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WO2008133218A1 - Magnesium alloy for casting and magnesium alloy cast - Google Patents

Magnesium alloy for casting and magnesium alloy cast Download PDF

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Publication number
WO2008133218A1
WO2008133218A1 PCT/JP2008/057646 JP2008057646W WO2008133218A1 WO 2008133218 A1 WO2008133218 A1 WO 2008133218A1 JP 2008057646 W JP2008057646 W JP 2008057646W WO 2008133218 A1 WO2008133218 A1 WO 2008133218A1
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WO
WIPO (PCT)
Prior art keywords
mass
magnesium alloy
compound
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.)
Ceased
Application number
PCT/JP2008/057646
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French (fr)
Japanese (ja)
Inventor
Yuki Okamoto
Kyoichi Kinoshita
Motoharu Tanizawa
Kazuhiko Yoshida
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Toyota Industries Corp
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Toyota Industries Corp
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Application filed by Toyota Industries Corp filed Critical Toyota Industries Corp
Priority to EP08740692A priority Critical patent/EP2138595A1/en
Priority to US12/596,815 priority patent/US20100209285A1/en
Publication of WO2008133218A1 publication Critical patent/WO2008133218A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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    • 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
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium

Definitions

  • the present invention relates to a magnesium alloy for fabrication suitable for use at high temperatures.
  • Magnesium alloys which are lighter than aluminum alloys, are being widely used as aviation vehicle materials and the like from the viewpoint of weight reduction.
  • the magnesium alloy is not sufficient in bowing and heat resistance depending on the application, and therefore further improvement in properties is required.
  • a common magnesium alloy is AZ 91D (ASTM symbol). Since the thermal conductivity of AZ91D is about 73 WZmK, if it is used for a member that is used in a high temperature environment or generates heat during use, heat dissipation may not be performed well, and the member may be thermally deformed. In particular, if a magnesium alloy with a low conductivity is used as the magnesium alloy used for the cylinder head of the inner thigh and the cylinder block, the cylinder head is thermally deformed, the heat is accumulated in the cylinder block and the cylinder bore is deformed. Adverse effects such as increased friction and reduced airtightness occur. For this reason, there is a need for a magnesium alloy that has high heat conductivity and that can perform heat dissipation well and is suitable for use at high temperatures.
  • Mg- 3% Cu- l% "mass 0/0" if thief (units of Ca :).
  • the creep resistance at high temperature is not sufficient depending on the usage conditions.
  • an object of the present invention is to provide a magnesium alloy for forging that is suitable for use at high temperatures. It is also intended to produce a ceramic material made of a magnesium alloy.
  • the present inventors have improved the cleaving resistance at high temperatures without adversely affecting the 3 ⁇ 4i conductivity of the magnesium alloy by adding tin as an alloying element of the magnesium alloy together with copper and strength russium. Based on this, the present inventors have reached the present invention.
  • the total magnesium alloy of the present invention is 100% by mass, 1% by mass to 5% by mass of copper (Cu) and 0.1% by mass or more and 5% by mass or less of canorecium ( (Ca), and a mass ratio (Sn / Ca) from 0.1 to 3 with respect to Ca, and the balance is composed of magnesium (Mg) and inevitable impurities.
  • Cu copper
  • Ca canorecium
  • Sn / Ca mass ratio
  • the magnesium alloy for forging of the present invention contains Cu, Ca, and Sn, so that a crystallized product of Mg—Ca—Sn compound together with Mg—Cu compound is network-like (at the grain boundary of Mg crystal grains). Crystallizes in a three-dimensional network.
  • the three-dimensional network structure suppresses intergranular slip, which becomes particularly active at high temperatures, and improves high-temperature strength and creep resistance at high temperatures.
  • Mg—Ca—S compounds are relatively brittle, but Mg—Ca—Sn compounds in which part of C— of Mg—Ca compounds is replaced with Sn have high strength.
  • 3 daughters of magnesium alloy improve.
  • Sn forms a compound preferentially with Ca, so it has less influence on conductivity than other additive elements such as aluminum.
  • X—Y compound or the like is, for example, a compound having X and ⁇ as shown by ⁇ 2 ⁇ in the composition formula.
  • the magnesium alloy product of the present invention is a magnesium alloy for use in the present invention. This is a fake.
  • the magnesium alloy porcelain of the present invention is
  • Fig. 1 is a graph showing the thermal conductivity of magnesium alloys with different alloy yarns.
  • Fig. 2 is a graph showing the amount of stress reduction 40 hours after the start of the test in the stress relaxation test of magnesium alloys with different alloy compositions.
  • Figure 3 is a graph plotting the compressive stress applied to the specimen every 10 minutes against the test time for stress relaxation difficulty.
  • FIG. 4A and FIG. 4B are photographs in place of drawings showing the metal «of Mg-3 mass% Cu-1 mass 0 / oCa alloy (# 01).
  • FIG. 5A and FIG. 5B are photographs in place of drawings showing the metal structure of the Mg-3 mass 0 / oCu-1 mass 0 / o Ca-0. 1 mass 0 / oS n (# 02) alloy.
  • Fig. 6 A and Fig. 6 B are Mg-3 mass% Cu 1 mass% Ca-1 mass% Sn
  • (# 0 3) is a drawing-substituting photograph showing a metal yarn cage of an alloy.
  • FIG. 7A and FIG. 7B are drawings-substituting photographs showing the metal structure of the Mg—3 mass% Cu—1 mass% Ca—2 mass% Sn (# 04) alloy.
  • FIG. 8 A and Fig. 8 B are Mg-3 mass% ⁇ u-1 mass.
  • FIG. 5 is a drawing-substituting photograph showing the metallographic structure of the / 0 Ca—4 mass% Sn (# 05) alloy. BEST MODE FOR CARRYING OUT THE INVENTION
  • the magnesium alloy for forging of the present invention comprises copper (Cu), calcium (C a) and tin (Sn), with the balance being magnesium (Mg) and inevitable impurities.
  • the crystallized product of Mg—Ca—Sn compound as well as Mg—Cu—S compound can be obtained. It crystallizes in a network (three-dimensional network) at the grain boundaries of Mg grains. Because it is a network with few discontinuous parts, it has a high effect of suppressing grain boundary sliding.
  • the Cu content is 1% by mass or more and 5% by mass when the total magnesium alloy is 100% by mass. /. It is as follows. If the Cu content is 1% by mass or more, Mg-Cu compounds will crystallize sufficiently at the grain boundaries. The Cu content is 1 mass. If it is less than 0 , the strength of the Mg-Cu compound is low due to insufficient crystallization at the grain boundaries. The preferred Cu content is 2% by mass or more. On the other hand, as the amount of Cu increases, the amount of Mg-Cu compound that crystallizes at the crystal grain boundary becomes excessive, resulting in a brittle paper weave. The preferred Cu content is 4 mass. /. It is as follows.
  • the magnesium alloy for forging of the present invention contains Ca and Sn together with Cu.
  • Ca and Sn, together with Cu, contribute to the formation of a three-dimensional network structure as a grain boundary.
  • the Mg-Ca-Sn compound and the Mg-Cu-Sn compound crystallize at the grain boundary, and a good three-dimensional network structure is formed with few discontinuities.
