JPH0625790A - High-strength magnesium alloy - Google Patents

High-strength magnesium alloy

Info

Publication number
JPH0625790A
JPH0625790A JP4097321A JP9732192A JPH0625790A JP H0625790 A JPH0625790 A JP H0625790A JP 4097321 A JP4097321 A JP 4097321A JP 9732192 A JP9732192 A JP 9732192A JP H0625790 A JPH0625790 A JP H0625790A
Authority
JP
Japan
Prior art keywords
weight
strength
magnesium alloy
alloy
high temperature
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.)
Granted
Application number
JP4097321A
Other languages
Japanese (ja)
Other versions
JP2741642B2 (en
Inventor
Ryuji Ninomiya
隆二 二宮
Kohei Kubota
耕平 久保田
Naite Guenter
ナイテ ギュンター
E Schmidt Eberhard
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.)
GEA Group 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

Landscapes

  • Compositions Of Macromolecular Compounds (AREA)

Abstract

PURPOSE: To provide a heat resistant light-weight magnesium alloy for general purpose which is excellent in strength both at a room temperature and at a high temperature and suitable for the engine parts of an automobile in which the light weight and heat resistance are requested.
CONSTITUTION: This magnesium alloy excellent in strength both at a room temp. and at a high temp. contains, by weight, 2-10% aluminum and 1.4-10% calcium wherein the ratio of Ca/Al is ≥0.7 and also contains, as necessary, each ≤2% zinc, silicon and at least one element selected from a group comprised of ≤4% rare earth metal element and the balance magnesium with inevitable impurities.
COPYRIGHT: (C)1994,JPO

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 high temperatures up to about 473K which is required for weight reduction of automobile engine parts. .

【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 Due to the increasing awareness of global environmental protection in recent years,
With the increasing demand for improved fuel efficiency of automobiles, 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。
Magnesium alloy has the lowest density among the metallic materials currently put into practical use, and is strongly expected as a lightweight material for automobiles in the future. Currently, the most commonly used magnesium alloy is Mg-Al-Zn-Mn.
System alloy (for example, AZ91 alloy = Mg-9Al-1Zn)
-0.5 Mn), peripheral technologies such as casting technology of this alloy are in the completion stage, and this alloy is first studied for weight reduction of automobiles. Further, as a heat-resistant magnesium alloy, an alloy in which a rare earth element (RE) is added to magnesium, such as an Mg-RE-Zr 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 393 K or higher and is not suitable for use in automobile engine parts where heat resistance is required. In addition, the above heat-resistant Mg-RE-
In a Zr-based alloy, since RE is a heavy element, RE tends to be biased downward in the molten metal, and addition of Zr, which is used as an essential component, is unstable, resulting in high 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 the above problems of the prior art, and an object of the present invention is a novel material suitable for a material for automobile engine parts which is required to have 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。
Means for Solving the Problems The inventors of the present invention have conducted various studies to solve the above problems, and as a result, by adding an appropriate amount of aluminum and an appropriate amount of calcium to magnesium at a predetermined ratio, It was found that the strength at high temperature 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 and the like. However, the amount of calcium added in these cases is generally 0.15% by weight or less, and it is merely used to complement the strength of the AZ alloy.
On the other hand, it was found that the strength at room temperature and high temperature was remarkably improved by setting the added amount of calcium to 1.4 to 10% by weight and the added amount of aluminum to 0.7 times or more, and arrived at the present invention. .

【0008】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1.4〜10重量%を含有し、Ca/Alの比
が0.7以上であり、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 magnesium alloy of the present invention excellent in strength at room temperature and high temperature 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, The balance is characterized by being composed of magnesium and inevitable impurities.

【0009】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、所望により、更にそれぞれ2重量%以下
の亜鉛、マンガン、ジルコニウム及びケイ素、及び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)からなる群
から選ばれた少なくとも1種の元素を含有することがで
きる。
If desired, the magnesium alloy excellent in room temperature and high temperature strength of the present invention further comprises 2% by weight or less of zinc, manganese, zirconium and silicon, respectively, and 4% by weight or less of a rare earth element (eg yttrium, neodymium, It can contain at least one element selected from the group consisting of lanthanum, cerium, and misch metal.

