US20020020475A1 - Heat-resistant magnesium alloy member - Google Patents

Heat-resistant magnesium alloy member Download PDF

Info

Publication number
US20020020475A1
US20020020475A1 US09/949,621 US94962101A US2002020475A1 US 20020020475 A1 US20020020475 A1 US 20020020475A1 US 94962101 A US94962101 A US 94962101A US 2002020475 A1 US2002020475 A1 US 2002020475A1
Authority
US
United States
Prior art keywords
molding
alloy
weight
magnesium alloy
heat
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
US09/949,621
Inventor
Kazuo Sakamoto
Yukio Yamamoto
Nobuo Sakate
Shoji Hirabara
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 US09/949,621 priority Critical patent/US20020020475A1/en
Publication of US20020020475A1 publication Critical patent/US20020020475A1/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
    • C22C23/02Alloys based on magnesium with aluminium as the next major constituent
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D17/00Pressure die casting or injection die casting, i.e. casting in which the metal is forced into a mould under high pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D21/00Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
    • B22D21/002Castings of light metals
    • B22D21/007Castings of light metals with low melting point, e.g. Al 659 degrees C, Mg 650 degrees C

Definitions

  • the present invention relates to a heat-resistant magnesium alloy member having an excellent molding property and. an excellent elongation property while keeping creep resistance property, its starting alloy compound, and a method of preparing the heat-resistant magnesium alloy member.
  • Magnesium alloy is the most low density one of the metal materials which are in practically use at present, and is strongly expected as a lightweight material for automobiles in future.
  • the magnesium alloy which is most popularly used at present is Mg—Al—Zn—Mn alloy (e.g., AZ91D alloy), and as it has a high strength at a room temperature and a good corrosion resistance, it is applied to transmission cases for an automobile, cylinder head covers, and the like.
  • Mg—Al—Zn—Mn alloy e.g., AZ91D alloy
  • Mg—Al—Zn—Mn alloy e.g., AZ91D alloy
  • it has such defects that, at a temperature range exceeding 120° C., it begins to show loss of strength characteristics, and especially becomes inferior in creep resistance, leading to a problem of yielding of bearing surface of the screw tightening part on the level of the packaged product.
  • Mg—Al—Si AS41 magnesium alloy As an aluminum alloy having an improved heat-resistance, there is used Mg—Al—Si AS41 magnesium alloy. However, though said alloy shows better creep resistance than the above AZ91D, it shows insufficient characteristics in the neighborhood of 150° C. of the use temperature, and moreover, as it shows low tensile strength characteristics at both room temperature and high temperature, it is required to be of thick wall to secure the required strength, thereby providing a problem of lowering the weight lightening effect due to magnesium materials.
  • a first object of the present invention is to provide a heat-resistant magnesium alloy member having excellent molding property and elongation while maintaining the physical properties, especially creep resistance, suited to the engine parts of automobiles and the like.
  • a second object of the present invention is to provide a pertinent molding method for preparing the above heat-resistant magnesium alloy member in place of conventional die-cast methods.
  • a third object of the present invention is to provide an alloy composition suited for producing a heat-resistant magnesium alloy member having the excellent molding property and elongation while maintaining the creep resistance.
  • the present inventors have found out that, in the Al—Ca magnesium alloy, when a semi-solid molding method of injection molding under the state of solid phase and liquid phase being present in mixture is applied in place of the die-cast method, the seizure of metal mold can be prevented, and also an excellent strength can be imparted to the molded member.
  • the addition amount of aluminum in order to maintain the state of presence in mixture of solid phase and liquid phase, it is necessary to increase the addition amount of aluminum as large as possible.
  • a magnesium alloy molding member comprising 2 to 6% by weight of aluminum and 0.5 to 4% by weight of calcium, and the balance of magnesium and unavoidable impurities, wherein a Ca/Al ratio is no more than 0.8, to have an excellent anti-creep property, molding property, and elongation.
  • Strontium is used as a micronizing agent in the casting of magnesium, and as it can display the micronizing effect in solid phase in the semi-solid injection molding of the present invention, it is preferably added.
  • the suitable addition amount is no more than 0.15% by weight.
  • the above molding member shows the crystal particle size of no more than 30 ⁇ m with the tensile strength of 180 Mpa (298° K.; ref. FIG. 9) or more, and excellent creep resistance of the minimum creep rate of no more than 4 ⁇ 10 ⁇ 10 /S under the test temperature of 150° C. and the test load of 50 MPa (according to JIS Z 2271 “method of tensile creep test of metal material”). Accordingly, it is suitable for the transmission part or engine part for automobiles. Especially, when the Ca/Al ratio is no more than 0.6, the molding member shows a more excellent creep resistance.
  • the present invention is to provide a heat-resistant magnesium alloy material to be molded by a semi-solid injection molding while maintaining excellent creep resistance property with the excellent molding property and elongation, comprising as an alloy material to be used for molding the above magnesium alloy molding part heat-resistant magnesium comprising 2 to 6% by weight of aluminum and 0.5 to 4% by weight of calcium, and the balance of magnesium and unavoidable impurities, and preferably further Sr of no more than 0.15% by weight, with adjustment, if necessary, of a Ca/Al ratio of no more than 0.8, preferably a Ca/Al ratio of no more than 0.6.
  • the alloy material in case of molding by a semi-solid injection molding method, it has been found that the material in the form of metal particles or pellets into which internal strain is introduced is effective for micronizing the crystals (ref. FIG. 10).
  • a cutting method is advantageous costwise.
  • the present invention is to provide a method for molding a heat-resistant magnesium alloy member characterized by carrying out a semi-solid injection molding, while maintaining an excellent creep resistance property with having an excellent molding property and elongation.
  • the die-cast method is in general to make injection into the metal mold at a temperature of 30-50° C. above a melting temperature
  • injection can be made at a temperature higher than the solidus temperature of the alloy and lower than the liquidus temperature, and accordingly the injection temperature is lowered by at least 30-60° C., so that the seizure to the metal mold can be prevented.
  • the solid phase ratio in the semi-solid state is preferably no more than 30%.
  • the solid phase ratio in the semi-solid state is preferably no more than 30%.
  • the above magnesium alloy may further contain no more than 2% by weight of at least one element selected from the group consisting of zinc, manganese, zirconium, and silicon, and/or no more than 4% by weight of a rare earth metal (e.g., yttrium, neodymium, lanthanum, cerium, misch metal). These are to improve the strength or high temperature strength of the above magnesium alloy effectively in the range no more than the upper limit thereof.
  • a rare earth metal e.g., yttrium, neodymium, lanthanum, cerium, misch metal.
  • FIG. 1 is a schematic diagram showing the constitution of the molding machine to be used for the semi-solid molding process and injection molding process according to the present invention.
  • FIG. 2 is a graph for making comparison of the creep characteristics of various magnesium alloy molding members.
  • FIG. 3 is a graph to show the relations between the Ca/Al ratio and the elongation at room temperature in various magnesium alloy molding members.
  • FIG. 4 is a schematic diagram showing a metal mold for testing casting cracks.
  • FIG. 5 is a graph showing the relation between the solid phase diameter and the staying time.
  • FIG. 6 is a graph showing the minimum creep strain rates of various magnesium alloy molding members.
  • FIG. 7 is a schematic diagram showing the metal mold for evaluating the flowing properties of various magnesium alloys.
  • FIG. 8 is a graph showing the relations between the solid phase ratio and the flowing length in the alloy composition in Example 2 measured by using a metal mold of FIG. 7.
  • FIG. 9 is a graph showing the relations between the average crystal particle size and the tensile strength of the member molded from the alloy composition of Example 3.
  • FIG. 10 is a schematic diagram showing the solid phase growth stages in the cases of using the metal particles having no work strain and those having the work strain.
  • FIG. 1 there is shown the whole constitution of the molding machine 1 to be used for the semi-solid molding method according to the present invention.
  • the material 3 of magnesium alloy metal particles or pellets (more than 3 mm in diameter) manufactured by the method of cutting or the like is charged into the hopper 8 in the drawing.
  • the material 3 is supplied to the cylinder 4 from the hopper 8 through the inlet 7 of argon atmosphere.
  • the material 3 is heated while being sent forward by the screw 2 . This heating zone is shown by the mark 10 .
  • the magnesium alloy material 3 shows a molten state, but at a level lower than the liquidus temperature the material becomes semi-solid condition in which the solid phase and the liquid phase are present in mixture, as illustrated. Also, in the magnesium alloy which is in a semi-solid condition, its shearing force acts to separate the solid phase finely as illustrated by agitation by the screw rotation.
  • the screw 2 is pushed forward with the rear high speed injection mechanism 5 , the molten material in which the solid phase has been finely cut under the semi-solid state is injected at high speed from the nozzle 9 as illustrated and filled in the metal mold 6 .
  • the contents in the metal mold are held under pressure until solidification, and thereafter the metal mold is opened to take out the molding product.
  • the semi-solid molding temperature was varied in the metal mold for evaluating flowing property as shown in FIG. 7, the molten material was introduced in the illustrated direction, and its flowing property was evaluated.
  • the results are shown in FIG. 8. From the results it can be seen that, when the solid phase rate exceeds 30%, the flow length is sharply lowered, and as this flow gives effect on the particle size of the texture crystals of the molding material, desirably the molding is made under the solid phase condition of no more than 30% in the semi-solid molding method.
  • the magnesium alloy material is used in the form of the metal particles or pellets.
  • the metal particles form the nuclei of recrystallization shortly after the heating, and increase the solid phase diameter. Therefore, when comparison is made between the case of using the metal particles having no work strain and that of using the metal particles having work strain, it can be understood that the growth rates of the solid phase are different as shown in FIG. 10, and the latter is superior to the former in the point of micronization of the crystal particle size of the molding member.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Forging (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)

