EP3561097A1 - Alliage de magnésium de résistance élevée présentant une excellente ininflammabilité, et son procédé de production - Google Patents

Alliage de magnésium de résistance élevée présentant une excellente ininflammabilité, et son procédé de production Download PDF

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Publication number
EP3561097A1
EP3561097A1 EP17883943.7A EP17883943A EP3561097A1 EP 3561097 A1 EP3561097 A1 EP 3561097A1 EP 17883943 A EP17883943 A EP 17883943A EP 3561097 A1 EP3561097 A1 EP 3561097A1
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EP
European Patent Office
Prior art keywords
magnesium alloy
flame retardancy
high strength
intermetallic compound
excellent flame
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.)
Withdrawn
Application number
EP17883943.7A
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German (de)
English (en)
Other versions
EP3561097A4 (fr
Inventor
Woo-Jin Park
Hyung-Sub EOM
Dae-Hwan Choi
Sang-Jin Kim
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.)
Research Institute of Industrial Science and Technology RIST
Posco Holdings Inc
Original Assignee
Posco Co Ltd
Research Institute of Industrial Science and Technology RIST
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Publication date
Application filed by Posco Co Ltd, Research Institute of Industrial Science and Technology RIST filed Critical Posco Co Ltd
Publication of EP3561097A1 publication Critical patent/EP3561097A1/fr
Publication of EP3561097A4 publication Critical patent/EP3561097A4/fr
Withdrawn legal-status Critical Current

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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
    • C22C23/02—Alloys based on magnesium with aluminium as the next major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/02—Making non-ferrous alloys by melting
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/02—Making non-ferrous alloys by melting
    • C22C1/03—Making non-ferrous alloys by melting using master alloys
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/002—Changing 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
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/06—Changing 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 disclosure relates to a high strength magnesium alloy having excellent flame retardancy, and a method of producing the same.
  • Magnesium is one of the lightest metals in practical use, and thus, may be applied to portable electronic products such as smart phones, tablet PCs, laptop computers, and structural materials of transportation means for vehicles, trains, aircraft and the like.
  • Magnesium alloys, having various elements added to magnesium, are attracting attention as eco-friendly lightweight metal materials.
  • Magnesium alloys have excellent castability. Therefore, casting products of magnesium alloy, which are mainly produced by die casting methods such as high pressure casting, low pressure casting or gravity casting, have been mainly applied to practical products. In recent years, development and market expansion of products for use in telegraph materials using magnesium alloys, which may be manufactured through processing such as rolling, extrusion or the like, have been promoted.
  • magnesium alloys used in magnesium alloys for casting or magnesium alloys for wrought product are similar. Most commonly used types of magnesium alloys are AZ-based alloys with Al and Zn added, and AM-based alloys with Al and Mn added. The two types of alloys commonly contain Al to improve the castability and tensile strength of magnesium.
  • the AZ and AM magnesium alloys which account for most of the commercial magnesium alloys, are suitable for producing various casting products due to improvement in the flowability of molten metal by Al addition, and are also suitable for billet casting and plate casting.
  • yield strength or tensile strength thereof is significantly lower than those of competitive aluminum alloys, and there is a problem in that a thickness of the product should be increased or the product shape should be modified.
  • the magnesium alloy has a high possibility of ignition due to high oxygen affinity, which limits the use conditions.
  • Patent Document 1 Korean Patent Laid-Open Publication No. 10-2015-0077494
  • An aspect of the present disclosure is to provide a high strength magnesium alloy having excellent flame retardancy and a method of producing the same.
  • a high strength magnesium alloy having excellent flame retardancy includes, by weight%, 2.0 to 13.0% of aluminum (Al), 0.1 to 0.5% of manganese (Mn), 0.0015 to 0.025% of boron (B), 0.1 to 1.0% of yttrium (Y), a remainder of magnesium (Mg), and unavoidable impurities, the high strength magnesium alloy including a Mg-Al intermetallic compound in a volume fraction of 6.5% or more.
