse quasicrystalline particles throughout the matrix, so as to provide the quasicrystalline phase-reinforced magnesium-based metallic alloy with improved strength and elongation.
4. The method as set forth in claim 3, further comprising the step of forming the warm- or hot-formed mass into a final product at the temperatures higher than one third of the melting temperature to further homogeneously distribute the quasicrystalline particles.
5. The method as set forth in claim 3, wherein the warm or hot forming step is carried out at a temperature ranging from half the melting point to the melting point and the quasicrystalline phase is present in an amount of 30% by volume or less.
US10/232,444 2001-04-11 2002-09-03 Quasicrystalline phase-reinforced Mg-based metallic alloy with high warm and hot formability and method of making the same Abandoned US20030029526A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US10/232,444 US20030029526A1 (en) 2001-04-11 2002-09-03 Quasicrystalline phase-reinforced Mg-based metallic alloy with high warm and hot formability and method of making the same

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
KR1020010019353A KR20020078936A (en) 2001-04-11 2001-04-11 Quasicrystalline phase hardened Mg-based metallic alloy exhibiting warm and hot formability
KR2001-19353 2001-04-11
US09/851,170 US6471797B1 (en) 2001-04-11 2001-05-09 Quasicrystalline phase-reinforced Mg-based metallic alloy with high warm and hot formability and method of making the same
US10/232,444 US20030029526A1 (en) 2001-04-11 2002-09-03 Quasicrystalline phase-reinforced Mg-based metallic alloy with high warm and hot formability and method of making the same

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US09/851,170 Division US6471797B1 (en) 2001-04-11 2001-05-09 Quasicrystalline phase-reinforced Mg-based metallic alloy with high warm and hot formability and method of making the same

Publications (1)

Publication Number Publication Date
US20030029526A1 true US20030029526A1 (en) 2003-02-13

Family

ID=19708105

Family Applications (2)

Application Number Title Priority Date Filing Date
US09/851,170 Expired - Lifetime US6471797B1 (en) 2001-04-11 2001-05-09 Quasicrystalline phase-reinforced Mg-based metallic alloy with high warm and hot formability and method of making the same
US10/232,444 Abandoned US20030029526A1 (en) 2001-04-11 2002-09-03 Quasicrystalline phase-reinforced Mg-based metallic alloy with high warm and hot formability and method of making the same

Family Applications Before (1)

Application Number Title Priority Date Filing Date
US09/851,170 Expired - Lifetime US6471797B1 (en) 2001-04-11 2001-05-09 Quasicrystalline phase-reinforced Mg-based metallic alloy with high warm and hot formability and method of making the same

Country Status (4)

Country Link
US (2) US6471797B1 (en)
JP (1) JP2002309332A (en)
KR (1) KR20020078936A (en)
WO (1) WO2002083964A1 (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1640466A1 (en) * 2004-09-28 2006-03-29 Kumamoto University Magnesium alloy and production process thereof
US20070125464A1 (en) * 2003-11-26 2007-06-07 Yoshihito Kawamura High strength and high toughness magnesium alloy and method of producing the same
CN100532605C (en) * 2007-12-06 2009-08-26 中国科学院长春应用化学研究所 A kind of magnesium-zinc-scandium alloy and preparation method thereof
CN100569976C (en) * 2007-05-30 2009-12-16 中国科学院金属研究所 Preparation method of effectively utilizing rare earth element Y to strengthen Mg-Zn-Y-Zr series magnesium alloy
CN102212727A (en) * 2011-06-10 2011-10-12 山东理工大学 Authigenic quasicrystal-reinforced Mg-Zn-Y alloy and smelting method thereof
US20110315282A1 (en) * 2009-01-19 2011-12-29 Hidetoshi Somekawa Mg-BASE ALLOY
CN104342591A (en) * 2014-11-03 2015-02-11 北京汽车股份有限公司 High-modulus magnesium matrix composite material containing SiC particles and preparation method thereof
CN111304471A (en) * 2020-02-18 2020-06-19 太原理工大学 Preparation method of low-alloying high-strength plastic magnesium alloy material
CN112359255A (en) * 2020-11-11 2021-02-12 沈阳工业大学 High-strength low-heat-cracking magnesium alloy
US12188108B2 (en) 2019-06-03 2025-01-07 Fort Wayne Metals Research Products Llc Magnesium-based absorbable alloys