Abstract

A heat-resistant magnesium alloy member having specially excellent molding property and elongation while keeping creep resistance property, which comprises 2 to 6% by weight of aluminum and 0.5 to 4% by weight of calcium, and the balance comprising magnesium and inevitable impurities, having a Ca/Al ratio of no more than 0.8, preferably no more than 0.6. The method of preparing the heat-resistant magnesium alloy member is characterized in a semi-solid injection molding at a range between a solidus temperaaature of the alloy and a liquidus temperature of the alloy.

Description

    TECHNICAL FIELD OF THE INVENTION
  • The present invention relates to a heat-resistant magnesium alloy member having an excellent molding property and. an excellent elongation property while keeping creep resistance property, its starting alloy compound, and a method of preparing the heat-resistant magnesium alloy member. [0001]
  • BACKGROUND OF THE INVENTION
  • Magnesium alloy is the most low density one of the metal materials which are in practically use at present, and is strongly expected as a lightweight material for automobiles in future. The magnesium alloy which is most popularly used at present is Mg—Al—Zn—Mn alloy (e.g., AZ91D alloy), and as it has a high strength at a room temperature and a good corrosion resistance, it is applied to transmission cases for an automobile, cylinder head covers, and the like. However, it has such defects that, at a temperature range exceeding 120° C., it begins to show loss of strength characteristics, and especially becomes inferior in creep resistance, leading to a problem of yielding of bearing surface of the screw tightening part on the level of the packaged product. [0002]
  • On the other hand, as an aluminum alloy having an improved heat-resistance, there is used Mg—Al—Si AS41 magnesium alloy. However, though said alloy shows better creep resistance than the above AZ91D, it shows insufficient characteristics in the neighborhood of 150° C. of the use temperature, and moreover, as it shows low tensile strength characteristics at both room temperature and high temperature, it is required to be of thick wall to secure the required strength, thereby providing a problem of lowering the weight lightening effect due to magnesium materials. [0003]
  • Besides, there are alloys such as QE22 with addition of silver or rare earth metals to improve a heat resistance thereof, but they have defects of being expensive and not suited to die-cast due to a poor casting property. [0004]
  • For the above reasons, there came to be newly proposed Mg—Al—Ca—Mn alloy (Japanese Laid-open Patent Publication HEI6-25790/1994) having excellent strength at high temperature. Here, it is said that, especially when the Ca/Al ratio is set to be more than 0.7, preferably more than 0.75, precipitates to be crystallized in the magnesium alloy convert into Mg—Ca compounds which crystallize, resulting in production of high temperature strength characteristics. [0005]
  • However, it has been found that, in a case of die-casting a member with a magnesium alloy having a high Ca/Al ratio, there often occur hot cracks, and due to a high melting temperature there easily occurs seizure to the metal mold. [0006]
  • SUMMARY OF THE INVENTION
  • In view of the problems held by the conventional techniques as above, a first object of the present invention is to provide a heat-resistant magnesium alloy member having excellent molding property and elongation while maintaining the physical properties, especially creep resistance, suited to the engine parts of automobiles and the like. [0007]
  • A second object of the present invention is to provide a pertinent molding method for preparing the above heat-resistant magnesium alloy member in place of conventional die-cast methods. [0008]
  • Further, a third object of the present invention is to provide an alloy composition suited for producing a heat-resistant magnesium alloy member having the excellent molding property and elongation while maintaining the creep resistance. [0009]
  • As a result of the repeated reviews to solve the above problems, the present inventors have found out that, in the Al—Ca magnesium alloy, when a semi-solid molding method of injection molding under the state of solid phase and liquid phase being present in mixture is applied in place of the die-cast method, the seizure of metal mold can be prevented, and also an excellent strength can be imparted to the molded member. However, in order to maintain the state of presence in mixture of solid phase and liquid phase, it is necessary to increase the addition amount of aluminum as large as possible. [0010]
  • On the other hand, aluminum dissolves in magnesium in solid state and shows age-hardening, and it is added to increase the mechanical properties of alloy, but it is recommended to add calcium so as to maintain the Ca/Al ratio to 0.7 or more to strengthen the high temperature strength which is in a tendency to be lowered by the addition of Al to Mg (Japanese Patent Laid-open Publication HEI6-25790/1994). However, when the Ca amount is large, casting cracks and seizure to metal mold often occur in molding, and additionally, a large amount of Mg—Ca compound crystallizes, with the result that there is a tendency of lowering of the elongation of the molded product, and it has been found that it is rather necessary to make the Ca/Al ratio no more than 0.8. [0011]
  • Accordingly, in the present invention, based on the above two findings, there is provided a magnesium alloy molding member comprising 2 to 6% by weight of aluminum and 0.5 to 4% by weight of calcium, and the balance of magnesium and unavoidable impurities, wherein a Ca/Al ratio is no more than 0.8, to have an excellent anti-creep property, molding property, and elongation. [0012]
  • In general, in the magnesium alloy, in order to obtain solid phase dissolution in magnesium, to exhibit age-hardening, and to elevate mechanical strength, it has been understood to be preferable to add 2-10% by weight of aluminum. While it is necessary in the present invention to add more than 2% by weight of aluminum, when the amount of addition exceeds 6% by weight, it has been found that the elongation is lowered even if the semi-solid injection molding would be carried out. Accordingly, in order to obtain the designed effect while carrying out the semi-solid injection molding, it has been found that the addition amount should be limited to no more than 6% by weight. On the other hand, calcium is added to increase the high temperature strength which is in a tendency to be lowered by the addition of aluminum to magnesium, but it has been found that it is necessary to suppress the Ca/Al ratio to no more than 0.8% by weight to prevent lowering of the molding property and elongation of the molding member, and in addition, the Ca amount should be limited to 0.5-4% by weight. [0013]
  • Strontium is used as a micronizing agent in the casting of magnesium, and as it can display the micronizing effect in solid phase in the semi-solid injection molding of the present invention, it is preferably added. The suitable addition amount is no more than 0.15% by weight. [0014]
