WO2005028691A1 - Heat resistant magnesium die casting alloys - Google Patents

Heat resistant magnesium die casting alloys Download PDF

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Publication number
WO2005028691A1
WO2005028691A1 PCT/JP2004/013974 JP2004013974W WO2005028691A1 WO 2005028691 A1 WO2005028691 A1 WO 2005028691A1 JP 2004013974 W JP2004013974 W JP 2004013974W WO 2005028691 A1 WO2005028691 A1 WO 2005028691A1
Authority
WO
WIPO (PCT)
Prior art keywords
die casting
content
heat resistant
alloy
resistant magnesium
Prior art date
Application number
PCT/JP2004/013974
Other languages
English (en)
French (fr)
Inventor
Takumi Hijii
Tomoyasu Kitano
Koichi Ohori
Yusuke Nakaura
Harutoshi Matsuyama
Original Assignee
Toyota Jidosha Kabushiki Kaisha
Mitsubishi Aluminum Company, 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 Toyota Jidosha Kabushiki Kaisha, Mitsubishi Aluminum Company, Ltd. filed Critical Toyota Jidosha Kabushiki Kaisha
Priority to AU2004274799A priority Critical patent/AU2004274799B2/en
Priority to EP04788132A priority patent/EP1685267B1/en
Priority to US10/568,775 priority patent/US20060222556A1/en
Priority to CA2536682A priority patent/CA2536682C/en
Priority to DE602004008797T priority patent/DE602004008797T2/de
Publication of WO2005028691A1 publication Critical patent/WO2005028691A1/en
Priority to NO20061193A priority patent/NO20061193L/no

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C23/00Alloys based on magnesium
    • C22C23/02Alloys based on magnesium with aluminium as the next major constituent

