CN107779711A - A kind of magnesium alloy stamping parts - Google Patents

A kind of magnesium alloy stamping parts Download PDF

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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
Authority
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.)
Pending
Application number
CN201610766713.8A
Other languages
Chinese (zh)
Inventor
徐亚敏
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.)
Jiangsu Fenghuang Wood Industry Co Ltd
Original Assignee
Jiangsu Fenghuang Wood Industry Co Ltd
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 Jiangsu Fenghuang Wood Industry Co Ltd filed Critical Jiangsu Fenghuang Wood Industry Co Ltd
Priority to CN201610766713.8A priority Critical patent/CN107779711A/en
Publication of CN107779711A publication Critical patent/CN107779711A/en
Pending 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

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

A kind of magnesium alloy stamping parts
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)

  1. 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.
  2. 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%.
  3. 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%.
  4. 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.
  5. 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.
CN201610766713.8A 2016-08-30 2016-08-30 A kind of magnesium alloy stamping parts Pending CN107779711A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
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
CN201610766713.8A CN107779711A (en) 2016-08-30 2016-08-30 A kind of magnesium alloy stamping parts

Publications (1)

Publication Number Publication Date
CN107779711A true CN107779711A (en) 2018-03-09

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610766713.8A Pending CN107779711A (en) 2016-08-30 2016-08-30 A kind of magnesium alloy stamping parts

Country Status (1)

Country Link
CN (1) CN107779711A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (7)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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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