CN105220041A - A kind of high-strength wrought magnesium alloys and preparation method thereof - Google Patents

A kind of high-strength wrought magnesium alloys and preparation method thereof Download PDF

Info

Publication number
CN105220041A
CN105220041A CN201410272831.4A CN201410272831A CN105220041A CN 105220041 A CN105220041 A CN 105220041A CN 201410272831 A CN201410272831 A CN 201410272831A CN 105220041 A CN105220041 A CN 105220041A
Authority
CN
China
Prior art keywords
alloy
strength
magnesium alloys
wrought magnesium
strength wrought
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
Application number
CN201410272831.4A
Other languages
Chinese (zh)
Other versions
CN105220041B (en
Inventor
陈荣石
闫宏
柯伟
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.)
Institute of Metal Research of CAS
Original Assignee
Institute of Metal Research of CAS
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 Institute of Metal Research of CAS filed Critical Institute of Metal Research of CAS
Priority to CN201410272831.4A priority Critical patent/CN105220041B/en
Publication of CN105220041A publication Critical patent/CN105220041A/en
Application granted granted Critical
Publication of CN105220041B publication Critical patent/CN105220041B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The invention discloses a kind of high-strength magnesium alloy and preparation method thereof, belong to light metal material technical field.Weight percentage, this magnesium alloy composition is: Zn2.0-6.5%, RE0.1-3.0%, Ca0.1-2.0%, and all the other are Mg and inevitable impurity; Also grain-refining agent Mn and/or Zr can be contained.Zn is main strengthening element in alloy, and it improves the room temperature strength of magnesium alloy by solution strengthening and Precipitation strengthening; Ca is for promoting precipitation, crystal grain thinning, raising alloy high-temp intensity; A small amount of RE is for suppressing recrystallize, and after refinement distortion, alloy grain and regulation and control texture, improve alloy plasticity.The present invention replaces expensive rare earth element by the common alloy element that employing is cheap, makes it to produce the strengthening effect same with rare-earth phase, replaces completely or reduces content of rare earth, while proof strength, reducing cost of alloy.

