AU2009208050A1 - Creep-resistant magnesium alloy - Google Patents
Creep-resistant magnesium alloy Download PDFInfo
- 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
Links
- 229910000861 Mg alloy Inorganic materials 0.000 title claims description 20
- 229910045601 alloy Inorganic materials 0.000 claims description 13
- 239000000956 alloy Substances 0.000 claims description 13
- 239000011575 calcium Substances 0.000 claims description 12
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 claims description 10
- 229910052791 calcium Inorganic materials 0.000 claims description 10
- 229910052782 aluminium Inorganic materials 0.000 claims description 9
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 9
- 229910052788 barium Inorganic materials 0.000 claims description 8
- DSAJWYNOEDNPEQ-UHFFFAOYSA-N barium atom Chemical compound [Ba] DSAJWYNOEDNPEQ-UHFFFAOYSA-N 0.000 claims description 8
- 239000011777 magnesium Substances 0.000 claims description 7
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims description 6
- 229910052749 magnesium Inorganic materials 0.000 claims description 6
- 238000004519 manufacturing process Methods 0.000 claims description 6
- 229910052684 Cerium Inorganic materials 0.000 claims description 3
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 3
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 claims description 3
- 229910052727 yttrium Inorganic materials 0.000 claims description 3
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims description 3
- 229910052725 zinc Inorganic materials 0.000 claims description 3
- 239000011701 zinc Substances 0.000 claims description 3
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 2
- 229910052779 Neodymium Inorganic materials 0.000 claims description 2
- 229910052777 Praseodymium Inorganic materials 0.000 claims description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 2
- 229910052744 lithium Inorganic materials 0.000 claims description 2
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 claims description 2
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 claims description 2
- PUDIUYLPXJFUGB-UHFFFAOYSA-N praseodymium atom Chemical compound [Pr] PUDIUYLPXJFUGB-UHFFFAOYSA-N 0.000 claims description 2
- 229910052718 tin Inorganic materials 0.000 claims description 2
- 239000004615 ingredient Substances 0.000 claims 1
- 229910052761 rare earth metal Inorganic materials 0.000 description 8
- 239000012535 impurity Substances 0.000 description 2
- 229910001092 metal group alloy Inorganic materials 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 208000037161 Laminin subunit alpha 2-related congenital muscular dystrophy Diseases 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 201000006948 congenital merosin-deficient muscular dystrophy 1A Diseases 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000007717 exclusion Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910052712 strontium Inorganic materials 0.000 description 1
- CIOAGBVUUVVLOB-UHFFFAOYSA-N strontium atom Chemical compound [Sr] CIOAGBVUUVVLOB-UHFFFAOYSA-N 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C23/00—Alloys based on magnesium
- C22C23/02—Alloys based on magnesium with aluminium as the next major constituent
Landscapes
- 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.
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
-
2008
- 2008-08-26 DE DE102008039683A patent/DE102008039683B4/en not_active Expired - Fee Related
-
2009
- 2009-08-07 AU AU2009208050A patent/AU2009208050A1/en not_active Abandoned
- 2009-08-10 IL IL200309A patent/IL200309A0/en unknown
- 2009-08-13 US US12/540,581 patent/US20100054985A1/en not_active Abandoned
- 2009-08-18 CA CA2675863A patent/CA2675863A1/en not_active Abandoned
- 2009-08-20 PT PT91682534T patent/PT2159293E/en unknown
- 2009-08-20 EP EP09168253.4A patent/EP2159293B1/en not_active Not-in-force
- 2009-08-20 ES ES09168253.4T patent/ES2548582T3/en active Active
- 2009-08-24 CN CN200910166342A patent/CN101676423A/en active Pending
- 2009-08-25 JP JP2009193787A patent/JP2010065318A/en not_active Withdrawn
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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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MK4 | Application lapsed section 142(2)(d) - no continuation fee paid for the application |