RU2361946C1 - Alloy on basis of magnesium - Google Patents
Alloy on basis of magnesium Download PDFInfo
- Publication number
- RU2361946C1 RU2361946C1 RU2008107830/02A RU2008107830A RU2361946C1 RU 2361946 C1 RU2361946 C1 RU 2361946C1 RU 2008107830/02 A RU2008107830/02 A RU 2008107830/02A RU 2008107830 A RU2008107830 A RU 2008107830A RU 2361946 C1 RU2361946 C1 RU 2361946C1
- Authority
- RU
- Russia
- Prior art keywords
- magnesium
- alloy
- basis
- yttrium
- cadmium
- Prior art date
Links
- 239000000956 alloy Substances 0.000 title claims abstract description 14
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 14
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 title claims abstract description 12
- 239000011777 magnesium Substances 0.000 title claims abstract description 12
- 229910052749 magnesium Inorganic materials 0.000 title claims abstract description 12
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims abstract description 8
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 8
- 229910052793 cadmium Inorganic materials 0.000 claims abstract description 8
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 claims abstract description 8
- 229910052727 yttrium Inorganic materials 0.000 claims abstract description 8
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims abstract description 8
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 8
- 239000011701 zinc Substances 0.000 claims abstract description 8
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 claims abstract description 7
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 7
- 239000011575 calcium Substances 0.000 claims abstract description 7
- 229910052791 calcium Inorganic materials 0.000 claims abstract description 7
- 239000010936 titanium Substances 0.000 claims abstract description 7
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 7
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims abstract description 5
- 229910052748 manganese Inorganic materials 0.000 claims abstract description 5
- 239000011572 manganese Substances 0.000 claims abstract description 5
- 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 3
- 238000004519 manufacturing process Methods 0.000 abstract description 2
- 238000005272 metallurgy Methods 0.000 abstract description 2
- 239000004411 aluminium Substances 0.000 abstract 1
- 239000000126 substance Substances 0.000 abstract 1
- 239000000203 mixture Substances 0.000 description 4
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- RAHZWNYVWXNFOC-UHFFFAOYSA-N Sulphur dioxide Chemical compound O=S=O RAHZWNYVWXNFOC-UHFFFAOYSA-N 0.000 description 2
- 230000004907 flux Effects 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229910004261 CaF 2 Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Powder Metallurgy (AREA)
Abstract
Description
Изобретение относится к области металлургии, в частности к составам сплавов на основе магния, которые могут быть использованы для изготовления деталей летательных аппаратов, автомобилей, бытовой техники.The invention relates to the field of metallurgy, in particular to the compositions of magnesium-based alloys, which can be used for the manufacture of parts for aircraft, automobiles, household appliances.
Известен сплав на основе магния, мас.%: алюминий, кадмий, марганец, иттрий, никель, цинк в сумме 0,1-10,0; магний остальное [1].Known alloy based on magnesium, wt.%: Aluminum, cadmium, manganese, yttrium, nickel, zinc in the amount of 0.1-10.0; magnesium is 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 алюминии, кадмий, марганец, иттрий, цинк, дополнительно включает титан и кальций при следующем соотношении компонентов, мас.%: алюминий 8,0-10,0; кадмий 0,5-0,9; марганец 0,2-0,3; иттрий 0,03-0,05; цинк 4,5-5,5; титан 0,1-0,15; кальций 0,02-0,04; магний остальное.The technical result is achieved in that the magnesium-based alloy containing aluminum, cadmium, manganese, yttrium, zinc, further includes titanium and calcium in the following ratio of components, wt.%: Aluminum 8.0-10.0; cadmium 0.5-0.9; manganese 0.2-0.3; yttrium 0.03-0.05; zinc 4.5-5.5; titanium 0.1-0.15; calcium 0.02-0.04; magnesium is the rest.
В таблице приведены составы сплава.The table shows the alloy compositions.
В составе сплава компоненты проявляют себя следующим образом. Алюминий, цинк и кадмий повышают механические свойства сплава, марганец увеличивает его коррозионную стойкость. Кальций понижает окисляемость. Иттрий препятствует развитию трещин. Титан измельчает структурные составляющие сплава.In the composition of the alloy, the components manifest themselves as follows. Aluminum, zinc and cadmium increase the mechanical properties of the alloy, manganese increases its corrosion resistance. Calcium lowers oxidation. Yttrium inhibits the development of cracks. Titanium grinds the structural components of the alloy.
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.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.
Сплав подлежит термообработке, включающей нагрев в печи (в атомосфере сернистого газа с принудительной циркуляцией) до температуры 530°С с выдержкой в течение 2 часов, закалку в воде с температурой 100°С, старение при температуре 175°С с выдержкой в течение 10 часов.The alloy is subject to heat treatment, including heating in a furnace (in the atomosphere of sulfur dioxide with forced circulation) to a temperature of 530 ° C with holding for 2 hours, quenching in water with a temperature of 100 ° C, aging at 175 ° C with holding for 10 hours .
Источник информацииThe source of information
1. JP 02-047238, С22 С 23/00, 1990.1.JP 02-047238, C22 C 23/00, 1990.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008107830/02A RU2361946C1 (en) | 2008-02-28 | 2008-02-28 | Alloy on basis of magnesium |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| RU2008107830/02A RU2361946C1 (en) | 2008-02-28 | 2008-02-28 | Alloy on basis of magnesium |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| RU2361946C1 true RU2361946C1 (en) | 2009-07-20 |
Family
ID=41047153
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| RU2008107830/02A RU2361946C1 (en) | 2008-02-28 | 2008-02-28 | Alloy on basis of magnesium |
Country Status (1)
| Country | Link |
|---|---|
| RU (1) | RU2361946C1 (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB596102A (en) * | 1945-07-19 | 1947-12-29 | Rupert Martin Bradbury | A new magnesium base alloy |
| GB637040A (en) * | 1948-01-06 | 1950-05-10 | Magnesium Elektron Ltd | Improvements in or relating to magnesium base alloys |
| RU2198234C2 (en) * | 2001-02-09 | 2003-02-10 | Государственное предприятие Всероссийский научно-исследовательский институт авиационных материалов | Magnesium-based alloy and article made from this alloy |
| WO2006000022A1 (en) * | 2004-06-24 | 2006-01-05 | Cast Centre Pty Ltd | Die cast magnesium alloy |
-
2008
- 2008-02-28 RU RU2008107830/02A patent/RU2361946C1/en active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB596102A (en) * | 1945-07-19 | 1947-12-29 | Rupert Martin Bradbury | A new magnesium base alloy |
| GB637040A (en) * | 1948-01-06 | 1950-05-10 | Magnesium Elektron Ltd | Improvements in or relating to magnesium base alloys |
| RU2198234C2 (en) * | 2001-02-09 | 2003-02-10 | Государственное предприятие Всероссийский научно-исследовательский институт авиационных материалов | Magnesium-based alloy and article made from this alloy |
| WO2006000022A1 (en) * | 2004-06-24 | 2006-01-05 | Cast Centre Pty Ltd | Die cast magnesium alloy |
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