Description

A kind of high-strength wrought magnesium alloys and preparation method thereof
Technical field
The present invention relates to light metal material technical field, be specifically related to a kind of high-strength wrought magnesium alloys and preparation method thereof.
Background technology
Magnesium alloy, as a kind of novel light metallic substance, has the series of advantages such as density is low, specific tenacity is high, shock resistance, reusable edible, has broad application prospects.Especially along with the high speed development of the military industry fields such as the traffic and transport field such as aviation, high ferro and space flight, day by day urgent to the demand of high-strength wrought magnesium alloys.
At present, the high-strength wrought magnesium alloys of business only has AZ80 (Mg-8Al-0.4Zn) and ZK60 (Mg-6Zn-0.5Zr).Their tensile strength after distortion+aging strengthening model is about 300-350MPa, room temperature elongation 8%.And be applied in the tensile strength of traffic and transport field as the aluminium alloy of structural part at present generally higher than 400MPa, therefore high-strength magnesium alloy to be made to replace part aluminium alloy and to be applied in traffic and transport field, 400MPa is greater than in the urgent need to development tensile strength, and cost and the close low-cost high-strength wrought magnesium alloys of aluminium alloy.
By adding a small amount of rare earth element (1-3%RE) to AZ80 and ZK60 alloy, utilizing ternary precipitated phase to improve intensity, thus obtaining high-strength wrought magnesium alloys.As Chinese invention patent (denomination of invention: a kind of weldable deformable rare earth magnesium alloy with high intensity and high toughness, application number: 200610172788.X) disclose a kind of Mg-(5.5wt% ~ 6.4wt%) Zn-(0.7wt.% ~ 1.7wt%) Ym-(0.45wt% ~ 0.8wt%) Zr alloy, this alloy is under As-extruded, and room temperature average tensile strength is 340MPa.Disclose a kind of high-strength deforming magnesium alloy in CN101805865A patent, its chemical composition is Al:7.8 ~ 9.2%, Zn:0.2 ~ 0.8%, Mn:0.2 ~ 0.5%, the rare earth of 0.5 ~ 2.0%, the maximum tensile strength of acquisition is 360MPa, and maximum room temperature elongation is 11.5%.Mg-(4.5wt% ~ 5.5wt%) Zn-(0.5wt.% ~ 2.5wt%) Ce-(0.01wt.% ~ 0.2wt%) Ti alloy is disclosed in the patent of " a kind of Wrought magnesium alloys in high intensity, high plasticity and preparation method thereof ", room temperature average tensile strength after extruding is 360MPa, yield strength is 245MPa, elongation after fracture 7%.Above-mentioned alloy is on the basis of ZK60 or AZ80, adds a small amount of rare earth element (1 ~ 3wt%), puies forward heavy alloyed room temperature strength, hot strength and welding property.But the content of rare earth added in these alloys is less, and precipitating reinforcing effect is undesirable, its deformation states strength of alloy, all lower than 400MPa, can not meet the requirement of traffic and transport field to light material intensity.
Subsequently, people are by reducing Zn content and increasing content of rare earth, content of rare earth is made to reach more than 10wt%, develop the Mg-RE-Zn-Zr system alloy of the low zinc of high rare earth, the intensity of alloy is further increased by techniques such as extruding or rollings, its intensity can more than 400MPa, and in high-strength and high-ductility magnesium alloy and manufacture method thereof disclosed in patent CN101705404A, the intensity of alloy part reaches 400MPa; Also has [T.Homma in document, N.Kunito, andS.Kamado, Fabricationofextraordinaryhigh-strengthmagnesiumalloybyh otextrusion.ScriptaMaterialia, 2009.61 (6): p.644-647] mention Mg-10Gd-3Y-1Zn-0.5Zr alloy, after extruding and thermal treatment, tensile strength reaches 450MPa, and elongation reaches 6%.Due to rare earth element (alloy Rare-Earth Content the is greater than 10%) element containing a large amount of costliness in the Mg-RE-Zn-Zr system alloy of the low zinc of this kind of high rare earth; cost of alloy is caused to be multiplied (20 yuan/kilogram, magnesium; rare earth 300-500 unit/kilogram), thus this kind of high strength Mg-RE-Zn-Zr alloy is difficult to industrially obtain mass-producing application.
In sum, there is the shortcomings such as intensity does not reach that requirement or intensity reach more than 400MPa but cost is too high in the distortion high-strength magnesium alloy developed now.Therefore, in the urgent need to exploring and develop the Low-cost wrought magnesium alloy that a kind of tensile strength is greater than 400MPa, in order to meet the demand of the fields such as communications and transportation to light-weight high-strength material, the industrial application process of high-strength wrought magnesium alloys is promoted.
Summary of the invention
The problem of undercapacity or high cost is there is for existing wrought magnesium alloys, the invention provides a kind of high-strength wrought magnesium alloys and preparation method thereof, expensive rare earth element is replaced by adopting cheap common alloy element, make it to produce the strengthening effect same with rare-earth phase, replace completely or reduce content of rare earth, while proof strength, reducing cost of alloy.
Technical solution of the present invention is:
A kind of high-strength wrought magnesium alloys, weight percentage, this magnesium alloy composition is: Zn2.0-6.5%, RE0.1-3.0%, Ca0.1-2.0%, and all the other are Mg and inevitable impurity; Wherein: RE is rare earth element, RE can be one or more in Gd, Y, Ce, La, Nd and Er.
Also containing grain-refining agent in this magnesium alloy, described crystalline substance material fining agent is Mn and/or Zr, and the content of described Mn is 0.2-2.0wt% (being preferably 0.3-1.5wt%), and the content of Zr is 0.01-0.8wt% (being preferably 0.3-0.7wt%).
In magnesium alloy of the present invention, Zn content is preferably 2.0-6.0wt%, and RE content is preferably 0.3-1.5wt%, and Ca content is preferably 0.2-1.5wt%.