  • the content of C a, upon the entire 3 ⁇ 4 for magnesium alloy is 100 mass 0/0, not more than 1 mass% to 5 mass% 0.5. If the content of C a is 0.1% by mass or more, the Mg—C a—Sn compound is sufficiently crystallized at the grain boundary. In addition, adding Ca to the magnesium alloy increases the ignition of the magnesium alloy, preventing combustion that may occur when the magnesium alloy is made intense. Preferred content of Ca is 0.5 mass. /. That's it. On the other hand, when the Ca content exceeds 5% by mass, the amount of grain boundary crystallized products increases, and mechanical properties such as tensile strength and elongation decrease, resulting in problems in post-processing. is there. A preferable Ca content is 3% by mass or less, and further 2% by mass or less.
  • the Sn content is 0.1 to 3 in terms of mass ratio (Sn / Ca) to calcium (Ca). If the Sn content is 0.1 mass% or more, Mg
  • the -Ca-Sn compound is sufficiently crystallized.
  • the Mg-Ca-Sn compound is divided from the three-dimensional network structure and crystallizes in the crystal grains, making it difficult to form a good three-dimensional network structure. As a result, the creep resistance tends to decrease.
  • produces not only Mg—Ca—Sn compounds but also Mg—Sn compounds. Mg-Sn compounds are low melting point compounds, and therefore creep resistance is improved. Therefore, the Sn content is 3 or less with SnZCa. If SnZCa is 3 or less, formation of a low melting point compound is suppressed.
  • SnZCa is 2 or less, a good three-dimensional network structure with little discontinuity is formed, and the high-temperature bow daughter and the creep resistance at high temperature are improved. That is, the preferred Sn content is 311 O &, 2 or less, and 1.5 or less.
  • Sn forms a compound with Ca preferentially over Mg and Cu. Therefore, Cu and Mg-Cu compounds with high thermal conductivity are not adversely affected, and as a result, the conductivity of the magnesium alloy is unlikely to decrease. From this, considering the stoichiometric ratio of SnZCa of MgCa-Sn compounds, the mass ratio of Sn to Ca (Sn / Ca) is 3 or less, or 0.1 or more 2 The following is preferable, and there is almost no Sn that forms a compound with an Mg—Cu compound, and crystallization of the low melting point compound described above is also suppressed.
  • the magnesium alloy for t according to the present invention described above can be used in various fields such as automobiles and electric power as well as space and aviation.
  • a product used under a high temperature environment for example, a compressor, a pump, various cases, etc.
  • Components used and engine parts used under high temperature and high load especially cylinder heads, cylinder blocks and oil vans for internal combustion engines, turbocharger impellers for internal combustion engines, and transmitters used for automobiles, etc. Case.
  • the magnesium alloy ceramic of the present invention is a ceramic made of the magnesium alloy for forging according to the present invention described in detail above. That is, the magnesium alloy case of the present invention is obtained through a pouring step and a solidification step, and the pouring step is 1% by mass or more and 5% by mass when the whole is 100% by mass. / 0 and less copper (Cu), 0.
  • the magnesium alloy of the present invention is not limited to normal gravity pressure fabrication, but may be die cast fabrication.
  • the sand mold, mold, etc. used for dredging can be used.
  • the solidification rate (cooling rate) in the solidification process and the solidification rate to the extent that a three-dimensional network structure is formed can be selected as appropriate according to the size of the clot. If solidified by general solidification, a network-like metal string is obtained.
  • the magnesium alloy and the magnesium compound for use in the present invention are preferably free materials. Furthermore, the characteristics of, may be improved by heat treatment later.
  • the present invention is not limited to the above embodiment.
  • the present invention can be implemented in various forms that have been changed or improved by those skilled in the art without departing from the scope of the present invention.
  • Chloride flux was applied to the inner surface of a crucible preheated in an electric furnace, and a large amount of pure magnesium ingot, pure Cu, and pure Sn as required were dissolved. Furthermore, weighed Ca was added to this molten metal kept at 750 ° C.
  • the agitation was sufficiently stirred to completely dissolve the raw materials, and then kept calm for a while.
  • the various molten alloys obtained in this way were poured into molds of a predetermined shape (the pouring process) and solidified in the atmosphere (solidification process). Forged.
  • the obtained test piece was 30 mm ⁇ 30 mm ⁇ 200 mm.
  • Table 1 shows the chemical composition of each specimen. Measurement of conductivity]
  • test pieces # 01 to # 05 shown in Table 1 were observed. The surface was observed by observing the cross section cut out from each specimen with a metal microscope. The forces shown in Fig. 4A to Fig. 8A and Fig. 4B to Fig. 8B, respectively, on the surface of # 01 to # 05 are shown in Fig. 4A to Fig. 8B. Magnification, Figures 4B-8B (b) The same section was observed at high magnification.
  • test piece # 01 as can be seen from FIG. 4A, a three-dimensional network structure strength formed by crystallization of an intermetallic compound at the grain boundary was obtained.
  • Fig. 4 (b) it is CuMg 2 that appears bright at the grain boundary, and Mg 2 C a that appears bright.
  • # 01 ⁇ The test piece of ⁇ 05 was superior in terms of convection and deviation than A ⁇ 91 D.
  • the thermal conductivity of the # 01 test piece not containing Sn was 155 WZmK, but no decrease in! Rf conductivity due to the addition of Sn was observed in the # 02 to # 04 test pieces.
  • # 05 where the Sn content is excessive although the excellence is superior to A Z 91 D, the difference in the inductivity from # 01 is large.
  • # 02 to # 04 specimens made of magnesium alloy containing Sn had less stress reduction than the specimen # 01 after 40B clearance from the start of wrinkle in the stress relaxation test at 200 ° C. .
  • the addition of Sn to the Mg-Cu-Ca alloy (# 01) improved the creep resistance at high temperatures. This is presumed to be because # 02 to # 04 have a higher 3D network structure than # 01, which has many discontinuous parts in the 3D network structure.
  • 2 masses of Sn. # 04 with / o has better creep resistance after 40 hours than # 01 without Sn, but inferior to # 02 and # 03.
  • the metal structure of # 04 is thought to be because the three-dimensional network structure was incompleter than # 02 and # 03. Contains 4% by mass of Sn # 05, three-dimensional network structure is incomplete, it is contemplated that M g 2 S n which is a low melting compound containing Mutame, creep resistance was Koma ⁇ .
  • # 02 and # 03 pieces had a greater stress drop than # 01 about 3 hours after starting, but the change in stress from 3 to 40 hours was small and stable.
  • # 04 specimen has a greater stress drop than # 01 and A Z9 ID about 3 hours after the start of the test, but the amount of stress change from 3 to 40 hours is small and stable. It was. (Figure 3)
  • each of the above-mentioned pieces has a constant (: 11 is 3% by mass and Ca is 1% by mass.
  • Cu is 2.7%. /. If it is 3 mass% or less, and Ca is 0.7 mass% or more and 1.3 mass% or less, it exhibits the same conductivity and surface creep properties as the above-mentioned pieces.
  • a magnesium alloy containing Cu, Ca and Sn with appropriate contents shows no deterioration in conductivity due to the addition of Sn, and is excellent in creep resistance at high temperatures.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Conductive Materials (AREA)
  • Forging (AREA)
  • Continuous Casting (AREA)