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7309412B2 (en) * 2003-04-11 2007-12-18 Lynntech, Inc. Compositions and coatings including quasicrystals
RU2243279C1 (en) * 2003-08-27 2004-12-27 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" Magnesium-based alloy and product made from the same
US20050194072A1 (en) * 2004-03-04 2005-09-08 Luo Aihua A. Magnesium wrought alloy having improved extrudability and formability
KR100605741B1 (en) * 2004-04-06 2006-08-01 김강형 Magnesium alloy annealed material with excellent corrosion resistance and plating
CN100338250C (en) * 2004-05-19 2007-09-19 中国科学院金属研究所 High strength and high toughness cast magnesium alloy and preparing process thereof
CN1297676C (en) * 2004-11-11 2007-01-31 重庆大学 High plasticity magnesium alloy containing rare-earth yttrium
CN100340684C (en) * 2005-08-04 2007-10-03 上海交通大学 Method for preparing pseudo-crystal granule magnesium base composite material using powder hot-press method
JP5429702B2 (en) * 2006-08-03 2014-02-26 独立行政法人物質・材料研究機構 Magnesium alloy and manufacturing method thereof
JP4849402B2 (en) * 2006-09-15 2012-01-11 トヨタ自動車株式会社 High strength magnesium alloy and method for producing the same
JP5300116B2 (en) * 2006-12-25 2013-09-25 国立大学法人長岡技術科学大学 Manufacturing method of magnesium sheet for stretch
CN100462456C (en) * 2007-05-24 2009-02-18 太原理工大学 Mg-Zn-Nd-Si-based spherical quasicrystal master alloy and its manufacturing method
JP5210590B2 (en) * 2007-10-12 2013-06-12 株式会社日本製鋼所 High specific strength Mg alloy material, method for producing the same, and Mg alloy undersea structural member
CN102046821B (en) * 2008-06-03 2013-03-27 独立行政法人物质·材料研究机构 Mg-base alloy
KR20100038809A (en) * 2008-10-06 2010-04-15 포항공과대학교 산학협력단 Magnesium alloy panel having high formability and method of manufacturing the same
JP5419071B2 (en) * 2009-03-17 2014-02-19 独立行政法人物質・材料研究機構 Mg alloy forged product and its manufacturing method
JP5403508B2 (en) 2009-03-24 2014-01-29 独立行政法人物質・材料研究機構 Mg alloy member.
CN102206782A (en) * 2011-04-14 2011-10-05 太原理工大学 Degradable Mg-Zn-Y-Ca intravascular stent material and preparation method thereof
CN102251199B (en) * 2011-07-12 2012-11-28 北京工业大学 Stress-induced multistage solid solution treatment process for Mg-Gd-Er-Zr alloy
CN102634709B (en) * 2012-05-03 2013-07-31 华东交通大学 Preparation method of quasi-crystal modified high-damping Mg-Si alloy
JP6373557B2 (en) * 2013-02-08 2018-08-15 国立研究開発法人物質・材料研究機構 Magnesium wrought alloy and method for producing the same
CN104388804B (en) * 2014-12-03 2016-08-24 中北大学 The preparation method that a kind of aluminum bronze ferrum standard is brilliant
CN104593652B (en) * 2015-02-06 2016-08-24 中北大学 Quasicrystal and alumina mixed particle reinforced magnesium-based composite material and manufacturing method thereof
CN107760892B (en) * 2017-10-25 2019-04-30 太原理工大学 A kind of method and application of the magnesium alloy of coal base solid waste enhancing Icosahedral phases enhancing
CN108342630B (en) * 2018-05-18 2020-03-31 句容百利镁合金材料科技有限公司 Magnesium alloy, preparation method of magnesium alloy profile and preparation method of magnesium alloy rim
KR20250050113A (en) * 2022-10-07 2025-04-14 고꾸리쯔다이가꾸호오진 구마모또 다이가꾸 Magnesium alloy and its manufacturing method
CN117187652A (en) * 2023-09-11 2023-12-08 中南大学 A method to simultaneously increase the yield strength and elongation of Mg-Gd-Y rare earth magnesium alloys

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4765954A (en) * 1985-09-30 1988-08-23 Allied Corporation Rapidly solidified high strength, corrosion resistant magnesium base metal alloys
US5139077A (en) * 1988-03-07 1992-08-18 Allied-Signal Inc. Ingot cast magnesium alloys with improved corrosion resistance
JPH0310042A (en) * 1989-06-06 1991-01-17 Nippon Tungsten Co Ltd Heat-resistant, high-temperature, high-strength molybdenum material and its manufacturing method
JP2963225B2 (en) * 1991-03-14 1999-10-18 健 増本 Manufacturing method of amorphous magnesium alloy
JPH06228720A (en) * 1993-02-02 1994-08-16 Mazda Motor Corp Production of member made of magnesium alloy
US5851317A (en) 1993-09-27 1998-12-22 Iowa State University Research Foundation, Inc. Composite material reinforced with atomized quasicrystalline particles and method of making same