By above-mentioned alloying constituent batch mixing also obtained alloy cast ingot, alloy cast ingot, through viscous deformation hot-work, obtains high-strength wrought magnesium alloys of the present invention; Described viscous deformation hot-work be carry out extruding, the viscous deformation processing such as rolling or forging.
Principle of design of the present invention is as follows:
The present invention is by Mg-Zn alloy, adding a small amount of rare earth element makes itself and Mg, Zn form Mg-Zn-RE ternary precipitated phase, add cheap Ca element makes itself and Mg, Zn form Mg-Zn-Ca ternary precipitated phase simultaneously, can replace part Mg-Zn-RE precipitation strength phase; Add a small amount of Mn and or Zr element, refinement as-cast grain, and in conjunction with the Grain Refinement Effect of RE and Ca element in deformation process, realize the complex intensifying of refined crystalline strengthening and precipitation strength, both the content of rare earth can have been reduced, intensity can also be improved further, obtain a kind of low-cost high-strength wrought magnesium alloys.
The present invention is selected alloying element by science, is optimized element proportioning, and regulation and control precipitated phase kind, quantity and distribution, strengthen precipitating reinforcing effect; The grain-size of refining alloy as-cast grain and the rear alloy of distortion, plays refined crystalline strengthening effect, utilizes the complex intensifying effect of precipitation strength and refined crystalline strengthening, improve magnesium alloy strength simultaneously.
The present invention, by adding specific alloy elements organization of regulation control structure to improve mechanical property, by Composition Design and the tissue modulation of alloy, and utilizes plastic working, obtains a kind of high-strength wrought magnesium alloys.With the high-strength ZK60 of business compared with the high-strength magnesium alloy prepared of AZ80 magnesium alloy, high rare earth high-strength magnesium alloy and special process, the present invention has a series of advantage:
1, high-strength wrought magnesium alloys Rare-Earth Content of the present invention is less than 3%, and its cost reduces by 2/3 than the cost of the Mg-RE-Zn-Zr alloy of high rare-earth content.
2, high-strength wrought magnesium alloys tensile strength of the present invention reaches more than 400MPa, and far above the high-strength magnesium alloy such as business ZK60 and AZ80, and cost only increases by 5%.
3, the preparation of high-strength wrought magnesium alloys of the present invention can pass through industrial conventional equipment, as common extruding or rolling can realize, can realize batch production on existing industrial equipments, and without the need to passing through special processing mode, tooling cost is low.
Accompanying drawing explanation
Fig. 1 is the tissue of low-cost high-strength wrought magnesium alloys in the embodiment of the present invention 1; Wherein: (a) as-cast structure, the tissue after (b) extruding.
Fig. 2 is the tissue of low-cost high-strength wrought magnesium alloys in the embodiment of the present invention 2; Wherein: (a) as-cast structure, the tissue after (b) extruding.
Fig. 3 is the tissue of low-cost high-strength wrought magnesium alloys in the embodiment of the present invention 3; Wherein: (a) as-cast structure, the tissue after (b) extruding.
Fig. 4 is the tissue of low-cost high-strength wrought magnesium alloys in the embodiment of the present invention 4; Wherein: (a) as-cast structure, the tissue after (b) extruding.
Embodiment
Be described in detail technical solution of the present invention below in conjunction with drawings and Examples, described example is only the present invention's part embodiment, instead of whole embodiments, is not also limitation of the invention.Based on the embodiment in invention, those skilled in the art, not making other embodiments all obtained under creative work prerequisite, belong to the scope of protection of the invention.
For low-cost high-strength wrought magnesium alloys Mg-Zn-RE-Ca-Mn-(Zr) alloy composition in embodiment of the present invention 1-5, (in table, data are chemico-analytic result to table 1; in mass percentage), the fractions be only in protection domain of filling a prescription described in table 1.Table 2 is the room temperature tensile mechanical property of embodiment 1-5 interalloy after extruding.Table 3 is the high-strength wrought magnesium alloys room-temperature mechanical property of existing business and research and development.
Embodiment 1
Adopting metal mold gravity casting to obtain the length of side is 200mm, and height is the square ingot casting of 150mm.Through chemical analysis, its chemical composition is: Mg-2.0Zn-0.8Gd-0.7Ca-0.5Mn.Its as-cast structure is as shown in Fig. 1 (a), and as-cast grain size is 50-100 micron.
Alloy cast ingot carries out Homogenization Treatments 16h at 420 DEG C; The extrusion billet that diameter is 50mm is cut into after process.Extrusion billet, 380 DEG C of insulations 2 hours, is put into container and is extruded, and obtaining diameter is the extruded rod of 12mm.The microtexture of extruded rod is as Fig. 1 (b); After extruding, grain refining is to 2-5 micron, and according to Hall-Petch relation, grain refining will put forward heavy alloyed intensity.Carry out Mechanics Performance Testing by GB GB/T228-2002, its tensile strength is 418MPa, yield strength 405MPa, and elongation 8.5% is as shown in table 2.
Embodiment 2
Adopting metal mold gravity casting to obtain the length of side is 200mm, and height is the square ingot casting of 150mm.Through chemical analysis, its chemical composition is: Mg-3.0Zn-0.2Gd-2.0Ca-0.2Mn-0.3Zr.Its as-cast structure is as shown in Fig. 2 (a), and as-cast grain size is 50-100 micron, due to the increase of Zn content, defines dendrite, and creates more second-phase.