Abstract

A casting magnesium alloy characterized by containing 1-5 mass% copper (Cu) and 0.1-5 mass% calcium (Ca) based on the whole alloy and containing tin (Sn) in such an amount that the ratio of the mass of Sn to that of the Ca, Sn/Ca, is 0.1-3, with the remainder being magnesium (Mg) and incidental impurities. Due to the incorporation of Cu, Ca, and Sn, crystals of not only an Mg-Cu compound but an Mg-Ca-Sn compound separate out so as to form a network structure (three-dimensional network structure) at the boundary between Mg crystal grains. The three-dimensional network structure inhibits boundary sliding, which is apt to occur especially at high temperatures, to improve high-temperature strength and high-temperature creep resistance. Since the Sn forms a compound preferentially with the Ca, it exerts less adverse influences on thermal conductivity than the other additive elements.

Description

明細書 ^ マグネシゥム合金およびマグネシゥム合^^ 技術分野  Description ^ Magnesium alloy and magnesium alloy ^^ Technical field

本発明は、 高温下での使用に適した铸造用マグネシウム合金に関するものであ る。 技歸景  The present invention relates to a magnesium alloy for fabrication suitable for use at high temperatures. Technical scene

アルミニウム合金よりもさらに軽量なマグネシウム合金は、 軽量化の観点から 航空餅才 車両材料などとして広く用いられつつある。 しかしながら、 マグネ シゥム合金は、 用途によっては弓 ¾や耐熱性などが充分ではないため、 さらなる 特性の向上が求められている。  Magnesium alloys, which are lighter than aluminum alloys, are being widely used as aviation vehicle materials and the like from the viewpoint of weight reduction. However, the magnesium alloy is not sufficient in bowing and heat resistance depending on the application, and therefore further improvement in properties is required.

たとえば、 一般的なマグネシウム合金として、 AZ 91D (ASTM記号) ある。 AZ91Dの熱伝導率は 73WZmK程度であるため、 使用環境が高温で あったり使用中に発熱したりする部材に用いられると、 放熱が良好に行われず、 部材に熱変形が生じることがある。 特に、 内腿関のシリンダヘッドゃシリンダ プロックに用いられるマグネシウム合金として謝云導率の低いマグネシウム合金 を用いると、 シリンダヘッドが熱変形したり、 シリンダブロック内に熱がこもり シリンダボアが変形することで、 摩擦が増大したり気密性が低下したりするなど の悪影響が生じる。 そのため、 高い ¾云導率をもつことで放熱が良好に行われ、 高温下での使用に好適なマグネシゥム合金が求められている。  For example, a common magnesium alloy is AZ 91D (ASTM symbol). Since the thermal conductivity of AZ91D is about 73 WZmK, if it is used for a member that is used in a high temperature environment or generates heat during use, heat dissipation may not be performed well, and the member may be thermally deformed. In particular, if a magnesium alloy with a low conductivity is used as the magnesium alloy used for the cylinder head of the inner thigh and the cylinder block, the cylinder head is thermally deformed, the heat is accumulated in the cylinder block and the cylinder bore is deformed. Adverse effects such as increased friction and reduced airtightness occur. For this reason, there is a need for a magnesium alloy that has high heat conductivity and that can perform heat dissipation well and is suitable for use at high temperatures.

たとえば、 Mg— 3%Cu— l%Caの合 賊 (単位は 「質量0 /0」 :). をもつ マグネシウム合金の謝云導率は、 云導率の高い Cuが含まれることで、 AZ9 1Dの flf云導率よりも高レ、。 しかしながら、 使用条件によっては高温での耐クリ ープ性などが十分ではなレ、^がある。 For example, Mg- 3% Cu- l% "mass 0/0" if thief (units of Ca :). Xie Unshiruberitsu magnesium alloys with, by including the high Unshiruberitsu Cu, AZ9 Higher than 1D flf conductivity. However, there are some cases where the creep resistance at high temperature is not sufficient depending on the usage conditions.

特開平 6— 25791号公報には、 0. 8〜5質量0 /0のカルシウム (Ca) と、JP-A-6- 25791, 0.8 to 5 mass 0/0 calcium and (Ca),

0〜 10質量0 /0の銅 ( C u ) と、 3〜 8質量0 /0の亜鉛 ( Z n ) と、 を含むマグネ シゥム合金が開示されている。 特開平 6— 25791号公報に記載のマグネシゥ ム合金は、 室温および高温において高い強 を示す力 謝云導率については記載 が無く、 亜鉛の添加がマグネシウム合金の熱伝導性に影響する力 かは不明であ る。 発明の開示 And 0-10 mass 0/0 copper (C u), and 3-8 mass 0/0 of zinc (Z n), the magnetic Shiumu alloy containing disclosed. Magnesium described in JP-A-6-25791 There is no description of the power-conductivity, which shows high strength at room temperature and high temperature, and it is unclear whether the addition of zinc affects the thermal conductivity of magnesium alloys. Disclosure of the invention

本発明は、 上記問題点に鑑み、 高温下での使用に適した鍀造用マグネシウム合 金を することを目的とする。 また、 その^用マグネシウム合金からなる铸 物を ^することを目的とする。  In view of the above problems, an object of the present invention is to provide a magnesium alloy for forging that is suitable for use at high temperatures. It is also intended to produce a ceramic material made of a magnesium alloy.

本発明者らは、 鋭意研究の結果、 マグネシウム合金の合金元素として、 銅と力 ルシゥムとともに錫を添加することで、 マグネシウム合金の ¾i云導性に悪影響を 与えることなく高温における耐クリーブ性を向上させることができることを見出 し、 これに基づき本発明を するに至った。  As a result of diligent research, the present inventors have improved the cleaving resistance at high temperatures without adversely affecting the ¾i conductivity of the magnesium alloy by adding tin as an alloying element of the magnesium alloy together with copper and strength russium. Based on this, the present inventors have reached the present invention.