  • The above molding member shows the crystal particle size of no more than 30 μm with the tensile strength of 180 Mpa (298° K.; ref. FIG. 9) or more, and excellent creep resistance of the minimum creep rate of no more than 4×10[0015] −10/S under the test temperature of 150° C. and the test load of 50 MPa (according to JIS Z 2271 “method of tensile creep test of metal material”). Accordingly, it is suitable for the transmission part or engine part for automobiles. Especially, when the Ca/Al ratio is no more than 0.6, the molding member shows a more excellent creep resistance.
  • The present invention is to provide a heat-resistant magnesium alloy material to be molded by a semi-solid injection molding while maintaining excellent creep resistance property with the excellent molding property and elongation, comprising as an alloy material to be used for molding the above magnesium alloy molding part heat-resistant magnesium comprising 2 to 6% by weight of aluminum and 0.5 to 4% by weight of calcium, and the balance of magnesium and unavoidable impurities, and preferably further Sr of no more than 0.15% by weight, with adjustment, if necessary, of a Ca/Al ratio of no more than 0.8, preferably a Ca/Al ratio of no more than 0.6. [0016]
  • Especially, as for the alloy material, in case of molding by a semi-solid injection molding method, it has been found that the material in the form of metal particles or pellets into which internal strain is introduced is effective for micronizing the crystals (ref. FIG. 10). As for the processing method for the metal particles or pellets, a cutting method is advantageous costwise. [0017]
  • Further, in case of applying a semi-solid injection molding wherein an injection molding is carried out in the state of a solid phase and a liquid phase being present in mixture, practice can be made at a temperature lower than a liquidus temperature. Accordingly, the present invention is to provide a method for molding a heat-resistant magnesium alloy member characterized by carrying out a semi-solid injection molding, while maintaining an excellent creep resistance property with having an excellent molding property and elongation. [0018]
  • Against the fact that the die-cast method is in general to make injection into the metal mold at a temperature of 30-50° C. above a melting temperature, in the semi-solid injection molding of the present invention, injection can be made at a temperature higher than the solidus temperature of the alloy and lower than the liquidus temperature, and accordingly the injection temperature is lowered by at least 30-60° C., so that the seizure to the metal mold can be prevented. [0019]
  • It can be understood that, since solidification takes place from a semi-solid state in the present invention, and coagulation stress therewith becomes small, generation of hot cracking can be prevented due to this method mechanism. [0020]
  • Especially, in the semi-solid molding method, in the range of no more than 30% by weight of the solid phase rate, these prevention and effect on a flow length become remarkable (ref. FIG. 8), and the generation of hot cracking can be effectively prevented. Accordingly, in case of carrying out the semi-solid molding, the solid phase ratio in the semi-solid state is preferably no more than 30%. In general, it has been understood that a higher solid phase ratio is more advantageous for the seizure and coagulation stress, but in the present invention method, when the solid phase rate is high, the fluidity is lowered to give a tendency of lowering in filling property and generation of cold shut, thereby making it difficult to obtain a sound molding member. [0021]
  • It has been found that, especially when the average particle size of these coagulation textures is no more than 30 μm, the elongation amount shows specially large improvement. [0022]
  • The above magnesium alloy may further contain no more than 2% by weight of at least one element selected from the group consisting of zinc, manganese, zirconium, and silicon, and/or no more than 4% by weight of a rare earth metal (e.g., yttrium, neodymium, lanthanum, cerium, misch metal). These are to improve the strength or high temperature strength of the above magnesium alloy effectively in the range no more than the upper limit thereof.[0023]
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a schematic diagram showing the constitution of the molding machine to be used for the semi-solid molding process and injection molding process according to the present invention. [0024]
  • FIG. 2 is a graph for making comparison of the creep characteristics of various magnesium alloy molding members. [0025]
  • FIG. 3 is a graph to show the relations between the Ca/Al ratio and the elongation at room temperature in various magnesium alloy molding members. [0026]
  • FIG. 4 is a schematic diagram showing a metal mold for testing casting cracks. [0027]
  • FIG. 5 is a graph showing the relation between the solid phase diameter and the staying time. [0028]
  • FIG. 6 is a graph showing the minimum creep strain rates of various magnesium alloy molding members. [0029]
  • FIG. 7 is a schematic diagram showing the metal mold for evaluating the flowing properties of various magnesium alloys. [0030]
  • FIG. 8 is a graph showing the relations between the solid phase ratio and the flowing length in the alloy composition in Example 2 measured by using a metal mold of FIG. 7. [0031]
  • FIG. 9 is a graph showing the relations between the average crystal particle size and the tensile strength of the member molded from the alloy composition of Example 3. [0032]
  • FIG. 10 is a schematic diagram showing the solid phase growth stages in the cases of using the metal particles having no work strain and those having the work strain.[0033]
  • DETAIED EXPLANATION OF THE INVENTION
  • In FIG. 1, there is shown the whole constitution of the [0034] molding machine 1 to be used for the semi-solid molding method according to the present invention. In the molding method of the present invention, the material 3 of magnesium alloy metal particles or pellets (more than 3 mm in diameter) manufactured by the method of cutting or the like is charged into the hopper 8 in the drawing. The material 3 is supplied to the cylinder 4 from the hopper 8 through the inlet 7 of argon atmosphere. In this cylinder 4, the material 3 is heated while being sent forward by the screw 2. This heating zone is shown by the mark 10. At an approximate liquidus temperature of heating, the magnesium alloy material 3 shows a molten state, but at a level lower than the liquidus temperature the material becomes semi-solid condition in which the solid phase and the liquid phase are present in mixture, as illustrated. Also, in the magnesium alloy which is in a semi-solid condition, its shearing force acts to separate the solid phase finely as illustrated by agitation by the screw rotation. Here, when the screw 2 is pushed forward with the rear high speed injection mechanism 5, the molten material in which the solid phase has been finely cut under the semi-solid state is injected at high speed from the nozzle 9 as illustrated and filled in the metal mold 6. Here, the contents in the metal mold are held under pressure until solidification, and thereafter the metal mold is opened to take out the molding product.