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10184165B2 (en) 2003-11-26 2019-01-22 Yoshihito Kawamura High strength and high toughness magnesium alloy and method of producing the same
US20070125464A1 (en) * 2003-11-26 2007-06-07 Yoshihito Kawamura High strength and high toughness magnesium alloy and method of producing the same
US20060065332A1 (en) * 2004-09-28 2006-03-30 Kumamoto University Magnesium alloy and production process thereof
EP1640466A1 (en) * 2004-09-28 2006-03-29 Kumamoto University Magnesium alloy and production process thereof
CN100569976C (en) * 2007-05-30 2009-12-16 中国科学院金属研究所 Preparation method of effectively utilizing rare earth element Y to strengthen Mg-Zn-Y-Zr series magnesium alloy
CN100532605C (en) * 2007-12-06 2009-08-26 中国科学院长春应用化学研究所 A kind of magnesium-zinc-scandium alloy and preparation method thereof
US20110315282A1 (en) * 2009-01-19 2011-12-29 Hidetoshi Somekawa Mg-BASE ALLOY
US9347123B2 (en) * 2009-01-19 2016-05-24 National Institute For Materials Science Mg-base alloy
CN102212727A (en) * 2011-06-10 2011-10-12 山东理工大学 Authigenic quasicrystal-reinforced Mg-Zn-Y alloy and smelting method thereof
CN104342591A (en) * 2014-11-03 2015-02-11 北京汽车股份有限公司 High-modulus magnesium matrix composite material containing SiC particles and preparation method thereof
US12188108B2 (en) 2019-06-03 2025-01-07 Fort Wayne Metals Research Products Llc Magnesium-based absorbable alloys
CN111304471A (en) * 2020-02-18 2020-06-19 太原理工大学 Preparation method of low-alloying high-strength plastic magnesium alloy material
CN112359255A (en) * 2020-11-11 2021-02-12 沈阳工业大学 High-strength low-heat-cracking magnesium alloy

Also Published As

Publication number Publication date
US6471797B1 (en) 2002-10-29
JP2002309332A (en) 2002-10-23
WO2002083964A1 (en) 2002-10-24
KR20020078936A (en) 2002-10-19

Similar Documents

Publication Publication Date Title
US6471797B1 (en) Quasicrystalline phase-reinforced Mg-based metallic alloy with high warm and hot formability and method of making the same
JP5239022B2 (en) High strength and high toughness magnesium alloy and method for producing the same
JP3194742B2 (en) Improved lithium aluminum alloy system
EP2492365B1 (en) Flame retardant magnesium alloy with excellent mechanical properties, and preparation method thereof
JP5047778B2 (en) Forged magnesium alloy having excellent formability and method for producing the same
JP4500916B2 (en) Magnesium alloy and manufacturing method thereof
JPH0328500B2 (en)
JPH02503331A (en) Magnesium alloy with high mechanical resistance and manufacturing method by rapid solidification of the alloy
CN102089450A (en) Aluminum alloy, method of casting aluminum alloy, and method of producing aluminum alloy product
JPS6221065B2 (en)
US20240263279A1 (en) High strength microalloyed magnesium alloy
WO2010056130A1 (en) Magnesium based alloys and processes for preparation thereof
JP3110512B2 (en) High strength and high toughness magnesium alloy material
KR20210130455A (en) Wrought magnesium alloys with high mechanical properties and method for preparing the same
JP5059505B2 (en) Aluminum alloy cold-rolled sheet that can be formed with high strength
JP2807374B2 (en) High-strength magnesium-based alloy and its solidified material
KR20210121541A (en) Wrought magnesium alloys with high mechanical properties and method for preparing the same
JPH05507766A (en) Forging method for rapidly solidifying magnesium-based metal alloy billets
US6893515B2 (en) Manufacturing process for highly ductile magnesium alloy
KR101001893B1 (en) High strength and high ductility magnesium alloy and its manufacturing method
JP3248255B2 (en) Al-Mg-Si alloy material for cryogenic forming
JP2007092103A (en) Magnesium-based metallic glass alloy-metal particle composite with ductility
JP2582027B2 (en) Manufacturing method of magnesium alloy casting
JP3485961B2 (en) High strength aluminum base alloy
US8016957B2 (en) Magnesium grain-refining using titanium

Legal Events

Date Code Title Description
STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION