JP2741642B2 - High strength magnesium alloy - Google Patents

High strength magnesium alloy

Info

Publication number
JP2741642B2
JP2741642B2 JP4097321A JP9732192A JP2741642B2 JP 2741642 B2 JP2741642 B2 JP 2741642B2 JP 4097321 A JP4097321 A JP 4097321A JP 9732192 A JP9732192 A JP 9732192A JP 2741642 B2 JP2741642 B2 JP 2741642B2
Authority
JP
Japan
Prior art keywords
weight
alloy
strength
magnesium alloy
magnesium
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 - Fee Related
Application number
JP4097321A
Other languages
Japanese (ja)
Other versions
JPH0625790A (en
Inventor
隆二 二宮
耕平 久保田
ナイテ ギュンター
イー シュミット エバハード
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.)
Metallgesellschaft AG
Mitsui Mining and Smelting Co Ltd
Original Assignee
Metallgesellschaft AG
Mitsui Mining and Smelting Co Ltd
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 Metallgesellschaft AG, Mitsui Mining and Smelting Co Ltd filed Critical Metallgesellschaft AG
Priority to JP4097321A priority Critical patent/JP2741642B2/en
Publication of JPH0625790A publication Critical patent/JPH0625790A/en
Application granted granted Critical
Publication of JP2741642B2 publication Critical patent/JP2741642B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】本発明は室温及び高温強度に優れ
たマグネシウム合金に関し、より詳しくは自動車エンジ
ン部品などの軽量化において要請されている473K程
度までの高温でも十分な強度を有するマグネシウム合金
に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a magnesium alloy having excellent strength at room temperature and high temperature, and more particularly to a magnesium alloy having sufficient strength even at a high temperature up to about 473 K required for weight reduction of automobile engine parts and the like. .

【0002】[0002]

【従来の技術】近年地球環境保全の意識の高まりから、
自動車の燃費向上の要請が強まり、自動車用軽量材料の
開発が強く求められようになってきた。
2. Description of the Related Art In recent years, awareness of global environmental conservation has increased,
The demand for improving the fuel efficiency of automobiles has increased, and the development of lightweight materials for automobiles has been strongly demanded.

【0003】マグネシウム合金は現在実用化されている
金属材料の中で最も低密度であり、今後の自動車用軽量
材料として強く期待されている。現在最も一般的に用い
られているマグネシウム合金はMg−Al−Zn−Mn
系合金(例えば、AZ91合金=Mg−9Al−1Zn
−0.5Mn)であり、この合金の鋳造技術等の周辺技
術は完成段階にあり、自動車軽量化にあたって先ずこの
合金が検討されている。また、耐熱用マグネシウム合金
としてマグネシウムに希土類元素(RE)を添加した合
金、例えばMg−RE−Zr系合金が開発されている。
[0003] Magnesium alloys have the lowest density among metallic materials currently in practical use, and are expected to be used as lightweight materials for automobiles in the future. At present, the most commonly used magnesium alloy is Mg-Al-Zn-Mn.
System alloy (for example, AZ91 alloy = Mg-9Al-1Zn
-0.5 Mn), and peripheral technologies such as the casting technology of this alloy are in the stage of completion, and this alloy is first studied for weight reduction of automobiles. Further, as a heat-resistant magnesium alloy, an alloy obtained by adding a rare earth element (RE) to magnesium, for example, an Mg-RE-Zr-based alloy has been developed.

【0004】[0004]

【発明が解決しようとする課題】しかしながら、上記の
Mg−Al−Zn−Mn系合金は393K以上で強度が
低下し、自動車エンジン部品の中でも耐熱性が要求され
る用途には適さない。また、上記の耐熱性Mg−RE−
Zr系合金においてはREは重元素であるため溶湯中で
REが下部に偏る傾向があり、また必須成分として用い
ているZrの添加が不安定であり、コスト高になる。
However, the above-mentioned Mg-Al-Zn-Mn-based alloy has a reduced strength at 393K or more, and is not suitable for applications requiring heat resistance among automobile engine parts. In addition, the heat-resistant Mg-RE-
In a Zr-based alloy, RE is a heavy element, so that RE tends to be biased downward in the molten metal, and addition of Zr used as an essential component is unstable, resulting in an increase in cost.