すなわち、 本発明の 用マグネシウム合金は、 全体を 100質量%としたと きに、 1質量%以上 5質量%以下の銅 (Cu) と、 0. 1質量%以上 5質量%以 下のカノレシゥム (Ca) と、 該 Caに ¾~Τる質量比 (Sn/Ca) で 0. 1以上 3以下の錫 (Sn) と、 を含み、 残部がマグネシウム (Mg) と不可避不純物と からなることを赚とする。  That is, when the total magnesium alloy of the present invention is 100% by mass, 1% by mass to 5% by mass of copper (Cu) and 0.1% by mass or more and 5% by mass or less of canorecium ( (Ca), and a mass ratio (Sn / Ca) from 0.1 to 3 with respect to Ca, and the balance is composed of magnesium (Mg) and inevitable impurities. And

本発明の铸造用マグネシウム合金は、 Cu、 Caおよび Snを含むことにより、 Mg-Cu系化合物とともに Mg— Ca— Sn系化合物の晶出物が、 M g結晶粒 の結晶粒界にネットワーク状 (三次元網目状) に晶出する。 三次元網目構造によ り、 高温になると特に活発になる粒界すべりが抑制され、 高温強度および高温で の耐クリープ性が向上する。 また、 Mg—C a系化合物は比較的脆いが、 Mg— C a系化合物の C Άの一部が Snと置換した Mg— Ca— Sn系化合物は強度が 高いため、 三次元網目構造の強度、 ひいてはマグネシウム合金の 3娘が向上する。 また、 後に詳説するが、 Snは、 C aと優先的に化合物を形成するため、 アル ミニゥム等の他の添加元素に比べて 云導性への影響が少なレ、。  The magnesium alloy for forging of the present invention contains Cu, Ca, and Sn, so that a crystallized product of Mg—Ca—Sn compound together with Mg—Cu compound is network-like (at the grain boundary of Mg crystal grains). Crystallizes in a three-dimensional network. The three-dimensional network structure suppresses intergranular slip, which becomes particularly active at high temperatures, and improves high-temperature strength and creep resistance at high temperatures. In addition, Mg—Ca—S compounds are relatively brittle, but Mg—Ca—Sn compounds in which part of C— of Mg—Ca compounds is replaced with Sn have high strength. As a result, 3 daughters of magnesium alloy improve. As will be explained in detail later, Sn forms a compound preferentially with Ca, so it has less influence on conductivity than other additive elements such as aluminum.

なお、 本明細書において、 「X— Y系化合物」 等の記載は、 たとえば、 組成式 で Χ2Υと示されるような Xと Υとを 分とする化合物である。 In the present specification, the description of “X—Y compound” or the like is, for example, a compound having X and 分 as shown by 示2で in the composition formula.

また、 本発明のマグネシウム合金铸物は、 本発明の «用マグネシウム合金か らなる铸物である。 本発明のマグネシウム合金铸物は、 In addition, the magnesium alloy product of the present invention is a magnesium alloy for use in the present invention. This is a fake. The magnesium alloy porcelain of the present invention is

全体を 1 00質量%としたときに、 1質量%以上 5質量%以下の銅 (Cu) と、 0. 1質量%以上 5質量0 /0以下のカルシウム (C a) と、 該 C aに ¾~Τる質量比When whole was 1 00 wt%, and 1 mass% or more to 5% by weight of copper (Cu), 0. 1 wt% to 5 wt 0/0 following calcium and (C a), to the C a ¾ to mass ratio

(Sn/C a) で 0. 1以上 3以下の錫 (Sn) と、 を含み、 残部がマグネシゥ ム (Mg) と不可避不純物とからなる合金激易を,に注湯する注湯工程と、 該注湯工程後の合金激昜を冷却させて凝固させる凝固工程と、 (Sn / C a) 0.1 to 3 tin (Sn), and a pouring process for pouring an alloy that consists of magnesium (Mg) and unavoidable impurities. A solidification step of cooling and solidifying the molten alloy after the pouring step;

を経て得られることを特徴とする。 図面の簡単な説明  It is obtained through the process. Brief Description of Drawings

図 1は、 合金糸 の異なるマグネシウム合金の熱伝導率を示すグラフである。 図 2は、 合金組成の異なるマグネシウム合金の応力緩和試験における、 試験開 始から 40時間後の応力低下量を示すダラフである。  Fig. 1 is a graph showing the thermal conductivity of magnesium alloys with different alloy yarns. Fig. 2 is a graph showing the amount of stress reduction 40 hours after the start of the test in the stress relaxation test of magnesium alloys with different alloy compositions.

図 3は、 応力緩和難の試験時間に対し、 試験片に付加される圧縮応力を 10 分毎にプロットしたグラフである。  Figure 3 is a graph plotting the compressive stress applied to the specimen every 10 minutes against the test time for stress relaxation difficulty.

図 4 Aおよび図 4 Bは、 Mg— 3質量%Cu— 1質量0 /oC a合金 (#01) の 金属, «を示す図面代用写真である。 FIG. 4A and FIG. 4B are photographs in place of drawings showing the metal «of Mg-3 mass% Cu-1 mass 0 / oCa alloy (# 01).

図 5Aおよび図 5Bは、 Mg— 3質量0 /oCu—l質量0 /oCa— 0. 1質量0 /oS n (# 02) 合金の金属組織を示す図面代用写真である。 FIG. 5A and FIG. 5B are photographs in place of drawings showing the metal structure of the Mg-3 mass 0 / oCu-1 mass 0 / o Ca-0. 1 mass 0 / oS n (# 02) alloy.

図 6 Aおよび図 6 Bは、 Mg— 3質量%C u— 1質量%C a - 1質量%S n Fig. 6 A and Fig. 6 B are Mg-3 mass% Cu 1 mass% Ca-1 mass% Sn

(# 0 3) 合金の金属糸纖を示す図面代用写真である。 (# 0 3) is a drawing-substituting photograph showing a metal yarn cage of an alloy.

図 7 Aおよび図 7 Bは、 M g— 3質量% Cu- 1質量% C a— 2質量% S n (# 04) 合金の金属組織を示す図面代用写真である。  FIG. 7A and FIG. 7B are drawings-substituting photographs showing the metal structure of the Mg—3 mass% Cu—1 mass% Ca—2 mass% Sn (# 04) alloy.

図 8 Aおよび図 8 Bは、 M g— 3質量%< u― 1質量。 /0C a— 4質量% S n (#05) 合金の金属組織を示す図面代用写真である。 発明を実施するための最良の形態 Fig. 8 A and Fig. 8 B are Mg-3 mass% <u-1 mass. FIG. 5 is a drawing-substituting photograph showing the metallographic structure of the / 0 Ca—4 mass% Sn (# 05) alloy. BEST MODE FOR CARRYING OUT THE INVENTION

以下に、 本発明の铸造用マグネシウム合金を実施するための最良の形態を説明 する。  The best mode for carrying out the forging magnesium alloy of the present invention will be described below.

本発明の铸造用マグネシウム合金は、 銅 (Cu) とカルシウム (C a) と錫 (Sn) とを含み、 残部がマグネシウム (Mg) と不可避不純物とからなること を特徴とする。 The magnesium alloy for forging of the present invention comprises copper (Cu), calcium (C a) and tin (Sn), with the balance being magnesium (Mg) and inevitable impurities.