  • EXAMPLES 1-7 AND COMPARATIVE EXAMPLES 1-5
  • An iron crucible is installed in a low frequency furnace, and while flowing 1% of the SF[0035] 6 gas (rest is dry air) on the surface of the molten material, the alloys having the components of Examples and Comparative Examples were prepared by melting. The resulting alloys were cast on a plate to prepare 3-5 mm diameter pellets by milling. Using these as raw materials, semi-solid molding was carried out by using the above molding machine.
    TABLE 1
    Chemical Composition (Wt. %)
    Al Ca Si Mn Sr Mg
    Example 1 Mg-3Al-2Ca 2.98 2.05 0.30 0.25 Remainder
    Example 2 Mg-4Al-2Ca 3.95 2.02 0.30 0.32
    Example 3 Mg-4Al-3Ca 4.02 3.06 0.25 0.28
    Example 4 Mg-6Al-3Ca 5.97 3.10 0.28 0.30
    Example 5 Mg-4Al-2Ca-0.03Sr 3.87 2.06 0.25 0.25 0.03
    Example 6 Mg-4Al-2Ca-0.09Sr 4.02 1.98 0.30 0.23 0.09
    Example 7 Mg-4Al-2Ca-0.15Sr 4.05 2.10 0.23 0.25 0.15
    Comparative ASTM AS41 4.39 0.45 0.28
    Example 1 Equivalent
    Comparative Mg-9Al-0.5Ca 8.70 0.49 0.90 0.21
    Example 2
    Comparative ASTM AZ91D 8.84 0.02 0.22
    Example 3 Equivalent
    Comparative Mg-4Al-4Ca 4.02 3.96 0.32 032
    Example 4
    Comparative Mg-3Al-3Ca 2.75 2.71 0.27 0.36
    Example 5
  • For the semi-solid molding, a machine having the clamping force of 450 t was used under the conditions of injection speed at the metal mold gate part of 50 m/s, injection pressure of about 700 kg/cm[0036] 2, and the temperature of the alloy at the nozzle part was set to be lower than the liquidus level of 550-580° C. Under the above molding conditions a tensile test piece (JIS No.4 test piece) was prepared, with which the creep property at 150° C., 50 MPa was examined by the tensile creep test method based on JIS Z 2271. The results are shown in FIG. 2. It can be seen that the magnesium alloy of the present invention is more excellent in creep resistance characteristic than AS41 which is commented as being superior in creep resistance to Az91D of Comparative Example 3.
  • Further, the breaking strength and breaking elongation were measured with an instron tensile tester at a cross head rate of 10 mm/min. and at a measuring temperature of 25° C. The results are shown in Table 2. It can be seen that, in comparison with Comparative Example 2 in which the aluminum content exceeds the present invention range of 2-6% by weight and Comparative Example 4 in which the aluminum and calcium contents lie within the present invention range but the Ca/Al ratio exceeds by 0.8, the Examples containing 2-6% by weight of aluminum and 0.5-4% by weight of calcium and having the Ca/Al ratio of no more than 0.8 show excellent elongation. [0037]
    TABLE 2
    Al amount Ca amount Elongation
    (Wt. %) (Wt. %) (%)
    Example 2 3.95 2.02 6.7
    Example 3 4.02 3.06 7.0
    Example 4 5.97 3.10 5.2
    Comparative Example 2 8.70 0.49 0.8
    Comparative Example 4 4.02 3.96 1.2
  • Then, in Examples and Comparative Examples, the relations between the Ca/Al ratio and the above elongation are illustrated in FIG. 3, from which it can be seen that when the Ca/Al ratio exceeds 0.8, the elongation is sharply lowered. In this connection, when the relations between the Ca/Al ratio and the minimum creep rate of strain are observed, as shown in FIG. 6, in case of the Ca/Al ratio being no more than 0.6 (Example 2), the smaller creep rate of strain is shown, and it can be seen that the creep resistance property becomes more excellent. [0038]
  • Further, when the semi-melting molding was carried out by using the metal mold for test as shown in FIG. 4 and securing the illustrated running, there were obtained the results as shown in Table 3. As a result, it-was seen that when the Ca/Al ratio approached 1, casting cracks were formed on the overflow side at the top end of the cylindrical part, but at the Ca/Al ratio of no more than 0.8, no such casting crack was formed at all. [0039]
    TABLE 3
    Ca/Al weight Casting crack
    ratio formed or not
    Example 1 0.69 No
    Example 2 0.51 No
    Example 3 0.76 No
    Example 4 0.52 No
    Comparative Example 1 0.99 Yes
    Comparative Example 5 0.99 Yes
  • In general, when the staying time in casting is extended, the solid phase diameter is sharply increased (Example in FIG. 5), but it can be seen that, when strontium is added, the crystal micronizing effect is actuated to suppress the increment in the solid phase diameter attributed to the staying time. [0040]
  • Using the alloy material of Example 2, the semi-solid molding temperature was varied in the metal mold for evaluating flowing property as shown in FIG. 7, the molten material was introduced in the illustrated direction, and its flowing property was evaluated. The results are shown in FIG. 8. From the results it can be seen that, when the solid phase rate exceeds 30%, the flow length is sharply lowered, and as this flow gives effect on the particle size of the texture crystals of the molding material, desirably the molding is made under the solid phase condition of no more than 30% in the semi-solid molding method. [0041]
  • In the semi-solid molding, the magnesium alloy material is used in the form of the metal particles or pellets. When work strain is given inside the metal particles by cutting work or the like, the metal particles form the nuclei of recrystallization shortly after the heating, and increase the solid phase diameter. Therefore, when comparison is made between the case of using the metal particles having no work strain and that of using the metal particles having work strain, it can be understood that the growth rates of the solid phase are different as shown in FIG. 10, and the latter is superior to the former in the point of micronization of the crystal particle size of the molding member. [0042]
  • As will be apparent from the above description, according to the present invention, it is possible to obtain a molding member having excellent creep resistance characteristic at high temperature by controlling Ca/Al ratio in Mg—Al—Ca heat resistant magnesium alloy member. Therefore, it is possible to produce the transmission parts for automobiles such as clutch piston and clutch drum and engine parts such as rocker arm with the lightweight magnesium alloy to give a sufficient durability. [0043]
  • Further, according to the present invention, by carrying out semi-solid molding at a temperature lower than the liquidus level, the problems of hot crack and seizure to the metal mold which had been remarkable in the conventional die-cast process are dissolved, and on the other hand, the strength at room temperature and high temperature along with elongation equivalent to or higher than those of the conventional process can be retained. [0044]

