EP0661384B1 - Hitzebeständige Magnesiumlegierung - Google Patents

Hitzebeständige Magnesiumlegierung Download PDF

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Publication number
EP0661384B1
EP0661384B1 EP19940108544 EP94108544A EP0661384B1 EP 0661384 B1 EP0661384 B1 EP 0661384B1 EP 19940108544 EP19940108544 EP 19940108544 EP 94108544 A EP94108544 A EP 94108544A EP 0661384 B1 EP0661384 B1 EP 0661384B1
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weight
magnesium alloy
heat resistant
resistant magnesium
amount
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EP0661384A1 (de
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Hideki Iba
Tadashi Takeuchi
Yasuyuki Suzuki
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Toyota Motor Corp
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Toyota Motor Corp
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    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C23/00—Alloys based on magnesium

Definitions

  • the present invention relates to a heat resistant Mg-Al-Zn-rare earth element magnesium alloy which is superior in heat resistance and strength characteristics.
  • Mg Magnesium (Mg) has a specific gravity of 1.74, it is the lightest metal among the industrial metallic materials, and it is as good as aluminum alloy in terms of the mechanical properties. Therefore, Mg has been observed as an industrial metallic material which can be used in aircraft, automobiles, or the like, and which can satisfy the light-weight requirements, the fuel-consumption reduction requirements, or the like.
  • an Mg-Al alloy for instance AM60B, AM50A, AM20A alloys, etc., as per ASTM, includes 2 to 12% by weight of aluminum (Al), and a trace amount of manganese (Mn) is added thereto.
  • Al aluminum
  • Mn manganese
  • phase diagram of the Mg-Al alloy there is a eutectic system which contains alpha-Mg solid solution and beta-Mg 17 Al 12 compound in the Mg-rich side.
  • Mg-Al-Zn alloy for instance an AZ91C alloy or the like as per ASTM, which includes 5 to 10% by weight of Al, and 1 to 3% by weight of zinc (Zn).
  • Mg-Al-Zn alloy there is a broad alpha solid solution area in the Mg-rich side where Mg-Al-Zn compounds crystallize.
  • the as-cast Mg-Al-Zn alloy is tough and excellent in corrosion resistance, but it is further improved in terms of the mechanical properties by age-hardening.
  • the Mg-Al-Zn compounds are precipitated like pearlite in the boundaries by quenching and tempering.
  • an as-cast Mg-Zn alloy In an as-cast Mg-Zn alloy, a maximum strength and elongation can be obtained when Zn is added to Mg in an amount of 2% by weight. In order to improve the castability and obtain failure-free castings, Zn is added more to Mg. However, an Mg-6% Zn alloy exhibits a tensile strength as low as 17 kgf/mm 2 when it is as-cast. Although its tensile strength can be improved by the T6 treatment (i.e., an artificial hardening after a solution treatment), it is still inferior to that of the Mg-Al alloy. As the Mg-Zn alloy, a ZCM630A (e.g., Mg-6% Zn-3% Cu-0.2% Mn) has been available.
  • a ZCM630A e.g., Mg-6% Zn-3% Cu-0.2% Mn
  • a magnesium alloy has been investigated which is superior in heat resistance and accordingly which is suitable for high temperature applications.
  • a magnesium alloy with rare earth element hereinafter abbreviated to "R.E." added has been developed.
  • This magnesium alloy has mechanical properties somewhat inferior to those of aluminum alloy at an ordinary temperature, but it exhibits mechanical properties as good as those of the aluminum alloy at a high temperature of from 250 to 300 °C.
  • the following magnesium alloys which include R.E.
  • an EK30A alloy which is free from Zn (e.g., Mg-2.5 to 4% R.E.-0.2% Zr), and a ZE41A alloy which includes Zn (e.g., Mg-1% R.E.-2% Zn-0.6% Zr).
  • the Mg-Al or Mg-Al-Zn alloy is less expensive in the costs, it can be die-cast, and it is being employed gradually in members which are used at a low temperature of 60 °C at the highest.
  • the Mg-Al alloy has a low melting point and since it is unstable at elevated temperatures, its high temperature strength deteriorates and its creep resistance degrades considerably at high temperatures.
  • AZ91D alloy one of the Mg-Al-Zn alloys similar to the AZ91C alloy, is good in terms of castability, corrosion resistance and tensile strength at room temperature and up to 150 °C, but it is inferior in terms of creep resistance at temperatures of 100 °C or more.
  • the creep resistance is low at elevated temperatures, there arises a problem in that component parts made of such alloys exhibit deteriorating tightening forces (i.e., axial forces) at the portions, for instance at the portions tightened with a bolt, when the temperature is raised during their service.
  • tightening forces i.e., axial forces
  • the aluminum contained in the magnesium alloys forms Mg 17 Al 12 crystals during the solidification.
  • areas i.e., the dendritic cells
  • areas which contain the solute atoms e.g., aluminum atoms
  • the grain boundary diffusion is active in the environment where the temperature is elevated, and accordingly it is believed that the unstable aluminum atoms facilitate the creep deformations.
  • EP-A-0 524 644 discloses a heat resistant Mg-Al-Zn-R.E.M. alloy with good creep resistance, corrosion resistance and castability.
  • the present invention has been developed in order to solve the aforementioned problems of the conventional Mg-Al magnesium alloy for die casting, e.g., their inferior creep resistance. It is therefore an object of the present invention to provide a heat resistante magnesium alloy whose creep properties are improved at 150 °C, which securely exhibits a predetermined tensile strength at room temperature and up to 100 °C, and whose castability and corrosion resistance are enhanced.
  • the present inventors investigated the aluminum concentrations in magnesium alloys at which no dendritic cells are formed. As a result, they found that the dendritic cells can be inhibited from forming by restricting the aluminum concentration in a range of from 1.0 to 3.0% by weight. Further, they found that zinc can be added effectively to magnesium alloys in an amount of from 0.25 to 3.0% by weight to securely give the resulting products a predetermined tensile strength and elongation at room temperature and up to 100 °C.
  • a rare earth element for example cerium (Ce) and neodymium (Nd), capable of forming crystals of high melting points in grain boundaries of magnesium alloys can be added to magnesium alloys in an amount of from 0.5 to 4.0% by weight to strengthen the grain boundaries of the resulting magnesium alloys.
  • manganese (Mn) can be added to magnesium alloys in an amount of from 0.1 to 1.0% by weight to enhance the proof stress, and that it can be added in a limited amount of from 0.2 to 0.3% by weight thereto to enhance the corrosion resistance as well.
  • the present inventors completed a heat resistant magnesium alloy according to the present invention, which is defined in claim 1.
  • the present heat resistant magnesium alloy is enhanced, if necessary, in terms of the proof stress by including Mn in an amount of from 0.1 to 1.0% by weight. Furthermore, it is improved, if required, in terms of the corrosion resistance as well by limitedly including Mn in an amount of from 0.2 to 0.3% by weight.
  • the resulting products made of the present heat resistant magnesium alloy are improved in terms of the creep resistance at elevated temperatures of 100 °C or more. Further, since Zn is added in the amount of from 0.25 to 3.0% by weight, the resulting products made thereof are enhanced in terms of the tensile strength and elongation at room temperature and up to 100 °C, and they are simultaneously upgraded in terms of the castability.
  • a rare earth element for example Ce and Nd
  • Ce and Nd is added in the amount of from 0.5 to 4.0% by weight, there are formed the high melting point crystals in the grain boundaries of the present heat resistance magnesium alloy so as to strengthen the grain boundaries, and thereby the resulting products made thereof are improved in terms of the creep properties at 150 °C.
  • Mn when Mn is added to the present heat resistant magnesium alloy in the amount of 0.1 to 1.0% by weight, the resulting products made thereof exhibit an improved proof stress and a less degrading initial bolt tightening axial force. Mn can dissolve into grains even in a small addition amount, thereby effecting the solution strengthening or hardening. As a result, Mn improves the proof stress of the resulting products made thereof at room temperature and at elevated temperatures. Since the deterioration of the initial axial force depends on the proof stress of materials (i.e., members to be tightened), the addition of Mn is believed to result in the improvement. Moreover, when Mn is added thereto in the limited amount of 0.2 to 0.3% by weight, the resulting products made thereof exhibit enhanced corrosion resistance as well.
  • FIG. 1 illustrates the results of an evaluation on the variation in the axial force retention rate of the test specimen made of a magnesium alloy which comprised Zn in an amount of 2.0% by weight, R.E. in an amount of 2.9% by weight, Mn in an amount of 0.2% by weight and balance of Mg and inevitable impurities, and to which Al was added in amounts of from 0 to 4.0% by weight.
  • a target value of the axial force retention rate was designed to be 50% after degrading the test specimen at 150 °C for 300 hours.
  • the Al content of 3.0% by weight satisfying the target value was taken as the upper limit.
  • Figure 2 illustrates the results of an evaluation on the hot tearings occurrence rate of the test specimen made of the same magnesium alloy.
  • the Al content was less than 1.0% by weight, the hot tearings were more likely to occur.
  • the Al content of 1.0% by weight was taken as the lower limit.
  • the present heat resistant magnesium alloy includes Al in an amount of from 1.5 to 2.5% by weight.
  • a tensile creep test was carried out in order to measure the creep deformation amounts of the test specimens.
  • the magnesium alloys were melted and processed into a cylindrical test specimen having an inside diameter of 7 mm, an outside diameter of 15 mm and a length of 25 mm by die casting with a hot chamber at a casting temperature of 690 °C, at mold temperatures of 80 to 120 °C and under a casting pressure of 300 kgf/cm 2 .
  • This cylindrical test specimen was tightened with a bolt and a nut at the ends under a surface pressure of 6.5 kgf/mm 2 at ordinary temperature, it was held in an oven whose temperature was raised to 150 °C for 300 hours, and thereafter an elongation of the bolt was measured in order to examine for an axial force retention rate of the test specimen.
  • the magnesium alloys were processed into a square-shaped box test specimen having corners of predetermined radii hereinafter described in detail.
  • the test specimen 10 for die cast hot tearings occurrence test was a cylindrical body which had a square shape in a cross section, it had a thickness of 3 to 4 mm, and each of whose side had a length of 200 mm.
  • a sprue 12 was disposed on a side 14, and a heat insulator 18 was disposed on a side 16 which was opposite to the side 14 with the sprue 12 disposed.
  • One end of the side 16 was made into a round corner 20 having a radius of 1.0 mm, and the other end of the side 16 was made into a round corner 22 having a radius of 0.5 mm.
  • This die cast hot tearings test specimen was intended for examining the hot tearings which were caused either in the round corner 20 or 22 by the stress resulting from the solidification shrinkage.
  • the solidification shrinkage resulted from the solidification time difference between the portion covered with the heat insulator 18 and the other portions. 0.25 to 3.0% by weight of Zn:
  • Figure 4 illustrates the results of an evaluation on the variation in the room temperature tensile strength of the test specimen made of a magnesium alloy which comprised Al in an amount of 2.0% by weight, R.E. in an amount of 2.9% by weight, Mn in an amount of 0.2% by weight and balance of Mg and inevitable impurities, and to which Zn was added in amounts of from 0 to 4.0% by weight.
  • Figure 5 illustrates the results of an evaluation on the variation in the elongation of the test specimen made of the same magnesium alloy at 100 °C.
  • the tensile strength test was carried out onto the test specimens which had a dumbbell-shaped configuration and dimensions in accordance with ASTM "80-91,” paragraph 12.2.1.
