CN102618759B - Low-shrinkage magnesium alloy - Google Patents

Low-shrinkage magnesium alloy Download PDF

Info

Publication number
CN102618759B
CN102618759B CN201210107724.7A CN201210107724A CN102618759B CN 102618759 B CN102618759 B CN 102618759B CN 201210107724 A CN201210107724 A CN 201210107724A CN 102618759 B CN102618759 B CN 102618759B
Authority
CN
China
Prior art keywords
magnesium alloy
alloy
present
shrinkage
weight percent
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.)
Expired - Fee Related
Application number
CN201210107724.7A
Other languages
Chinese (zh)
Other versions
CN102618759A (en
Inventor
冯俊
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.)
Su Xiaohu
Sun Guirong
Wang Xinhong
Xia Yunyun
Original Assignee
Jianghan University
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 Jianghan University filed Critical Jianghan University
Priority to CN201210107724.7A priority Critical patent/CN102618759B/en
Publication of CN102618759A publication Critical patent/CN102618759A/en
Application granted granted Critical
Publication of CN102618759B publication Critical patent/CN102618759B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Manufacture And Refinement Of Metals (AREA)

Abstract

The invention discloses low-shrinkage magnesium alloy, and belongs to the field of magnesium alloy. The low-shrinkage magnesium alloy comprises the following elements in percent by weight: 1.5 to 25% of Al (aluminium), 0.13 to 2% of Mn (manganese), 0.0002 to 16% of rare earth, 0.0002 to 4% of Nb (niobium), 0.0002 to 9% of Li (lithium), and Mg (magnesium) in balancing amount. The beta-phase structure is changed by adding the rare earth element and the Nb element in the magnesium alloy, the grain refinement is achieved through adding the Li element, and through the combination of the elements, the crystallization latent heat is changed in alloy solidification, thereby obtaining the low-shrinkage magnesium alloy which has an excellent filling capacity, low shrinkage, excellent mechanical property, machinability, flowability and good die-casting performance and is suitable for casting.