Claims (3)

What is claimed is:
1. A method of molding a heat-resistant magnesium alloy member having a creep resistance property of no more than 4×10−10/S of minimum creep rate under the test temperature of 150° C. and the test load of 50 MPa, comprising the steps of;
providing aluminum and calcium;
preparing an alloy composition comprising 2 to 6% by weight of said aluminum and 0.5 to 4% by weight of said calcium, and no more than 2% by weight of at least one element selected from the group consisting of zinc, manganese, zirconium, and silicon, and/or no more than 4% by weight of a rare earth metal, and the balance of magnesium and inevitable impurities, wherein a Ca/Al ratio of said alloy composition is no more than 0.8 and the average particle size of the crystal is no more than 30 μm,
processing said alloy composition by a cutting method so that said alloy composition is in the form of metal particles or pellets into which internal strain is introduced, and
subjecting said alloy composition to a semi-solid injection molding by using an injection molding machine having a cylinder and a screw at a temperature range between a solidus temperature of the alloy and a liquidus temperature of the alloy, wherein a solid phase ratio in semi-solid state is no more than 30% at the time of carrying out an injection molding.
2. The method of molding a heat-resistant magnesium alloy member according to claim 1, wherein said Ca/Al ratio is no more than 0.6.
3. The method of molding a heat-resistant magnesium alloy member according to claim 1, wherein the magnesium alloy further contains 0.03 to 0.15% by weight of Sr.
US09/949,621 1996-04-04 2001-09-12 Heat-resistant magnesium alloy member Abandoned US20020020475A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US09/949,621 US20020020475A1 (en) 1996-04-04 2001-09-12 Heat-resistant magnesium alloy member