  • the Mg-Al intermetallic compound has an average particle diameter of 20 to 500 nm.
  • a method of producing a high strength magnesium alloy having excellent flame retardancy includes:
  • an effect of providing a high strength magnesium alloy having excellent flame retardancy and a method of producing the same is provided.
  • the present inventors have found that a large amount of intermetallic compounds may be finely distributed by adding B and Y in combination and performing an aging treatment thereon, and thus excellent flame retardancy and high strength thereof may be secured, and the present disclosure has been obtained.
  • a high strength magnesium alloy having excellent flame retardancy includes, by weight%, 2.0 to 13.0% of Al, 0.1 to 0.5% of Mn, 0.0015 to 0.025% of B, 0.1 to 1.0% of Y, a remainder of Mg, and unavoidable impurities, and includes a Mg-Al intermetallic compound in a volume fraction of not less than 6.5%.
  • An average grain size of the Mg-Al intermetallic compound is 20 to 500 nm.
  • the alloy composition according to an embodiment will be described in detail.
  • the unit of each element content refers to weight% unless otherwise specified.
  • Al increases the tensile strength or yield strength, and improves the castability by improving the fluidity of alloy molten metal.
  • the Al content is less than 2.0%, the above-mentioned effect is insufficient. On the other hand, if the Al content exceeds 13.0%, the brittleness may be increased and the workability and ductility may be reduced. Therefore, the Al content may be 2.0 to 13.0%.
  • a lower limit of the Al content may be 2.5%, and in further detail, the lower limit thereof may be 6.5% to secure a tensile strength of 160 MPa or more.
  • an upper limit of the Al content may be 12.0%, and in more detail, the upper limit thereof may be 11.0%.
  • Mn is an element contributing to an increase in tensile strength by forming an intermetallic compound with Al to allow for fine grains.
  • Mn serves to lower a corrosion rate of magnesium by lowering Fe, which is a typical impurity element unnecessary for a magnesium alloy, through intermetallic compound formation.
  • the Mn content is less than 0.1%, the above-mentioned effect is insufficient. On the other hand, if the Mn content exceeds 0.5%, brittleness due to excessive formation of an acicular intermetallic compound may be caused. Therefore, the Mn content may be 0.1 to 0.5%.
  • a lower limit of the Mn content may be 0.11%, and in further detail, an upper limit thereof may be 0.45%.
  • B (boron) has a significantly high melting point, and solubility thereof in a magnesium solid phase or liquid phase is close to zero.
  • B is known as an element not commonly used in general magnesium alloys.
  • B is added to ensure flame retardancy and high strength.
  • B contributes to forming a large amount of Mg-Al intermetallic compound by adding B and Y in combination to a magnesium alloy and performing an aging treatment thereon, thereby improving tensile strength.
  • flame retardancy and strength may be further improved as compared with the case in which B is added alone.
  • B since B may contribute to prevention of oxidation of molten metal to reduce the amount of expensive SF 6 gas used for preventing oxidation of molten metal and SO 2 gas which may cause environmental pollution, B may contribute to reduction in production costs and environmental protection.
  • the B content is less than 0.0015%, the above-mentioned effect is insufficient.
  • the B content exceeds 0.025%, there is a problem in which an Al-B compound is formed on grain boundaries, reducing ductility. Therefore, the B content may be 0.0015 to 0.025%.
  • a lower limit of the B content may be 0.002%, and in more detail, an upper limit thereof may be 0.02%.
  • Y bonds with Al to form a precipitate, to contribute to the improvement of strength, and is an element that has a high oxygen affinity to firmly protect a surface protective film of molten metal to suppress oxidation of the molten metal.
  • Y is an element to improve flame retardancy even after solidification.
  • Y is added together with B in combination to be subjected to an aging treatment, thereby contributing to formation of a large amount of Mg-Al intermetallic compound to improve tensile strength. Furthermore, in this case, flame retardancy may be further improved as compared with the case in which Y is added alone.
