EP0799901B1 - Heat-resistant magnesium alloy member - Google Patents

Heat-resistant magnesium alloy member Download PDF

Info

Publication number
EP0799901B1
EP0799901B1 EP97105641A EP97105641A EP0799901B1 EP 0799901 B1 EP0799901 B1 EP 0799901B1 EP 97105641 A EP97105641 A EP 97105641A EP 97105641 A EP97105641 A EP 97105641A EP 0799901 B1 EP0799901 B1 EP 0799901B1
Authority
EP
European Patent Office
Prior art keywords
molding
weight
alloy
semi
magnesium alloy
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.)
Expired - Lifetime
Application number
EP97105641A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP0799901A1 (en
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.)
Mazda Motor Corp
Original Assignee
Mazda Motor Corp
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 Mazda Motor Corp filed Critical Mazda Motor Corp
Publication of EP0799901A1 publication Critical patent/EP0799901A1/en
Application granted granted Critical
Publication of EP0799901B1 publication Critical patent/EP0799901B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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 method of preparing a heat-resistant magnesium alloy member having an excellent molding property and an excellent elongation property while keeping creep resistance property.
  • 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.
  • 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.
  • JP-A-8 041 576 discloses a high strength magnesium alloy excellent in tensile strength and creep resistance having a composition consisting of 1.0 - 4.0 wt.-% Al, 1.0-8.0 wt.-% rare earth element, 0.3 - 1.3 wt.-% Ca, 0.1 - 2.0 wt.-% Mn, the balance of magnesium and inevitable impurities.
  • JP-A-7 331 375 discloses a heat resistant magnesium alloy for casting having a composition consisting of 1-3.5 wt.-% Al, 0.25 - 3.5 wt.-% Zn, 0.5 - 4.0 wt.-% rare earth component, 0.1-1.0 wt.-% Mn, 0.1 - 1.0 wt.-% Ca, the balance of Mg and inevitable impurities.
  • JP-A-7 278 717 discloses a member of a magnesium alloy excellent in creep resistance in the pressurized part having a composition including 1.5 to 10.0 wt.-% aluminum, less than 2.5 wt.-% rare earth (RE) component(s), 0.2 to 5.5 wt.-% calcium and the balance of magnesium with impurities.
  • JP-A-7 118 785 discloses a magnesium alloy for casting and non porosity magnesium alloy castings therefrom containing 0.5 - 10 wt.-% calcium.
  • an object of the present invention is to provide a molding method for preparing 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, in place of conventional die-cast methods.
  • 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 method of molding a magnesium alloy molding member comprising 2 to 6% by weight of aluminum and 0.5 to 4% by weight of calcium and contains no more than 0.15 % by weight of Sr, and the balance of magnesium and unavoidable impurities which may 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 rare earth metals, wherein a Ca/Al ratio is 0.49 to 0.8, to have an excellent anti-creep property, molding property, and elongation.
  • 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.
  • 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 x 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 0.49 to 0.6, the molding member shows a more excellent creep resistance.
  • 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.
  • 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.
  • 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.

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)
EP97105641A 1996-04-04 1997-04-04 Heat-resistant magnesium alloy member Expired - Lifetime EP0799901B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP82832/96 1996-04-04
JP8283296 1996-04-04
JP08283296A JP3415987B2 (ja) 1996-04-04 1996-04-04 耐熱マグネシウム合金成形部材の成形方法

Publications (2)

Publication Number Publication Date
EP0799901A1 EP0799901A1 (en) 1997-10-08
EP0799901B1 true EP0799901B1 (en) 2001-09-19

Family

ID=13785388

Family Applications (1)

Application Number Title Priority Date Filing Date
EP97105641A Expired - Lifetime EP0799901B1 (en) 1996-04-04 1997-04-04 Heat-resistant magnesium alloy member

Country Status (6)

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

Families Citing this family (71)

