CN101381831A - High plasticity magnesium alloy - Google Patents
High plasticity magnesium alloy Download PDFInfo
- Publication number
- CN101381831A CN101381831A CNA2008101720502A CN200810172050A CN101381831A CN 101381831 A CN101381831 A CN 101381831A CN A2008101720502 A CNA2008101720502 A CN A2008101720502A CN 200810172050 A CN200810172050 A CN 200810172050A CN 101381831 A CN101381831 A CN 101381831A
- Authority
- CN
- China
- Prior art keywords
- magnesium alloy
- magnesium
- mass ratio
- alloy
- total mass
- 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.)
- Granted
Links
- 229910000861 Mg alloy Inorganic materials 0.000 title claims abstract description 70
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims abstract description 22
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical group [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims abstract description 22
- 229910052744 lithium Inorganic materials 0.000 claims abstract description 22
- 229910052749 magnesium Inorganic materials 0.000 claims abstract description 22
- 239000011777 magnesium Substances 0.000 claims abstract description 22
- 229910052727 yttrium Inorganic materials 0.000 claims abstract description 20
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims abstract description 20
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims abstract description 19
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims abstract description 19
- 229910052725 zinc Inorganic materials 0.000 claims abstract description 19
- 239000011701 zinc Substances 0.000 claims abstract description 19
- 229910052726 zirconium Inorganic materials 0.000 claims abstract description 19
- 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 abstract description 16
- 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
- 229920003023 plastic Polymers 0.000 claims description 19
- 239000004033 plastic Substances 0.000 claims description 19
- 239000013078 crystal Substances 0.000 abstract description 4
- 229910000765 intermetallic Inorganic materials 0.000 abstract description 4
- 238000005275 alloying Methods 0.000 abstract description 2
- 239000000203 mixture Substances 0.000 abstract description 2
- 229910045601 alloy Inorganic materials 0.000 description 9
- 239000000956 alloy Substances 0.000 description 9
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 238000000034 method Methods 0.000 description 8
- 229910000838 Al alloy Inorganic materials 0.000 description 6
- 238000003723 Smelting Methods 0.000 description 6
- 239000000306 component Substances 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 5
- 239000000758 substrate Substances 0.000 description 5
- 238000005266 casting Methods 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 239000004411 aluminium Substances 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 230000006698 induction Effects 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 230000035939 shock Effects 0.000 description 3
- 238000005496 tempering Methods 0.000 description 3
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 description 1
- 229910052684 Cerium Inorganic materials 0.000 description 1
- 229910001051 Magnalium Inorganic materials 0.000 description 1
- 229910000914 Mn alloy Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 229910052776 Thorium Inorganic materials 0.000 description 1
- 229910001093 Zr alloy Inorganic materials 0.000 description 1
- UQCVYEFSQYEJOJ-UHFFFAOYSA-N [Mg].[Zn].[Zr] Chemical compound [Mg].[Zn].[Zr] UQCVYEFSQYEJOJ-UHFFFAOYSA-N 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 239000003513 alkali Substances 0.000 description 1
- 239000002585 base Substances 0.000 description 1
- 229910052793 cadmium Inorganic materials 0.000 description 1
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 1
- ZMIGMASIKSOYAM-UHFFFAOYSA-N cerium Chemical compound [Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce][Ce] ZMIGMASIKSOYAM-UHFFFAOYSA-N 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 238000006477 desulfuration reaction Methods 0.000 description 1
- 230000023556 desulfurization Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- KBMLJKBBKGNETC-UHFFFAOYSA-N magnesium manganese Chemical group [Mg].[Mn] KBMLJKBBKGNETC-UHFFFAOYSA-N 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000003756 stirring Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Landscapes
- Manufacture And Refinement Of Metals (AREA)
Abstract
The invention discloses a high plasticity magnesium alloy, which comprises the compositions of magnesium, zinc and zirconium in set percentage by mass, and also comprises 23 to27 mass percent of lithium, 7 to 9 mass percent of manganese, and 4 to 6 mass percent of yttrium; and the mass percentages of magnesium, zinc and zirconium are 80 to 83 percent , 12 to 15 percent and 2 to 8 percent respectively. The high plasticity magnesium alloy avoids forming intermetallic compounds by adding such alloying element such as lithium, manganese and yttrium to change the crystal form of magnesium alloy, thereby improving the ductility and the processability of magnesium alloy.