  • the Y content is less than 0.1%, the above-mentioned effect is insufficient. On the other hand, if the Y content exceeds 1.0%, ductility may be reduced due to formation of a coarse Al-Y compound. Therefore, the Y content may be 0.1 to 1.0%.
  • a lower limit of the Y content may be 0.11%, and in more detail, an upper limit thereof may be 0.95%.
  • the remainder component is magnesium (Mg).
  • impurities which are not intended may be mixed from a raw material or a surrounding environment, which cannot be excluded. These impurities are known to any person skilled in the art, and thus, are not specifically mentioned in this specification.
  • the impurities may be Fe, Cu, Ni, Ca, Na, Ba, F, S, N or the like.
  • Zn is a solid solution strengthening element and is an element which promotes formation of Mg 17 Al 12 phase or improves tensile strength by forming a separate intermetallic compound containing Zn such as in Mg 2 Zn or the like.
  • the Zn content is less than 0.3%, the above-mentioned effect is insufficient.
  • the Zn content exceeds 3.0%, a large amount of a separate intermetallic compound including Zn, such as Mg 2 Zn or the like, is formed to increase brittleness, which may lead to a decrease in ductility and toughness.
  • the Zn content may be 0.3 to 3.0%.
  • the Zn content may be within a range of from 0.5 to 1.5 wt%, considering the improvement of the strength and the reduction in brittleness.
  • a high-strength magnesium alloy having excellent flame retardancy according to an embodiment in the present disclosure not only satisfies the alloy composition described above, but also contains a Mg-Al intermetallic compound in a volume fraction of 6.5% or more.
  • An average grain size of the Mg-Al intermetallic compound is 20 to 500 nm.
  • an Mg-Al intermetallic compound may be formed, and a typical Mg-Al intermetallic compound is Mg 17 Al 12 phase.
  • the Mg-Al intermetallic compound serves to secure high strength.
  • a maximum addition amount of Al or other alloying elements to be added to a magnesium alloy is smaller than a maximum high capacity of each alloying element to Mg, most Al is solidified in the Mg matrix, rather than inducing intermetallic compound formation in the grain, and thus, formation of an Mg-Al intermetallic compound is not a general phenomenon. Thus, it is difficult to form a large amount of an Mg-Al intermetallic compound.
  • a large amount of Mg-Al intermetallic compound may be secured by adding B and Y in combination and performing an aging treatment thereon.
  • the volume fraction of the Mg-Al intermetallic compound is less than 6.5%, it is difficult to ensure high strength. Accordingly, the volume fraction of the Mg-Al intermetallic compound may be 6.5% or more, in detail, 7.0% or more, in further detail, 7.5% or more.
  • An upper limit of the volume fraction of the Mg-Al intermetallic compound is not particularly limited, but if the content thereof exceeds 30%, the grain size of the Mg-Al intermetallic compound may be coarsened, and brittleness may be increased. Thus, the volume fraction of the Mg-Al intermetallic compound may be 30% or less, and in detail, may be 25% or less.
  • the average grain size of the Mg-Al intermetallic compound is less than 20 nm, the fraction of the Mg-Al intermetallic compound is low and it is difficult to secure high strength. If the average grain size thereof is more than 500 nm, brittleness increases.
  • one or more of an Al-Mn intermetallic compound and an Al-Y intermetallic compound is further included, and the total amount thereof may be 5% or less in a volume fraction. If the total amount thereof exceeds 5%, the Mn and Y contents are excessive and thus, brittleness may increase.
  • the magnesium alloy according to an embodiment in the present disclosure may have an ignition temperature of 700°C or higher.
  • the magnesium alloy according to an embodiment in the present disclosure may have a hardness of 70 Hv or more.
  • the magnesia alloy according to an embodiment in the present disclosure may have a tensile strength of 130 MPa or more and an elongation of 3% or more. Further, a tensile strength of 160 MPa or more may be secured by controlling the Al content and the like.