  • the test specimen was improved not only in the room temperature tensile strength but also in the 100 °C elongation by adding Zn in an amount of 0.25% by weight or more.
  • Zn is added preferably in a range of 10% by weight or more.
  • Figure 3 which illustrates the results of an evaluation on the variation in the axial force retention rate of the test specimen made of the same magnesium alloy, when Zn was added in a large amount, the axial force retention rate was deteriorated. Therefore, the Zn content of 3.0% by weight satisfying the aforementioned target axial force retention rate was taken as the upper limit.
  • the present heat resistant magnesium alloy includes Zn in an amount of from 0.5 to 1.5% by weight.
  • Figure 6 illustrates the results of an evaluation on the variation in the axial force retention rate of the test specimen made of a magnesium alloy which comprised Al in an amount of 2.0% by weight, Zn in an amount of 2.0% by weight, Mn in an amount of 0.2% by weight and balance of Mg and inevitable impurities, and to which R.E. was added in amounts of from 0 to 4.0% by weight.
  • the test specimen was sharply improved in the axial force retention rate by adding R.E. in an amount of 0.5% by weight or more.
  • Figure 7 illustrates the results of an evaluation on the variation in the room temperature tensile strength of the test specimen made of the same magnesium alloy, when R.E.
  • the present heat resistant magnesium alloy includes R.E. in an amount of from 2.5 to 3.5% by weight.
  • a misch metal containing cerium (Ce) as a major component can be employed preferably, but magnesium alloys in which neodymium (Nd) substituted for the misch metal equally produced the advantageous effects.
  • R.E. is a misch metal which includes cerium (Ce) at least. It is moreover preferred that the misch metal includes Ce in an amount of 45 to 55% by weight. 0.1 to 0.1% by weight of Mn:
  • Mn dissolves into grains, thereby effecting the solution strengthening or hardening.
  • the resulting products made of magnesium alloys containing Mn can be inhibited from deteriorating in the initial axial force.
  • the advantageous effect of inhibiting the initial axial force deterioration is saturated by adding Mn thereto in an amount of around 0.4% by weight.
  • Mn-Al-R.E. crystals are produced, thereby causing the hot tearings.
  • the upper limit of the Mn addition is set at 1.0% by weight.
  • Mn and Al simultaneously operate so as to remove Fe which adversely affects the corrosion resistance of the resulting products.
  • Mn is added thereto in an amount of more than 0.3% by weight, no improvement can be appreciated in the corrosion resistance. Therefore, when improved corrosion resistance is desired, it is preferable to set the upper limit of the Mn addition at 0.3% by weight.
  • the aluminum content "a,” the zinc content “b” and the R.E. content “c” are arranged so as to satisfy the relationship, "c” ⁇ “a” + 1.0, when “b” is in the range, 0.25 ⁇ “b” ⁇ 1.0, and the relationship “c” ⁇ "a” + “b” ⁇ (1/2)"c” + 4.0, when “b” is in the range, 1.0 ⁇ "b” ⁇ 3.0. They are designed so as to satisfy the relationships because the resulting products are degraded in the room temperature tensile strength when R.E.
  • Al content is added in an amount of more than an amount calculated from the Al content, i.e., the Al content with a factor of 1.0 added thereto (e.g., "a" + 1.0), and because the resulting products are deteriorated in the creep properties at elevated temperatures when Al and Zn are added in total more than an amount calculated from the R.E. content, i.e., the R.E. content multiplied by half and a factor of 4.0 added thereto (e.g., (1/2)"c" + 4.0).
  • the present heat resistance magnesium alloy is expressed by the general formulae, given in claim 1. Since the aluminum content is restricted in the range of from 1.0 to 3.0% by weight where no dendritic cells are formed, the resulting products made of the present heat resistant magnesium alloy can be improved in terms of the creep resistance at elevated temperatures of 100 °C or more. Since Zn is added in the amount of from 0.25 to 3.0% by weight, the resulting products made thereof can securely exhibit the tensile strength and elongation at room temperature and up to 100 °C and it can be simultaneously enhanced in terms of the castability.