本発明の铸造用マグネシウム合金は、 Cu、 C aおよび Snの含有量を適切な 量とすることで、 M g— C u系ィ匕合物とともに Mg— Ca— Sn系化合物の晶出 物が、 Mg結晶粒の結晶粒界にネットワーク状 (三次元網目状) に晶出する。 不 連続部分の少ないネットワーク状であるため、 粒界すべりの抑制効果が高レ、。  In the magnesium alloy for forging of the present invention, by adjusting the contents of Cu, Ca and Sn to appropriate amounts, the crystallized product of Mg—Ca—Sn compound as well as Mg—Cu—S compound can be obtained. It crystallizes in a network (three-dimensional network) at the grain boundaries of Mg grains. Because it is a network with few discontinuous parts, it has a high effect of suppressing grain boundary sliding.

Cuの含有量は、 用マグネシウム合金全体を 100質量%としたときに、 1質量%以上 5質量。/。以下である。 C uの含有量が 1質量%以上であれば、 結晶 粒界に M g-Cu系化合物が十分に晶出する。 C uの含有量が 1質量。 /0未満では、 Mg-Cu系化合物の結晶粒界への晶出が不十分なため、 強度が低レ、。 好ましレヽ Cuの含有量は、 2質量%以上である。 一方、 Cuが多い程、 結晶粒界に晶出す る M g— C u系化合物の量が過剰となり、 脆レヽ紙織となるため強度は低下する。 好ましい Cuの含有量は、 4質量。 /。以下である。 The Cu content is 1% by mass or more and 5% by mass when the total magnesium alloy is 100% by mass. /. It is as follows. If the Cu content is 1% by mass or more, Mg-Cu compounds will crystallize sufficiently at the grain boundaries. The Cu content is 1 mass. If it is less than 0 , the strength of the Mg-Cu compound is low due to insufficient crystallization at the grain boundaries. The preferred Cu content is 2% by mass or more. On the other hand, as the amount of Cu increases, the amount of Mg-Cu compound that crystallizes at the crystal grain boundary becomes excessive, resulting in a brittle paper weave. The preferred Cu content is 4 mass. /. It is as follows.

本発明の铸造用マグネシウム合金は、 Cuとともに Caおよび Snを含む。 C aおよび Snは、 Cuとともに結晶粒界に して、 三次元網目構造の形成に寄 与する。 具体的には、 Mg— Cu系化合物とともに Mg— Ca— Sn系化合物が 結晶粒界に晶出して、 不連続部分の少なレ、良好な三次元網目構造が形成される。  The magnesium alloy for forging of the present invention contains Ca and Sn together with Cu. Ca and Sn, together with Cu, contribute to the formation of a three-dimensional network structure as a grain boundary. Specifically, the Mg-Ca-Sn compound and the Mg-Cu-Sn compound crystallize at the grain boundary, and a good three-dimensional network structure is formed with few discontinuities.

C aの含有量は、 ¾ 用マグネシウム合金全体を 100質量0 /0としたときに、 0. 1質量%以上 5質量%以下である。 C aの含有量が 0. 1質量%以上であれ ば、 結晶粒界に Mg—C a—Sn系化合物が十分に晶出する。 また、 マグネシゥ ム合金へ C aを添ロするとマグネシウム合金の発火 が上昇するため、 マグネ シゥム合金を激易にしたときに発生することがある燃焼が防止される。 好ましレ、 C aの含有量は、 0. 5質量。 /。以上である。 一方、 C aの含有割合が 5質量%を 超えると、 粒界晶出物の生成量が多くなりすぎて、 引張強度や伸びなどの機械的 性質が低下し、 後加工で問題を生じることがある。 好ましい Caの含有量は、 3 質量%以下さらには 2質量%以下である。 The content of C a, upon the entire ¾ for magnesium alloy is 100 mass 0/0, not more than 1 mass% to 5 mass% 0.5. If the content of C a is 0.1% by mass or more, the Mg—C a—Sn compound is sufficiently crystallized at the grain boundary. In addition, adding Ca to the magnesium alloy increases the ignition of the magnesium alloy, preventing combustion that may occur when the magnesium alloy is made intense. Preferred content of Ca is 0.5 mass. /. That's it. On the other hand, when the Ca content exceeds 5% by mass, the amount of grain boundary crystallized products increases, and mechanical properties such as tensile strength and elongation decrease, resulting in problems in post-processing. is there. A preferable Ca content is 3% by mass or less, and further 2% by mass or less.

Snの含有量は、 カルシウム (Ca) に対する質量比 (Sn/Ca) で 0. 1 以上 3以下である。 Snの含有量が 0. 1質量%以上であれば、 結晶粒界に Mg The Sn content is 0.1 to 3 in terms of mass ratio (Sn / Ca) to calcium (Ca). If the Sn content is 0.1 mass% or more, Mg

-Ca-Sn系化合物が十分に晶出する。 一方、 S nの含有割合が多くなると、 Mg-Ca-S n系化合物が三次元網目構造から分力れて結晶粒内に'も晶出する ようになり、 良好な三次元網目構造が形成され難ぐなる。 その結果、 耐クリープ 性が低下する傾向にある。 また、 余剰に Snを添 卩した:^には、 Mg— Ca— Sn系化合物だけでなく、 Mg— Sn系化合物を生じる。 Mg— Sn系化合物は、 低融点の化合物であるため、 耐クリープ性を 匕させる。 そのため、 Snの含有 量は、 SnZCaで 3以下とする。 S nZC aが 3以下であれば、 低融点化合物 の形成が抑制される。 さらに、 SnZCaが 2以下であれば、 不連^分が少な く良好な三次元網目構造が形成されて高温弓娘や高温での耐クリープ性が向上す る。 すなわち、 好ましい Snの含有量は、 311 〇&で2以下さらには1. 5以 下である。 The -Ca-Sn compound is sufficiently crystallized. On the other hand, when the content ratio of Sn increases, The Mg-Ca-Sn compound is divided from the three-dimensional network structure and crystallizes in the crystal grains, making it difficult to form a good three-dimensional network structure. As a result, the creep resistance tends to decrease. In addition, when Sn is added excessively, ^ produces not only Mg—Ca—Sn compounds but also Mg—Sn compounds. Mg-Sn compounds are low melting point compounds, and therefore creep resistance is improved. Therefore, the Sn content is 3 or less with SnZCa. If SnZCa is 3 or less, formation of a low melting point compound is suppressed. Further, if SnZCa is 2 or less, a good three-dimensional network structure with little discontinuity is formed, and the high-temperature bow daughter and the creep resistance at high temperature are improved. That is, the preferred Sn content is 311 O &, 2 or less, and 1.5 or less.

