EP2706127A1 - Élément en alliage de magnésium complexe et son procédé de production - Google Patents

Élément en alliage de magnésium complexe et son procédé de production Download PDF

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Publication number
EP2706127A1
EP2706127A1 EP13183125.7A EP13183125A EP2706127A1 EP 2706127 A1 EP2706127 A1 EP 2706127A1 EP 13183125 A EP13183125 A EP 13183125A EP 2706127 A1 EP2706127 A1 EP 2706127A1
Authority
EP
European Patent Office
Prior art keywords
alloy
magnesium alloy
cast
complex
alloy composition
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
EP13183125.7A
Other languages
German (de)
English (en)
Other versions
EP2706127B1 (fr
Inventor
Hiroyuki Kawabata
Hajime Kato
Yasushi Iwata
Isamu Ueda
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.)
Toyota Central R&D Labs Inc
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Toyota Central R&D Labs Inc
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Publication date
Application filed by Toyota Central R&D Labs Inc filed Critical Toyota Central R&D Labs Inc
Publication of EP2706127A1 publication Critical patent/EP2706127A1/fr
Application granted granted Critical
Publication of EP2706127B1 publication Critical patent/EP2706127B1/fr
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/06Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of magnesium or alloys based thereon
    • 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
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • C22C23/02Alloys based on magnesium with aluminium as the next major constituent

