EP1685267A1 - Alliages de moulage mecanique de magnesium resistant a la chaleur - Google Patents

Alliages de moulage mecanique de magnesium resistant a la chaleur

Info

Publication number
EP1685267A1
EP1685267A1 EP04788132A EP04788132A EP1685267A1 EP 1685267 A1 EP1685267 A1 EP 1685267A1 EP 04788132 A EP04788132 A EP 04788132A EP 04788132 A EP04788132 A EP 04788132A EP 1685267 A1 EP1685267 A1 EP 1685267A1
Authority
EP
European Patent Office
Prior art keywords
die casting
content
heat resistant
alloy
resistant magnesium
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP04788132A
Other languages
German (de)
English (en)
Other versions
EP1685267B1 (fr
Inventor
Takumi Toyota Jidosha Kabushiki Kaisha HIJII
Tomoyasu Toyota Jidosha Kabushiki Kaisha KITANO
Koichi Mitsubishi Aluminum Company Ltd. OHORI
Yusuke Mitsubishi Aluminum Company Ltd. NAKAURA
Harutoshi Mitsubishi Aluminum Comp.Ltd MATSUYAMA
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 Motor Corp
MA Aluminum Corp
Original Assignee
Mitsubishi Aluminum Co Ltd
Toyota Motor Corp
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 Mitsubishi Aluminum Co Ltd, Toyota Motor Corp filed Critical Mitsubishi Aluminum Co Ltd
Publication of EP1685267A1 publication Critical patent/EP1685267A1/fr
Application granted granted Critical
Publication of EP1685267B1 publication Critical patent/EP1685267B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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.

Landscapes

  • 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)

Abstract

L'invention concerne un alliage de moulage mécanique de magnésium résistant à la chaleur amélioré simultanément sur le plan de la résistance à la chaleur et de la coulabilité et élargi à une certaine gamme d'applications. Cet alliage contient, en % en poids, la composition suivante: Al: plus de 6 % jusqu'à maximum 10 %, Ca: 1,8 à 5 %, Sr: 0,05 à 1 %, Mn: 0,1 à 0,6 %, et Bal: Mg et des impuretés inévitables, le rapport Ca/Al de la teneur en Ca par rapport à la teneur en Al étant comprise entre 0,3 et 0,5. En vue d'améliorer la résistance à la corrosion, 0,1 à 3 % de métal des terres rares (RE) peuvent également être ajoutés.
EP04788132A 2003-09-18 2004-09-16 Alliages de moulage mecanique de magnesium resistant a la chaleur Expired - Fee Related EP1685267B1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
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
PCT/JP2004/013974 WO2005028691A1 (fr) 2003-09-18 2004-09-16 Alliages de moulage mecanique de magnesium resistant a la chaleur

Publications (2)

Publication Number Publication Date
EP1685267A1 true EP1685267A1 (fr) 2006-08-02
EP1685267B1 EP1685267B1 (fr) 2007-09-05

Family

ID=34380325

Family Applications (1)

Application Number Title Priority Date Filing Date
EP04788132A Expired - Fee Related EP1685267B1 (fr) 2003-09-18 2004-09-16 Alliages de moulage mecanique de magnesium resistant a la chaleur

Country Status (9)

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

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
CN111344422B (zh) * 2017-11-17 2022-07-12 住友电气工业株式会社 镁合金和镁合金构件
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

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2662707B1 (fr) * 1990-06-01 1992-07-31 Pechiney Electrometallurgie Alliage de magnesium a haute resistance mecanique contenant du strontrium et procede d'obtention par solidification rapide.
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
JP3229954B2 (ja) * 1996-02-27 2001-11-19 本田技研工業株式会社 耐熱性マグネシウム合金
JP3415987B2 (ja) * 1996-04-04 2003-06-09 マツダ株式会社 耐熱マグネシウム合金成形部材の成形方法
US6264763B1 (en) * 1999-04-30 2001-07-24 General Motors Corporation Creep-resistant magnesium alloy die castings
CA2337630C (fr) * 2000-02-24 2005-02-01 Mitsubishi Aluminum Co., Ltd. Alliage de magnesium pour moulage sous pression
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
IL146336A0 (en) * 2001-11-05 2002-07-25 Dead Sea Magnesium Ltd High strength creep resistant magnesium alloy

