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AU2009208050A1 - Creep-resistant magnesium alloy - Google Patents

Creep-resistant magnesium alloy Download PDF

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Publication number
AU2009208050A1
AU2009208050A1 AU2009208050A AU2009208050A AU2009208050A1 AU 2009208050 A1 AU2009208050 A1 AU 2009208050A1 AU 2009208050 A AU2009208050 A AU 2009208050A AU 2009208050 A AU2009208050 A AU 2009208050A AU 2009208050 A1 AU2009208050 A1 AU 2009208050A1
Authority
AU
Australia
Prior art keywords
weight
magnesium alloy
creep
magnesium
alloy according
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.)
Abandoned
Application number
AU2009208050A
Inventor
Hajo Dieringa
Norbert Hort
Karl Ulrich Kainer
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.)
GKSS Forshungszentrum Geesthacht GmbH
Original Assignee
GKSS Forshungszentrum Geesthacht GmbH
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 GKSS Forshungszentrum Geesthacht GmbH filed Critical GKSS Forshungszentrum Geesthacht GmbH
Publication of AU2009208050A1 publication Critical patent/AU2009208050A1/en
Abandoned legal-status Critical Current

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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

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)
  • Manufacture And Refinement Of Metals (AREA)
  • Gears, Cams (AREA)
  • Compounds Of Alkaline-Earth Elements, Aluminum Or Rare-Earth Metals (AREA)
  • Compositions Of Macromolecular Compounds (AREA)

Description

Australian Patents Act 1990 - Regulation 3.2 ORIGINAL COMPLETE SPECIFICATION STANDARD PATENT Invention Title Creep-resistant magnesium alloy The following statement is a full description of this invention, including the best method of performing it known to me/us: P/00/0 li S102 - la The present invention relates to a creep-resistant magnesium alloy. Metal alloys containing magnesium are used extensively in the automotive industry, electronic industry, aerospace industry and several other technical areas. Those alloys are especially advantageous, which are high temperature creep-resistant and therefore usable in a high temperature environment. Several different magnesium alloys have been developed and standardized, such as the magnesium alloys JIS H 5203 (MC1 MC10) and JIS H 5303 (MDC1A, MDClB). Alloy A having the composition Mg-4%Al-2%RE (RE = rare earth elements) , which has been developed by the company Dow Chemical, is also well known for high temperature use. However, such heat-resistant magnesium alloys are quite inapplicable in casting, wherein the metal object must be cooled rapidly after shaping. DE 44 46 898 Al discloses creep-resistant magnesium alloys, containing: 1.5 to 10 % by weight of aluminum (Al) , less than 2 % by weight of rare earth elements (RE), 0.25 to 5.5 % by weight of calcium (Ca), the balance being magnesium. In addition, the alloy may contain 0.2 to 2.5 % by weight of copper and/or zinc. The rare earth elements contained in such alloys, however, increase the costs of the alloy. DE 22 01 460 Al also discloses creep-resistant magnesium alloys containing aluminum and optionally an additional element selected from calcium, zirconium, titanium, silicon, -2 strontium, yttrium, cerium or barium. Barium and calcium in combination are not disclosed as additional elements. It is therefore the object of the present invention to provide a magnesium alloy, which is able to overcome the above mentioned disadvantages of the state of the art and, moreover, has a higher creep resistance. The object is solved by a metal alloy containing magnesium or magnesium alloy, containing 1 to 9 % by weight of aluminum (Al), 0.5 to 5 % by weight of barium (Ba), 0.5 to 5 %- by weight of calcium (Ca) , the balance being magnesium (Mg) and inevitable production-related impurities, based on the total weight of the alloy. Preferably, the inevitable production related impurities amount in total to no more than 2 % by weight, based on the total weight of the alloy. The proportion of aluminum is preferably 2 to 7 % by weight, more preferably 3 to 6 % by weight. The proportion of barium is preferably 1 to 4 % by weight, more preferably 1.5 to 3 % by weight. The proportion of calcium is preferably 1 to 4 % by weight, more preferably 1.5 to 3 % by weight. The magnesium alloy of the invention may additionally include zinc, tin, lithium, manganese, yttrium, neodymium, cerium and/or praseodymium in proportions of up to 7 % by weight, respectively. The magnesium alloy of the invention may be used in a multiplicity of application areas; preferably it is used in the production of components for automotives, vessels and/or aeroplanes, more preferably in the production of power trains and components thereof. The invention is further illustrated with reference to the attached figure. In figure 1, the creep deformation as a -3 function of time with an applied strain of 80 MPa and a temperature of 2000C of two inventive magnesium alloys (ABC alloys) containing about 4 % by weight of aluminum, about 2 % by weight of barium and about 1 % by weight of calcium (ABC421) and about 4 % by weight of aluminum, about 2 % by weight barium and about 2 % by weight of calcium (ABC422), respectively, is shown in comparison to a conventional alloy AE42, wherein E denotes rare earth elements, and an alloy produced by the company Dead Sea Magnesium under the name of MRI230D, which contains rare earth elements in addition to aluminum and calcium. The inventive alloys have a considerably lower creep deforma tion than the respective comparison alloys. This leads to the conclusion that, with constant strain, the temperature may be increased even further, or that a component may be strained for considerably prolonged times. Throughout this specification and the claims which follow, unless the context requires otherwise, the word "comprise", and variations such as "comprises" or "comprising", will be understood to imply the inclusion of a stated integer or step or group of integers or steps but not the exclusion of any other integer or step or group of integers or steps. The reference in this specification to any prior publication (or information derived from it), or to any matter which is known, is not, and should not be taken as an acknowledgment or admission or any form of suggestion that that prior publication (or information derived from it) or known matter forms part of the common general knowledge in the field of endeavour to which this specification relates.