【0005】本発明は、このような従来技術の有する課
題に鑑みてなされたものであり、本発明の目的は、耐熱
性と室温強度の両方が要求される自動車エンジン部品用
材料に適した新規な高強度マグネシウム合金を提供する
ことにある。
The present invention has been made in view of such problems of the prior art, and an object of the present invention is to provide a novel material suitable for a material for an automobile engine part which requires both heat resistance and room temperature strength. To provide a high strength magnesium alloy.

【0006】[0006]

【課題を解決するための手段】本発明者等は上記の課題
を解決するために種々検討を重ねた結果、マグネシウム
に適量のアルミニウムと適量のカルシウムとを所定の比
率で添加することにより室温及び高温での強度が向上す
ることを見出した。
The present inventors have made various studies to solve the above-mentioned problems, and as a result, by adding an appropriate amount of aluminum and an appropriate amount of calcium to magnesium at a predetermined ratio, the room temperature and the temperature are reduced. It has been found that the strength at high temperatures is improved.

【0007】上記AZ合金等にカルシウムを添加するこ
とにより室温及び高温での強度が向上することは既に知
られている。しかしながら、これらの場合のカルシウム
添加量は一般に0.15重量%以下であり、AZ合金の
強度を補完するする程度に用いられているに過ぎない。
これに対し、カルシウム添加量を1.4〜10重量%と
し、且つアルミニウム添加量の0.7倍以上とすること
により室温及び高温での強度が著しく向上することを見
出し、本発明に到達した。
It is already known that the strength at room temperature and high temperature is improved by adding calcium to the AZ alloy or the like. However, the amount of calcium added in these cases is generally 0.15% by weight or less, and is merely used to complement the strength of the AZ alloy.
On the other hand, it has been found that the strength at room temperature and high temperature is remarkably improved by setting the addition amount of calcium to 1.4 to 10% by weight and 0.7 times or more of the addition amount of aluminum, and reached the present invention. .

【0008】[0008]

【0009】即ち、本発明の室温及び高温強度に優れた
マグネシウム合金はアルミニウム2〜10重量%及びカ
ルシウム1.6〜10重量%を含有し、Ca/Alの比
が0.7以上であり、更にそれぞれ1.6〜2重量%の
ケイ素、及び(又は)4重量%以下の希土類元素(例え
ば、イットリウム、ネオジム、ランタン、セリウム、ミ
ッシュメタル)と2重量%以下のジルコニウムとの組合
わせを含有し、残部がマグネシウムと不可避の不純物か
らなることを特徴とする。
That is, the present invention has excellent strength at room temperature and high temperature.
Magnesium alloy contains 2 to 10% by weight of aluminum and
It contains 1.6 to 10% by weight of calcium and has a Ca / Al ratio of
Is not less than 0.7, and 1.6 to 2% by weight of silicon and / or 4% by weight or less of a rare earth element (e.g., yttrium, neodymium, lanthanum, cerium, misch metal) . Combination with 2% by weight or less of zirconium
And the balance consists of magnesium and inevitable impurities.

【0010】本発明の室温及び高温強度に優れたマグネ
シウム合金においては、アルミニウムはマグネシウム
固溶し、時効硬化性を示し、合金の機械的性質を向上さ
せる。アルミニウムの添加効果はその添加量の増加に伴
って増加するが、2重量%未満では不十分であり、また
10重量%で飽和に達する。更にアルミニウムの添加量
が増加するに従って合金の伸びが低下する。従って、本
発明の室温及び高温強度に優れたマグネシウム合金にお
いてはアルミニウム添加量を2〜10重量%、好ましく
は3〜9重量%とする。
In the magnesium alloy of the present invention having excellent strength at room temperature and high temperature, aluminum dissolves in magnesium , exhibits age hardening properties, and improves the mechanical properties of the alloy. The effect of adding aluminum increases with the amount of aluminum added, but less than 2% by weight is insufficient, and reaches saturation at 10% by weight. Further, as the amount of aluminum added increases, the elongation of the alloy decreases. Therefore, in the magnesium alloy excellent in room temperature and high temperature strength of the present invention, the amount of aluminum added is set to 2 to 10% by weight, preferably 3 to 9% by weight.