  • a method of producing a high strength magnesium alloy having excellent flame retardancy including: preparing a molten metal satisfying the above-described alloy composition; casting the molten metal to obtain a magnesium alloy casting material; subjecting the magnesium alloy casting material to a solution treatment at a temperature ranging from 370 to 490°C for 2 to 20 hours to obtain a magnesium alloy; cooling the magnesium alloy to 100°C or lower; and aging the cooled magnesium alloy at a temperature of 150 to 250°C for 2 to 48 hours.
  • a molten metal satisfying the above alloy composition is prepared.
  • the molten metal is prepared through general molten metal preparation for magnesium alloy, without particular limitation.
  • the above-described alloying elements are prepared in accordance with the proposed composition range, and then charged into a crucible for melting, to then be subjected to a melting operation. Since the melting point of the magnesium alloy is relatively low, any method using a gas furnace, an electric furnace, an induction melting furnace, or the like may be used.
  • each alloy element may be prepared in a pure form, but the alloying elements may also be charged into the crucible in the form of a master alloy in which Mn, B and Y are mixed with Mg or Al.
  • B, Y and Mn have high melting points and may thus be charged into the crucible in the form of master alloy mixed with Mg or Al, which is advantageous in terms of dissolving.
  • the material when the prepared dissolving material is charged into the crucible, the material may be charged into the crucible in order from the element having a low melting point, which may be advantageous in terms of dissolving work.
  • the molten metal is cast to obtain a magnesium alloy casting material.
  • the casting is not particularly limited as in the case of the molten metal preparation.
  • a method using a movable mold and a method using a fixed mold may be used.
  • Representative examples of the method using the movable mold include twin roll casting and belt casting using a movable mold such as a twin roll or a twin belt.
  • representative examples of the method using the fixed mold include semi-continuous casting or continuous casting such as billet casting, and may also include mold casting such as high-pressure casting, low-pressure casting and gravity casting.
  • the mold should be cooled, with cooling water.
  • cooling water the mold surface should be maintained at room temperature or more before casting so that the condensed water on the surface of the mold may be removed, and then should be maintained at room temperature or lower after the condensed water is removed.
  • the magnesium alloy casting material is subjected to a solution treatment at a temperature ranging from 370 to 490°C for 2 to 20 hours to obtain a magnesium alloy. Since a Mg-Al intermetallic compound is formed in the magnesium alloy casting material, but is formed in the form of coarse Mg-Al or mixed with a Mg matrix (Lamellar Mg-Al), the solution treatment is performed to enable such an adverse Mg-Al intermetallic compound to a solid solution treatment.
  • the solution treatment temperature is less than 370°C or the holding time is less than 2 hours, the entire Mg-Al intermetallic compound is difficult to be solidified. If the solution treatment temperature exceeds 490°C or the retention time is more than 20 hours, production costs may be increased and productivity may be lowered, and an ignition phenomenon by oxidation may occur before B and Y are added. Therefore, in more detail, the solution treatment may be carried out within a temperature range of 400 to 460 °C for 2 to 20 hours.
  • the magnesium alloy is cooled to 100°C or lower, to significantly reduce a natural aging phenomenon that may appear before aging treatment.
  • the cooling rate may be 1 to 100°C/second, and the natural aging phenomenon that may occur during cooling is significantly reduced and the solidified Al element may be prevented from being precipitated at random.
  • rapid cooling may be preferably performed by forced blowing, water cooling, oil cooling, or the like.
  • the cooled magnesium alloy is aged at 150 to 250°C for 2 to 48 hours.
  • most of the Al element added as the alloying element does not form a separate intermetallic compound in a state of solid solution solidified in the Mg matrix, so that the strength of the material may not be efficiently increased. Therefore, in the case of an embodiment of the present disclosure, a large amount of Mg-Al intermetallic compound is precipitated through aging to increase the strength and to secure excellent flame retardancy.