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
JP08-082832 1996-04-04
JP08283296A JP3415987B2 (en) 1996-04-04 1996-04-04 Molding method of heat-resistant magnesium alloy molded member
US83480597A 1997-04-03 1997-04-03
US09/949,621 US20020020475A1 (en) 1996-04-04 2001-09-12 Heat-resistant magnesium alloy member

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US83480597A Division 1996-04-04 1997-04-03

Publications (1)

Publication Number Publication Date
US20020020475A1 true US20020020475A1 (en) 2002-02-21

Family

ID=13785388

Family Applications (1)

Application Number Title Priority Date Filing Date
US09/949,621 Abandoned US20020020475A1 (en) 1996-04-04 2001-09-12 Heat-resistant magnesium alloy member

Country Status (6)

Country Link
US (1) US20020020475A1 (en)
EP (1) EP0799901B1 (en)
JP (1) JP3415987B2 (en)
KR (1) KR970070224A (en)
CN (1) CN1065003C (en)
DE (1) DE69706737T2 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6904954B2 (en) 2001-04-09 2005-06-14 Sumitomo Electric Industries, Ltd. Magnesium alloy material and method of manufacturing the alloy material
US20050150577A1 (en) * 2004-01-09 2005-07-14 Takata Corporation Magnesium alloy and magnesium alloy die casting
US20050194072A1 (en) * 2004-03-04 2005-09-08 Luo Aihua A. Magnesium wrought alloy having improved extrudability and formability
US20070258845A1 (en) * 2004-06-15 2007-11-08 Katsuyoshi Kondoh High-Strength and High-Toughness magnesium Based Alloy, Driving System Part Using the Same and Manufacturing Method of High-Strength and High-Toughness magnesium Based Alloy Material
US20130144290A1 (en) * 2010-07-06 2013-06-06 Ait Austrian Institute Of Technology Gmbh Magnesium alloy
US20220154314A1 (en) * 2019-03-12 2022-05-19 Honda Motor Co., Ltd. Flame-resistant magnesium alloy and method for producing the same
US11959155B2 (en) 2019-03-29 2024-04-16 Kurimoto, Ltd. Heat-resistant magnesium alloy for casting