Description
Technical field
The present invention relates to a kind of alloy, relate in particular to a kind of high plastic magnesium alloy.
Background technology
So-called magnesium alloy is to be that base adds other elementary composition alloys with magnesium.Be characterized in: density little (about 1.8g/cm3), the specific tenacity height, Young's modulus is big, and shock absorbing is good, and the loading capacity that withstands shocks is bigger than aluminium alloy, and the corrosive nature of anti-organism and alkali is good.Main alloy element has aluminium, zinc, manganese, cerium, thorium and a small amount of zirconium or cadmium etc.
What use was the widest at present is magnalium, secondly is magnesium-manganese alloy and magnesium zinc zirconium alloy.Be mainly used in industrial sectors such as Aeronautics and Astronautics, transportation, chemical industry, rocket.Be divided into wrought magnesium alloys and cast magnesium alloys two classes by the moulding method.
Magnesium alloy is the lightest metal in practical metal, and the proportion of magnesium approximately is 2/3 of aluminium, is 1/4 of iron.Therefore, magnesium alloy is widely used in portable apparatus and the automobile industry, reaches light-weighted purpose.
Though the proportion of magnesium alloy is heavier than plastics,, the intensity of unit weight and spring rate be than plastics height, so under the situation of same intensity component, it is thin and light that the component of magnesium alloy can be done than plastics.In addition, because therefore the specific tenacity of magnesium alloy, under the intensity that does not reduce component, can alleviate the weight of the component of aluminium or iron also than aluminium alloy and iron height.
Though the thermal conductivity of magnesium alloy is not as good as aluminium alloy,, exceed tens of times than plastics, therefore, used for magnesium alloy can be effectively be dispersed into the outside with the heat of inside on electric equipment products.
Therefore the electromagnetic wave shielding performance of magnesium alloy, uses magnesium alloy can save the electroplating work procedure of electromagnetic shielding film than electroplate the effective of screened film on plastics.
In elastic range, when magnesium alloy is subjected to shock load, the energy of absorption than Al-alloy parts big half, so magnesium alloy has good antidetonation noise abatement performance.
The magnesium alloy fusing point is lower than aluminium alloy fusing point, and the die cast performance is good.Mg alloy castings tensile strength and aluminum alloy casting are suitable, generally can reach 250MPA, reach as high as Mpa more than 600.
Magnesium alloy is also individual excellent corrosion resisting performance, capability of electromagnetic shielding, and shielding property can be accomplished 100% recycling.
Along with market constantly widening to magnesium products demand Application Areas, widespread use from Aeronautics and Astronautics, automobile component, iron and steel desulfurization, alloy pressuring casting, 3C Product, continuous research and development to the product for civilian use, and the further research of magnesium alloy technology, the development of magnesium products more and more shows the irreplaceable advantage of its uniqueness.But the manufacturing of magnesium alloy component mainly relies on casting, fusing/solidifying process, and bad processibility has at ambient temperature but become the bottleneck place of its widespread use.
Summary of the invention
The object of the present invention is to provide a kind of high plastic magnesium alloy,, improve the ductility of magnesium alloy under normal temperature environment whereby by adding the crystal habit that other metallic elements change magnesium alloy.
High plastic magnesium alloy of the present invention comprises magnesium, zinc, the zirconium of setting mass ratio, also comprises: to account for total mass ratio and be 23～27% lithium, account for total mass ratio be 7～9% manganese, account for total mass ratio is 4～6% yttrium; And the ratio of described magnesium, zinc, zirconium is respectively 80～83%, 12～15%, 2～8%.