Description

A kind of low-shrinkage magnesium alloy
Technical field
The present invention relates to a kind of magnesium alloy, particularly a kind of MgAlMn is low-shrinkage magnesium alloy.
Background technology
Along with scientific and technological development, the vehicles taking automobile as representative need to, by alleviating the weight of vehicle body, further be researched and developed the product innovation that fuel availability is higher.In automobile industry, magnesium alloy, as a kind of novel lightweight metal material, is used for substituting traditional cast iron by automaker, to realize the object that alleviates tare.
At present, domestic MgAlMn is that the diecast magnesium alloy trade mark has YM202, YM203, YM204, YM205; The MgAlMn of USS ASTM B is that the diecast magnesium alloy trade mark has AM50A, AM60A, AM60B; The MgAlMn of Nippon Standard JIS H is that the diecast magnesium alloy trade mark has MDC2B, MDC4, MDC5; The MgAlMn of European standard EN is that the diecast magnesium alloy trade mark has EN-MC21210, EN-MC21220, EN-MC21230.The alloy of these trades mark, mobility, mechanical property, die casting performance are all very good, are widely used in the cast forms such as permanent mold casting, precision casting, low-pressure casting, die casting, semi-solid casting, sand mold casting.
Find that prior art at least exists following problem realizing contriver in process of the present invention: magnesium alloy is in the time of casting, molten metal, in the process that is frozen into solid, is subject to the impact of volumetric shrinkage, and internal stress is very large, easily cause cast(ing) surface cracking, the phenomenon that foundry goods die sinking ruptures even occurs.The impact that this decrepitation is serious the application of cast magnesium alloys, have influence on magnesium alloy member size and qualification rate.Above-mentioned diecast magnesium alloy linear shrinkage ratio is 1.5-2%, cannot effectively avoid the cast(ing) surface cracking phenomena causing because of volumetric shrinkage.
Summary of the invention
In order to solve above-mentioned problems of the prior art, the embodiment of the present invention provides a kind of low-shrinkage magnesium alloy.Described technical scheme is as follows:
A kind of low-shrinkage magnesium alloy, described magnesium alloy is made up of Mg, Al, Mn, rare earth (RE), Nb, Li, its weight percent consists of Al 1.5-25%, Mn 0.13-2%, rare earth 0.0002-16%, Nb 0.0002-4%, Li 0.0002-9%, and all the other are Mg.
Wherein, described rare earth is at least one in Gd, Y, Sc, Sm, Pr, Yb, Nd, La, Ce, Tb, Dy, Ho and Er.
Preferably, described rare earth is at least one in Gd or Gd and Y, Sc, Sm, Pr, Yb, Nd, La, Ce, Tb, Dy, Ho and Er.
Preferably, its weight percent consists of Al 1.6-6.5%, Mn 0.13-0.7%, Gd 0.1-2%, Nb 0.05-1%, Li 0.02-2%, and all the other are Mg.
More have choosing, its weight percent consists of Al 4.4-6.5%, Mn 0.26-0.6%, Gd 0.1-0.8%, Nb 0.05-0.6%, Li 0.02-2%, and all the other are Mg.
Most preferably, its weight percent consists of Al 6%, Mn 0.45%, Gd 0.4%, Nb 0.2%, Li 0.5%, and all the other are Mg.
The beneficial effect that the technical scheme that the embodiment of the present invention provides is brought is: in magnesium alloy provided by the invention, RE can form MgRE compound with Mg, Nb can form some resistant to elevated temperatures metallic compounds with other elements (as Al), and Li has strong crystal grain thinning and purifies aluminium alloy effect.Due to the combined action of above-mentioned element, while making alloy graining, latent heat changes, under the heat absorption of above-mentioned element, heat release combined action, it is diecast magnesium alloy that the time that aluminium alloy provided by the invention keeps liquid in mould is obviously longer than existing AM, make alloy in process of setting, feeding is abundant, built-in thermal stress is little, heat crack resistance is good, simultaneously, because magnesium alloy liquid volume and solid-state volume variation that the embodiment of the present invention provides are very little, therefore there is the feature that cavity filling ability is good, shrinking percentage is low.The characteristics such as alloy of the present invention also has good mechanical property, and machinability, mobility and die casting are good.
Embodiment
For making the object, technical solutions and advantages of the present invention clearer, below embodiment of the present invention is described further in detail.
Manufacture craft, the heat treating method of the magnesium alloy that the embodiment of the present invention provides are described as follows:
1, the magnesium alloy that the embodiment of the present invention provides can be made by following three kinds of melting technologies:
Technique one: the magnesium alloy composition and the content alloyage that provide according to the embodiment of the present invention; in resistance furnace, add magnesium ingot, aluminium ingot, MgMn master alloy, AlNb master alloy or NbAl master alloy; heat up to resistance furnace used, in the time that the above-mentioned metal adding melts soon, adopt argon shield or magnesium alloy covering agent protection.While being warmed up to 720 DEG C-780 DEG C, add MgRE master alloy (as MgGd, MgY, MgNd etc.) or AlRE master alloy, AlLi master alloy or MgLi master alloy, and stir, leave standstill insulation 30 minutes at 720 DEG C-780 DEG C, obtain aluminium alloy.Water a fritter sample with gained aluminium alloy, detect its Melting Quality, as: carry out gas content inspection according to gas content inspection method, if second-rate, need carry out refining treatment; If up-to-standard, described aluminium alloy temperature adjustment to 700 DEG C-740 DEG C is skimmed, then pour into a mould, obtain the foundry goods of alloy of the present invention.