Families Citing this family (64)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AUPP060497A0 (en) 1997-11-28 1998-01-08 Commonwealth Scientific And Industrial Research Organisation Magnesium pressure die casting
JPH11323474A (en) * 1998-05-13 1999-11-26 Mazda Motor Corp Magnesium alloy casting member
IL125681A (en) * 1998-08-06 2001-06-14 Dead Sea Magnesium Ltd Magnesium alloy for high temperature applications
JP2000104137A (en) * 1998-09-30 2000-04-11 Mazda Motor Corp Magnesium alloy forging stock, forged member and production of the forged member
JP3521773B2 (en) * 1998-11-30 2004-04-19 セイコーエプソン株式会社 Method of manufacturing watch parts, watch parts, and watch
DE19915277A1 (en) * 1999-04-03 2000-10-05 Volkswagen Ag Magnesium alloy used e.g. in the manufacture of a wheel rim contains traces of cadmium, copper, iron, nickel and lanthanum and yttrium
US6264763B1 (en) * 1999-04-30 2001-07-24 General Motors Corporation Creep-resistant magnesium alloy die castings
WO2001015836A1 (en) * 1999-08-30 2001-03-08 Hitachi, Ltd. Method and device for metal injection molding and product
JP2001073059A (en) * 1999-09-06 2001-03-21 Mazda Motor Corp Magnesium alloy formed member
JP3611759B2 (en) * 1999-10-04 2005-01-19 株式会社日本製鋼所 Magnesium alloy and magnesium alloy heat-resistant member with excellent heat resistance and castability
US6808679B2 (en) * 1999-12-15 2004-10-26 Noranda, Inc. Magnesium-based casting alloys having improved elevated temperature performance, oxidation-resistant magnesium alloy melts, magnesium-based alloy castings prepared therefrom and methods for preparing same
CA2337630C (en) 2000-02-24 2005-02-01 Mitsubishi Aluminum Co., Ltd. Die casting magnesium alloy
JP2001247926A (en) * 2000-03-03 2001-09-14 Japan Steel Works Ltd:The Magnesium alloy excellent in fluidity and magnesium alloy material
JP3551121B2 (en) * 2000-04-07 2004-08-04 マツダ株式会社 Manufacturing method of light metal moldings
JP2001316753A (en) * 2000-05-10 2001-11-16 Japan Steel Works Ltd:The Magnesium alloy and magnesium alloy member excellent in corrosion resistance and heat resistance
US6342180B1 (en) 2000-06-05 2002-01-29 Noranda, Inc. Magnesium-based casting alloys having improved elevated temperature properties
AUPQ967800A0 (en) 2000-08-25 2000-09-21 Commonwealth Scientific And Industrial Research Organisation Aluminium pressure casting
JP2002275569A (en) * 2001-03-14 2002-09-25 Ryobi Ltd CREEP RESISTANT Mg ALLOY
AU2005200721B2 (en) * 2001-04-09 2007-11-15 Sumitomo Electric Industries, Ltd. Magnesium Alloy Material and Method of Manufacturing the Alloy Material
JP4661857B2 (en) * 2001-04-09 2011-03-30 住友電気工業株式会社 Magnesium alloy material and method for producing the same
WO2002099147A1 (en) * 2001-06-06 2002-12-12 Noranda, Inc. Magnesium-based casting alloys having improved elevated temperature properties
JP3869255B2 (en) 2001-06-14 2007-01-17 富士通株式会社 Metal molded body manufacturing method and metal molded body manufactured thereby
JP3723522B2 (en) 2001-08-03 2005-12-07 富士通株式会社 Metal body manufacturing method
JP2003129161A (en) * 2001-08-13 2003-05-08 Honda Motor Co Ltd Heat resistant magnesium alloy
CN1317412C (en) 2001-08-13 2007-05-23 本田技研工业株式会社 Magnesium alloy
JP2003129160A (en) * 2001-08-13 2003-05-08 Honda Motor Co Ltd Heat resistant magnesium alloy
KR100421102B1 (en) * 2001-08-22 2004-03-04 미츠비시 알루미늄 컴파니 리미티드 Die casting magnesium alloy
JP3592659B2 (en) 2001-08-23 2004-11-24 株式会社日本製鋼所 Magnesium alloys and magnesium alloy members with excellent corrosion resistance
IL146336A0 (en) 2001-11-05 2002-07-25 Dead Sea Magnesium Ltd High strength creep resistant magnesium alloy
IL146335A0 (en) 2001-11-05 2002-07-25 Dead Sea Magnesium Ltd Creep resistant magnesium alloys with improved castability
JP3861720B2 (en) * 2002-03-12 2006-12-20 Tkj株式会社 Forming method of magnesium alloy
DE10221720A1 (en) * 2002-05-16 2003-11-27 Bayerische Motoren Werke Ag Magnesium-based alloy for die casting of cylinder crank housings of internal combustion engines contains alloying additions of aluminum, calcium and strontium
JP3476814B1 (en) * 2002-06-21 2003-12-10 宇部興産機械株式会社 Mold for semi-solid metal molding
JP2004162090A (en) * 2002-11-11 2004-06-10 Toyota Industries Corp Heat resistant magnesium alloy
CN100366775C (en) * 2003-01-07 2008-02-06 死海鎂有限公司 High strength creep-resisting magnetium base alloy
JP4575645B2 (en) * 2003-01-31 2010-11-04 株式会社豊田自動織機 Heat-resistant magnesium alloy for casting and heat-resistant magnesium alloy casting
JP2004230445A (en) * 2003-01-31 2004-08-19 Ahresty Corp Die for magnesium die-casting
US8123877B2 (en) 2003-01-31 2012-02-28 Kabushiki Kaisha Toyota Jidoshokki Heat-resistant magnesium alloy for casting heat-resistant magnesium alloy cast product, and process for producing heat-resistant magnesium alloy cast product
KR100494514B1 (en) * 2003-04-21 2005-06-10 현대자동차주식회사 Method for manufacturing of magnesium alloy billets for thixoforming process
JP4202298B2 (en) * 2003-09-18 2008-12-24 トヨタ自動車株式会社 Heat-resistant magnesium alloy for die casting and die-cast products of the same alloy
JP4289613B2 (en) * 2004-02-27 2009-07-01 日精樹脂工業株式会社 Low melting point metal alloy forming method
JP4009601B2 (en) * 2004-02-27 2007-11-21 日精樹脂工業株式会社 Low melting point metal alloy forming method
JP4051350B2 (en) * 2004-03-05 2008-02-20 日精樹脂工業株式会社 Low melting point metal alloy forming method
EP1857203B1 (en) 2005-02-22 2013-05-15 Hitachi Metals Precision, Ltd. Impeller for supercharger and method of manufacturing the same
JP2007198544A (en) * 2006-01-27 2007-08-09 Toyota Motor Corp Fastening structure of magnesium alloy
JP4539572B2 (en) * 2006-01-27 2010-09-08 株式会社豊田中央研究所 Magnesium alloys and castings for casting
EP2135965A4 (en) * 2007-04-03 2010-03-31 Toyota Jidoshokki Kk Heat-resistant magnesium alloy
JP4051393B2 (en) * 2007-06-13 2008-02-20 日精樹脂工業株式会社 Low melting point metal alloy forming method
JP5136169B2 (en) * 2008-04-04 2013-02-06 宇部興産機械株式会社 Semi-molten metal mold
JP2009007676A (en) * 2008-07-30 2009-01-15 Toyota Industries Corp Heat resistant magnesium alloy for casting, and heat resistant magnesium alloy casting
JP5388277B2 (en) 2009-02-20 2014-01-15 Ntn株式会社 Cage, rolling bearing, cage manufacturing method and injection mold
CN101818293B (en) * 2010-04-21 2012-05-30 广州有色金属研究院 Heat resistant magnesium alloy
JP5700005B2 (en) * 2012-09-05 2015-04-15 株式会社豊田中央研究所 Composite magnesium alloy member and manufacturing method thereof
JP6596236B2 (en) 2015-05-27 2019-10-23 本田技研工業株式会社 Heat-resistant magnesium alloy and method for producing the same
CN105817602B (en) * 2015-09-09 2018-05-08 广东鸿泰南通精机科技有限公司 A kind of automobile gearbox upper valve board production technology
CN107541627B (en) * 2016-06-24 2019-09-06 北京科技大学 A kind of wrought magnesium alloy plate and preparation method thereof with good room temperature formability
JP2018193592A (en) * 2017-05-19 2018-12-06 株式会社豊田中央研究所 Magnesium alloy, magnesium alloy cast, and manufacturing method therefor
JP2019063835A (en) * 2017-10-04 2019-04-25 株式会社日本製鋼所 Method for producing stock for forging made of magnesium alloy
CN110195181B (en) * 2018-02-26 2021-10-22 中国宝武钢铁集团有限公司 Die-casting magnesium alloy with high-temperature heat resistance and manufacturing method thereof
CN109913720B (en) * 2019-03-27 2020-11-24 东北大学 High-calcium high-aluminum-content high-elasticity-modulus magnesium-based composite material and preparation method thereof
CN109957692A (en) * 2019-03-27 2019-07-02 东北大学 A kind of the casting magnesium-based composite material and preparation method of high calcium high aluminium content
CN111155011A (en) * 2020-02-21 2020-05-15 江苏理工学院 High-performance Mg-Al-Ca magnesium alloy and preparation method thereof
CN112725673A (en) * 2020-12-28 2021-04-30 中信戴卡股份有限公司 Mg-Al alloy and preparation method thereof
CN113005347B (en) * 2021-02-25 2021-10-08 吉林大学 High-plasticity Mg-Al-Ca magnesium alloy and preparation method thereof