In the high plastic magnesium alloy of the present invention, the ratio of described magnesium, zinc, zirconium is respectively 80%, 15%, 5%.
In the high plastic magnesium alloy of the present invention, described lithium accounts for that total mass ratio is 25%, manganese accounts for that total mass ratio is 8%, to account for total mass ratio be 5% to yttrium.
High plastic magnesium alloy of the present invention by adding alloying elements such as lithium, manganese, yttrium to change the crystal habit of magnesium alloy, is avoided forming intermetallic compound, thereby is improved the ductility and the processibility of magnesium alloy.
Embodiment
Below high plastic magnesium alloy of the present invention is elaborated.
High plastic magnesium alloy of the present invention comprises magnesium, zinc, the zirconium of setting mass ratio, also comprises: to account for total mass ratio and be 23～27% lithium, account for total mass ratio be 7～9% manganese, account for total mass ratio is 4～6% yttrium; And the ratio of described magnesium, zinc, zirconium is respectively 80～83%, 12～15%, 2～8%.
Wherein, preferred version is: described lithium accounts for that total mass ratio is 25%, manganese accounts for that total mass ratio is 8%, to account for total mass ratio be 5% to yttrium.And the ratio of described magnesium, zinc, zirconium is respectively 80%, 15%, 5%.
High plastic magnesium alloy of the present invention can make according to following method:
Step 101 places crucible with magnesium, zinc, the zirconium of setting mass ratio, and wherein, the ratio of described magnesium, zinc, zirconium is respectively 80～83%, 12～15%, 2～8%; Described crucible places vacuum or is full of the smelting furnace of rare gas element.
Because magnesium and oxygen have very strong avidity, therefore when making high plastic magnesium alloy, need in vacuum melting furnace, handle magnesium alloy, or in the smelting furnace that is full of rare gas element of oxygen-free gas, handle.The vacuum tightness of smelting furnace or oxygen level can detect by outer connected control system.
The magnesium of described setting mass ratio, zinc, zirconium, specifically, the ratio of described magnesium, zinc, zirconium can be respectively 80%, 15%, 5%.
Step 102 is with material heat fused in the crucible and form even molten substrate.
In this step, can be by smelting furnace be carried out induction heating magnesium, zinc, the zirconium in the fusion crucible.When carrying out induction heating, described crucible is fixed in the interior induction heat coil of smelting furnace.
Step 103, to add in above-mentioned molten substrate that to account for total mass ratio be 23～27% lithium, account for total mass ratio be 7～9% manganese, account for total mass ratio is 4～6% yttrium, and fully stirs.
In this step, to account for total mass ratio be 25% lithium to preferred version in order to add in molten substrate, account for total mass ratio is 8% manganese, account for total mass ratio is 5% yttrium.
When adding to lithium, manganese, yttrium in the molten substrate, needing the control temperature of smelting furnace is between 650 to 680 degrees centigrade.
Step 104 molten substrate of having added above-mentioned lithium, manganese, yttrium is injected mold, and cooled and solidified forms magnesium alloy ingot.
The formed magnesium alloy ingot of this step can carry out extrusion molding at normal temperatures, and this magnesium alloy ingot has high plasticity.
For improving its performance, also can be before extruding, with ingot bar tempering 2 to 3 hours between 350 to 400 degrees centigrade, extruding when being cooled to 150 to 200 degrees centigrade again.Perhaps, with ingot bar tempering 2 to 3 hours between 350 to 400 degrees centigrade, push when being cooled to normal temperature again.
Following table has been listed the yield strength when metals such as lithium, manganese, yttrium, zinc, zirconium account for different total mass ratios in the magnesium alloy and the relativity of ductility.