【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1
0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 excellent in strength at room temperature and high temperature, aluminum is solid-dissolved in magnesium and exhibits age hardenability to improve the mechanical properties of the alloy. The effect of addition of aluminum increases with an increase in the amount of addition, but if it is less than 2% by weight, it is insufficient.
Saturation is reached at 0% by weight. Furthermore, as the amount of aluminum added increases, the elongation of the alloy decreases. Therefore, in the magnesium alloy of the present invention excellent in room temperature and high temperature strength, 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 of the present invention excellent in strength at room temperature and high temperature, calcium is an element effective for improving high temperature strength. However, the amount of calcium added is 1.4
If it is less than wt% or if the Ca / Al ratio is less than 0.7, the high temperature strength of the alloy is insufficient. Further, although the high temperature strength improves as the amount of calcium added increases, the cost increases. Considering the cost, there is no merit in adding calcium in excess of 10% by weight. When the ratio of Ca / Al is 0.7 or more, the structure morphology 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 calcium addition amount is 1.4 to 10% by weight, preferably 2 to 8% by weight, and the Ca / Al ratio is 0.7 or more, preferably It should be 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。
Zinc, which is generally added to the 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 the effect of improving strength. However, if the amount of zinc added exceeds 2% by weight, crystallization of the Mg-Al compound occurs, which is not preferable.

【0013】Mg合金に一般に2重量%以下の量で添加
されているジルコニウム及びマンガンは本発明のマグネ
シウム合金においても有効であり、組織を微細にし、強
度を向上させる効果を有する。
Zirconium and manganese, which are generally added to the Mg alloy in an amount of 2% by weight or less, are effective in the magnesium alloy of the present invention, and have the effects of making the structure fine and improving the strength.

【0014】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 of the present invention excellent in strength at room temperature and high temperature, the combination of silicon and calcium is extremely effective and has the effect of improving high temperature strength. However, if the amount of silicon added exceeds 2% by weight, the primary crystal Mg 2 Si will become coarse and the mechanical strength will decrease, such being undesirable.

【0015】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, neodymium and yttrium have been used especially in heat-resistant magnesium alloys. It was found that this effect is further improved by the combined use with calcium. The improvement of the effect by this combined use is saturated when the amount of the rare earth element added is 4% by weight.
Considering the cost, there is no merit in adding rare earth elements in excess of 4% by weight.

【0016】[0016]

【実施例】【Example】

実施例1〜12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 to 12 and Comparative Examples 1 to 3 Raw materials were charged and melted in a vacuum melting furnace in an argon atmosphere so that alloys having the compositions shown in Table 1 were obtained. SUS304 material was used as the crucible, and no flux or the like was used. The molten metal was cast into a mold of 25 mm × 50 mm × 300 mm to prepare a test casting. A JIS No. 4 test piece was prepared from the test casting thus obtained. The heat treatment is 500K for 10 hours. The following tests were carried out using these test pieces: Tensile test: Crosshead speed 10 mm / min, measuring temperature 298K and 473K, measuring unit of tensile strength = MPa, elongation at break =% by Instron tensile tester Measurement. The measurement results were as shown in Table 1 (% in the table is elongation at break).

【0017】[0017]

【表1】 [Table 1]

【0018】[0018]

【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。
INDUSTRIAL APPLICABILITY The magnesium alloy of the present invention is superior in room-temperature and high-temperature strength to the conventionally used general-purpose Mg-Al-Zn-Mn alloys, and is lightweight and heat-resistant automobile engine parts. It is a general-purpose heat-resistant lightweight magnesium alloy suitable for.

─────────────────────────────────────────────────────
─────────────────────────────────────────────────── ───

【手続補正書】[Procedure amendment]

【提出日】平成4年5月22日[Submission date] May 22, 1992

【手続補正1】[Procedure Amendment 1]

【補正対象書類名】明細書[Document name to be amended] Statement

【補正対象項目名】全文[Correction target item name] Full text

【補正方法】変更[Correction method] Change

【補正内容】[Correction content]

【書類名】 明細書[Document name] Statement

【発明の名称】 高強度マグネシウム合金[Title of Invention] High-strength magnesium alloy

【特許請求の範囲】[Claims]

【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 high temperatures up to about 473K which is required for weight reduction of automobile engine parts. .