  • a large amount of Mg-Al intermetallic compound may be precipitated through the aging treatment described above.
  • an Mg-Al intermetallic compound having a particle form, an average particle diameter, a volume fraction, and the like favorable for the improvement of strength and flame retardancy may be formed.
  • the aging treatment temperature is less than 150°C or the holding time thereof is less than 2 hours, it is difficult to sufficiently secure the Mg-Al intermetallic compound.
  • the aging treatment temperature is more than 250°C or the retention time is more than 48 hours, the Mg-Al intermetallic compound may be solidified, resulting in increased production costs and decreased productivity. Therefore, the aging treatment may be performed at 150 to 250°C for 2 to 48 hours.
  • the temperature and the holding time may be increased within the above temperature and holding time depending on the amount of Al added.
  • a magnesium alloy casting material having a thickness of 10 mm was cast by casting a molten metal having the composition shown in Table 1 below.
  • the magnesium alloy casting material was solution-treated at 420°C for 4 hours, cooled to 20°C, and aged at 200°C for 12 hours to produce a magnesium alloy.
  • Mg-Al intermetallic compound of the magnesium alloy Mechanical properties of a Mg-Al intermetallic compound of the magnesium alloy were measured and are shown in Table 1 below.
  • the size of the Mg-Al intermetallic compound was measured by an average size obtained by measuring a circle-equivalent diameter.
  • Mg-Al means a Mg-Al intermetallic compound.
  • inventive materials satisfying the alloy composition and the producing conditions proposed according to an embodiment in the present disclosure include a Mg-Al intermetallic compound in a volume fraction of 6.5% or more and the average particle diameter of the Mg-Al intermetallic compound satisfies 20 to 500 nm. Also, it can be confirmed that the flame retardancy is excellent as an ignition temperature is 700°C or more, and the mechanical properties are also superior to the comparative materials.
  • the comparative materials satisfied the producing conditions proposed according to an embodiment in the present disclosure, but did not satisfy the alloy composition, so that Mg-Al intermetallic compounds were not sufficiently secured.
  • the flame retardancy is poor and the mechanical properties are also inferior to those of the inventive materials.
  • FIGS. 1A and 1B are images of the microstructures of the magnesium alloy casting materials of comparative material 1 (a) and inventive material 7(b).
  • the casting structure of the comparative member 1 is composed of a Mg matrix and coarse Mg-Al intermetallic compound, a Mg matrix + Mg-Al intermetallic compound mixed structure (Lamellar Mg-Al), and an Al-Mn intermetallic compound.
  • an Al-Y intermetallic compound (Al-Y) was observed in addition to the above-mentioned structure, and no boron-containing intermetallic compound was observed separately.
  • the hardness values of the comparative material 1(a) and the inventive material 7(b) were measured at 200°C according to the aging time. As a result, it can be confirmed that the hardness of the inventive material is significantly high. Also, the hardness value of the comparative material 1 barely changes according to the aging time, but it can be confirmed that the hardness value of the inventive material greatly increases when the aging time exceeds 1 hour.
  • a maximum hardness value corresponding to peak aging is shown, and the hardness value at this time is a value of 97 to 107 Hv which is a value increased 60% or more, as compared with the average hardness value of the casting material aged for 1 hour or less.
  • a maximum hardness value of the inventive material 7 is about two times the maximum hardness value of the comparative material.
  • FIGS. 5A to 5C are images showing the microstructures of the magnesium alloys after the aging treatment of the comparative material 1(a), the inventive material 7 (b) and the comparative material 5(c). It can be confirmed that a large amount of Mg-Al intermetallic compound having a size of several tens of nanometers is precipitated in the inventive material 7, which shows that the hardness value of the inventive material is significantly increased.
  • FIG. 6 illustrates changes in the hardness value (rhombus) and the size (square) of the Mg-Al intermetallic compound in the crystal grains with respect to the aging time of the inventive material 7, and
  • FIG. 7 illustrates a volume fraction of Mg-Al intermetallic compounds with aging time.