* 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 (ja) * 1998-05-13 1999-11-26 Mazda Motor Corp マグネシウム合金鋳物部材
IL125681A (en) * 1998-08-06 2001-06-14 Dead Sea Magnesium Ltd Magnesium alloy for high temperature applications
JP2000104137A (ja) * 1998-09-30 2000-04-11 Mazda Motor Corp マグネシウム合金鍛造素材、及び鍛造部材並びに該鍛造部材の製造方法
JP3521773B2 (ja) * 1998-11-30 2004-04-19 セイコーエプソン株式会社 時計用部品の製造方法、時計部品及び時計
DE19915277A1 (de) * 1999-04-03 2000-10-05 Volkswagen Ag Magnesiumlegierungen hoher Duktilität, Verfahren zu deren Herstellung und deren Verwendung
US6264763B1 (en) * 1999-04-30 2001-07-24 General Motors Corporation Creep-resistant magnesium alloy die castings
WO2001015836A1 (fr) * 1999-08-30 2001-03-08 Hitachi, Ltd. Procede et dispositif de moulage par injection de metal et produit obtenu
JP2001073059A (ja) * 1999-09-06 2001-03-21 Mazda Motor Corp マグネシウム合金成形部材
JP3611759B2 (ja) * 1999-10-04 2005-01-19 株式会社日本製鋼所 耐熱性と鋳造性に優れたマグネシウム合金およびマグネシウム合金耐熱部材
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 (ja) * 2000-03-03 2001-09-14 Japan Steel Works Ltd:The 流動性に優れたマグネシウム合金およびマグネシウム合金材
JP3551121B2 (ja) * 2000-04-07 2004-08-04 マツダ株式会社 軽金属成形材の製造方法
JP2001316753A (ja) * 2000-05-10 2001-11-16 Japan Steel Works Ltd:The 耐食性および耐熱性に優れたマグネシウム合金およびマグネシウム合金部材
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 (ja) * 2001-03-14 2002-09-25 Ryobi Ltd 耐クリープMg合金
AU2005200721B2 (en) * 2001-04-09 2007-11-15 Sumitomo Electric Industries, Ltd. Magnesium Alloy Material and Method of Manufacturing the Alloy Material
JP4661857B2 (ja) * 2001-04-09 2011-03-30 住友電気工業株式会社 マグネシウム合金材およびその製造方法
WO2002083341A1 (fr) 2001-04-09 2002-10-24 Sumitomo Electric Industries, Ltd. Materiau en alliage de magnesium et son procede de fabrication
WO2002099147A1 (en) * 2001-06-06 2002-12-12 Noranda, Inc. Magnesium-based casting alloys having improved elevated temperature properties
JP3869255B2 (ja) 2001-06-14 2007-01-17 富士通株式会社 金属成形体製造方法およびこれにより製造される金属成形体
JP3723522B2 (ja) 2001-08-03 2005-12-07 富士通株式会社 金属成形体製造方法
JP2003129161A (ja) * 2001-08-13 2003-05-08 Honda Motor Co Ltd 耐熱マグネシウム合金
CN1317412C (zh) 2001-08-13 2007-05-23 本田技研工业株式会社 镁合金
JP2003129160A (ja) * 2001-08-13 2003-05-08 Honda Motor Co Ltd 耐熱マグネシウム合金
KR100421102B1 (ko) * 2001-08-22 2004-03-04 미츠비시 알루미늄 컴파니 리미티드 다이 캐스팅 마그네슘 합금
JP3592659B2 (ja) 2001-08-23 2004-11-24 株式会社日本製鋼所 耐食性に優れたマグネシウム合金およびマグネシウム合金部材
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 (ja) * 2002-03-12 2006-12-20 Tkj株式会社 マグネシウム合金の成形方法
DE10221720A1 (de) * 2002-05-16 2003-11-27 Bayerische Motoren Werke Ag Magnesiumlegierung
JP3476814B1 (ja) * 2002-06-21 2003-12-10 宇部興産機械株式会社 半溶融金属成形用金型
JP2004162090A (ja) * 2002-11-11 2004-06-10 Toyota Industries Corp 耐熱性マグネシウム合金
CN100366775C (zh) * 2003-01-07 2008-02-06 死海鎂有限公司 高强度抗蠕变镁基合金
JP4575645B2 (ja) * 2003-01-31 2010-11-04 株式会社豊田自動織機 鋳造用耐熱マグネシウム合金および耐熱マグネシウム合金鋳物
JP2004230445A (ja) * 2003-01-31 2004-08-19 Ahresty Corp マグネシウムダイカスト用金型
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 (ko) * 2003-04-21 2005-06-10 현대자동차주식회사 반용융 성형용 마그네슘합금 빌렛의 제조방법
JP4202298B2 (ja) * 2003-09-18 2008-12-24 トヨタ自動車株式会社 ダイカスト用耐熱マグネシウム合金および同合金のダイカスト製品
KR101127113B1 (ko) * 2004-01-09 2012-03-26 켄지 히가시 다이캐스트용 마그네슘 합금 및 이것을 사용한 마그네슘다이캐스트 제품
JP4289613B2 (ja) * 2004-02-27 2009-07-01 日精樹脂工業株式会社 低融点金属合金の成形方法
JP4009601B2 (ja) * 2004-02-27 2007-11-21 日精樹脂工業株式会社 低融点金属合金の成形方法
US20050194072A1 (en) * 2004-03-04 2005-09-08 Luo Aihua A. Magnesium wrought alloy having improved extrudability and formability
JP4051350B2 (ja) * 2004-03-05 2008-02-20 日精樹脂工業株式会社 低融点金属合金の成形方法
JP2006002184A (ja) * 2004-06-15 2006-01-05 Toudai Tlo Ltd 高強靭性マグネシウム基合金およびそれを用いた駆動系部品並びに高強靭性マグネシウム基合金素材の製造方法
EP1857203B1 (en) 2005-02-22 2013-05-15 Hitachi Metals Precision, Ltd. Impeller for supercharger and method of manufacturing the same
JP2007198544A (ja) * 2006-01-27 2007-08-09 Toyota Motor Corp マグネシウム合金の締結構造
JP4539572B2 (ja) * 2006-01-27 2010-09-08 株式会社豊田中央研究所 鋳造用マグネシウム合金および鋳物
EP2135965A4 (en) * 2007-04-03 2010-03-31 Toyota Jidoshokki Kk HEAT RESISTANT MAGNESIUM ALLOY
JP4051393B2 (ja) * 2007-06-13 2008-02-20 日精樹脂工業株式会社 低融点金属合金の成形方法
JP5136169B2 (ja) * 2008-04-04 2013-02-06 宇部興産機械株式会社 半溶融金属成形用金型
JP2009007676A (ja) * 2008-07-30 2009-01-15 Toyota Industries Corp 鋳造用耐熱マグネシウム合金および耐熱マグネシウム合金鋳物
JP5388277B2 (ja) 2009-02-20 2014-01-15 Ntn株式会社 保持器、転がり軸受、保持器の製造方法および射出成形用の型
CN101818293B (zh) * 2010-04-21 2012-05-30 广州有色金属研究院 一种耐热镁合金
AT510087B1 (de) * 2010-07-06 2012-05-15 Ait Austrian Institute Of Technology Gmbh Magnesiumlegierung
JP5700005B2 (ja) * 2012-09-05 2015-04-15 株式会社豊田中央研究所 複合マグネシウム合金部材およびその製造方法
JP6596236B2 (ja) 2015-05-27 2019-10-23 本田技研工業株式会社 耐熱性マグネシウム合金及びその製造方法
CN105817602B (zh) * 2015-09-09 2018-05-08 广东鸿泰南通精机科技有限公司 一种汽车变速箱上阀板生产工艺
CN107541627B (zh) * 2016-06-24 2019-09-06 北京科技大学 一种具有良好室温成形性的变形镁合金板材及其制备方法
JP2018193592A (ja) * 2017-05-19 2018-12-06 株式会社豊田中央研究所 マグネシウム合金、マグネシウム合金鋳物およびその製造方法
JP2019063835A (ja) * 2017-10-04 2019-04-25 株式会社日本製鋼所 マグネシウム合金からなる鍛造用素材の製造方法
CN110195181B (zh) * 2018-02-26 2021-10-22 中国宝武钢铁集团有限公司 一种具有高温耐热性能的压铸镁合金及其制造方法
JP6814446B2 (ja) * 2019-03-12 2021-01-20 本田技研工業株式会社 難燃性マグネシウム合金およびその製造方法
CN109913720B (zh) * 2019-03-27 2020-11-24 东北大学 一种高钙高铝含量的高弹性模量镁基复合材料及制备方法
CN109957692A (zh) * 2019-03-27 2019-07-02 东北大学 一种高钙高铝含量的铸造镁基复合材料及制备方法
US11959155B2 (en) 2019-03-29 2024-04-16 Kurimoto, Ltd. Heat-resistant magnesium alloy for casting
CN111155011A (zh) * 2020-02-21 2020-05-15 江苏理工学院 一种高性能Mg-Al-Ca镁合金及其制备方法
CN112725673A (zh) * 2020-12-28 2021-04-30 中信戴卡股份有限公司 一种Mg-Al合金及其制备方法
CN113005347B (zh) * 2021-02-25 2021-10-08 吉林大学 一种高塑性Mg-Al-Ca镁合金及其制备方法