【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 Due to the increasing awareness of global environmental protection in recent years,
With the increasing demand for improved fuel efficiency of automobiles, 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。
Magnesium alloy has the lowest density among the metallic materials currently put into practical use, and is strongly expected as a lightweight material for automobiles in the future. Currently, the most commonly used magnesium alloy is Mg-Al-Zn-Mn.
System alloy (for example, AZ91 alloy = Mg-9Al-1Zn)
-0.5 Mn), peripheral technologies such as casting technology of this alloy are in the completion stage, and this alloy is first studied for weight reduction of automobiles. Further, as a heat-resistant magnesium alloy, an alloy in which a rare earth element (RE) is added to magnesium, such as an Mg-RE-Zr 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 393 K or higher and is not suitable for use in automobile engine parts where heat resistance is required. In addition, the above heat-resistant Mg-RE-
In a Zr-based alloy, since RE is a heavy element, RE tends to be biased downward in the molten metal, and addition of Zr, which is used as an essential component, is unstable, resulting in high 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 the above problems of the prior art, and an object of the present invention is a novel material suitable for a material for automobile engine parts which is required to have 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。
Means for Solving the Problems The inventors of the present invention have conducted various studies to solve the above problems, and as a result, by adding an appropriate amount of aluminum and an appropriate amount of calcium to magnesium at a predetermined ratio, It was found that the strength at high temperature 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 and the like. However, the amount of calcium added in these cases is generally 0.15% by weight or less, and it is merely used to complement the strength of the AZ alloy.
On the other hand, it was found that the strength at room temperature and high temperature was remarkably improved by setting the added amount of calcium to 1.4 to 10% by weight and the added amount of aluminum to 0.7 times or more, and arrived at the present invention. .

【0008】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1.4〜10重量%を含有し、Ca/Alの比
が0.7以上であり、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 magnesium alloy of the present invention excellent in strength at room temperature and high temperature 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, The balance is characterized by being composed of magnesium and inevitable impurities.

【0009】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、所望により、更にそれぞれ2重量%以下
の亜鉛及びケイ素、及び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)からなる群から選ばれた少なくとも1
種の元素を含有することができる。
[0009] at room temperature and excellent magnesium alloy high-temperature strength of the present invention optionally, further each 2 wt% or less of nitrous Namari及 beauty silicon, and 4 wt% or less of rare earth elements (e.g., yttrium, neodymium, lanthanum, cerium,
At least one selected from the group consisting of misch metal)
It may contain seed elements.

【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。
[0010] In excellent magnesium alloy to room temperature and high temperature strength of the present invention, aluminum is <br/> solid solution in magnesium, shows the age-hardening properties, improve the mechanical properties of the alloy. The effect of addition of aluminum increases as the amount of aluminum added increases, but it is insufficient at less than 2% by weight and reaches saturation at 10% by weight. Furthermore, as the amount of aluminum added increases, the elongation of the alloy decreases. Therefore, in the magnesium alloy of the present invention excellent in room temperature and high temperature strength, 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 of the present invention excellent in strength at room temperature and high temperature, calcium is an element effective for improving high temperature strength. However, the amount of calcium added is 1.4
If it is less than wt% or if the Ca / Al ratio is less than 0.7, the high temperature strength of the alloy is insufficient. Further, although the high temperature strength improves as the amount of calcium added increases, the cost increases. Considering the cost, there is no merit in adding calcium in excess of 10% by weight. When the ratio of Ca / Al is 0.7 or more, the structure morphology 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 calcium addition amount is 1.4 to 10% by weight, preferably 2 to 8% by weight, and the Ca / Al ratio is 0.7 or more, preferably It should be 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。
Zinc, which is generally added to the 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 the effect of improving strength. However, if the amount of zinc added 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 of the present invention which is excellent in room temperature and high temperature strength, the combination of silicon and calcium is extremely effective and has an effect of improving high temperature strength. However, if the amount of silicon added exceeds 2% by weight, the primary crystal Mg 2 Si will become coarse and the mechanical strength will decrease, such being undesirable.

【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, neodymium and yttrium have been used especially in heat-resistant magnesium alloys. It was found that this effect is further improved by the combined use with calcium. The improvement of the effect by this combined use is saturated when the amount of the rare earth element added is 4% by weight.
Considering the cost, there is no merit in adding rare earth elements in excess of 4% by weight.