In this technique, resistance furnace also can replace with other smelting furnaces; Magnesium alloy covering agent and master alloy product are market sale product; Refining treatment method adopts the ordinary method of the industry.
Technique two: the magnesium alloy composition and the content alloyage that provide according to the embodiment of the present invention, in vacuum oven, add aluminium ingot, Mn or Mn agent, AlNb master alloy or NbAl master alloy, be warming up to 820 DEG C, insulation 2-8 hour, then cool to 720 DEG C-780 DEG C, add magnesium ingot, RE, AlLi master alloy or MgLi master alloy.After added melting of metal, 720 DEG C-780 DEG C insulations 30 minutes, obtain aluminium alloy, adopt argon shield or magnesium alloy covering agent protection to prevent aluminium alloy oxidation.Water a fritter sample with gained aluminium alloy, detect its Melting Quality, as: the inspection of gas content, if second-rate, need carry out refining treatment; If up-to-standard, described aluminium alloy temperature adjustment to 700 DEG C-740 DEG C is skimmed, then pour into a mould, obtain the foundry goods of alloy of the present invention.
In this technique, vacuum oven can substitute with other smelting furnaces such as main frequency furnaces; Magnesium alloy covering agent, rare earth, Mn agent, master alloy are sell goods on market; Refining treatment method adopts the ordinary method of the industry.
Technique three: the magnesium alloy composition and the content alloyage that provide according to the embodiment of the present invention; in smelting furnace, adding standard brand MgAlMn is diecast magnesium alloy, AlNb master alloy or NbAl master alloy, and above-mentioned metal adopts argon shield or magnesium alloy covering agent protection while fusing soon.While being warmed up to 720 DEG C-780 DEG C, add MgRE master alloy (as MgGd, MgY, MgNd etc.) or AlRE master alloy, AlLi master alloy or MgLi master alloy, and stir, leave standstill insulation 30 minutes at 720 DEG C-780 DEG C, obtain aluminium alloy.Water a fritter sample with gained aluminium alloy, detect its Melting Quality, as: carry out gas content inspection according to gas content inspection method, if second-rate, need carry out refining treatment; If up-to-standard, described aluminium alloy temperature adjustment to 700 DEG C-740 DEG C is skimmed, then pour into a mould, obtain the foundry goods of alloy of the present invention.
In this technique, magnesium alloy covering agent and master alloy are sell goods on market; Refining treatment method adopts the ordinary method of the industry.
Thermal treatment and the treatment process thereof of the magnesium alloy that 2, the embodiment of the present invention provides:
Die casting in the magnesium alloy that the embodiment of the present invention provides can not heat-treated, and the cast member of other form can be heat-treated, and generally adopts T4 solution treatment.T4 solid solution treatment process is: cast member is warming up in chamber type electric resistance furnace to 390 DEG C, argon shield, is incubated 16 hours, cast member come out of the stove after shrend, 50 DEG C of water temperatures.
Be subject to fusion process to select the impact of some other inevitable factor in the purity of raw material and melting, castingprocesses, the diecast magnesium alloy that the embodiment of the present invention provides may contain inevitable impurity, as Zn, Fe, Cu, Be etc., as long as described impurity does not cause obvious impact to the performance of magnesium alloy, and total impurities is controlled at the weight percent < 0.5% in described magnesium alloy finished product, in the weight percent < 0.1% of single contaminant in described magnesium alloy finished product, exist trace impurity also to allow.
Embodiment 1
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts die cast, and the weight percent of described magnesium alloy consists of Al 1.5%, Mn 0.13%, Sm 0.0002%, Nb 0.0002%, Li 0.0002%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 2
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts semi-solid casting, and the weight percent of described magnesium alloy consists of Al 25%, Mn 2%, Y 16%, Nb 4%, Li 9%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 3
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts Hpdc, and the weight percent of magnesium alloy consists of Al 6%, Mn 0.2%, Gd 0.2%, Nb 1%, Li 0.6%, and all the other are Mg;
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 4
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts low-pressure casting, and the weight percent of described magnesium alloy consists of Al 1.6%, Mn 0.13%, Ho 0.1%, Nb 0.05%, Li 0.02%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 5
Prepare magnesium alloy by step described in above-mentioned technique three, described standard brand diecast magnesium alloy used in preparation process is AM60B, foundry goods adopts precision casting, and the weight percent of described magnesium alloy consists of Al 6.5%, Mn 0.7%, Gd 2%, Nb 1%, Li 2%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 6