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2642439B2 (zh) * 1988-02-26 1993-04-16 Pechiney Electrometallurgie
DE69007920T2 (de) * 1989-08-24 1994-07-21 Norsk Hydro As Hochfeste Magnesiumlegierungen und Verfahren zu ihrer Herstellung durch rasche Erstarrung.
JP2730847B2 (ja) * 1993-06-28 1998-03-25 宇部興産株式会社 高温クリープ強度に優れた鋳物用マグネシウム合金
JPH07118785A (ja) * 1993-10-25 1995-05-09 Mitsui Mining & Smelting Co Ltd 鋳物用マグネシウム合金、無気孔性マグネシウム合金鋳物及びそれらの製造方法
JPH07278717A (ja) * 1994-04-12 1995-10-24 Ube Ind Ltd 加圧部での耐へたり性に優れたマグネシウム合金製部材
JPH07331375A (ja) * 1994-06-06 1995-12-19 Toyota Motor Corp 鋳造用耐熱マグネシウム合金
JPH0841576A (ja) * 1994-07-28 1996-02-13 Honda Motor Co Ltd 高強度マグネシウム合金及びマグネシウム合金鋳物の熱処理方法
AU4617796A (en) * 1995-02-17 1996-09-04 Institute De La Technologie Du Magnesium, Inc Creep resistant magnesium alloys for die casting