【0011】本発明の室温及び高温強度に優れたマグネ
シウム合金においては、カルシウムは高温強度の向上に
有効な元素である。しかしカルシウムの添加量が1.4
重量%未満の場合及びCa/Alの比が0.7未満の場
合にはその合金の高温強度が不十分である。またカルシ
ウム添加量の増加に伴って高温強度は向上するが、コス
ト高になる。コスト面を考慮するとカルシウムを10重
量%を越えて添加してもメリットがない。Ca/Alの
比を0.7以上にするとマグネシウム合金中に晶出する
析出物の組織形態が変化し、Mg−Ca化合物が晶出し
て優れた高温強度特性を示すようになる。従って、本発
明の室温及び高温強度に優れたマグネシウム合金におい
てはカルシウム添加量を1.4〜10重量%、好ましく
は2〜8重量%とし、Ca/Alの比を0.7以上、好
ましくは0.75以上とする。
In the magnesium alloy excellent in room temperature and high temperature strength of the present invention, calcium is an element effective for improving high temperature strength. However, the amount of calcium added was 1.4.
When the amount is less than 0.7% by weight or when the ratio of Ca / Al is less than 0.7, the high-temperature strength of the alloy is insufficient. Further, the high-temperature strength is improved as the amount of added calcium is increased, but the cost is increased. Considering cost, there is no merit in adding calcium in excess of 10% by weight. When the Ca / Al ratio is 0.7 or more, the microstructure of the precipitate crystallized in the magnesium alloy changes, and the Mg-Ca compound crystallizes to exhibit excellent high-temperature strength characteristics. Therefore, in the magnesium alloy excellent in room temperature and high temperature strength of the present invention, the amount of added calcium is set to 1.4 to 10% by weight, preferably 2 to 8% by weight, and the ratio of Ca / Al is 0.7 or more, preferably 0.75 or more.

【0012】Mg−Al合金に一般に2重量%以下の量
で添加されている亜鉛は本発明のマグネシウム合金にお
いても有効であり、強度を向上させる効果を有する。し
かし亜鉛の添加量が2重量%を越えるとMg−Al化合
物の晶出が生じるので好ましくない。
[0012] Zinc, which is generally added to an Mg-Al alloy in an amount of 2% by weight or less, is also effective in the magnesium alloy of the present invention, and has an effect of improving strength. However, if the amount of zinc exceeds 2% by weight, crystallization of the Mg-Al compound occurs, which is not preferable.

【0013】本発明の室温及び高温強度に優れたマグネ
シウム合金においては、ケイ素とカルシウムとの組合わ
せは極めて有効であり、高温強度を向上させる効果を有
する。しかしケイ素の添加量が2重量%を越えると初晶
Mg2 Siが粗大となり、機械的強度が低下するので好
ましくない。
In the magnesium alloy excellent in room temperature and high temperature strength of the present invention, the combination of silicon and calcium is extremely effective and has an effect of improving high temperature strength. However, if the addition amount of silicon exceeds 2% by weight, the primary crystal Mg 2 Si becomes coarse, and the mechanical strength decreases, which is not preferable.

【0014】希土類元素(例えば、イットリウム、ネオ
ジム、ランタン、セリウム、ミッシュメタル)はマグネ
シウム合金の高温強度を向上させることは公知であり、
最近は、特にネオジム及びイットリウムが耐熱用マグネ
シウム合金に使われている。この効果はカルシウムとの
併用により更に向上することが判明した。この併用によ
る効果の向上は希土類元素添加量4重量%で飽和する。
コスト面を考慮すると希土類元素を4重量%を越えて添
加してもメリットがない。
It is known that rare earth elements (eg, yttrium, neodymium, lanthanum, cerium, misch metal) improve the high temperature strength of magnesium alloys,
Recently, especially neodymium and yttrium have been used for magnesium alloys for heat resistance. It was found that this effect was further improved by the combined use with calcium. The improvement of the effect by this combination is saturated at the rare earth element addition amount of 4% by weight.
Considering the cost, there is no merit in adding the rare earth element in excess of 4% by weight.