【0015】[0015]

【実施例】 実施例1〜10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)。
A vacuum melting furnace of EXAMPLE 1-10 and Comparative Examples 1 to 3 an argon atmosphere, the way raw wood charge the alloys having compositions shown in Table 1 and charging and dissolved. SUS304 material was used as the crucible, and no flux or the like was used. The molten metal was cast into a mold of 25 mm × 50 mm × 300 mm to prepare a test casting. A JIS No. 4 test piece was prepared from the test casting thus obtained. The heat treatment is 500K for 10 hours. The following tests were carried out using these test pieces: Tensile test: Crosshead speed 10 mm / min, measuring temperature 298K and 473K, measuring unit of tensile strength = MPa, elongation at break =% by Instron tensile tester Measurement. The measurement results were as shown in Table 1 (% in the table is elongation at break).

【0016】[0016]

【表1】 [Table 1]

【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。
INDUSTRIAL APPLICABILITY The magnesium alloy of the present invention is superior in room-temperature and high-temperature strength to the conventionally used general-purpose Mg-Al-Zn-Mn alloys, and is lightweight and heat-resistant automobile engine parts. It is a 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 ─────────────────────────────────────────────────── ─── Continuation of front page (72) Inventor Ryuji Ninomiya 1333-2 Hara-shi, Ageo-shi, Saitama Mitsui Mining & Smelting Co., Ltd. (72) Kohei Kubota 1333-2 Hara-shi, Ageo-shi, Saitama Mitsui Mining & Smelting Co., Ltd. Research Institute (72) Inventor Günter Naite Germany Federal Republic of Germany D-6350 Bad Nauheim Mainus Strasse 9 (72) Inventor Eberhard Eschmidt Federal Republic of Germany D-8755 Arsenau Eye Unter Frankfurt Iglauer Strasse 2E

Claims (2)

【特許請求の範囲】[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、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
マグネシウム合金。
1. An aluminum alloy containing 2 to 10% by weight of aluminum and 1.4 to 10% by weight of calcium, a Ca / Al ratio of 0.7 or more, and the balance being magnesium and inevitable impurities. A magnesium alloy with excellent room temperature and high temperature strength.
【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、更にそれぞれ2重量%以下の亜鉛、
マンガン、ジルコニウム及びケイ素、及び4重量%以下
の希土類元素からなる群から選ばれた少なくとも1種の
元素を含有し、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マグ
ネシウム合金。
2. Zinc containing 2 to 10% by weight of aluminum and 1.4 to 10% by weight of calcium, and having a Ca / Al ratio of 0.7 or more and further 2% by weight or less, respectively.
Excellent at room temperature and high temperature strength characterized by containing at least one element selected from the group consisting of manganese, zirconium and silicon, and 4% by weight or less of a rare earth element, and the balance being magnesium and inevitable impurities. Magnesium alloy.
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 true JPH0625790A (en) 1994-02-01
JP2741642B2 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 (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0711374A (en) * 1993-06-28 1995-01-13 Ube Ind Ltd Magnesium alloy
JPH0748646A (en) * 1993-03-15 1995-02-21 Toyota Motor Corp High strength magnesium base alloy and production thereof
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
US5811058A (en) * 1996-02-27 1998-09-22 Honda Giken Kogyo Kabushiki Kaisha Heat-resistant magnesium alloy
EP1048743A1 (en) * 1999-04-30 2000-11-02 General Motors Corporation Creep-resistant magnesium alloy die castings
EP1060817A1 (en) * 1999-06-04 2000-12-20 Mitsui Mining and Smelting Co., Ltd Pressure die-casting process of magnesium alloys
JP2004162090A (en) * 2002-11-11 2004-06-10 Toyota Industries Corp Heat resistant magnesium alloy
FR2850672A1 (en) * 2003-01-31 2004-08-06 Toyota Jidoshokki Kk HEAT RESISTANT MOLDING MAGNESIUM ALLOY AND HEAT RESISTANT MAGNESIUM ALLOY MOLDED MOLD
JP2004238678A (en) * 2003-02-05 2004-08-26 Dead Sea Magnesium Ltd Magnesium alloy
US6846451B2 (en) 2001-08-23 2005-01-25 The Japan Steel Works, Ltd. Magnesium alloy and magnesium alloy member superior in corrosion resistance
US7153374B2 (en) 2001-08-13 2006-12-26 Honda Giken Kogyo Kabushiki Kaisha Magnesium alloy
EP1816223A1 (en) * 2006-01-27 2007-08-08 Aisin Seiki Kabushiki Kaisha Magnesium alloy and casting
JP2008081773A (en) * 2006-09-26 2008-04-10 Sumitomo Electric Ind Ltd Magnesium-alloy material and production method therefor
WO2008072435A1 (en) * 2006-12-11 2008-06-19 Kabushiki Kaisha Toyota Jidoshokki Casting magnesium alloy and process for production of cast magnesium alloy
WO2008120497A1 (en) * 2007-04-03 2008-10-09 Kabushiki Kaisha Toyota Jidoshokki 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
WO2010038893A1 (en) * 2008-10-03 2010-04-08 株式会社豊田自動織機 Heat-resistant magnesium alloy
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
WO2013157653A1 (en) * 2012-04-19 2013-10-24 国立大学法人 熊本大学 Magnesium alloy and method for producing same
JP2014196525A (en) * 2013-03-29 2014-10-16 株式会社栗本鐵工所 Heat-resistant magnesium alloy
JP2016222947A (en) * 2015-05-27 2016-12-28 本田技研工業株式会社 Heat resistant magnesium alloy and manufacturing method therefor
US10550453B2 (en) 2015-02-26 2020-02-04 Kurimoto, Ltd. Heat-resistant magnesium alloy
WO2020183980A1 (en) 2019-03-12 2020-09-17 本田技研工業株式会社 Flame-retardant magnesium alloy and method for producing same