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts sand mold casting, and the weight percent of described magnesium alloy consists of Al 4.4%, Mn 0.26%, Gd 0.1%, Nb 0.05%, Li 0.02%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 7
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts Hpdc, and the weight percent of described magnesium alloy consists of Al 6.5%, Mn 0.6%, Gd 0.8%, Nb 0.6%, Li 2%, and all the other are Mg.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 8
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts Hpdc, and the weight percent of described magnesium alloy consists of Al 6.5%, Mn 0.6%, Gd 0.4%, Nd 0.4%, Nb 0.6%, Li 2%, and all the other are Mg.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 9
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts Hpdc, and the weight percent of described magnesium alloy consists of Al 6.5%, Mn 0.6%, Ce 0.8%, Nb 0.6%, Li 2%, and all the other are Mg.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 10
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts die cast, and the weight percent of described magnesium alloy consists of Al 2%, Mn 0.2%, La 1.2%, Nb 0.8%, Li 0.1%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 11
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts sand mold casting, and the weight percent of described magnesium alloy consists of Al 6%, Mn 0.5%, Tb 0.6%, Nb 0.4%, Li 0.5%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 12
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts die cast, and the weight percent of described magnesium alloy consists of Al 10%, Mn 1%, Dy 8%, Nb 2%, Li 1.5%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 13
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts die cast, and the weight percent of described magnesium alloy consists of Al 3%, Mn 0.65%, Er 1%, Nb 0.7%, Li 0.8%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 14
Prepare magnesium alloy by step described in above-mentioned technique two, foundry goods adopts die cast, and the weight percent of described magnesium alloy consists of Al 5%, Mn 0.5%, Sc 0.5%, Nb 0.8%, Li 0.4%, and all the other are Mg.
Foundry goods is heat-treated.The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Embodiment 15
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts Hpdc, and described magnesium alloy weight percent consists of Al6%, Mn 0.45%, Gd 0.4%, Nb 0.2%, Li 0.5%, and all the other are Mg.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Comparative example 1
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts Hpdc, and described magnesium alloy weight percent consists of Al6%, Mn 0.45%, Gd 0.4%, Nb 0.2%, and all the other are Mg and inevitable impurity.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Comparative example 2
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts Hpdc, and described magnesium alloy weight percent consists of Al6%, Mn 0.45%, Gd 0.4%, Li 0.5%, and all the other are Mg and inevitable impurity.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
Comparative example 3
Prepare magnesium alloy by step described in above-mentioned technique one, foundry goods adopts Hpdc, and described magnesium alloy weight percent consists of Al6%, Mn 0.45%, Gd 0.4%, and all the other are Mg and inevitable impurity.
The performance of the Mg alloy castings that the present embodiment provides is referring to table 1.
The Mg alloy castings that each embodiment provides above can contain micro-impurity, the weight percent < 0.5% of described inevitable total impurities in described magnesium alloy finished product, the weight percent < 0.1% of single contaminant in described magnesium alloy finished product.
The linear shrinkage ratio of the Mg alloy castings that various embodiments of the present invention and comparative example provide is referring to table 1.
The linear shrinkage ratio table of the Mg alloy castings that the each embodiment of table 1 provides
As shown in Table 1, the linear shrinkage ratio of the Mg alloy castings that the embodiment of the present invention provides is all less than 1%, is diecast magnesium alloy well below existing MgAlMn, has good hot-cracking resistance; Simultaneously referring to embodiment 15 and comparative example 1-3, the Mg alloy castings that the embodiment of the present invention provides, compared with not adding Li or Nb or Mg alloy castings that both all do not add, has better hot-cracking resistance; The linear shrinkage ratio of embodiment 7,8 and 15 is lower than other embodiment, and the scope of embodiment 7,8 and 15 each components is in Al4.4-6.5%, Mn 0.26-0.6%, Gd 0.1-0.8%, Nb 0.05-0.6%, Li 0.02-2%; By the contrast between embodiment 7-9, the known RE containing has the effect of Gd better; The linear shrinkage ratio of the Mg alloy castings that embodiment 15 provides is minimum, and the cast magnesium alloys hot-cracking resistance that embodiment 15 provides is the strongest.
The foregoing is only preferred embodiment of the present invention, in order to limit the present invention, within the spirit and principles in the present invention not all, any amendment of doing, be equal to replacement, improvement etc., within all should being included in protection scope of the present invention.