Definitions

  • the present invention relates to a complex magnesium alloy member configured such that magnesium alloys having different alloy compositions are merged into one another, and a method for producing the same.
  • Magnesium (Mg) is the most lightweight metal among practical metals and has a high specific strength, and resources of magnesium are rich. In recent years where weight saving and reduction of environmental burdens etc. are strongly needed, magnesium is a promising metal material, and magnesium alloys have been being used for various products.
  • Magnesium alloys have different characteristics depending on their alloy compositions, so that an appropriate alloy composition for each product has been selected.
  • the conventional magnesium alloy product may have been such that the whole is formed of the same alloy composition, or may have been a cast member (complex member) in which the magnesium alloy is cast with a heterogeneous member (cast-in material) such as formed of steel material to a site where a certain strength and/or stiffness are required.
  • a cast member complex member
  • a heterogeneous member such as formed of steel material to a site where a certain strength and/or stiffness are required.
  • relevant descriptions are disclosed in Patent Literature below, for example.
  • the conventional cast member as disclosed in Patent Literature 1 may readily cause delamination or other troubles at the bonded interface between the cast-in material (steel material) and the cast material (magnesium alloy), and cannot be used for a product that requires hermetic properties, such as liquid-tightness and gas-tightness.
  • production cost of the cast member becomes high because the cast-in material may have to be preliminarily formed thereon with retaining grooves or other appropriate means by machining process.
  • the present invention has been created in view of such circumstances, and objects of the present invention include providing a complex magnesium alloy member in which, different from the conventional cast member and other members, magnesium alloys having different alloy compositions are integrated with one another, and also providing a method for producing the same.
  • a complex member can be obtained in which an appropriate magnesium alloy can be located at an appropriate location and which can enhance the mechanical characteristics and other properties as well as reduce the raw material cost, and further improve the productivity, such as casting ability.
  • the complex member according to the present invention may be such that the whole is formed of magnesium alloys, thereby not impairing the lightweight property, and necessary treatment such as heat treatment and machining process can be conducted like in the prior art, and recyclability etc. may be sufficient when discarded.
  • the boundary portion according to the present invention between the abutting first portion and second portion is a portion in which the first magnesium alloy that constitutes the first portion and the second magnesium alloy that constitutes the second portion are merged into each other, and thus different from a bonded portion such as caused by pressure bonding and adhesion.
  • the boundary portion comprises the intermediate magnesium alloy having the intermediate alloy composition between the first magnesium alloy (first alloy composition) and the second magnesium alloy (second alloy composition).
  • This intermediate magnesium alloy is in general such that the alloy composition varies continuously or gradually along from the first magnesium alloy to the second magnesium alloy.
  • the boundary portion according to the present invention does not comprise a sharply-defined interface at which the alloy composition and the structure etc. rapidly vary.
  • the boundary portion is configured of a boundary region (the width may be about several to several tens micro meters) in which the alloy composition varies relatively gently between the abutting magnesium alloys.
  • a boundary region the width may be about several to several tens micro meters
  • the alloy composition varies relatively gently between the abutting magnesium alloys.
  • the complex member according to the present invention is configured such that magnesium alloys having different alloy compositions are continuously integrated as if they act as one magnesium alloy bulk. Therefore, unlike in the conventional cast member, troubles such as delamination and liquid-leakage may not occur at the boundary portion.
  • both sides of the boundary portion are provided with the same kind of metal (magnesium alloys), so that any intermetallic compound or the like (crystallized substance or precipitated substance), which is likely to be formed between dissimilar metals in general, may not be formed in the boundary portion, and the boundary portion can thus be prevented from being fracture origin.
  • the first portion and the second portion according to the present invention merge into each other in the boundary portion thereby to enhance the heat conductivity and the electrical conductivity etc. between the first portion and the second portion.
  • the form of the cast-in material, the shape of the cavity, the casting conditions and other factors in the production method of the present invention may not be limited.
  • at least a part of the cast-in material may be heated before the pouring step thereby to adjust the form of the bonded portion (boundary portion) formed between the cast-in material and the cast material.
  • the complex magnesium alloy member obtained after the solidification step may additionally be subjected to at least one subsequent step, such as heat treatment or plastic working.
  • the first alloy composition is not limited, but may preferably comprise, when the whole thereof is assumed to be 100 mass% (referred simply to as "%"), Al: 5-18%, Ca: 1-12%, and the balance: Mg and modifying elements or inevitable impurities, for example.
  • the magnesium alloy having this alloy composition may develop excellent heat resistance due to Ca even without using expensive rare elements and cause the liquidus temperature (TL1) to be relatively low.
  • the liquidus temperature may be 530 to 600 degrees C depending on the alloy composition.
  • the second alloy composition may preferably comprise, when the whole thereof is assumed to be 100%, Al: 2.5-15% and the balance: Mg and modifying elements or inevitable impurities.
  • the magnesium alloy having this alloy composition may have versatility and excellent casting ability and allow magnesium alloy products to be produced efficiently at low cost by die-casting etc.
  • the liquidus temperature (TL2) is relatively high, and may be 580 to 640 degrees C depending on the alloy composition.
  • the complex member according to the present invention may be suitable as a member in which various sites require different characteristics. Examples of such a member include various cases and containers in which only the site to be connected with another member requires heat resistance and/or strength.
  • samples were prepared as a plurality of complex members each produced by casting, with a cast-in material comprising its respective alloy composition (first alloy composition), a cast material comprising an alloy composition (second alloy composition) different from the first alloy composition.
  • the cast-in material is a cylindrical solid piece (diameter: 20 mm, height: 10 mm) cut out from an ingot obtained by gravity casting using a boat-shaped steel mold.
  • commercially available alloy or pure metal was used as a raw material. The same applies to the cast material that will be described later.
  • Symbols shown in columns of alloy compositions in Table 1 comply with ASTM standard or JIS which represents each alloy composition.
  • the above cylindrical solid piece was set at the center area of a die-casting mold having a cavity with cylindrical shape (diameter: 50 mm, height: 30 mm) (locating step).
  • Each molten alloy for the cast material as shown in Table 1 was poured into the cavity at the molten alloy temperature shown in the table (pouring step). Thereafter, the mold was cooled to solidify the cast material, and a complex member was obtained to be cast therein with the cylindrical solid piece (solidification step).
  • This operation was conducted under die-casting conditions of the injection speed: 0.4 m/s and the injection pressure: 64 MPa.
  • Fig. 1A to Fig. 1C are photographs each showing the metallographic structure of the bonded portion between the cast-in material and the cast material obtained in such a manner. Note that the metallographic structure of Sample 2 was substantially the same form as that of Sample 1 ( Fig. 1A ).
  • Fig. 1C shows that, even in the case where the liquidus temperature of the cast-in material is lower than that of the cast material, if they have different main components (types of basis), then any bonded portion (boundary portion) as shown in Fig. 1A cannot be obtained. It has further been found that a boundary layer comprising an intermetallic compound (Al-Mg compound) based on those main components appears in the bonded portion between the cast-in material and the cast material. Such a boundary layer may cause deterioration in strength of the complex member.
  • Al-Mg compound an intermetallic compound

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Forging (AREA)
  • Continuous Casting (AREA)
EP13183125.7A 2012-09-05 2013-09-05 Élément en alliage de magnésium complexe et son procédé de production Not-in-force EP2706127B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2012194953A JP5700005B2 (ja) 2012-09-05 2012-09-05 複合マグネシウム合金部材およびその製造方法