  • a rare earth element for example Ce and Nd
  • Ce and Nd is added in the amount of from 0.5 to 4.0% by weight
  • the high melting point crystals in the grain boundaries of the present heat resistance magnesium alloy so as to strengthen the grain boundaries, and thereby the resulting products made thereof are upgraded in terms of the creep properties at 150 °C.
  • Mn is further added in the amount of from 0.1 to 1.0% by weight
  • the resulting products can be inhibited from deteriorating in terms of the initial axial force, and, in particular, in the case that Mn is further added in the limited amount of from 0.2 to 0.3% by weight, the resulting products can be further enhanced in terms of the corrosion resistance as well.
  • the four alloys i.e., the Alloys "A” through “D,” were melted and processed into the aforementioned cylindrical test specimens and the dumbbell-shaped test specimens designated in ASTM "80-91,” paragraph 12.2.1.
  • the cylindrical test specimens were examined for their axial force retention rate after they were left in the 150 °C oven for 300 hours, and the dumbbell-shaped test specimens were examined for their tensile strength at room temperature.
  • the obtained results are illustrated in Figures 8, 9, 10 and 11 on the Alloys "A,” “B,” “C” and “D,” respectively.
  • magnesium alloys are marked with "x" which produced the cylindrical test specimens exhibiting an axial force retention rate of 50% or less, magnesium alloys are marked with solid triangles ( ⁇ ) which produced the dumbbell-shaped test specimens exhibiting a room temperature tensile strength of 200 MPa or less, and magnesium alloys are marked with solid circles ( ⁇ ) which produced the cylindrical test specimens exhibiting an axial force retention rate of 50% or more and the dumbbell-shaped test specimens exhibiting a room temperature tensile strength of 200 MPa or more.
  • alloys which are marked with solid circles ( ⁇ ) and whose aluminum content "a,” zinc content “b” and R.E.
  • Magnesium alloys having the following chemical compositions as set forth in Table 1 below were melted and processed into the aforementioned cylindrical test specimens and the dumbbell-shaped test specimens designated in ASTM "80-91," paragraph 12.2.1 by die casting with a cold chamber.
  • I.D. No. 1 is the present heat resistant magnesium alloy.
  • I.D. No. 2 is a comparative magnesium alloy which included Al and Zn in amounts more than the present composition range.
  • I.D. No. 3 is a conventional magnesium alloy which is equivalent to the AZ91D alloy.
  • Figures 12 and 13 are traces of microphotographs showing the comparative magnesium alloy and the present heat resistant magnesium alloy, respectively.
  • the comparative magnesium alloy there existed the areas containing the solute atoms, which did not produce the crystals, in high concentrations adjacent to the grain boundaries, because the cooling rate was faster. When these areas are present, the solute atoms are facilitated to diffuse in the vicinity of the grain boundaries, and the high temperature creep properties are believed to be adversely affected.
  • the present heat resistant magnesium alloy there existed no such areas, because the Al and Zn concentrations were kept low. Accordingly, the present heat resistant magnesium alloy are superior in terms of the high temperature creep properties.
  • the dumbbell-shaped test specimens made of the comparative magnesium alloy exhibited a room temperature tensile strength of 220 MPa which was almost equivalent to that of the dumbbell-shaped test specimens made of the conventional AZ91D alloy.
  • the cylindrical test specimens made of the comparative magnesium alloy were inferior in the bolt loosening characteristic which was associated with the high temperature creep properties, and thereby they exhibited an axial force retention rate of 30%.
