CN107779711A - A kind of magnesium alloy stamping parts - Google Patents
A kind of magnesium alloy stamping parts Download PDFInfo
- Publication number
- CN107779711A CN107779711A CN201610766713.8A CN201610766713A CN107779711A CN 107779711 A CN107779711 A CN 107779711A CN 201610766713 A CN201610766713 A CN 201610766713A CN 107779711 A CN107779711 A CN 107779711A
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- CN
- China
- Prior art keywords
- magnesium alloy
- stamping parts
- good
- magnesium
- present
- 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.)
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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
- C22C23/02—Alloys based on magnesium with aluminium as the next major constituent
Abstract
The present invention relates to a kind of magnesium alloy stamping parts, electric accessory motor is mainly used as.The magnesium alloy stamping parts of the present invention is made up of the following material in terms of mass fraction:Aluminium 7.5 8.5%, zinc 1.0 1.5%, manganese 0.25 0.5%, zirconium 0.3 0.45%, lithium 0.05 0.15%, silicon 0.019 0.025%, remaining is magnesium and other impurities.The present invention is used as electric accessory motor, has the characteristics that frivolous, rigidly good, good stability of the dimension, ageing resistace are good, and the present invention improves magnesium alloy formula so that magnesium alloy tensile property as stamping material is good, corrosion stability is strong, intensity is high.
Description
Technical field
The present invention relates to punching parts preparation field, more particularly to a kind of magnesium alloy stamping parts.
Technical background
Magnesium-aluminium alloy material has that light, hard, decay resistance is strong, thermal diffusivity is good and good damping performance, closely
Various industries, such as cell phone, removable computer, automobile, electric car are widely used in over year.
Magnesium alloy intensity of the prior art is high, stable performance, but often relatively difficult when carrying out punch steps,
Reason is that existing magnesium alloy tensile property is poor.
The content of the invention
In order to solve the above technical problems, provide a kind of not only with high intensity but also with the magnesium alloy of good tensile property
Stamping parts, the present invention provide following technical scheme:
A kind of magnesium alloy stamping parts, it is made up of the following material in terms of mass fraction:Aluminium 7.5-8.5%, zinc 1.0-
1.5%th, manganese 0.25-0.5%, zirconium 0.3-0.45%, lithium 0.05-0.15%, silicon 0.019-0.025%, remaining be magnesium and other
Impurity.A small amount of zinc can significantly improve the tensile property of alloy with zirconium, and manganese can then increase the corrosion stability of alloy, add a small amount of
Lithium causes alloy strength to greatly improve.
Further, the other impurities content is no more than 0.2%.Impurity content is too high to influence the overall stabilization of alloy
Property.
Further, single impurity content is no more than 0.02% in the other impurities, and single impurity content is too high to be made
Alloy is obtained toughness deficiency occur or influence tensile property.
Further, the stamping parts thickness is no more than 6mm, and because alloy rigidity is high, more than 6mm, then ram ratio is relatively tired
It is difficult.
Further, it is made up of the following material in terms of mass fraction:Aluminium 8%, zinc 1.0%, manganese 0.35%, zirconium 0.3%,
Lithium 0.06%, silicon 0.02%, remaining is magnesium and other impurities.
The beneficial effects of the present invention are:The present invention is used as electric accessory motor, has frivolous, the good, dimensional stability of rigidity
Well, the features such as ageing resistace is good, and the present invention improves magnesium alloy formula so that the magnesium alloy as stamping material is drawn
Stretch that performance is good, corrosion stability is strong, intensity is high.
Embodiment
Embodiment 1,
A kind of magnesium alloy stamping parts, it is made up of the following material in terms of mass fraction:Aluminium 8%, zinc 1.0%, manganese
0.35%th, zirconium 0.3%, lithium 0.06%, silicon 0.02%, remaining is magnesium and other impurities, and wherein other impurities are no more than 0.2%,
Single impurity content is no more than 0.02%.
Embodiment 2,
A kind of magnesium alloy stamping parts, it is made up of the following material in terms of mass fraction:Aluminium 8.5%, zinc 1.5%, manganese
0.4%th, zirconium 0.4%, lithium 0.08%, silicon 0.025%, remaining is magnesium and other impurities.Wherein other impurities are no more than 0.2%,
Single impurity content is no more than 0.02%.
Claims (5)
- A kind of 1. magnesium alloy stamping parts, it is characterised in that:It is made up of the following material in terms of mass fraction:Aluminium 7.5-8.5%, Zinc 1.0-1.5%, manganese 0.25-0.5%, zirconium 0.3-0.45%, lithium 0.05-0.15%, silicon 0.019-0.025%, remaining is magnesium And other impurities.