Publications (2)

Publication Number Publication Date
EP2706127A1 true EP2706127A1 (fr) 2014-03-12
EP2706127B1 EP2706127B1 (fr) 2014-12-24

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EP13183125.7A Not-in-force EP2706127B1 (fr) 2012-09-05 2013-09-05 Élément en alliage de magnésium complexe et son procédé de production

Country Status (2)

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EP (1) EP2706127B1 (fr)
JP (1) JP5700005B2 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113999999A (zh) * 2021-10-29 2022-02-01 华中科技大学 稀土增强固液复合铸造镁/铝双金属的制备方法及产品

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2021157748A1 (fr) * 2020-02-07 2021-08-12 国立大学法人 熊本大学 Alliage de magnésium et procédé de production associé

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09183379A (ja) 1995-12-29 1997-07-15 Tokyo Seat Kk ステアリングホイールダイカスト芯金のインサートボス
EP0799901A1 (fr) * 1996-04-04 1997-10-08 Mazda Motor Corporation Alliage à base de magnesium résistant à la chaleur
EP2631312A1 (fr) * 2010-10-29 2013-08-28 Sanden Corporation Élément en alliage de magnésium, compresseur destiné à être utilisé dans un conditionneur d'air et procédé de fabrication d'un élément en alliage de magnésium

Family Cites Families (14)

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Publication number Priority date Publication date Assignee Title
JPS60257947A (ja) * 1984-06-04 1985-12-19 Kawasaki Steel Corp クラツド鋳塊の製造方法
JPH08300137A (ja) * 1995-05-01 1996-11-19 Suzuki Motor Corp 複合部材の製造方法
JP3663867B2 (ja) * 1997-12-24 2005-06-22 いすゞ自動車株式会社 鋳ぐるみ鋳造方法
JP3233095B2 (ja) * 1998-03-25 2001-11-26 日本軽金属株式会社 アルミ鋳ぐるみ製品の製造方法
JP2001205419A (ja) * 2000-01-24 2001-07-31 Matsushita Electric Ind Co Ltd マグネシウム合金の射出成形方法およびそれによって得られた成形品
JP3849092B2 (ja) * 2001-03-13 2006-11-22 古河スカイ株式会社 アルミニウム合金クラッド材の製造方法
JP3861720B2 (ja) * 2002-03-12 2006-12-20 Tkj株式会社 マグネシウム合金の成形方法
JP2004223532A (ja) * 2003-01-21 2004-08-12 Aisin Takaoka Ltd 複合鋳造品及びその製造方法
JP4575645B2 (ja) * 2003-01-31 2010-11-04 株式会社豊田自動織機 鋳造用耐熱マグネシウム合金および耐熱マグネシウム合金鋳物
JP2005177834A (ja) * 2003-12-22 2005-07-07 Toyota Industries Corp ダイカスト方法
KR101374657B1 (ko) * 2006-03-30 2014-03-17 젯트에프 프리드리히스하펜 아게 다층구조의 이중 재질 물품을 제조하는 방법
JP2008212981A (ja) * 2007-03-05 2008-09-18 Nippon Kinzoku Co Ltd マグネシウム及びマグネシウム合金構造体及びその製造方法
JP4972021B2 (ja) * 2008-03-26 2012-07-11 ジヤトコ株式会社 鋳ぐるみ品の製造方法
JP2009248132A (ja) * 2008-04-07 2009-10-29 Toyota Motor Corp 鋳包み鋳造方法

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09183379A (ja) 1995-12-29 1997-07-15 Tokyo Seat Kk ステアリングホイールダイカスト芯金のインサートボス
EP0799901A1 (fr) * 1996-04-04 1997-10-08 Mazda Motor Corporation Alliage à base de magnesium résistant à la chaleur
EP2631312A1 (fr) * 2010-10-29 2013-08-28 Sanden Corporation Élément en alliage de magnésium, compresseur destiné à être utilisé dans un conditionneur d'air et procédé de fabrication d'un élément en alliage de magnésium

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113999999A (zh) * 2021-10-29 2022-02-01 华中科技大学 稀土增强固液复合铸造镁/铝双金属的制备方法及产品

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Publication number Publication date
JP2014051688A (ja) 2014-03-20
JP5700005B2 (ja) 2015-04-15
EP2706127B1 (fr) 2014-12-24

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