【0015】実施例1,2及び比較例1〜3 アルゴン雰囲気の真空溶解炉に、表1に示す組成の合金
となるように原材料をを装入し、溶解させた。坩堝とし
てSUS304材を使用し、フラックス等は使用しなか
った。その溶湯を25mm×50mm×300mmの金型中に
鋳込んで試験用鋳物を作成した。このようにして得た試
験用鋳物からJIS4号試験片を作成した。なお、熱処
理はいずれも500K、10時間である。これらの試験
片を用いて以下の試験を実施した: 引張試験:インストロン引張試験機によりクロスヘッド
速度10mm/min、測定温度298K及び473K、引張
強度の測定単位=MPa、破断時伸び=%で測定。 測定結果は表1に示す通りであった(表中の%は破断時
伸びである)。
Examples 1 and 2 and Comparative Examples 1 to 3 Raw materials were charged and melted in a vacuum melting furnace in an argon atmosphere so as to obtain an alloy having the composition shown in Table 1. SUS304 material was used as the crucible, and no flux or the like was used. The molten metal was cast into a 25 mm × 50 mm × 300 mm mold to prepare a test casting. A JIS No. 4 test piece was prepared from the test casting thus obtained. The heat treatment is performed at 500 K for 10 hours. The following tests were carried out using these test pieces: Tensile test: Crosshead speed 10 mm / min using an Instron tensile tester, measuring temperatures 298 K and 473 K, measuring unit of tensile strength = MPa, elongation at break =% Measurement. The measurement results were as shown in Table 1 (% in the table is elongation at break).

【0016】[0016]

【表1】 合 金 組 成 298K 473K 例番号 Al Ca Mg その他 引張強度 引張強度 実施例 3.0 3.0 残 Si:1.8 260 4 190 8 比較例1 3.0 1.0 残 240 4 110 8 比較例2 6.0 3.0 残 260 3 120 7 比較例3 9.0 5.0 残 280 3 130 7 Table 1 Alloy composition 298K 473K Example No. Al Ca Mg Other tensile strength % Tensile strength % Example 1 3.0 3.0 Remaining Si: 1.8 260 4 190 8 Comparative Example 1 3.0 1.0 Remaining 240 4 110 8 Comparative Example 2 6.0 3.0 Remaining 260 3 120 7 Comparative Example 3 9.0 5.0 Remaining 280 3 130 7

【0017】[0017]

【発明の効果】本発明のマグネシウム合金は、従来実用
されている汎用のMg−Al−Zn−Mn系合金よりも
室温及び高温強度に優れており、軽量且つ耐熱性が要求
される自動車エンジン部品に適した汎用の耐熱性軽量マ
グネシウム合金である。
The magnesium alloy of the present invention is superior in room temperature and high-temperature strength to conventional general-purpose Mg-Al-Zn-Mn alloys, and is required to be lightweight and heat-resistant. General-purpose heat-resistant lightweight magnesium alloy suitable for

───────────────────────────────────────────────────── フロントページの続き (72)発明者 二宮 隆二 埼玉県上尾市原市1333−2 三井金属鉱 業株式会社総合研究所内 (72)発明者 久保田 耕平 埼玉県上尾市原市1333−2 三井金属鉱 業株式会社総合研究所内 (72)発明者 ギュンター ナイテ ドイツ連邦共和国 D−6350 バッド ナウハイム マイヌスストラッセ 9 (72)発明者 エバハード イー シュミット ドイツ連邦共和国 D−8755 アルゼナ ウ アイ ウンターフランクフルト イ グラウワー ストラッセ 2E (56)参考文献 特開 平3−90530(JP,A) 特開 平3−97824(JP,A) 特開 平3−47941(JP,A) 特開 昭50−115606(JP,A) 特開 昭61−3863(JP,A) 特公 昭45−2813(JP,B1) ──────────────────────────────────────────────────続 き Continuing on the front page (72) Inventor Ryuji Ninomiya 1333-2, Hara-shi, Ageo-shi, Saitama Mitsui Kinzoku Mining Co., Ltd. (72) Inventor Kohei Kubota 1333-2, Hara-shi, Ageo-shi, Saitama Mitsui Mining Inside the Research Institute, Inc. (72) Inventor Gunter Naite D-6350 Bad Nauheim Meinusstrasse 9 (72) Inventor Eberhard E. Schmidt D-8755 Arzena U I Unter Frankfurt i Grauer Strasse 2E (56) JP-A-3-90530 (JP, A) JP-A-3-97824 (JP, A) JP-A-3-47941 (JP, A) JP-A-50-115606 (JP, A) JP-A-61 −3863 (JP, A) JP-B 45-2813 (JP, B1)