  • the inventive material 7 is aged for 3 hours or more, it can be seen that the Mg-Al intermetallic compounds are grown to 20 nm or more and 10 vol% or more, respectively, in the average size and the volume fraction.

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  • 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)
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EP17883943.7A 2016-12-21 2017-12-21 Alliage de magnésium de résistance élevée présentant une excellente ininflammabilité, et son procédé de production Withdrawn EP3561097A4 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
KR1020160176119A KR101858856B1 (ko) 2016-12-21 2016-12-21 난연성이 우수한 고강도 마그네슘 합금 및 그 제조방법
PCT/KR2017/015291 WO2018117713A1 (fr) 2016-12-21 2017-12-21 Alliage de magnésium de résistance élevée présentant une excellente ininflammabilité, et son procédé de production

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EP3561097A1 true EP3561097A1 (fr) 2019-10-30
EP3561097A4 EP3561097A4 (fr) 2019-10-30

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US (1) US20200087757A1 (fr)
EP (1) EP3561097A4 (fr)
JP (1) JP2020509196A (fr)
KR (1) KR101858856B1 (fr)
CN (1) CN110114485A (fr)
WO (1) WO2018117713A1 (fr)

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KR102271295B1 (ko) * 2018-07-18 2021-06-29 주식회사 포스코 마그네슘 합금 판재 및 이의 제조방법

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JP3107267B2 (ja) * 1992-12-04 2000-11-06 トヨタ自動車株式会社 耐熱マグネシウム合金
JP3229954B2 (ja) * 1996-02-27 2001-11-19 本田技研工業株式会社 耐熱性マグネシウム合金
CN101982259B (zh) * 2004-06-30 2013-04-17 住友电气工业株式会社 镁合金材料的制造方法
KR100993840B1 (ko) * 2008-01-30 2010-11-11 포항공과대학교 산학협력단 고강도 마그네슘 합금 판재 및 그 제조방법
US9222161B2 (en) * 2010-11-16 2015-12-29 Sumitomo Electric Industries, Ltd. Magnesium alloy sheet and method for producing same
JP5769003B2 (ja) * 2010-12-24 2015-08-26 住友電気工業株式会社 マグネシウム合金材
KR101258470B1 (ko) * 2011-07-26 2013-04-26 한국기계연구원 고강도 고연성 난연성 마그네슘 합금
CN102618757B (zh) * 2012-04-13 2014-10-29 江汉大学 一种耐热镁合金
WO2015060459A1 (fr) * 2013-10-23 2015-04-30 国立大学法人 熊本大学 Alliage de magnésium et son procédé de fabrication
KR20150077494A (ko) 2013-12-27 2015-07-08 재단법인 포항산업과학연구원 마그네슘 합금, 압출재, 압연재 및 주조재
CN103695747B (zh) * 2014-01-16 2015-11-04 陆明军 一种高强耐热镁合金及其制备方法
CN104233027B (zh) * 2014-06-06 2017-03-22 河南科技大学 一种阻燃高强镁合金及其制备方法
JP2014237896A (ja) 2014-08-07 2014-12-18 住友電気工業株式会社 マグネシウム合金板
CN105039816B (zh) * 2015-07-20 2017-05-31 河南科技大学 一种低成本高强耐热镁合金及其制备方法
CN105543603B (zh) * 2016-02-05 2017-04-19 重庆大学 一种低稀土高强度变形镁合金及其制备方法
CN106041015B (zh) * 2016-06-29 2017-12-12 宁波胜景传动科技有限公司 一种减速器齿轮箱端盖及其制备方法

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WO2018117713A1 (fr) 2018-06-28
JP2020509196A (ja) 2020-03-26
KR101858856B1 (ko) 2018-05-17
CN110114485A (zh) 2019-08-09
EP3561097A4 (fr) 2019-10-30
US20200087757A1 (en) 2020-03-19

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