なお、 Snは、 Mgや Cuよりも C aと優先的に化合物を作る。 そのため、 熱 伝導率が高い C uや Mg— C u系化合物に悪影響を与えることがなく、 その結果、 マグネシウム合金の 云導性が低下し難くなると考えられる。 このことから、 M g-C a -S n系化合物の S nZC aの化学量論比から考えて、 S nの C aに対 する質量比 (Sn/Ca) を 3以下さらには 0. 1以上 2以下とするのが好まし く、 Mg—Cu系化合物と化合物を形成する Snはほとんどなく、 前述の低融点 化合物の晶出も抑制される。  Sn forms a compound with Ca preferentially over Mg and Cu. Therefore, Cu and Mg-Cu compounds with high thermal conductivity are not adversely affected, and as a result, the conductivity of the magnesium alloy is unlikely to decrease. From this, considering the stoichiometric ratio of SnZCa of MgCa-Sn compounds, the mass ratio of Sn to Ca (Sn / Ca) is 3 or less, or 0.1 or more 2 The following is preferable, and there is almost no Sn that forms a compound with an Mg—Cu compound, and crystallization of the low melting point compound described above is also suppressed.

以上説明した本発明の^ t用マグネシウム合金は、 宇宙、 航空の分野をはじめ とし、 自動車、 電^^など、 各種分野で用いることができる。 また、 本発明の 铸造用マグネシウム合金からなる部材としては、 その高温での特性を生かして、 高温環境下で使用される製品、 たとえば、 使用中に高温となるコンプレッサー、 ポンプ類、 各種ケース類を構成する部品、 また、 高温および高負荷の下で用いら れるエンジン部品、 特に、 内燃機関のシリンダヘッド、 シリンダブロックやオイ ルバン、 内燃機関のターボチャージヤー用インペラ、 自動車等に用いられるトラ ンスミツションケース等が挙げられる。  The magnesium alloy for t according to the present invention described above can be used in various fields such as automobiles and electric power as well as space and aviation. In addition, as a member made of a magnesium alloy for forging according to the present invention, a product used under a high temperature environment, for example, a compressor, a pump, various cases, etc. Components used and engine parts used under high temperature and high load, especially cylinder heads, cylinder blocks and oil vans for internal combustion engines, turbocharger impellers for internal combustion engines, and transmitters used for automobiles, etc. Case.

また、 本発明のマグネシウム合金錄物は、 以上詳説した本発明の铸造用マグネ シゥム合金からなる铸物である。 すなわち、 本発明のマグネシウム合金铸物は注 湯工程と凝固工程とを経て得られる,であって、 注湯工程は、 全体を 100質 量%としたときに、 1質量%以上 5質量。 /0以下の銅 (Cu) と、 0. 1質量0 /0以 上 5質量0 /0以下のカルシウム (Ca) と、 該 C aに対する質量比 (Sn/Ca) で 0. 1以上 3以下の錫 (Sn) と、 を含み、 残部がマグネシウム (Mg) と不 可避不純物とからなる合金溶湯を,に注湯する工程、 凝固工程は、 注湯工程後 の合金激昜を冷却させて凝固させる工程、 である。 The magnesium alloy ceramic of the present invention is a ceramic made of the magnesium alloy for forging according to the present invention described in detail above. That is, the magnesium alloy case of the present invention is obtained through a pouring step and a solidification step, and the pouring step is 1% by mass or more and 5% by mass when the whole is 100% by mass. / 0 and less copper (Cu), 0. 1 mass 0/0 or more The upper 5 mass 0/0 following calcium (Ca), weight ratio of the C a and (Sn / Ca) in 0.1 to 3 of tin (Sn), wherein the balance magnesium (Mg) not The process of pouring molten alloy composed of unavoidable impurities into the molten metal and the solidification process are processes of cooling and solidifying the alloy after the pouring process.

本発明のマグネシウム合^ は、 通常の重力^^加圧铸造に限らず、 ダイ カスト錶造したものでもよい。 また、 髓に使用される羅も砂型、 金型等を問 わない。 凝固工程における凝固速度 (冷却速度) にも特に限定はなく、 三次元網 目構造が形成される程度の凝固速度を铸塊のサイズに応じて適宜選択すればょレ、。 なお、 一般的な凝固 で凝固させれば、 ネットワーク状の金属糸纖が得られる。 また、 本発明の,用マグネシウム合金およびマグネシウム合^^物は、 铸放 し材であるのが望ましい。 さらに、 後に熱処理することにより、 ,の特性 を向上させてもよレ、。  The magnesium alloy of the present invention is not limited to normal gravity pressure fabrication, but may be die cast fabrication. In addition, the sand mold, mold, etc. used for dredging can be used. There is no particular limitation on the solidification rate (cooling rate) in the solidification process, and the solidification rate to the extent that a three-dimensional network structure is formed can be selected as appropriate according to the size of the clot. If solidified by general solidification, a network-like metal string is obtained. In addition, the magnesium alloy and the magnesium compound for use in the present invention are preferably free materials. Furthermore, the characteristics of, may be improved by heat treatment later.

以上、 本発明の铸造用マグネシゥム合金およびマグネシゥム合^物の実施形 態を説明したが、 本発明は、 上記実施形態に限定されるものではない。 本発明の 要旨を逸脱しない範囲において、 当業者が行い得る変更、 改良等を施した種々の 形態にて実施することができる。  As described above, the embodiment of the forging magnesium alloy and the magnesium compound of the present invention has been described, but the present invention is not limited to the above embodiment. The present invention can be implemented in various forms that have been changed or improved by those skilled in the art without departing from the scope of the present invention.

以下に実施例を挙げて、 本発明を具体的に説明する。  Hereinafter, the present invention will be specifically described with reference to examples.

マグネシウム合金中の合金元素の含有量を変更した試験片を複数製作し、 それ らの特'性の評価およ 属 の観察を行つた。  Several specimens with different alloy element contents in the magnesium alloy were manufactured, and their characteristics were evaluated and their properties were observed.

[試験片 #01〜#05の細  [Specimens # 01 ~ # 05

電気炉中で予熱した るつぼの内面に塩化物系のフラックスを塗布し、 その 中に枰量した純マグネシゥム地金、 純 C uおよび必要に応じて純 S nを投入して 溶解した。 さらに、 750°Cに保持したこの溶湯中に秤量した C aを添加した 纖調製工程) o  Chloride flux was applied to the inner surface of a crucible preheated in an electric furnace, and a large amount of pure magnesium ingot, pure Cu, and pure Sn as required were dissolved. Furthermore, weighed Ca was added to this molten metal kept at 750 ° C.

この激昜を十分に攪拌し、 原料を完全に溶解させた後、 同 でしばらく沈静 保持した。 こうして得た各種の合金溶湯を所定の形状の金型に流し込み (注湯ェ 程) 、 大気雰囲気中で凝固させて (凝固工程) 、 #01〜#05の試験片 (マグ ネシゥム合金铸物) を铸造した。 なお、 得られた試験片は、 30mmX 30m mX 200 mmであった。 各試験片の化学組成を表 1に示す。 云導率の測定] The agitation was sufficiently stirred to completely dissolve the raw materials, and then kept calm for a while. The various molten alloys obtained in this way were poured into molds of a predetermined shape (the pouring process) and solidified in the atmosphere (solidification process). Forged. The obtained test piece was 30 mm × 30 mm × 200 mm. Table 1 shows the chemical composition of each specimen. Measurement of conductivity]

上記の手順で作製した # 01〜# 05の試験片に加え、 市販の AZ 91 D (組 成は表 1に記載) カゝら作製した同様の 片について、 レーザーフラッシュ法に より熱伝導率を求めた。 試験結果を表 1およぴ図 1に示す。  In addition to the # 01 to # 05 test pieces prepared in the above procedure, the commercially available AZ 91 D (composition is shown in Table 1). Asked. The test results are shown in Table 1 and Fig. 1.