Alloy cast ingot carries out Homogenization Treatments 12h at 400 DEG C; The extrusion billet that diameter is 50mm is cut into after process.Extrusion billet, 380 DEG C of insulations 2 hours, is put into container and is extruded, and obtaining diameter is the extruded rod of 12mm.The microtexture of extruded rod is as Fig. 2 (b); After extruding, grain refining is to 1-5 micron, and creates a lot of fine particle precipitated phase, grain refining and precipitation hardenedly further increase intensity.Carry out Mechanics Performance Testing by GB GB/T228-2002, its tensile strength is 425MPa, yield strength 409MPa, and elongation 7.3% is as shown in table 2.
Embodiment 3
Adopting metal mold gravity casting to obtain the length of side is 200mm, and height is the square ingot casting of 150mm.Through chemical analysis, its chemical composition is: Mg-4.1Zn-3Y-0.2Ca-2.0Mn.Its as-cast structure is as shown in Fig. 3 (a), and as-cast grain size is 50-100 micron, and because the continuation of Zn content increases, dentrite quantity is more, and second-phase quantity also increases.
Alloy cast ingot carries out Homogenization Treatments 12h at 380 DEG C; The extrusion billet that diameter is 50mm is cut into after process.Extrusion billet, 380 DEG C of insulations 2 hours, is put into container and is extruded, and obtaining diameter is the extruded rod of 12mm.The microtexture of extruded rod is as Fig. 3 (b); After extruding, grain refining is to 1-5 micron, and creates a lot of fine particle precipitated phase, and also there are some thick second-phases, grain refining and precipitation hardened complex intensifying improve the intensity of alloy simultaneously.Carry out Mechanics Performance Testing by GB GB/T228-2002, its tensile strength is 439MPa, yield strength 422MPa, and elongation 7.0% is as shown in table 2.
Embodiment 4
Adopting metal mold gravity casting to obtain the length of side is 200mm, and height is the square ingot casting of 150mm.Through chemical analysis, its chemical composition is: Mg-6.0Zn-1.5Y-1.0Ca-0.6Mn-0.8Zr.Its as-cast structure is as shown in Fig. 4 (a), and as-cast grain size is 50-100 micron, and because the continuation of Zn content increases, dentrite quantity is more, and second-phase quantity also increases.
Alloy cast ingot carries out Homogenization Treatments 12h at 380 DEG C; The extrusion billet that diameter is 50mm is cut into after process.Extrusion billet, 360 DEG C of insulations 2 hours, is put into container and is extruded, and obtaining diameter is the extruded rod of 12mm.The microtexture of extruded rod is as Fig. 4 (b); After extruding, grain refining is to 1-5 micron, and creates a lot of fine particle precipitated phase, and also there are some thick second-phases, grain refining and precipitation hardened complex intensifying improve the intensity of alloy simultaneously.Carry out Mechanics Performance Testing by GB GB/T228-2002, its tensile strength is 460MPa, yield strength 446MPa, and elongation 6.5% is as shown in table 2.
Embodiment 5
Adopting metal mold gravity casting to obtain the length of side is 200mm, and height is the square ingot casting of 150mm.Through chemical analysis, its chemical composition is: Mg-5.9Zn-0.9Ce-0.5Ca-0.5Zr.Its as-cast structure as-cast grain size is 50-100 micron, there is a lot of dendrite and second-phase quantity, the interpolation of Zr, as-cast grain is reduced to some extent.
Alloy cast ingot carries out Homogenization Treatments 12h at 380 DEG C; The extrusion billet that diameter is 50mm is cut into after process.Extrusion billet, 360 DEG C of insulations 2 hours, is put into container and is extruded, and obtaining diameter is the extruded rod of 12mm.The grain refining of extruded rod, to 1-5 micron, also also exists a lot of fine particle precipitated phase, and some thick second-phases, and grain refining and precipitation hardened complex intensifying are the major causes that alloy strength improves.Carry out Mechanics Performance Testing by GB GB/T228-2002, its tensile strength is 462MPa, yield strength 445MPa, and elongation 6.8% is as shown in table 2.
Embodiment 6
Adopting metal mold gravity casting to obtain the length of side is 200mm, and height is the square ingot casting of 150mm.Through chemical analysis, its chemical composition is: Mg-5.2Zn-1.1Gd-1.2Ca.Its as-cast structure as-cast grain size is 100-200 micron, there is a lot of dendrite and second-phase quantity.
Alloy cast ingot carries out Homogenization Treatments 12h at 380 DEG C; The extrusion billet that diameter is 50mm is cut into after process.Extrusion billet, 360 DEG C of insulations 2 hours, is put into container and is extruded, and obtaining diameter is the extruded rod of 12mm.The grain refining of extruded rod, to 2-5 micron, also also exists a lot of fine particle precipitated phase, and some thick second-phases.Carry out Mechanics Performance Testing by GB GB/T228-2002, its tensile strength is 443MPa, yield strength 425MPa, and elongation 6.9% is as shown in table 2.
Mg-Zn-RE-Ca-Mn-(Zr) alloy composition (wt%) in table 1 embodiment 1-6
Numbering Zn RE Ca Mn Zr Mg
Alloy 1 2.0 0.8 0.7 0.5 0 Surplus
Alloy 2 3.0 0.2 2.0 0.2 0.3 Surplus
Alloy 3 4.1 3 0.2 2.0 0 Surplus
Alloy 4 6.0 1.5 1.0 0.6 0.8 Surplus
Alloy 5 5.9 0.9 0.5 0 0.5 Surplus
Alloy 6 5.2 1.1 1.2 0 0 Surplus
Mechanical property after Mg-Zn-RE-Ca-Mn-(Zr) alloy extrusion in table 2 embodiment 1-6
Numbering Yield strength (MPa) Tensile strength (MPa) Stretch Long rate
Alloy 1 405 418 8.5
Alloy 2 409 425 7.3
Alloy 3 422 439 7.0
Alloy 4 446 460 6.5
Alloy 5 445 462 6.8
Alloy 6 425 443 6.9
The high-strength wrought magnesium alloys room-temperature mechanical property of table 3 business and research and development
Alloys (wt.%) Processing mode Yield strength MPa Tensile strength/MPa
Mg-6.0Zn-0.4Zr(ZK60) Extruding 275 380
Mg-8Al-0.4Zn-0.2Mn(AZ80) Extruding 305 365
Mg-6.0Zn-0.4Ag-0.2Ca-0.6Zr Extruding 288 351
Mg-9.8Sn-1.2Zn-1.0Al Extruding 280 308
Mg-14.0Gd-2.3Zn Extruding 345 380
Mg-10.0Gd-5.7Y-1.6Zn-0.6Zr Extruding 419 461
Mg-10.0Gd-3Y-1Zn-0.5Zr Extruding 401 450