Definitions

  • the present invention relates -to a heat resistant magnesium die casting alloy and a d ⁇ e cast product of that alloy.
  • BACKGROUND ART In recent years, to deal with -the demand for reduction of the weight of vehicles , greater application of alloys of magnesium, the lightest of the practical metals, has been desired.
  • conventional die casting magnesium alloys greatly deform at high temperatures. Not much progress has been made for parts having bolted portions exposed to high temperature environments (120°C or more).
  • various heat resistant magnesium die casting alloys have been developed, but it has not been possible to simultaneously improve the heat resistance (high temperature strength and creep resistance) and castability (hot-cracking resistance and die-sticking resistance during die casting) and therefore the range of application has been limited.
  • JP-A-2001-316752 has proposed a die casting magnesium alloy comprised of 2 to 6 wt% Al, 0.3 to 2 wt% Ca, 0.01 to 1 wt% Sr, 0.1 to 1 wt% Mn, and the balance of Mg and unavoidable impurities. Due to this, it becomes possible to simultaneously improve the heat resistance and castability and expand the range of application. Even with the magnesium alloy of the above proposal, however, it has not been possible to sufficiently cover the range of applications required, so development of a heat resistant magnesium die casting alloy with further improved combination of heat resistance and castability has been desired.
  • the present invention has as its object to provide a heat resistant magnesium die casting alloy simultaneously improved in heat resistance and castability and expanded in range of applications and a die cast product of the same alloy.
  • a heat resistant magnesium die casting alloy comprising, by wt%, the following composition: Al: over 6% to not more than 10%, Ca: 1.8 to 5%, Sr: 0.05 to 1.0%, Mn: 0.1 to 0.6%, and Bal: Mg and unavoidable impurities, the ratio Ca/Al of the Ca content to the Al content being 0.3 to 0.5.
  • the present invention is characterized by limiting the ratio Ca/Al of the contents of Al and Ca to within a predetermined range so as to improve the combination of the heat resistance and castability over the conventional limits without causing deterioration of characteristics even if adding Al and Ca to high contents considered unsuitable in the past.
  • JP-A-2001-316752 sets the upper limit of -the Al content to 6 wt% and the upper limit of the Ca content to 2 wt%.
  • the reason for the limitations is explained as being that if the Al content is over 6 wt%, the creep resistance rapidly deteriorates, while if the Ca content exceeds 2 wt%, casting cracks easily occur (see paragraph 0010 to 0012 of the publication).
  • FIG. 1 is a graph comparing the retained bolt loads of various types of Mg alloys.
  • FIG. 2 is a graph of the relationship between the high temperature retained bolt load and.
  • FIG. 3 is a graph of the relationship between the casting crack length and Ca/Al ratio.
  • FIGS. 4A and 4B are graphs of the (A) change in corrosion weight loss and (B) change in corrosion rate with respect to the test duration of a salt water spray test for Mg alloys with various RE contents.
  • FIG. 5 is a graph of the change in the corrosion rate with respect to the RE content for specific test durations (numbers of days).
  • FIGs. 6A and 6B are graphs of the (A) 0.2% proof stress and tensile strength and the (B) elongation in the temperature range of room temperature to 250 °C.
  • composition of the heat resistant magnesium die casting alloy of the present invention is limited due to the following reasons. Note that in this description, unless otherwise specified, the "%" in the indications of the content of the components mean "wt%”. [Al: over 6% to not more than 10%] Al raises the strength at room temperature and high temperature by dispersion strengthening (in particular grain boundary strengthening) by forming Al-Ca-based, Al- Sr-based, and Mg-Al-based intermetallic compounds.
  • the Ca content 1.8% to 5% under a predetermined range of the Ca/Al ratio, ⁇ t is possible to improve the proof strength and creep resistance over the conventional limits in the copresence with Al.
  • the upper limit of the Ca content is made 5%.
  • the Ca content is preferably over 2% and not more than 5%, more preferably 2.5 to 3.5%.
  • Sr 0.05 to 1.0%
  • Sr is added to further improve the effect of prevention of casting cracks and securing creep resistance. To obtain this effect, it is necessary to add Sr to at least 0.05%. The effect becomes greater with increasing the amount of addition. However, even if added over 1.0%, the effect does not increase not much at all.
  • Mn 0.1 to 0.6%
  • Mn is added to secure a good corrosion resistance. To obtain this effect, it is necessary to make the Mn content at least 0.1%. However, if Mn is present in excess, free Mn precipitates and embrittlement occurs, so the upper limit of the Mn content is made 0.6%.
  • the magnesium alloy of the present invention is remarkably improved in corrosion resistance by further adding a rare earth metal (RE) to the above composition in the range of 0.1 to 3%. To realize this effect, it is necessary to make the RE content at least 0.1%. However, if the RE content exceeds 3%, the castability rapidly deteriorates, casting cracks and misruns end up occurring, and a sound casting is not obtained, so the upper limit of the RE content is made 3%.
  • the heat resistant magnesium alloy of the present invention is particularly limited to one for die casting. By die casting, a fine network comprised of Al-Ca-based or Al-Sr-based intermetallic compounds is formed and a good heat resistance can be secured.
  • the basic process for obtaining a product by applying the alloy of the present invention to die casting is as follows: Alloy metal ⁇ charging into crucible (*1) ⁇ melting ⁇ temperature adjustment ⁇ die casting (*2) ⁇ removal of product *1)
  • the crucible used is made of iron. *2)
  • the die casting is by a cold chamber, hot chamber, etc.