[応力緩和試験]  [Stress relaxation test]

表 1に示した ,片 #01〜#05および AZ 91Dから «した試験片につ いて、 応力緩和 を行レ、、 マグネシウム合金の耐クリープ性を調べた。 応力緩 和試験は、 試験片に試験時間中、 所定の変形量まで荷重を加えたときの応力が、 時間とともに減少する過程を測定する。 具体的には、 200°Cの大気雰囲気中に おいて、 纖片に 10 OMP aの圧縮応力を負荷し、 そのときの纖片の変位が 一定に保たれるように、 時間の経過に併せてその圧縮応力を低下させていった。 試験開始から 40時間後の応力低下量を、 表 1および図 2に示す。 また、 片 に付加される圧縮応力を 10分毎にプロッ卜して作成したグラフを図 3に示す。  For the specimens # 01 to # 05 and AZ91D shown in Table 1, stress relaxation was performed and the creep resistance of the magnesium alloy was examined. The stress relaxation test measures the process by which the stress when a load is applied to a specified amount of deformation during the test time decreases with time. Specifically, in an air atmosphere at 200 ° C, a compressive stress of 10 OMPa was applied to the piece, and the displacement of the piece at that time was kept constant so as to keep constant. The compressive stress was reduced. Table 1 and Fig. 2 show the amount of stress reduction 40 hours after the start of the test. Figure 3 shows a graph created by plotting the compressive stress applied to the piece every 10 minutes.

[金属繊の観察]  [Observation of metal fibers]

表 1に示した試験片 # 01〜 # 05の表面を観察した。 表面観察は、 各試験片 から切り出された断面を金属顕^^で観察して行った。 #01〜#05の表面の 金属糸赚を、 それぞれ図 4 A〜図 8 Aおよび図 4 B〜図 8 Bに示す力 各図にお いて、 図 4 A〜図 8 Aは (a) 低倍率、 図 4B〜図 8Bは (b) 高倍率で同じ断 面を観察した。  The surfaces of test pieces # 01 to # 05 shown in Table 1 were observed. The surface was observed by observing the cross section cut out from each specimen with a metal microscope. The forces shown in Fig. 4A to Fig. 8A and Fig. 4B to Fig. 8B, respectively, on the surface of # 01 to # 05 are shown in Fig. 4A to Fig. 8B. Magnification, Figures 4B-8B (b) The same section was observed at high magnification.

試験片 #01では、 図 4Aからわかるように、 結晶粒界に金属間化合物が晶出 してなる三次元網目構造力 ¾ί ^された。 また、 図 4 Βにおいて、 結晶粒界で明る く見えるのは CuMg 2であり、 喑く見えるのは Mg2C aであることを EPMIn test piece # 01, as can be seen from FIG. 4A, a three-dimensional network structure strength formed by crystallization of an intermetallic compound at the grain boundary was obtained. In Fig. 4 (b), it is CuMg 2 that appears bright at the grain boundary, and Mg 2 C a that appears bright.

A (エレク トロンプローブマイクロアナライザ) および XRD (X線回折) によ り確認した。 また、 片 #02および #03では、 図 5Aおよび図 6Aからわ かるように、 #01よりも網目が細かく連緣性の高い三次元網目構造が^:され た。 また、 図 5 Bおよび図 6 Bにおいて、 結晶粒界で明るく見えるのは CuMgThis was confirmed by A (electron probe microanalyzer) and XRD (X-ray diffraction). In addition, as shown in Figs. 5A and 6A, the pieces # 02 and # 03 have a three-dimensional network structure with finer and more connected mesh than # 01. In Fig. 5B and Fig. 6B, CuMg appears bright at the grain boundaries.

2であり、 喑く見えるのは Mg2Caおよひ TVIgCa Snであることを EPMA および XRDにより確認した。 一方、 試験片 #04および #05では、 図 7A、 図 7Bおよび図 8A、 図 8Bの各図からわかるように、 晶出物が結晶粒の内部に も晶出したことで、 三次元網目構造が完全に形成されなかった。 ここで、 図 7B および図 8 Bに、 粒界およひ立内に晶出した晶出物を少なくとも一力所、 矢印で 示す。 図 7 Bおよび図 8 Bにおいて、 Gaは粒内晶出物、 G bは粒界晶出物であ る。 粒内に晶出するのは MgC a Snであることを EPMAおよび XRDにより 確認した。 さらに、 試験片 #05では、 低融点化合物である Mg2Snが XRD により検出された。 2, look喑Ku was confirmed by EPMA and XRD to be a Mg 2 Ca Oyohi TVIgCa Sn. On the other hand, in specimens # 04 and # 05, as can be seen from each of FIGS. 7A, 7B, 8A, and 8B, the crystallized material is inside the crystal grains. As a result of crystallization, a three-dimensional network structure was not completely formed. Here, in FIG. 7B and FIG. 8B, the crystallized material crystallized in the grain boundary and in the vertical axis is indicated by arrows at least one place. In FIG. 7B and FIG. 8B, Ga is an intragranular crystallized product and Gb is a grain boundary crystallized product. EPMA and XRD confirmed that MgC a Sn crystallized in the grains. In addition, in specimen # 05, Mg 2 Sn, a low melting point compound, was detected by XRD.

[表 1]  [table 1]

Figure imgf000010_0001
Figure imgf000010_0001

# 01〜: ίί 05の試験片は、 レ、ずれも A Ζ 91 Dよりも 云導性に優れた。 S nを含まない # 01の試験片の熱伝導率は 155 WZmKであったが、 # 02〜 #04の試験片では、 Snの添加による !rf云導性の低下は見られなかった。 一方、 S nの含有量が過剰である #05では、 A Z 91 Dよりも謝云導性に優れるもの の、 # 01との 云導率の差が大きかった。  # 01〜: The test piece of ίί05 was superior in terms of convection and deviation than A Ζ 91 D. The thermal conductivity of the # 01 test piece not containing Sn was 155 WZmK, but no decrease in! Rf conductivity due to the addition of Sn was observed in the # 02 to # 04 test pieces. On the other hand, in # 05 where the Sn content is excessive, although the excellence is superior to A Z 91 D, the difference in the inductivity from # 01 is large.