Described magnesium alloy (common) is the commercially available ordinary magnesium alloy product that does not add metallic elements such as lithium, manganese, yttrium, described magnesium alloy 1～magnesium alloy 5 is the magnesium alloy ingot among the present invention who gets according to the aforesaid method manufacturing, the size of described each magnesium alloy ingot is 100mm*80mm*50mm, and, be squeezed into the thick thin plate of 0.15mm at normal temperatures 350 degrees centigrade of tempering 2 hours.The magnesium alloy ingot that should be noted that the method for the invention manufacturing can not only be squeezed into thin plate, but can be squeezed into any desired form.
| Lithium (%) | Yttrium (%) | Manganese (%) | Zinc (%) | Zirconium (%) | Yield strength (MPa) | Ductility (%) | |
| Magnesium alloy (common) | 5 | 110 | 13 | ||||
| Magnesium alloy 1 | 23.1 | 4.3 | 7.5 | 7.8 | 5.2 | 145 | 45 |
| Magnesium alloy 2 | 24.3 | 4.9 | 7.8 | 7.6 | 5.04 | 163 | 42 |
| Magnesium alloy 3 | 25 | 5 | 8 | 7.4 | 4.96 | 175 | 45 |
| Magnesium alloy 4 | 25.1 | 5.1 | 8.3 | 7.38 | 4.92 | 171 | 47 |
| Magnesium alloy 5 | 26.8 | 5.6 | 8.8 | 7.06 | 4.7 | 141 | 49 |
As can be seen from the above table:
From the contrast of the yield strength of ordinary magnesium alloy, magnesium alloy 1, magnesium alloy 2, magnesium alloy 3, magnesium alloy 4, magnesium alloy 5 and ductility as can be seen, added after lithium, manganese, the yttrium, the yield strength and the ductility of magnesium alloy are significantly improved.And when interpolation accounted for total mass ratio and is 25% lithium, 5% yttrium, 8% manganese, its yield strength reached maximum, and afterwards, along with the rising that lithium, manganese, yttrium account for total mass ratio, its yield strength begins to reduce, and ductility then is to strengthen always.
The characteristic of magnesium, manganese, lithium, yittrium alloy is to have higher intensity, higher ductility and lower density, meets light, thin, short and little industrial requirements.When lithium content surpass mass percent 10% the time, can form body-centered cubic structure.By increasing lithium content, body-centered cubic structure increases, and this means the ductility that can improve alloy apace.Yet excessive additional elements will hinder alloy strength, therefore, add yttrium again and will keep alloy strength.
The reason that magnesium alloy has bad ductility is its hexagonal lattice structure and forms hard intermetallic compound.In the method for the invention, change the magnesium alloy crystal habit and avoid forming intermetallic compound by adding the specific alloy element, thereby improve ductility and processibility.The high ductibility magnesium alloy that gets according to the method for the invention manufacturing can be squeezed into 0.15 millimeter thin plate, and can carry out deep stamping at normal temperatures, thereby can be applied on automobile, 3C Product, vessel and some the office automation products.
Although embodiment of the present invention are open as above, but it is not restricted to listed utilization in specification sheets and the embodiment, it can be applied to various suitable the field of the invention fully, for those skilled in the art, can easily realize other modification, therefore under the universal that does not deviate from claim and equivalency range and limited, the legend that the present invention is not limited to specific details and illustrates here and describe.
Claims (3)
1. a high plastic magnesium alloy comprises magnesium, zinc, the zirconium of setting mass ratio, it is characterized in that, also comprises: to account for total mass ratio and be 23～27% lithium, account for total mass ratio be 7～9% manganese, account for total mass ratio is 4～6% yttrium;
And the ratio of described magnesium, zinc, zirconium is respectively 80～83%, 12～15%, 2～8%.
2. high plastic magnesium alloy as claimed in claim 1 is characterized in that the ratio of described magnesium, zinc, zirconium is respectively 80%, 15%, 5%.