  • the die casting heat resistance magnesium alloy of the present invention is particularly advantageous when applied to parts requiring heat resistance such as parts of automobile engines, in particular, oil pans, headlight covers, etc. and also transmission cases.
  • EXAMPLES [Example 1] The following experiment was performed to confirm the effect of improvement of the castability and heat resistance by alloy compositions of the present invention.
  • Mg alloys of the compositions of Table 1 were die cast under the following conditions using a 135 ton cold chamber die casting machine.
  • the obtained alloy samples were subjected to tensile tests (test temperature: room temperature (RT), 150°C) and measured for crack length at casting and bolt load retention. As the bolt load retention, the retained bolt load was measured under the following conditions. The measurement results are shown all together in Table 2 and Table 3.
  • FIG. 1 is a graph showing the high temperature retained bolt loads of different alloy samples
  • FIG. 2 the relationship between the high temperature retained bolt load and Ca/Al ratio
  • FIG. 3 the relationship between the casting crack length and Ca/Al ratio.
  • the retained bolt load increases with increasing the Ca/Al ratio and that to secure the practically required retained bolt load of at least 70%, it is necessary that Ca/Al ratio ⁇ 0.3. From the results of FIG.
  • Example 2 The following experiment was performed to confirm the effect of improvement of the corrosion resistance by RE addition in the alloy composition of the present invention.
  • the Mg alloys of the compositions of Table 4 were die cast in the same way as in Example 1.
  • the alloy compositions of No. 101 to 105 shown in Table 4 were basically comprised (target values) of 7%Al-3%Ca-0.5%Sr- 0.3%Mn with amounts of RE added (target values) of successively 0% (no addition), 0.1%, 0.5%, 2.0%, and 3.0% (analysis values of added RE elements of 0.08%, 0.44%, 1.77%, and 2.68%).
  • a Ce-rich (50%) misch metal was used for the RE addition.
  • the obtained alloy samples were subjected to salt water spray tests under the following conditions to evaluate the corrosion resistance.
  • ⁇ Salt Spray Test Method> 1. Cut out test piece (width 70 mm x length 50 mm x thickness 3 mm) from the die cast product in the as- cast state. 2. Immerse the test piece in acetone and ultrasonically clean it for 15 minutes, then measure its weight (initial weight). 3. Mask the parts of the surface of the test piece finished being measured for weight other than the as-cast surface (test surface). 4. Perform the salt spray test by a 5% NaCl aqueous solution under conditions defined in JIS Z2371. 5.
  • FIG. 4A and FIG. 4B show changes in the corrosion weight loss and corrosion rate for different test durations (numbers of days). Compared with the no-RE material 101, the RE-added materials 102 to 105 all had small corrosion weight losses and small corrosion rates. At FIG. 4A showing the change along with time of the corrosion weight loss, the curves are convex upward. In FIG.
  • FIG. 5 is a graph of the effects of the RE content on the progression of corrosion.
  • the corrosion rate was plotted against the RE content for a test duration of one day and 10 days. At both test durations, the corrosion rate clearly decreases by the addition of 0.08% of RE as compared with no RE (0%). With increasing the amount of addition of 0.44% and 1.77%, the corrosion rate further decreases. However, if increasing the amount of addition to 2.68%, the corrosion rate conversely starts to increase, but even so the corrosion rate is far smaller than with no addition.
  • FIGS. 6A and 6B show the (A) 0.2% proof strength and tensile strength and (B) elongation at the test temperature from room temperature to 250°C. At all test temperatures, it was learned that the 0.44% RE material ( ⁇ plot) was provided with similar strength characteristics to the non-addition material (0 plot) .
  • FIG. 7 compares the high temperature retained bolt loads of a 0.44% RE material (103), a non-addition material (101), and an AZ91D (typical known heat resistant Mg die casting alloy). The test procedure was the same as that in Example 1.
  • the alloy of the present invention is far larger in retained bolt load compared with the conventional use alloy AZ91D regardless of the addition of RE. Further, in the alloys of the present invention, the 0.44% RE material (103) fell in retained bolt load by about 10% compared with the non-addition material (101), but sufficiently secured the practically required at least 70%, so was provided with both the practically sufficient heat resistance and corrosion resistance. Simultaneously, an excellent castability was also provided and it was possible to die cast without any problem. Table 4
  • a heat resistant magnesium die casting alloy simultaneously improved in heat resistance and castability and able to be used for a wider range of applications than the past is provided. Further, due to the RE addition, in addition to the heat resistance and castability, the corrosion resistance may also be simultaneously improved.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Forging (AREA)
  • Continuous Casting (AREA)
  • Prevention Of Electric Corrosion (AREA)
PCT/JP2004/013974 2003-09-18 2004-09-16 Heat resistant magnesium die casting alloys WO2005028691A1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
AU2004274799A AU2004274799B2 (en) 2003-09-18 2004-09-16 Heat resistant magnesium die casting alloys
EP04788132A EP1685267B1 (en) 2003-09-18 2004-09-16 Heat resistant magnesium die casting alloys
US10/568,775 US20060222556A1 (en) 2003-09-18 2004-09-16 Heat resistant magnesium die casting alloys
CA2536682A CA2536682C (en) 2003-09-18 2004-09-16 Heat resistant magnesium die casting alloys
DE602004008797T DE602004008797T2 (de) 2003-09-18 2004-09-16 Wärmebeständige druckguss-magnesiumlegierungen
NO20061193A NO20061193L (no) 2003-09-18 2006-03-14 Varmebestandige magnesiumlegeringer for formstøping