Families Citing this family (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

Citations (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
JPH0347941A (en) * 1989-07-13 1991-02-28 Yoshida Kogyo Kk <Ykk> High strength magnesium base alloy
JPH0390530A (en) * 1989-08-24 1991-04-16 Pechiney Electrometall Magnesium alloy high in mechanical strength and quick hardening method for its manufacture
JPH0397824A (en) * 1989-08-24 1991-04-23 Pechiney Rech Group Interet Economique Method for manufacture of magnesium alloy and alloy obtained by said method

Patent Citations (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
JPH0347941A (en) * 1989-07-13 1991-02-28 Yoshida Kogyo Kk <Ykk> High strength magnesium base alloy
JPH0390530A (en) * 1989-08-24 1991-04-16 Pechiney Electrometall Magnesium alloy high in mechanical strength and quick hardening method for its manufacture
JPH0397824A (en) * 1989-08-24 1991-04-23 Pechiney Rech Group Interet Economique Method for manufacture of magnesium alloy and alloy obtained by said method

Cited By (38)

* 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
JPH0711374A (en) * 1993-06-28 1995-01-13 Ube Ind Ltd Magnesium alloy
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
US5811058A (en) * 1996-02-27 1998-09-22 Honda Giken Kogyo Kabushiki Kaisha Heat-resistant magnesium alloy
EP1048743A1 (en) * 1999-04-30 2000-11-02 General Motors Corporation Creep-resistant magnesium alloy die castings
EP1060817A1 (en) * 1999-06-04 2000-12-20 Mitsui Mining and Smelting Co., Ltd Pressure die-casting process of magnesium alloys
US6467527B1 (en) 1999-06-04 2002-10-22 Mitsui Mining And Smelting Co., Ltd. Pressure die-casting process of magnesium alloys
US7153374B2 (en) 2001-08-13 2006-12-26 Honda Giken Kogyo Kabushiki Kaisha Magnesium alloy
US6846451B2 (en) 2001-08-23 2005-01-25 The Japan Steel Works, Ltd. Magnesium alloy and magnesium alloy member superior in corrosion resistance
JP2004162090A (en) * 2002-11-11 2004-06-10 Toyota Industries Corp Heat resistant magnesium alloy
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
JP2004232060A (en) * 2003-01-31 2004-08-19 Toyota Industries Corp Heat resistant magnesium alloy for casting and heat resistant magnesium alloy casting
FR2850672A1 (en) * 2003-01-31 2004-08-06 Toyota Jidoshokki Kk HEAT RESISTANT MOLDING MAGNESIUM ALLOY AND HEAT RESISTANT MAGNESIUM ALLOY MOLDED MOLD
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
JP2004238678A (en) * 2003-02-05 2004-08-26 Dead Sea Magnesium Ltd Magnesium alloy
EP1816223A1 (en) * 2006-01-27 2007-08-08 Aisin Seiki Kabushiki Kaisha Magnesium alloy and casting
JP2008081773A (en) * 2006-09-26 2008-04-10 Sumitomo Electric Ind Ltd Magnesium-alloy material and production method therefor
WO2008072435A1 (en) * 2006-12-11 2008-06-19 Kabushiki Kaisha Toyota Jidoshokki Casting magnesium alloy and process for production of cast magnesium alloy
JP5146767B2 (en) * 2006-12-11 2013-02-20 株式会社豊田自動織機 Magnesium alloy for casting and method for producing magnesium alloy casting
WO2008120497A1 (en) * 2007-04-03 2008-10-09 Kabushiki Kaisha Toyota Jidoshokki Heat-resistant magnesium alloy