3. high plastic magnesium alloy as claimed in claim 1 or 2 is characterized in that, described lithium accounts for that total mass ratio is 25%, manganese accounts for that total mass ratio is 8%, to account for total mass ratio be 5% to yttrium.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2008101720502A CN101381831B (en) | 2008-10-29 | 2008-10-29 | High plasticity magnesium alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2008101720502A CN101381831B (en) | 2008-10-29 | 2008-10-29 | High plasticity magnesium alloy |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101381831A true CN101381831A (en) | 2009-03-11 |
| CN101381831B CN101381831B (en) | 2010-06-09 |
Family
ID=40461882
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2008101720502A Expired - Fee Related CN101381831B (en) | 2008-10-29 | 2008-10-29 | High plasticity magnesium alloy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101381831B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106244879A (en) * | 2016-08-26 | 2016-12-21 | 余姚市婉珍五金厂 | Alloy material that a kind of railroad rail is special and preparation method thereof |
| CN106811640A (en) * | 2015-11-30 | 2017-06-09 | 中国科学院金属研究所 | A kind of high-strength high-plastic magnesium lithium alloy of novel ultra-light and preparation method thereof |
| EP3650561A1 (en) | 2018-11-08 | 2020-05-13 | Citic Dicastal Co., Ltd. | Plastic wrought magnesium alloy and preparation method thereof |
| EP4144875A1 (en) | 2021-09-03 | 2023-03-08 | CITIC Dicastal Co., Ltd | Magnesium alloy for wheel and preparation method thereof |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1187305A (en) * | 1967-05-22 | 1970-04-08 | Dow Chemical Co | Process for production of Extruded Magnesium-Lithium Alloy Articles |
| CN1238544C (en) * | 2003-06-17 | 2006-01-25 | 沈阳工业大学 | Magnesium-manganese intermediate alloy and preparing method thereof |
| CN1297676C (en) * | 2004-11-11 | 2007-01-31 | 重庆大学 | High plasticity magnesium alloy containing rare-earth yttrium |
| CN1281776C (en) * | 2004-12-01 | 2006-10-25 | 北京航空航天大学 | Aluminum magnesium containing alloy materials and method for making same |
| CN100432258C (en) * | 2006-11-01 | 2008-11-12 | 中国科学院金属研究所 | Quasi crystal phase fortified magnesium lithium alloy and its preparation method |
| CN101020981A (en) * | 2007-03-26 | 2007-08-22 | 重庆大学 | Mg-Zn-Mn alloy material with high Zn content |
| CN100436624C (en) * | 2007-06-22 | 2008-11-26 | 西安工业大学 | High-intensity thermal deformation resistant magnesium alloy |
-
2008
- 2008-10-29 CN CN2008101720502A patent/CN101381831B/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106811640A (en) * | 2015-11-30 | 2017-06-09 | 中国科学院金属研究所 | A kind of high-strength high-plastic magnesium lithium alloy of novel ultra-light and preparation method thereof |
| CN106244879A (en) * | 2016-08-26 | 2016-12-21 | 余姚市婉珍五金厂 | Alloy material that a kind of railroad rail is special and preparation method thereof |
| EP3650561A1 (en) | 2018-11-08 | 2020-05-13 | Citic Dicastal Co., Ltd. | Plastic wrought magnesium alloy and preparation method thereof |
| EP4144875A1 (en) | 2021-09-03 | 2023-03-08 | CITIC Dicastal Co., Ltd | Magnesium alloy for wheel and preparation method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101381831B (en) | 2010-06-09 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN101463440B (en) | Aluminum based composite material for piston and preparation thereof | |
| CN100547100C (en) | Contain the magnesium alloy of mishmetal, the wrought magnesium alloy of producing the method for the wrought magnesium alloy that contains mishmetal and producing thus | |
| EP3392358B1 (en) | Low-cost high-heat-conduction die-casting magnesium alloy and manufacturing method therefor | |
| CN110218885B (en) | High-strength and high-toughness extrusion casting aluminum alloy and preparation method thereof | |
| CN109518041B (en) | It is a kind of while improving that pack alloy is thermally conductive and the compounding method of mechanical property | |