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2642439B2 (en) * 1988-02-26 1993-04-16 Pechiney Electrometallurgie
DE69007920T2 (en) * 1989-08-24 1994-07-21 Norsk Hydro As High-strength magnesium alloys and processes for their production through rapid solidification.
JP2730847B2 (en) * 1993-06-28 1998-03-25 宇部興産株式会社 Magnesium alloy for castings with excellent high temperature creep strength
JPH07118785A (en) * 1993-10-25 1995-05-09 Mitsui Mining & Smelting Co Ltd Mg alloy for casting, non porosity mg alloy casting and their production
JPH07278717A (en) * 1994-04-12 1995-10-24 Ube Ind Ltd Magnesium alloy member excellent in settling resistance in pressurized part
JPH07331375A (en) * 1994-06-06 1995-12-19 Toyota Motor Corp Heat resistant magnesium alloy for casting
JPH0841576A (en) * 1994-07-28 1996-02-13 Honda Motor Co Ltd High strneght magnesium alloy and heat treatment for magnesium alloy casting
AU4617796A (en) * 1995-02-17 1996-09-04 Institute De La Technologie Du Magnesium, Inc Creep resistant magnesium alloys for die casting

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050158202A1 (en) * 2001-04-09 2005-07-21 Sumitomo Electric Industries, Ltd. Magnesium alloy material and method of manufacturing the alloy material
US6904954B2 (en) 2001-04-09 2005-06-14 Sumitomo Electric Industries, Ltd. Magnesium alloy material and method of manufacturing the alloy material
US7478665B2 (en) 2001-04-09 2009-01-20 Sumitomo Electric Industries, Ltd. Method of manufacturing magnesium alloy material
US20090056907A1 (en) * 2001-04-09 2009-03-05 Sumitomo Electric Industries, Ltd. Method of manufacturing magnesium alloy material
US7779891B2 (en) 2001-04-09 2010-08-24 Sumitomo Electric Industries, Ltd. Method of manufacturing magnesium alloy material
US20050150577A1 (en) * 2004-01-09 2005-07-14 Takata Corporation Magnesium alloy and magnesium alloy die casting
US7967928B2 (en) 2004-03-04 2011-06-28 GM Global Technologies Operations LLC Methods of extruding magnesium alloys
US20050194072A1 (en) * 2004-03-04 2005-09-08 Luo Aihua A. Magnesium wrought alloy having improved extrudability and formability
US20080017286A1 (en) * 2004-03-04 2008-01-24 Gm Global Technology Operations, Inc. Methods of extruding magnesium alloys
US20070258845A1 (en) * 2004-06-15 2007-11-08 Katsuyoshi Kondoh High-Strength and High-Toughness magnesium Based Alloy, Driving System Part Using the Same and Manufacturing Method of High-Strength and High-Toughness magnesium Based Alloy Material
US7922967B2 (en) 2004-06-15 2011-04-12 Toudai TLD, Ltd. High-strength and high-toughness magnesium based alloy, driving system part using the same and manufacturing method of high-strength and high-toughness magnesium based alloy material
US20100226812A1 (en) * 2004-06-15 2010-09-09 Katsuyoshi Kondoh High-strength and high-toughness magnesium based alloy, driving system part using the same and manufacturing method of high-strength and high-toughness magnesium based alloy material
US20130144290A1 (en) * 2010-07-06 2013-06-06 Ait Austrian Institute Of Technology Gmbh Magnesium alloy
US9775647B2 (en) * 2010-07-06 2017-10-03 Ait Austrian Institute Of Technology Gmbh Magnesium alloy
US20220154314A1 (en) * 2019-03-12 2022-05-19 Honda Motor Co., Ltd. Flame-resistant magnesium alloy and method for producing the same
US11959155B2 (en) 2019-03-29 2024-04-16 Kurimoto, Ltd. Heat-resistant magnesium alloy for casting

Also Published As

Publication number Publication date
JP3415987B2 (en) 2003-06-09
EP0799901A1 (en) 1997-10-08
KR970070224A (en) 1997-11-07
EP0799901B1 (en) 2001-09-19
CN1065003C (en) 2001-04-25
DE69706737D1 (en) 2001-10-25
CN1174243A (en) 1998-02-25
JPH09272945A (en) 1997-10-21
DE69706737T2 (en) 2002-07-04

Similar Documents

Publication Publication Date Title
US20020020475A1 (en) Heat-resistant magnesium alloy member
CN105525158B (en) A kind of semisolid pressure casting aluminum alloy materials and the method using the material die cast
US6719857B2 (en) Die casting magnesium alloy
CN109881063B (en) High-strength, high-toughness and high-modulus die-casting magnesium alloy and preparation method thereof
US5855697A (en) Magnesium alloy having superior elevated-temperature properties and die castability
JP3522963B2 (en) Method for producing heat-resistant magnesium alloy member, magnesium alloy used therefor, and magnesium alloy molded member
US9180515B2 (en) Magnesium alloy and magnesium-alloy cast product
KR20160011136A (en) Magnesium alloy having improved corrosion resistance and method for manufacturing magnesium alloy member using the same
US7041179B2 (en) High strength creep resistant magnesium alloys
JP4852082B2 (en) Magnesium alloy
JP2002327231A (en) Cast article of heat-resistant magnesium alloy, and manufacturing method therefor
JP4145242B2 (en) Aluminum alloy for casting, casting made of aluminum alloy and method for producing casting made of aluminum alloy
US5023051A (en) Hypoeutectic aluminum silicon magnesium nickel and phosphorus alloy
JP3737371B2 (en) Magnesium alloy for die casting
JP2004238676A (en) Magnesium alloy
CN109852856B (en) High-strength, high-toughness and high-modulus metal mold gravity casting magnesium alloy and preparation method thereof
US5551996A (en) Si-containing magnesium alloy for casting with melt thereof
JP4285188B2 (en) Heat-resistant magnesium alloy for casting, casting made of magnesium alloy and method for producing the same
EP0241193B1 (en) Process for producing extruded aluminum alloys
JP2001107171A (en) Magnesium alloy and magnesium alloy heat resistant member excellent in heat resistance and castability
JPS6328979B2 (en)
JPH07224342A (en) Magnesium alloy for pressure casting
KR20030016879A (en) Die casting magnesium alloy

Legal Events

Date Code Title Description
STCB Information on status: application discontinuation

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