  • the dumbbell-shaped test specimens made of the present heat resistant magnesium alloy also exhibited a room temperature tensile strength of 220 MPa which was almost equivalent to that of the dumbbell-shaped test specimens made of the conventional AZ91D alloy. Moreover, the cylindrical test specimens made thereof exhibited an axial force retention rate of 70%. Thus, the present heat resistant magnesium alloy was improved in terms of the high temperature creep properties without loss of the tensile properties.
  • a magnesium alloy was melted which comprised 2% by weight of Al, 2% by weight of Zn, 3% by weight of R.E., and balance of Mg and inevitable impurities, and Mn was added to the resulting molten metal in an amount which varied in a range of 0 to 1.0% by weight.
  • the thus prepared magnesium alloys were processed into the aforementioned cylindrical test specimens by die casting with a cold chamber.
  • the resulting test specimens were subjected to the bolt loosening test, in which they were left in the 150 °C oven for 1 hour, in order to examine for their initial axial force retention rates.
  • the results obtained are illustrated in Figure 15 as a relationship between the Mn contents and the initial axial force retention rates.
  • the magnesium alloys prepared as above were melted and cast into the square-shaped box test specimens for the die cast hot tearings occurrence test illustrated in Figure 17.
  • the resulting test specimens were subjected to the die cast hot tearings occurrence test in order to examine for their hot tearings occurrence rates at the round corner 20 having a radius of 1.0 mm as set forth above.
  • the results obtained are illustrated in Figure 16 as a relationship between the Mn contents and the hot tearings occurrence rates.
  • Another magnesium alloy was melted which comprised 3% by weight of Al, 2% by weight of Zn, 3% by weight of R.E., and balance of Mg and inevitable impurities, and Mn was added to the resulting molten metal in an amount which varied in a range of 0 to 1.6% by weight.
  • the thus prepared another magnesium alloys were cast into the square-shaped box test specimens for the die cast hot tearings occurrence test, and they were similarly examined for their hot tearings occurrence rates at the round corner 20 having a radius of 1.0 mm. The results obtained are also illustrated in Figure 16 as another relationship between the Mn contents and the hot tearings occurrence rates.

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Claims (11)

  1. Hitzebeständige Magnesiumlegierung, die durch die allgemeine Formel Mg-("a" Gewichts-%) Al-("b" Gewichts-%) Zn-("c" Gewichts-%) Seltenerdmetall oder ein Mischmetall aus mehr als einem Seltenerdmetall ausgedrückt wird, in der
    "a" für einen Aluminiumgehalt in einem Bereich von 1,0 bis 3,0 Gewichts-% steht;
    "b" für einen Zinkgehalt in einem Bereich von 0,25 bis 3,0 Gewichts-% steht;
    "c" für einen Seltenerdmetall- oder einen Mischmetallgehalt in einem Bereich von 0,5 bis 4,0 Gewichts-% steht; wobei der Rest aus Magnesium und unvermeidlichen Verunreinigungen oder Magnesium, Mangan (Mn) in einer Menge von 0,1 bis 1,0 Gewichts-% und unvermeidlichen Verunreinigungen besteht, und wobei
    wenn "b" in einem Bereich von 0,25 ≤ "b" ≤ 1,0 liegt, "a" und "c" der Beziehung "c" ≤ "a" + 1,0 genügen; und
    wenn "b" in einem Bereich von 1,0 ≤ "b" ≤ 3,0 liegt, "a", "b" und "c" der Beziehung "c" ≤ "a" + "b" ≤ (1/2) "c" + 4,0 genügen.
  2. Hitzebeständige Magnesiumlegierung nach Anspruch 1, wobei die hitzebeständige Magnesiumlegierung das Mangan in einer Menge von 0,2 bis 0,3 Gewichts-% einschließt.
  3. Hitzebeständige Magnesiumlegierung nach Anspruch 1, wobei die hitzebeständige Magnesiumlegierung das Aluminium in einer Menge von 1,5 bis 2,5 Gewichts-% einschließt.