Claims (2)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 アルミニウム2〜10重量%及びカルシ
ウム1.4〜10重量%を含有し、Ca/Alの比が
0.7以上であり、更に1.6〜2重量%のケイ素を含
有し、残部がマグネシウムと不可避の不純物からなるこ
とを特徴とする室温及び高温強度に優れた鋳造用マグネ
シウム合金。
An aluminum alloy containing 2 to 10% by weight of aluminum and 1.4 to 10% by weight of calcium, a ratio of Ca / Al of 0.7 or more, and further containing 1.6 to 2% by weight of silicon. A magnesium alloy for casting excellent in room temperature and high temperature strength, the balance being composed of magnesium and unavoidable impurities.
【請求項2】 アルミニウム2〜10重量%及びカルシ
ウム1.4〜10重量%を含有し、Ca/Alの比が
0.7以上であり、更に4重量%以下の希土類元素と2
重量%以下のジルコニウムとの組合わせを含有し、残部
がマグネシウムと不可避の不純物からなることを特徴と
する室温及び高温強度に優れた鋳造用マグネシウム合
金。
2. The composition according to claim 1, wherein the alloy contains 2 to 10% by weight of aluminum and 1.4 to 10% by weight of calcium and has a Ca / Al ratio of 0.7 or more, and further contains 4% by weight or less of a rare earth element.
A magnesium alloy for casting excellent in room temperature and high temperature strength, comprising a combination with zirconium of not more than% by weight and a balance consisting of magnesium and unavoidable impurities.
JP4097321A 1992-03-25 1992-03-25 High strength magnesium alloy Expired - Fee Related JP2741642B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP4097321A JP2741642B2 (en) 1992-03-25 1992-03-25 High strength magnesium alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP4097321A JP2741642B2 (en) 1992-03-25 1992-03-25 High strength magnesium alloy

Publications (2)

Publication Number Publication Date
JPH0625790A JPH0625790A (en) 1994-02-01
JP2741642B2 true JP2741642B2 (en) 1998-04-22

Family

ID=14189221

Family Applications (1)

Application Number Title Priority Date Filing Date
JP4097321A Expired - Fee Related JP2741642B2 (en) 1992-03-25 1992-03-25 High strength magnesium alloy

Country Status (1)

Country Link
JP (1) JP2741642B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109022973A (en) * 2018-06-26 2018-12-18 无锡福镁轻合金科技有限公司 A kind of deformed magnesium alloy material and its preparation process of middle high-strength and high-plasticity

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0748646A (en) * 1993-03-15 1995-02-21 Toyota Motor Corp High strength magnesium base alloy and production thereof
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
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
JPH08134581A (en) * 1994-11-14 1996-05-28 Mitsui Mining & Smelting Co Ltd Production of magnesium alloy
JPH08269609A (en) * 1995-03-27 1996-10-15 Toyota Central Res & Dev Lab Inc Mg-al-ca alloy excellent in die castability
JP3229954B2 (en) * 1996-02-27 2001-11-19 本田技研工業株式会社 Heat resistant magnesium alloy
US6264763B1 (en) * 1999-04-30 2001-07-24 General Motors Corporation Creep-resistant magnesium alloy die castings
EP1060817B1 (en) * 1999-06-04 2004-09-15 Mitsui Mining and Smelting Co., Ltd Pressure die-casting process of magnesium alloys
GB2384248B (en) 2001-08-13 2005-06-22 Honda Motor Co Ltd 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
JP2004162090A (en) * 2002-11-11 2004-06-10 Toyota Industries Corp Heat resistant magnesium 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
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
JP4526769B2 (en) * 2003-02-05 2010-08-18 デッド シー マグネシウム エルティーディー 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
JP5046178B2 (en) * 2006-09-26 2012-10-10 住友電気工業株式会社 Magnesium alloy material and manufacturing method thereof
EP2088217A1 (en) * 2006-12-11 2009-08-12 Kabushiki Kaisha Toyota Jidoshokki Casting magnesium alloy and process for production of cast magnesium alloy
JPWO2008120497A1 (en) * 2007-04-03 2010-07-15 株式会社豊田自動織機 Heat resistant magnesium alloy
JP2009007676A (en) * 2008-07-30 2009-01-15 Toyota Industries Corp Heat resistant magnesium alloy for casting, and heat resistant magnesium alloy casting
JP5445820B2 (en) * 2008-10-03 2014-03-19 株式会社豊田自動織機 Heat resistant magnesium alloy
EP2840156B1 (en) * 2012-04-19 2020-05-06 National University Corporation Kumamoto University Magnesium alloy and method for producing same
JP5852039B2 (en) * 2013-03-29 2016-02-03 株式会社栗本鐵工所 Heat-resistant magnesium alloy
EP3263725B1 (en) 2015-02-26 2022-03-30 Kurimoto, Ltd. Heat-resistant magnesium alloy
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
JP6814446B2 (en) 2019-03-12 2021-01-20 本田技研工業株式会社 Flame-retardant magnesium alloy and its manufacturing method