Claims (7)

1. Magnesium alloy, containing the following ingredients, based on total weight of the alloy: 1 to 9 % by weight of aluminum 0.5 to 5 % by weight of barium 0.5 to 5 % by weight of calcium and the balance being magnesium.
2. The magnesium alloy according to claim 1, characterized in that it additionally includes zinc, tin, lithium, manganese, yttrium, neodymium, cerium and/or praseodymium in proportions of up to 7 % by weight, respectively.
3. The magnesium alloy according to any of the previous claims, characterized in that the proportion of aluminum is 2 to 7 % by weight, preferably 3 to 6 % by weight.
4. The magnesium alloy according to any of the previous claims, characterized in that the proportion of barium is 1 to 4 % by weight, preferably 1.5 to 3 % by weight.
5. The magnesium alloy according to any of the previous claims, characterized in that the proportion of calcium is 1 to 4 % by weight, preferably 1.5 to 3 % by weight.
6. Use of a magnesium alloy according to any of the claims 1 to 5 in the production of components of automotives, vessels and/or aeroplanes.
7. Use of a magnesium alloy according to any of the claims 1 to 5 in the production of power trains or components thereof.
AU2009208050A 2008-08-26 2009-08-07 Creep-resistant magnesium alloy Abandoned AU2009208050A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102008039683A DE102008039683B4 (en) 2008-08-26 2008-08-26 Creep resistant magnesium alloy
DE102008039683.4 2008-08-26

Publications (1)

Publication Number Publication Date
AU2009208050A1 true AU2009208050A1 (en) 2010-03-18

Family

ID=41404299

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2009208050A Abandoned AU2009208050A1 (en) 2008-08-26 2009-08-07 Creep-resistant magnesium alloy

Country Status (10)