また、 Snを含むマグネシウム合金からなる #02〜#04の試験片は、 20 0°Cでの応力緩和試験における纖開始から 40Bき間後の応力低下量が、 試験片 #01よりも少なかった。 すなわち、 Mg— Cu— Ca合金 (#01) に Snを 添加することで、 高温における耐クリープ性が向上した。 これは、 三次元網目構 造に不連続な部分が多い #01にくらべ、 #02〜# 04のほうが連^ 14の高い 三次元網目構造を有するからであると推測される。 一方で、 Snを 2質量。 /o含む #04では、 S nを含まない # 01よりは 40時間後の耐クリープ性に優れるも のの、 # 02および # 03には劣った。 #04の金属組織が、 三次元網目構造が #02や #03よりも不完全であったためだと考えられる。 S nを 4質量%含む # 05は、 三次元網目構造が不完全であり、 低融点化合物である M g 2 S nを含 むため、 耐クリープ性が駒匕したと考えられる。 In addition, the # 02 to # 04 specimens made of magnesium alloy containing Sn had less stress reduction than the specimen # 01 after 40B clearance from the start of wrinkle in the stress relaxation test at 200 ° C. . In other words, the addition of Sn to the Mg-Cu-Ca alloy (# 01) improved the creep resistance at high temperatures. This is presumed to be because # 02 to # 04 have a higher 3D network structure than # 01, which has many discontinuous parts in the 3D network structure. Meanwhile, 2 masses of Sn. # 04 with / o has better creep resistance after 40 hours than # 01 without Sn, but inferior to # 02 and # 03. The metal structure of # 04 is thought to be because the three-dimensional network structure was incompleter than # 02 and # 03. Contains 4% by mass of Sn # 05, three-dimensional network structure is incomplete, it is contemplated that M g 2 S n which is a low melting compound containing Mutame, creep resistance was Koma匕.

さらに、 # 02および # 03の,片は、 ,開始後約 3時間後の応力低下量 が #01よりも多いが、 3〜40時間までの応力の変化量は小さく、 安定してい た。 また、 #04の試験片は、 試験開始後約 3時間後の応力低下量が #01や A Z9 IDよりも多いが、 3〜40時間までの応力の変ィ匕量は小さく、 安定してい た。 (図 3)  In addition, the # 02 and # 03 pieces had a greater stress drop than # 01 about 3 hours after starting, but the change in stress from 3 to 40 hours was small and stable. In addition, the # 04 specimen has a greater stress drop than # 01 and A Z9 ID about 3 hours after the start of the test, but the amount of stress change from 3 to 40 hours is small and stable. It was. (Figure 3)

なお、 上記の各纖片は、 (:11を3質量%、 C aを 1質量%で一定とした。 い ずれの試験片においても、 Cuであれば 2. 7質量。/。以上 3. 3質量%以下、 C aであれば 0. 7質量%以上 1. 3質量%以下の範囲で、 上記の各,片と同程 度の 云導率およひ面クリープ性を示す。  In addition, each of the above-mentioned pieces has a constant (: 11 is 3% by mass and Ca is 1% by mass. In any of the test pieces, Cu is 2.7%. /. If it is 3 mass% or less, and Ca is 0.7 mass% or more and 1.3 mass% or less, it exhibits the same conductivity and surface creep properties as the above-mentioned pieces.

すなわち、 適切な含有量の C u、 C aおよび S nを含むマグネシウム合金は、 Snの添加による 云導性の低下がみられず、 高温における耐クリープ性に優れ る。  That is, a magnesium alloy containing Cu, Ca and Sn with appropriate contents shows no deterioration in conductivity due to the addition of Sn, and is excellent in creep resistance at high temperatures.

Claims

請求の範囲 The scope of the claims 1. 全体を 100質量%としたときに、 1質量%以上 5質量%以下の銅 (C u) と、 0. 1質量0 /o以上 5質量%以下のカルシウム (Ca) と、 該 Caに る質量比 (Sn/Ca) で 0. 1以上 3以下の錫 (Sn) と、 を含み、 残部がマ グネシゥム (Mg) と不可避不純物とからなることを とする^ t用マグネシ ゥム合金。 1. When the total is 100 mass%, 1 mass% to 5 mass% of copper (Cu), 0.1 mass 0 / o to 5 mass% of calcium (Ca), and the Ca A magnesium alloy for ^ t, which contains tin (Sn) with a mass ratio (Sn / Ca) of 0.1 or more and 3 or less, with the balance being magnesium (Mg) and inevitable impurities. 2. 前記銅 (Cu) は、 2質量%以上 4質量%以下である請求の範囲第 1項記 載の^ t用マグネシウム合金。  2. The magnesium alloy for t according to claim 1, wherein the copper (Cu) is 2% by mass or more and 4% by mass or less. 3. 前記カルシウム (Ca) は、 0. 5質量0 /0以上 3質量0 /0以下である請求の 範囲第 1項記載の铸造用マグネシウム合金。 3. The calcium (Ca) is 0.5 mass 0/0 to 3 mass 0/0 less is claims铸造for magnesium alloy as set forth in claim 1, wherein. 4. 前記錫 (Sn) は、 前記カルシウム (Ca) に対する質量比 (SnZC a) で 0. 1以上 2以下である請求の範囲第 1項記載の铸造用マグネシウム合金。 4. The magnesium alloy for forging according to claim 1, wherein the tin (Sn) has a mass ratio (SnZC a) to the calcium (Ca) of 0.1 or more and 2 or less. 5. Mg-Cu系化合物お O^Mg—Ca— Sn系化合物が M g結晶粒の結晶 粒界にネットワーク状に晶出した組織をもつ請求の範囲第 1項記載の铸造用マグ ネシゥム合金。 5. The magnesium alloy for fabrication according to claim 1, wherein the Mg—Cu compound and the O ^ Mg—Ca—Sn compound have a structure crystallized in a network form at the grain boundary of the Mg crystal grains. 6. 全体を 100質量%としたときに、 1質量%以上 5質量%以下の銅 (C u) と、 0. 1質量0 /o以上 5質量0 /0以下のカルシウム (Ca) と、 該 Caに ¾~Τ る質量比 (Sn/Ca) で 0. 1以上 3以下の錫 (Sn) と、 を含み、 残部がマ グネシゥム (Mg) と不可避不純物とからなる合金激昜を に注湯する注湯ェ 程と、 6. When the entirety is taken as 100 mass%, 1 mass% to 5 mass% of copper (C u), 0. 1 mass 0 / o or 5 mass 0/0 following calcium and (Ca), the Pouring a hot metal alloy containing tin (Sn) with a mass ratio (Sn / Ca) of 0.1 to 3 in Ca, and the balance of magnesium (Mg) and inevitable impurities. The pouring hot water 該注湯工程後の合金激昜を冷却させて凝固させる凝固工程と、  A solidification step of cooling and solidifying the molten alloy after the pouring step; を経て得られることを特徴とするマグネシゥム合^ ¾ Magnesium combination characterized by being obtained through ^ ¾ 7. Mg-Cu系化合物および Mg— Ca— Sn系化合物が M g結晶粒の結晶 粒界にネットワーク状に晶出した組織をもつ請求の範囲第 6項記載のマグネシゥ ム合^ ¾  7. The magnesium compound according to claim 6, wherein the Mg—Cu compound and the Mg—Ca—Sn compound have a network crystallized structure at the grain boundaries of the Mg crystal grains.
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