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS50115606A (en) * 1974-02-26 1975-09-10
JPS613863A (en) * 1984-06-15 1986-01-09 Ube Ind Ltd Die casting magnesium alloy
JP2511526B2 (en) * 1989-07-13 1996-06-26 ワイケイケイ株式会社 High strength magnesium base alloy
DE69007920T2 (en) * 1989-08-24 1994-07-21 Pechiney Electrometallurgie High-strength magnesium alloys and processes for their production through rapid solidification.
FR2651244B1 (en) * 1989-08-24 1993-03-26 Pechiney Recherche PROCESS FOR OBTAINING MAGNESIUM ALLOYS BY SPUTTERING.

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109022973A (en) * 2018-06-26 2018-12-18 无锡福镁轻合金科技有限公司 A kind of deformed magnesium alloy material and its preparation process of middle high-strength and high-plasticity

Also Published As

Publication number Publication date
JPH0625790A (en) 1994-02-01

Similar Documents

Publication Publication Date Title
JP2741642B2 (en) High strength magnesium alloy
JP2604670B2 (en) High strength magnesium alloy
JP3229954B2 (en) Heat resistant magnesium alloy
JP2725112B2 (en) High strength magnesium alloy
US7153374B2 (en) Magnesium alloy
EP2369025B1 (en) Magnesium alloy and magnesium alloy casting
JPH0718364A (en) Heat resistant magnesium alloy
JPH06279906A (en) Lightweight highly strong magnesium alloy for casting
JP2004162090A (en) Heat resistant magnesium alloy
JPH07122115B2 (en) High strength magnesium alloy containing gadolinium and samarium
JPH06279905A (en) Superplastic magnesium alloy
CN109161767B (en) Creep-resistant magnesium alloy containing W phase and preparation method thereof
JP3865430B2 (en) Heat and wear resistant magnesium alloy
JPH0649579A (en) Gadolinium-containing high-strength magnesium alloy
JPH05255794A (en) Heat resistant magnesium alloy
JP2003129161A (en) Heat resistant magnesium alloy
JPH07122110B2 (en) High strength magnesium alloy
JP3387548B2 (en) Manufacturing method of magnesium alloy molded product
JPH1161299A (en) Heat resistant zinc alloy and formed part
JP2691488B2 (en) Zinc alloy for die casting and zinc alloy die casting products
JPH0823057B2 (en) Superplastic magnesium alloy
JPH06200350A (en) Terbium-containing high-strength magnesium alloy
JPH06235041A (en) Magnesium base alloy for casting excellent in heat resistance
JPH0649576A (en) Superplastic magnesium alloy
JP2003129160A (en) Heat resistant magnesium alloy

Legal Events

Date Code Title Description
R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20090130

Year of fee payment: 11

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20100130

Year of fee payment: 12

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20100130

Year of fee payment: 12

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20110130

Year of fee payment: 13

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20120130

Year of fee payment: 14

LAPS Cancellation because of no payment of annual fees