RU2615934C1 - Alloy on base of magnesium - Google Patents
Alloy on base of magnesium Download PDFInfo
- Publication number
- RU2615934C1 RU2615934C1 RU2016124012A RU2016124012A RU2615934C1 RU 2615934 C1 RU2615934 C1 RU 2615934C1 RU 2016124012 A RU2016124012 A RU 2016124012A RU 2016124012 A RU2016124012 A RU 2016124012A RU 2615934 C1 RU2615934 C1 RU 2615934C1
- Authority
- RU
- Russia
- Prior art keywords
- magnesium
- alloy
- neodymium
- zirconium
- titanium
- Prior art date
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Classifications
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- 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
- C22C23/04—Alloys based on magnesium with zinc or cadmium as the next major constituent
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- 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
- C22C23/06—Alloys based on magnesium with a rare earth metal as the next major constituent
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- Continuous Casting (AREA)
Abstract
Description
Изобретение относится к области цветной металлургии, в частности к составам сплавов на основе магния, которые могут быть использованы для изготовления корпусов бытовой техники, шпулек и катушек текстильных станков, подставок для телекамер и других изделий.The invention relates to the field of non-ferrous metallurgy, in particular to the compositions of magnesium-based alloys, which can be used for the manufacture of housings for household appliances, bobbins and coils of textile machines, stands for television cameras and other products.
Известен сплав на основе магния, содержащий, мас.%: цинк 1,8-2,5; неодим 0,8-1,2; цирконий 0,7-1,0; титан 0,1-0,2; магний - остальное [1].Known magnesium-based alloy containing, wt.%: Zinc 1.8-2.5; neodymium 0.8-1.2; zirconium 0.7-1.0; titanium 0.1-0.2; magnesium - the rest [1].
Задачей изобретения является повышение прочности сплава.The objective of the invention is to increase the strength of the alloy.
Технический результат достигается тем, что сплав на основе магния, содержащий цинк, неодим, цирконий, титан, магний, дополнительно включает никель и серебро, причем компоненты находятся при следующем соотношении, мас.%: цинк 1,8-2,5; неодим 0,8-1,2; цирконий 0,6-0,9; титан 0,1-0,2; никель 1,0-2,0; серебро 0,6-1,0; магний - остальное.The technical result is achieved in that the magnesium-based alloy containing zinc, neodymium, zirconium, titanium, magnesium, additionally includes nickel and silver, and the components are in the following ratio, wt.%: Zinc 1.8-2.5; neodymium 0.8-1.2; zirconium 0.6-0.9; titanium 0.1-0.2; nickel 1.0-2.0; silver 0.6-1.0; magnesium is the rest.
В таблице приведены составы сплава.The table shows the alloy compositions.
Повышение прочности сплава на основе магния достигается комплексным влиянием компонентов, входящих в его состав. Цинк в сочетании с цирконием, неодимом и серебром повышает прочность сплава на основе магния. Никель увеличивает твердость и плотность сплава, титан способствует измельчению его структурных составляющих.Increasing the strength of an alloy based on magnesium is achieved by the complex influence of the components that make up its composition. Zinc in combination with zirconium, neodymium and silver increases the strength of the magnesium-based alloy. Nickel increases the hardness and density of the alloy, titanium contributes to the grinding of its structural components.
Сплав выплавляют под флюсом ВИ2 (флюс содержит, мас.%: MgCl2 40,0-48,0; KCl 30,0-40,0; BaCl2 5,0; CaF2 3,0-5,0) в стационарных толстостенных стальных тиглях. После рафинирования и модифицирования расплав отстаивают в течение 10-15 мин при температуре 700-720°С и разливают по металлическим формам (при заливке форм струю металла припудривают молотой серой для предотвращения загорания).The alloy is melted under a VI2 flux (the flux contains, wt.%: MgCl 2 40.0-48.0; KCl 30.0-40.0; BaCl 2 5.0; CaF 2 3.0-5.0) in stationary thick-walled steel crucibles. After refining and modification, the melt is settled for 10-15 minutes at a temperature of 700-720 ° C and poured into metal molds (when pouring molds, a stream of metal is dusted with ground sulfur to prevent sunburn).
Источники информацииInformation sources
1. SU 1678881, С22С 23/04, 1991.1. SU 1678881, C22C 23/04, 1991.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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RU2016124012A RU2615934C1 (en) | 2016-06-16 | 2016-06-16 | Alloy on base of magnesium |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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RU2016124012A RU2615934C1 (en) | 2016-06-16 | 2016-06-16 | Alloy on base of magnesium |
Publications (1)
Publication Number | Publication Date |
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RU2615934C1 true RU2615934C1 (en) | 2017-04-11 |
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Family Applications (1)
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RU2016124012A RU2615934C1 (en) | 2016-06-16 | 2016-06-16 | Alloy on base of magnesium |
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Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EA000092B1 (en) * | 1995-02-06 | 1998-06-25 | Бритиш Алюминиум Холдингз Лимитед | Magnesium alloys |
US20050002821A1 (en) * | 2002-06-21 | 2005-01-06 | Bettles Colleen Joyce | Creep resistant magnesium alloy |
WO2007125532A2 (en) * | 2006-04-28 | 2007-11-08 | Biomagnesium Systems Ltd. | Biodegradable magnesium alloys and uses thereof |
RU2351675C2 (en) * | 2003-10-10 | 2009-04-10 | Магнезиум Электрон Лимитед | Castable magnesium alloy |
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2016
- 2016-06-16 RU RU2016124012A patent/RU2615934C1/en active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EA000092B1 (en) * | 1995-02-06 | 1998-06-25 | Бритиш Алюминиум Холдингз Лимитед | Magnesium alloys |
US20050002821A1 (en) * | 2002-06-21 | 2005-01-06 | Bettles Colleen Joyce | Creep resistant magnesium alloy |
RU2351675C2 (en) * | 2003-10-10 | 2009-04-10 | Магнезиум Электрон Лимитед | Castable magnesium alloy |
WO2007125532A2 (en) * | 2006-04-28 | 2007-11-08 | Biomagnesium Systems Ltd. | Biodegradable magnesium alloys and uses thereof |
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