Country Link
US (1) US20100054985A1 (en)
EP (1) EP2159293B1 (en)
JP (1) JP2010065318A (en)
CN (1) CN101676423A (en)
AU (1) AU2009208050A1 (en)
CA (1) CA2675863A1 (en)
DE (1) DE102008039683B4 (en)
ES (1) ES2548582T3 (en)
IL (1) IL200309A0 (en)
PT (1) PT2159293E (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
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US8435444B2 (en) 2009-08-26 2013-05-07 Techmag Ag Magnesium alloy
KR101080164B1 (en) 2011-01-11 2011-11-07 한국기계연구원 Magnesium alloy with excellent ignition resistance and mechanical properties and its manufacturing method
CN102242298A (en) * 2011-07-04 2011-11-16 四川大学 Al and Zn strengthened Mg-Sn-RE-based high-toughness heat-resistant magnesium alloy
CN103789589B (en) * 2014-03-04 2015-09-09 南京信息工程大学 A kind of high anode utilization rate battery material and preparation method
CN104087803B (en) * 2014-07-28 2016-08-24 王雨晴 A kind of creep resistance Dow metal and preparation method thereof
CN105543522A (en) * 2016-01-06 2016-05-04 安徽祈艾特电子科技股份有限公司 Nano zirconium boride modified Mg-Al-Zn series magnesium alloy material for casting automobile parts and preparation method of nano zirconium boride modified Mg-Al-Zn series magnesium alloy material
CN106521274A (en) * 2016-10-27 2017-03-22 江苏理工学院 High-strength Mg-Li-Al-Y-Ca alloy and preparation method thereof
CN106566966B (en) * 2016-11-18 2018-06-26 哈尔滨理工大学 The magnesium-based composite material of a kind of high-entropy alloy as enhancing base and preparation method thereof
US20200232070A1 (en) * 2019-01-18 2020-07-23 Divergent Technologies, Inc. Aluminum alloy compositions
CN111726655B (en) * 2020-07-02 2022-09-06 中影华夏寰宇(北京)电影科技有限公司 Video processing device, method and system
CN112442620B (en) * 2020-10-29 2021-10-01 航天材料及工艺研究所 A 300MPa grade magnesium-lithium alloy material and preparation method thereof
WO2023278878A1 (en) 2021-07-01 2023-01-05 Divergent Technologies, Inc. Al-mg-si based near-eutectic alloy composition for high strength and stiffness applications
DE102022109070A1 (en) 2022-04-13 2023-10-19 Soluterials Verwaltungs und Verwertungs UG (haftungsbeschränkt) Light metal matrix composite material based on magnesium and process for its production

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AT123225B (en) * 1927-11-09 1931-06-10 Anton Ing Kratky Process for cleaning cerium-aluminum-magnesium alloys by treatment with fluorides.
US2747991A (en) * 1945-09-14 1956-05-29 Olin Mathieson Magnesium-base alloys
DE1259578B (en) * 1959-05-01 1968-01-25 Dow Chemical Co Process for the powder metallurgical production of a dispersion strengthened magnesium alloy
US3182390A (en) * 1959-05-01 1965-05-11 Dow Chemical Co Method of die-expressing a magnesiumbase alloy
US3119684A (en) * 1961-11-27 1964-01-28 Dow Chemical Co Article of magnesium-base alloy and method of making
DE2201460A1 (en) 1972-01-13 1973-07-19 Erdmann Jesnitzer Friedrich Pr Magnesium alloy contg aluminium - with high creep resistance
JP2705996B2 (en) * 1990-06-13 1998-01-28 健 増本 High strength magnesium based alloy
JP3110117B2 (en) * 1991-12-26 2000-11-20 健 増本 High strength magnesium based alloy
JP2730847B2 (en) * 1993-06-28 1998-03-25 宇部興産株式会社 Magnesium alloy for castings with excellent high temperature creep strength
JP3522963B2 (en) * 1996-04-04 2004-04-26 三井金属鉱業株式会社 Method for producing heat-resistant magnesium alloy member, magnesium alloy used therefor, and magnesium alloy molded member
JP3611759B2 (en) * 1999-10-04 2005-01-19 株式会社日本製鋼所 Magnesium alloy and magnesium alloy heat-resistant member with excellent heat resistance and castability
JP3592659B2 (en) * 2001-08-23 2004-11-24 株式会社日本製鋼所 Magnesium alloys and magnesium alloy members with excellent corrosion resistance
JP3852769B2 (en) * 2002-11-06 2006-12-06 三菱製鋼株式会社 Room temperature formable magnesium alloy with excellent corrosion resistance
JP2004162090A (en) * 2002-11-11 2004-06-10 Toyota Industries Corp Heat resistant magnesium alloy
KR101127113B1 (en) * 2004-01-09 2012-03-26 켄지 히가시 Magnesium alloy for die cast and magnesium die cast products using the same

Also Published As

Publication number Publication date
US20100054985A1 (en) 2010-03-04
EP2159293A2 (en) 2010-03-03
EP2159293A3 (en) 2012-05-30
IL200309A0 (en) 2010-05-31
CA2675863A1 (en) 2010-02-26
DE102008039683B4 (en) 2010-11-04
CN101676423A (en) 2010-03-24
ES2548582T3 (en) 2015-10-19
JP2010065318A (en) 2010-03-25
EP2159293B1 (en) 2015-07-08
PT2159293E (en) 2015-09-16
DE102008039683A1 (en) 2010-03-04

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MK4 Application lapsed section 142(2)(d) - no continuation fee paid for the application