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
JP2003-326563 2003-09-18
JP2003326563 2003-09-18
JP2004150393A JP4202298B2 (ja) 2003-09-18 2004-05-20 ダイカスト用耐熱マグネシウム合金および同合金のダイカスト製品
JP2004-150393 2004-05-20

Publications (1)

Publication Number Publication Date
WO2005028691A1 true WO2005028691A1 (en) 2005-03-31

Family

ID=34380325

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2004/013974 WO2005028691A1 (en) 2003-09-18 2004-09-16 Heat resistant magnesium die casting alloys

Country Status (9)

Country Link
US (1) US20060222556A1 (ja)
EP (1) EP1685267B1 (ja)
JP (1) JP4202298B2 (ja)
KR (1) KR20060040745A (ja)
AU (1) AU2004274799B2 (ja)
CA (1) CA2536682C (ja)
DE (1) DE602004008797T2 (ja)
NO (1) NO20061193L (ja)
WO (1) WO2005028691A1 (ja)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4539572B2 (ja) * 2006-01-27 2010-09-08 株式会社豊田中央研究所 鋳造用マグネシウム合金および鋳物
JP5327515B2 (ja) 2008-11-14 2013-10-30 株式会社豊田自動織機 鋳造用マグネシウム合金およびマグネシウム合金鋳物
US8435444B2 (en) 2009-08-26 2013-05-07 Techmag Ag Magnesium alloy
CN102304631B (zh) * 2011-10-17 2013-03-20 闻喜县瑞格镁业有限公司 一种耐热抗蠕变低成本镁合金的制备方法
KR101325642B1 (ko) 2012-11-23 2013-11-05 서울대학교산학협력단 크리프 특성이 우수한 주조용 마그네슘합금
KR101941774B1 (ko) 2017-05-29 2019-01-24 서울대학교산학협력단 고강도 다이캐스팅용 마그네슘 합금
DE112018005870T5 (de) * 2017-11-17 2020-08-06 National University Corporation University Of Toyama Magnesium-Legierung und Magnesium-Legierungsteil
KR102197773B1 (ko) 2018-09-06 2021-01-04 서울대학교산학협력단 강도와 연신율이 우수한 고압 다이캐스팅용 마그네슘 합금 및 이 합금의 제조방법
CN109182860A (zh) 2018-11-08 2019-01-11 中信戴卡股份有限公司 一种高强韧镁合金及制备方法

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5147603A (en) * 1990-06-01 1992-09-15 Pechiney Electrometallurgie Rapidly solidified and worked high strength magnesium alloy containing strontium
JPH07278717A (ja) * 1994-04-12 1995-10-24 Ube Ind Ltd 加圧部での耐へたり性に優れたマグネシウム合金製部材
EP0791662A1 (en) * 1996-02-27 1997-08-27 Honda Giken Kogyo Kabushiki Kaisha Heat-resistant magnesium alloy
EP0799901A1 (en) * 1996-04-04 1997-10-08 Mazda Motor Corporation Heat-resistant magnesium alloy member
EP1048743A1 (en) * 1999-04-30 2000-11-02 General Motors Corporation Creep-resistant magnesium alloy die castings
EP1127950A1 (en) * 2000-02-24 2001-08-29 Mitsubishi Aluminum Co.,Ltd. Die casting magnesium alloy
EP1308531A1 (en) * 2001-11-05 2003-05-07 Dead Sea Magnesium Ltd. High strength and creep resistant magnesium alloys

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3737440B2 (ja) * 2001-03-02 2006-01-18 三菱アルミニウム株式会社 耐熱マグネシウム合金鋳造品およびその製造方法
JP3592659B2 (ja) * 2001-08-23 2004-11-24 株式会社日本製鋼所 耐食性に優れたマグネシウム合金およびマグネシウム合金部材

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5147603A (en) * 1990-06-01 1992-09-15 Pechiney Electrometallurgie Rapidly solidified and worked high strength magnesium alloy containing strontium
JPH07278717A (ja) * 1994-04-12 1995-10-24 Ube Ind Ltd 加圧部での耐へたり性に優れたマグネシウム合金製部材
EP0791662A1 (en) * 1996-02-27 1997-08-27 Honda Giken Kogyo Kabushiki Kaisha Heat-resistant magnesium alloy
EP0799901A1 (en) * 1996-04-04 1997-10-08 Mazda Motor Corporation Heat-resistant magnesium alloy member
EP1048743A1 (en) * 1999-04-30 2000-11-02 General Motors Corporation Creep-resistant magnesium alloy die castings
EP1127950A1 (en) * 2000-02-24 2001-08-29 Mitsubishi Aluminum Co.,Ltd. Die casting magnesium alloy
EP1308531A1 (en) * 2001-11-05 2003-05-07 Dead Sea Magnesium Ltd. High strength and creep resistant magnesium alloys

Also Published As

Publication number Publication date
AU2004274799B2 (en) 2008-05-22
NO20061193L (no) 2006-04-12
DE602004008797T2 (de) 2008-06-12
JP4202298B2 (ja) 2008-12-24
US20060222556A1 (en) 2006-10-05
EP1685267A1 (en) 2006-08-02
CA2536682A1 (en) 2005-03-31
KR20060040745A (ko) 2006-05-10
AU2004274799A1 (en) 2005-03-31
DE602004008797D1 (de) 2007-10-18
EP1685267B1 (en) 2007-09-05
JP2005113260A (ja) 2005-04-28
CA2536682C (en) 2010-11-23

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