- A kind of 2. magnesium alloy stamping parts as claimed in claim 1, it is characterised in that:The other impurities content is no more than 0.2%.
- A kind of 3. magnesium alloy stamping parts as claimed in claim 2, it is characterised in that:Single impurity contains in the other impurities Amount is no more than 0.02%.
- A kind of 4. magnesium alloy stamping parts as claimed in claim 1, it is characterised in that:The stamping parts thickness is no more than 6mm.
- A kind of 5. magnesium alloy stamping parts as claimed in claim 1, it is characterised in that:By the following material in terms of mass fraction It is made:Aluminium 8%, zinc 1.0%, manganese 0.35%, zirconium 0.3%, lithium 0.06%, silicon 0.02%, remaining is magnesium and other impurities.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201610766713.8A CN107779711A (en) | 2016-08-30 | 2016-08-30 | A kind of magnesium alloy stamping parts |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201610766713.8A CN107779711A (en) | 2016-08-30 | 2016-08-30 | A kind of magnesium alloy stamping parts |
Publications (1)
Publication Number | Publication Date |
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CN107779711A true CN107779711A (en) | 2018-03-09 |
Family
ID=61440973
Family Applications (1)
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CN201610766713.8A Pending CN107779711A (en) | 2016-08-30 | 2016-08-30 | A kind of magnesium alloy stamping parts |
Country Status (1)
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CN (1) | CN107779711A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108411175A (en) * | 2018-04-19 | 2018-08-17 | 合肥博创机械制造有限公司 | A kind of corrosion resistance magnesium alloy and preparation method thereof |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1471591A (en) * | 2000-10-23 | 2004-01-28 | ��ɭ��³�������ɷݹ�˾ | Method for producing a magnesium hot strip |
CN1907833A (en) * | 2006-08-11 | 2007-02-07 | 苏州江南嘉捷电梯集团有限公司 | Steps of moving staircase and die casting technique thereof |
CN102424927A (en) * | 2011-12-06 | 2012-04-25 | 常熟市碧溪新城特种机械厂 | Magnesium-aluminum alloy and preparation method thereof |
CN103469131A (en) * | 2013-09-16 | 2013-12-25 | 内蒙古科技大学 | Intermediate billet preparation methods for analyzing texture and performance unevenness of magnesium alloy |
CN103572118A (en) * | 2013-11-01 | 2014-02-12 | 张家港市昊天金属科技有限公司 | Magnesium-aluminum alloy and production method thereof |
CN103643096A (en) * | 2013-12-13 | 2014-03-19 | 内蒙古科技大学 | Preparation method of high-performance magnesium alloy plate with double-phase structure |
CN104294123A (en) * | 2013-11-22 | 2015-01-21 | 深圳市长盈精密技术股份有限公司 | Magnesium-aluminum alloy material |
-
2016
- 2016-08-30 CN CN201610766713.8A patent/CN107779711A/en active Pending
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1471591A (en) * | 2000-10-23 | 2004-01-28 | ��ɭ��³�������ɷݹ�˾ | Method for producing a magnesium hot strip |
CN1907833A (en) * | 2006-08-11 | 2007-02-07 | 苏州江南嘉捷电梯集团有限公司 | Steps of moving staircase and die casting technique thereof |
CN102424927A (en) * | 2011-12-06 | 2012-04-25 | 常熟市碧溪新城特种机械厂 | Magnesium-aluminum alloy and preparation method thereof |
CN103469131A (en) * | 2013-09-16 | 2013-12-25 | 内蒙古科技大学 | Intermediate billet preparation methods for analyzing texture and performance unevenness of magnesium alloy |
CN103572118A (en) * | 2013-11-01 | 2014-02-12 | 张家港市昊天金属科技有限公司 | Magnesium-aluminum alloy and production method thereof |
CN104294123A (en) * | 2013-11-22 | 2015-01-21 | 深圳市长盈精密技术股份有限公司 | Magnesium-aluminum alloy material |
CN103643096A (en) * | 2013-12-13 | 2014-03-19 | 内蒙古科技大学 | Preparation method of high-performance magnesium alloy plate with double-phase structure |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108411175A (en) * | 2018-04-19 | 2018-08-17 | 合肥博创机械制造有限公司 | A kind of corrosion resistance magnesium alloy and preparation method thereof |
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