Claims (10)

1. a high-strength wrought magnesium alloys, is characterized in that: weight percentage, and this magnesium alloy composition is: Zn2.0-6.5%, RE0.1-3.0%, Ca0.1-2.0%, and all the other are Mg and inevitable impurity; Wherein RE is rare earth element.
2. high-strength wrought magnesium alloys according to claim 1, is characterized in that: also containing grain-refining agent in this magnesium alloy, and described crystalline substance material fining agent is Mn and/or Zr.
3. high-strength wrought magnesium alloys according to claim 2, is characterized in that: the content of described Mn is the content of 0.2-2.0wt%, Zr is 0.01-0.8wt%.
4. high-strength wrought magnesium alloys according to claim 2, is characterized in that: the content of described Mn is the content of 0.3-1.5wt%, Zr is 0.3-0.7wt%.
5., according to the arbitrary described high-strength wrought magnesium alloys of claim 1-4, it is characterized in that: described Zn content is 2.0-6.0wt%.
6., according to the arbitrary described high-strength wrought magnesium alloys of claim 1-4, it is characterized in that: described RE content is 0.3-1.5wt%.
7., according to the arbitrary described high-strength wrought magnesium alloys of claim 1-4, it is characterized in that: described Ca content is 0.2-1.5wt%.
8. high-strength wrought magnesium alloys according to claim 1, is characterized in that: described RE can be one or more in Gd, Y, Ce, La, Nd and Er.
9. the preparation method of high-strength wrought magnesium alloys according to claim 1, is characterized in that: by required alloying constituent batch mixing also obtained alloy cast ingot, alloy cast ingot, through viscous deformation hot-work, obtains described high-strength wrought magnesium alloys.
10. the preparation method of high-strength wrought magnesium alloys according to claim 9, is characterized in that: described viscous deformation hot-work be carry out extruding, the viscous deformation processing such as rolling or forging.
CN201410272831.4A 2014-06-18 2014-06-18 A kind of high-strength wrought magnesium alloys and preparation method thereof Active CN105220041B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410272831.4A CN105220041B (en) 2014-06-18 2014-06-18 A kind of high-strength wrought magnesium alloys and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410272831.4A CN105220041B (en) 2014-06-18 2014-06-18 A kind of high-strength wrought magnesium alloys and preparation method thereof