Claims (6)

1. a low-shrinkage magnesium alloy, it is characterized in that, described magnesium alloy is made up of Mg, Al, Mn, rare earth, Nb, Li, its weight percent consists of Al1.5-25%, Mn0.13-2%, rare earth 0.0002-16%, Nb0.0002-4%, Li0.0002-9%, all the other are Mg, described Nb adds in described magnesium alloy by the form of AlNb master alloy or NbAl master alloy, described Li adds in described magnesium alloy by the form of AlLi master alloy or MgLi master alloy, and the smelting temperature of the master alloy of described Nb is 720 DEG C-780 DEG C or 820 DEG C.
2. magnesium alloy according to claim 1, is characterized in that, described rare earth is at least one in Gd, Y, Sc, Sm, Pr, Yb, Nd, La, Ce, Tb, Dy, Ho and Er.
3. magnesium alloy according to claim 1 and 2, is characterized in that, described rare earth is at least one in Gd or Gd and Y, Sc, Sm, Pr, Yb, Nd, La, Ce, Tb, Dy, Ho and Er.
4. magnesium alloy according to claim 3, is characterized in that, its weight percent consists of Al1.6-6.5%, Mn0.13-0.7%, Gd0.1-2%, Nb0.05-1%, Li0.02-2%, and all the other are Mg.
5. magnesium alloy according to claim 4, is characterized in that, its weight percent consists of Al4.4-6.5%, Mn0.26-0.6%, Gd0.1-0.8%, Nb0.05-0.6%, Li0.02-2%, and all the other are Mg.
6. magnesium alloy according to claim 5, is characterized in that, its weight percent consists of Al6%, Mn0.45%, Gd0.4%, Nb0.2%, Li0.5%, and all the other are Mg.
CN201210107724.7A 2012-04-13 2012-04-13 Low-shrinkage magnesium alloy Expired - Fee Related CN102618759B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201210107724.7A CN102618759B (en) 2012-04-13 2012-04-13 Low-shrinkage magnesium alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210107724.7A CN102618759B (en) 2012-04-13 2012-04-13 Low-shrinkage magnesium alloy

Publications (2)

Publication Number Publication Date
CN102618759A CN102618759A (en) 2012-08-01
CN102618759B true CN102618759B (en) 2014-10-29

Family

ID=46558958

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201210107724.7A Expired - Fee Related CN102618759B (en) 2012-04-13 2012-04-13 Low-shrinkage magnesium alloy

Country Status (1)

Country Link
CN (1) CN102618759B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105256208A (en) * 2015-10-09 2016-01-20 天长市兴宇铸造有限公司 Boron nitride nanotube modifying Mg-Al-Mn magnesium alloy material for casting automobile parts and preparation method thereof
CN107779708B (en) * 2017-12-08 2019-08-23 浙江海洋大学 A kind of high intensity super-light Mg-Li alloy and preparation method thereof
JP2023132433A (en) * 2022-03-11 2023-09-22 株式会社日本製鋼所 Magnesium-lithium-aluminum-based alloy, method for manufacturing the same, and method for manufacturing molding composed of magnesium-lithium-aluminum-based alloy