  4. Hitzebeständige Magnesiumlegierung nach Anspruch 1, wobei die hitzebeständige Magnesiumlegierung das Zink in einer Menge von 0,5 bis 1,5 Gewichts-% einschließt.
  5. Hitzebeständige Magnesiumlegierung nach Anspruch 1, wobei die hitzebeständige Magnesiumlegierung das Seltenerdmetall in einer Menge von 2,5 bis 3,5 Gewichts-% einschließt.
  6. Hitzebeständige Magnesiumlegierung nach Anspruch 1, wobei die hitzebeständige Magnesiumlegierung in ihrer Metallstruktur frei von dendritischen Zellen ist.
  7. Hitzebeständige Magnesiumlegierung nach Anspruch 1, wobei ein aus der hitzebeständigen Magnesiumlegierung gefertigter zylindrischer Probekörper ein Axialkraft-Retentions-verhältnis von 50% oder mehr zeigt, nachdem er 300 Stunden lang bei 150 °C in einem Ofen belassen wurde, und ein daraus hergestellter stabförmiger Probekörper bei Raumtemperatur eine Zugfestigkeit von 200 MPa oder mehr reigt.
  8. Formgegossene Struktur, gebildet aus der hitzebeständigen Magnesiumlegierung nach Anspruch 1.
  9. Hitzebeständige Magnesiumlegierung nach Anspruch 1, wobei das Seltenerdmetall ein Mischmetall ist.
  10. Hitzebeständige Magnesiumlegierung nach Anspruch 9, wobei das Mischmetall mindestens Cer (Ce) einschließt.
  11. Hitzebeständige Magnesiumlegierung nach Anspruch 10, wobei das Mischmetall das Cer in einer Menge von 45 bis 55 Gewichts-% einschließt.
EP19940108544 1993-12-03 1994-06-03 Hitzebeständige Magnesiumlegierung Expired - Lifetime EP0661384B1 (de)

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JP304031/93 1993-12-03
JP05304031A JP3107267B2 (ja) 1992-12-04 1993-12-03 耐熱マグネシウム合金

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EP0661384B1 true EP0661384B1 (de) 1997-04-02

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JP3592310B2 (ja) * 2001-06-05 2004-11-24 住友電工スチールワイヤー株式会社 マグネシウム基合金ワイヤおよびその製造方法
CN101824571B (zh) * 2010-03-09 2011-12-07 扬州宏福铝业有限公司 含铈镧混合稀土的Mg-Al-Zn-RE变形镁合金的生产方法、应用
CN104109788A (zh) * 2013-04-18 2014-10-22 嘉兴中科亚美合金技术有限责任公司 适用于型材的变形镁合金及制备方法
CN104109787A (zh) * 2013-04-18 2014-10-22 嘉兴中科亚美合金技术有限责任公司 适用于板材的含铈变形镁合金及制备方法
CN107164674B (zh) * 2017-05-27 2018-12-18 东北大学 一种镁铝锌钆铈合金及其制备方法和应用
CN112522561A (zh) * 2020-12-03 2021-03-19 广东省科学院材料与加工研究所 一种压铸镁合金及其制备方法
CN114855041A (zh) * 2022-05-06 2022-08-05 上海大学 一种含稀土的压铸镁合金及其成型工艺
CN114892055B (zh) * 2022-05-25 2023-09-05 鹤壁海镁科技有限公司 一种高强韧Mg-Al-Zn镁合金及其制备方法

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DE69214735T2 (de) * 1991-07-26 1997-03-20 Toyota Motor Co Ltd Hitzebeständiges Magnesiumlegierung

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CN1119679A (zh) 1996-04-03
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AU666268B2 (en) 1996-02-01
DE69402406D1 (de) 1997-05-07
DE69402406T2 (de) 1997-08-28
CA2124512C (en) 2001-02-20
EP0661384A1 (de) 1995-07-05
AU6319394A (en) 1995-06-08

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