| CN104789805B (en) | A kind of preparation method of carbon nano-tube reinforced metal-matrix composite material | |
| JP5035717B2 (en) | Superplastic magnesium alloy manufacturing method from grain boundary precipitation type magnesium alloy scrap | |
| CN104561688A (en) | Heat-resistant cast aluminum alloy and gravity casting method thereof | |
| CN110643862A (en) | Aluminum alloy for new energy automobile battery shell and pressure casting preparation method thereof | |
| JP2007040914A (en) | Aluminum powder alloy composite for absorbing neutron, manufacturing method therefor, and basket manufactured using the same | |
| CN103667809B (en) | High-strength anti-corrosion samarium-yttrium rare earth aluminum alloy for heat exchanger and manufacture method thereof | |
| CN116200632B (en) | High-strength and high-toughness die-casting aluminum alloy, and preparation method and application thereof | |
| CN101381831B (en) | High plasticity magnesium alloy | |
| CN107937768B (en) | Extrusion casting aluminum alloy material and preparation method thereof | |
| CN108118226B (en) | High-thermal-conductivity, corrosion-resistant and heat-resistant die-casting magnesium alloy and manufacturing method thereof | |
| CN101423899B (en) | Method for manufacturing high plastic magnesium alloy ingot | |
| CN102534311A (en) | Aluminium calcium carbon grain refiner for Mg-Al series magnesium alloy and preparation method and application thereof | |
| CN101407018B (en) | Method for manufacturing magnesium alloy extruded tube | |
| CN101381830B (en) | magnesium alloy with high ductibility | |
| CN101418405B (en) | Method for manufacturing wrought magnesium alloy for high-speed extrusion | |
| CN101407865B (en) | Method for manufacturing high ductibility magnesium alloy | |
| CN105986136A (en) | High-performance aluminum alloy added with rare earth element and preparation method of high-performance aluminum alloy | |
| CN112894191B (en) | Band-shaped brazing filler metal for lap brazing of copper plates and aluminum plates and preparation method thereof | |
| CN104561717A (en) | High-performance heat-resistant cast magnesium alloy and preparation method thereof | |
| CN101407898B (en) | Method for manufacturing magnesium alloy extrusion parts |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: BEIJING NORTH CHINA LIGHT ALLOY CO., LTD. Free format text: FORMER OWNER: TONG ZHONGSHENG Effective date: 20110318 Free format text: FORMER OWNER: SUN JINFENG WU XUEYUN |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 037500 XIMAZHUANG VILLAGE, GUANGLING COUNTY, DATONG CITY, SHANXI PROVINCE TO: 102211 NO. 594, MENGZU VILLAGE, BAISHAN TOWN, CHANGPING DISTRICT, BEIJING |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20110318 Address after: 102211 Beijing city of Changping District Bai Shan Zhen Meng Lizu Village No. 594 Patentee after: BEIJING NORTH LIGHT ALLOY Co.,Ltd. Address before: 037500 Shanxi province Datong Guangling County Horse Village Co-patentee before: Sun Jinfeng Patentee before: Tong Zhong Sheng Co-patentee before: Wu Xueyun |
|
| ASS | Succession or assignment of patent right |
Owner name: TONG ZHONGSHENG Effective date: 20120627 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20120627 Address after: 102211 Beijing city of Changping District Bai Shan Zhen Meng Lizu Village No. 594 Co-patentee after: Tong Zhong Sheng Patentee after: BEIJING NORTH LIGHT ALLOY Co.,Ltd. Address before: 102211 Beijing city of Changping District Bai Shan Zhen Meng Lizu Village No. 594 Patentee before: BEIJING NORTH LIGHT ALLOY Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210308 Address after: 037304 no.1169 Yunzhou street, equipment manufacturing industrial park, Datong City, Shanxi Province Patentee after: Datong shangmg Technology Co.,Ltd. Address before: No. 594, Menciu village, Baishan Town, Beijing, Beijing Patentee before: BEIJING NORTH LIGHT ALLOY Co.,Ltd. Patentee before: Tong Zhong Sheng |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20100609 |