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1276276A (en) * 1999-06-08 2000-12-13 三井金属矿业株式会社 Metal die device, die-casting method and die-cast articles
CN102230116A (en) * 2011-06-23 2011-11-02 江汉大学 High-hardness cast magnesium alloy

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08134581A (en) * 1994-11-14 1996-05-28 Mitsui Mining & Smelting Co Ltd Production of magnesium alloy

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1276276A (en) * 1999-06-08 2000-12-13 三井金属矿业株式会社 Metal die device, die-casting method and die-cast articles
CN102230116A (en) * 2011-06-23 2011-11-02 江汉大学 High-hardness cast magnesium alloy

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
JP特开平8-134581A 1996.05.28

Also Published As

Publication number Publication date
CN102618759A (en) 2012-08-01

Similar Documents

Publication Publication Date Title
CN102618758B (en) Cast magnesium alloy of low linear shrinkage
CN102618762B (en) Heat-resisting magnesium alloy
CN102618760B (en) MgAlZn series heat resistant magnesium alloy containing niobium
CN102994834B (en) Heatproof magnesium alloy containing Nb
CN102618757B (en) Heat-resistant magnesium alloy
CN102994835B (en) Heatproof magnesium alloy
CN102618764A (en) Magnesium alloy with hot cracking resistance and low linear shrinkage
JP2005264301A (en) Casting aluminum alloy, casting of aluminum alloy and manufacturing method therefor
CN101748299A (en) Method for manufacturing cast magnesium alloy
KR20160011136A (en) Magnesium alloy having improved corrosion resistance and method for manufacturing magnesium alloy member using the same
CN101671787A (en) Natural destressing die-casting aluminum alloy and preparation method thereof
CN102618765B (en) Magnesium alloy with hot cracking resistance and low linear shrinkage
CN105779838A (en) High-thermal-conductivity die-casting magnesium alloy and preparation technology thereof
CN102994847B (en) Heatproof magnesium alloy
CN105401013A (en) Cast aluminum alloy for automotive structural parts and preparation method thereof
CN103993213A (en) Method for preparing dual special structure combined reinforced Mg-Zn-Y alloy
CN102618759B (en) Low-shrinkage magnesium alloy
CN112981190A (en) Aluminum alloy for die casting and method for manufacturing cast aluminum alloy using the same
CN102994840B (en) MgAlZn heat resistance magnesium alloy
CN103667759B (en) Al-Mg-Si system alloy ��-Al grain-refining agent and its preparation method
JP4145242B2 (en) Aluminum alloy for casting, casting made of aluminum alloy and method for producing casting made of aluminum alloy
CN102618763A (en) Heat resistant magnesium alloy
CN106435304A (en) Anti-cracking aluminum alloy special for motor train unit gear case body and preparing method of anti-cracking aluminum alloy
CN102994836B (en) Tough magnesium alloy with high elongation rate
CN102994838B (en) MgAlSi heat resistance magnesium alloy

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
CB03 Change of inventor or designer information

Inventor after: Su Xiaohu

Inventor after: Sun Guirong

Inventor after: Wang Xinhong

Inventor after: Xia Yunyun

Inventor before: Feng Jun

CB03 Change of inventor or designer information
TR01 Transfer of patent right

Effective date of registration: 20171016

Address after: 025265 the Inner Mongolia Autonomous Region Chifeng City Linxi County Xinchengzi village four groups against the Kun Zhen Gang Gang

Co-patentee after: Sun Guirong

Patentee after: Su Xiaohu

Co-patentee after: Wang Xinhong

Co-patentee after: Xia Yunyun

Address before: 430056 Hubei, Zhuankou economic and Technological Development Zone, the new road,, Jianghan University, No. 8

Patentee before: Jianghan University

TR01 Transfer of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20141029

Termination date: 20180413

CF01 Termination of patent right due to non-payment of annual fee