EP2135965A1 (en) * 2007-04-03 2009-12-23 Kabushiki Kaisha Toyota Jidoshokki Heat-resistant magnesium alloy
EP2135965A4 (en) * 2007-04-03 2010-03-31 Toyota Jidoshokki Kk Heat-resistant 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
JP2010090405A (en) * 2008-10-03 2010-04-22 Toyota Industries Corp Heat-resistant magnesium alloy
WO2010038893A1 (en) * 2008-10-03 2010-04-08 株式会社豊田自動織機 Heat-resistant magnesium alloy
WO2013157653A1 (en) * 2012-04-19 2013-10-24 国立大学法人 熊本大学 Magnesium alloy and method for producing same
JPWO2013157653A1 (en) * 2012-04-19 2015-12-21 国立大学法人 熊本大学 Magnesium alloy and manufacturing method thereof
EP2840156A4 (en) * 2012-04-19 2016-04-20 Univ Kumamoto Nat Univ Corp Magnesium alloy and method for producing same
US10358702B2 (en) 2012-04-19 2019-07-23 National University Corporation Kumamoto University Magnesium alloy and production method of the same
JP2014196525A (en) * 2013-03-29 2014-10-16 株式会社栗本鐵工所 Heat-resistant magnesium alloy
US10550453B2 (en) 2015-02-26 2020-02-04 Kurimoto, Ltd. Heat-resistant magnesium alloy
JP2016222947A (en) * 2015-05-27 2016-12-28 本田技研工業株式会社 Heat resistant magnesium alloy and manufacturing method therefor
US10808301B2 (en) 2015-05-27 2020-10-20 Honda Motor Co., Ltd. Magnesium alloy and method of manufacturing same
WO2020183980A1 (en) 2019-03-12 2020-09-17 本田技研工業株式会社 Flame-retardant magnesium alloy and method for producing same

Also Published As

Publication number Publication date
JP2741642B2 (en) 1998-04-22

Similar Documents

Publication Publication Date Title
JP2741642B2 (en) High strength magnesium alloy
JP2604670B2 (en) High strength magnesium alloy
JP2725112B2 (en) High strength magnesium alloy
CN109881062B (en) High-strength, high-toughness and high-modulus extrusion casting magnesium alloy and preparation method thereof
US20040045639A1 (en) Magnesium alloy
EP2369025B1 (en) Magnesium alloy and magnesium alloy casting
CN101228286A (en) Hpdc magnesium alloy
WO2011090451A1 (en) CASTING ALLOY OF THE AIMgSI TYPE
JPH06279906A (en) Lightweight highly strong magnesium alloy for casting
JP2004162090A (en) Heat resistant magnesium alloy
WO2024066022A1 (en) Rare earth-alkaline earth element compounded magnesium-based alloy and preparation method therefor
JPH07122115B2 (en) High strength magnesium alloy containing gadolinium and samarium
JPH06279905A (en) Superplastic magnesium alloy
JPH0649579A (en) Gadolinium-containing high-strength magnesium alloy
CN110306084B (en) High-strength low-friction low-expansion high-silicon aluminum alloy and preparation method thereof
CN109161767B (en) Creep-resistant magnesium alloy containing W phase and preparation method thereof
JP3865430B2 (en) Heat and wear resistant magnesium alloy
JPH05255794A (en) Heat resistant magnesium alloy
JPH07122110B2 (en) High strength magnesium alloy
JP2003129161A (en) Heat resistant magnesium alloy
JPH06235041A (en) Magnesium base alloy for casting excellent in heat resistance
JPH06200350A (en) Terbium-containing high-strength magnesium alloy
JPH0823057B2 (en) Superplastic magnesium alloy
JP2003129160A (en) Heat resistant magnesium alloy
JPH0649576A (en) Superplastic 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