Also Published As

Publication number Publication date
JP3415987B2 (ja) 2003-06-09
EP0799901A1 (en) 1997-10-08
KR970070224A (ko) 1997-11-07
US20020020475A1 (en) 2002-02-21
CN1065003C (zh) 2001-04-25
DE69706737D1 (de) 2001-10-25
CN1174243A (zh) 1998-02-25
JPH09272945A (ja) 1997-10-21
DE69706737T2 (de) 2002-07-04

Similar Documents

Publication Publication Date Title
EP0799901B1 (en) Heat-resistant magnesium alloy member
EP1127950B1 (en) Die casting magnesium alloy
EP1957221B1 (en) A combination of casting process and alloy compositions resulting in cast parts with superior combination of elevated temperature creep properties, ductility and corrosion performance
AU2004260006B2 (en) Aluminum alloy for engine blocks
CN109881063B (zh) 一种高强韧高模量压铸镁合金及其制备方法
AU730893B2 (en) Magnesium alloy having superior elevated-temperature properties and die castability
US5879478A (en) Process for semi-solid forming of thixotropic aluminum-silicon-copper alloy
AU2007285076B2 (en) Combination of casting process and alloy composition
JP3522963B2 (ja) 耐熱マグネシウム合金部材の製造方法およびそれに用いるマグネシウム合金、並びにマグネシウム合金成形部材
CA2366610C (en) High strength creep resistant magnesium alloy
US20080219880A1 (en) Creep-resistant magnesium alloy for casting
JP4526768B2 (ja) マグネシウム合金
US7169240B2 (en) Creep resistant magnesium alloys with improved castability
JP2001316752A (ja) ダイカスト用マグネシウム合金
JP2004238678A (ja) マグネシウム合金
Tsukeda et al. Effects of Alloying Elements of the Creep Resistance of Thixomolded Mg‐Al‐Ca‐X (X= Si, Zn, Mm, Ba, Sr) Alloys
Abbott et al. Properties of magnesium die castings for structural applications
CN113913652A (zh) 铝合金及其铸件和制备方法
MX2008006088A (en) A combination of casting process and alloy compositions resulting in cast parts with superior combination of elevated temperature creep properties, ductility and corrosion performance
MXPA98002487A (en) Zinc-based alloys improved containing tita

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE FR GB IT

17P Request for examination filed

Effective date: 19980408

17Q First examination report despatched

Effective date: 19980616

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAG Despatch of communication of intention to grant

Free format text: ORIGINAL CODE: EPIDOS AGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAH Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOS IGRA

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE FR GB IT

REF Corresponds to:

Ref document number: 69706737

Country of ref document: DE

Date of ref document: 20011025

REG Reference to a national code

Ref country code: GB

Ref legal event code: IF02

ET Fr: translation filed
PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed
PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20040331

Year of fee payment: 8

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: FR

Payment date: 20040408

Year of fee payment: 8

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20050404

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20050404

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20050404

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: FR

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20051230

REG Reference to a national code

Ref country code: FR

Ref legal event code: ST

Effective date: 20051230

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20110330

Year of fee payment: 15

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 69706737

Country of ref document: DE

Effective date: 20121101

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20121101