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2005028691A1 *

Also Published As

Publication number Publication date
DE602004008797T2 (de) 2008-06-12
CA2536682C (fr) 2010-11-23
WO2005028691A1 (fr) 2005-03-31
JP2005113260A (ja) 2005-04-28
JP4202298B2 (ja) 2008-12-24
AU2004274799B2 (en) 2008-05-22
US20060222556A1 (en) 2006-10-05
KR20060040745A (ko) 2006-05-10
AU2004274799A1 (en) 2005-03-31
DE602004008797D1 (de) 2007-10-18
EP1685267B1 (fr) 2007-09-05
NO20061193L (no) 2006-04-12
CA2536682A1 (fr) 2005-03-31

Similar Documents

Publication Publication Date Title
CA2238070C (fr) Alliage de magnesium presentant une tenue amelioree aux temperatures elevees et une aptitude amelioree au moulage sous pression
US6767506B2 (en) High temperature resistant magnesium alloys
CA3021397C (fr) Alliage de coulee sous pression
EP2369025B1 (fr) Alliage de magnésium et pièce coulée en alliage de magnésium
US7445751B2 (en) Creep resistant magnesium alloy
US7041179B2 (en) High strength creep resistant magnesium alloys
AU2004274799B2 (en) Heat resistant magnesium die casting alloys
EP1241276A1 (fr) Alliage de magnesium résistant au fluage
JP4526768B2 (ja) マグネシウム合金
JP4526769B2 (ja) マグネシウム合金
JP5383314B2 (ja) 耐クリープマグネシウム合金
CN100366775C (zh) 高强度抗蠕变镁基合金
KR100252237B1 (ko) 고압주조용 마그네슘 합금
CA3135702C (fr) Alliage d'aluminium de coulee
JP3509163B2 (ja) マグネシウム合金製部材の製造方法
JPH11152552A (ja) Al−Zn−Si系合金の加工方法
CN100385029C (zh) 耐热镁压铸合金和该合金的压铸产品
JP2007270159A (ja) 耐クリープマグネシウム合金
JP2005240130A (ja) 耐熱マグネシウム合金鋳造品
WO2022259136A1 (fr) Alliage de moulage aluminium-silicium et pièces moulées réalisées à partir dudit alliage
JPH0971834A (ja) 高耐熱性アルミニウム合金
JP2005187894A (ja) 耐熱マグネシウム合金鋳造品

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20060223

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): BE DE GB IT NL

17Q First examination report despatched

Effective date: 20060925

DAX Request for extension of the european patent (deleted)
RBV Designated contracting states (corrected)

Designated state(s): BE DE GB IT NL

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): BE DE GB IT NL

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

REF Corresponds to:

Ref document number: 602004008797

Country of ref document: DE

Date of ref document: 20071018

Kind code of ref document: P

PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20080606

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: DE

Payment date: 20100908

Year of fee payment: 7

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20110914

Year of fee payment: 8

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: NL

Payment date: 20110922

Year of fee payment: 8

Ref country code: IT

Payment date: 20110920

Year of fee payment: 8

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: BE

Payment date: 20110913

Year of fee payment: 8

BERE Be: lapsed

Owner name: TOYOTA JIDOSHA K.K.

Effective date: 20120930

Owner name: MITSUBISHI ALUMINUM CO.,LTD.

Effective date: 20120930

REG Reference to a national code

Ref country code: NL

Ref legal event code: V1

Effective date: 20130401

GBPC Gb: european patent ceased through non-payment of renewal fee

Effective date: 20120916

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: DE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20130403

Ref country code: GB

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120916

Ref country code: BE

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120930

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: NL

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20130401

Ref country code: IT

Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES

Effective date: 20120916

REG Reference to a national code

Ref country code: DE

Ref legal event code: R119

Ref document number: 602004008797

Country of ref document: DE

Effective date: 20130403