Publications (2)

Publication Number Publication Date
CN105220041A true CN105220041A (en) 2016-01-06
CN105220041B CN105220041B (en) 2018-06-19

Family

ID=54989305

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410272831.4A Active CN105220041B (en) 2014-06-18 2014-06-18 A kind of high-strength wrought magnesium alloys and preparation method thereof

Country Status (1)

Country Link
CN (1) CN105220041B (en)

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105886866A (en) * 2016-06-22 2016-08-24 重庆大学 High-formability magnesium alloy
CN106987747A (en) * 2017-03-23 2017-07-28 济南大学 A kind of even corrosion resistant Biological magnesium alloy and preparation method thereof
CN107201471A (en) * 2017-07-28 2017-09-26 山东省科学院新材料研究所 A kind of wrought magnesium alloy and preparation method thereof
CN107475590A (en) * 2017-08-21 2017-12-15 中北大学 A kind of High-strength high-plasticity cast magnesium alloy and preparation method thereof
CN107541627A (en) * 2016-06-24 2018-01-05 北京科技大学 A kind of wrought magnesium alloy sheet material with good room temperature formability and preparation method thereof
CN108359870A (en) * 2018-04-13 2018-08-03 东北大学 The high energy-absorbing magnesium alloy of middle plasticity and can depth clod wash tubing preparation facilities and method
CN108385008A (en) * 2018-04-13 2018-08-10 东北大学 The high energy-absorbing magnesium alloy of middle intensity and can depth clod wash tubing preparation facilities and method
CN108425054A (en) * 2018-04-13 2018-08-21 东北大学 The high energy-absorbing magnesium alloy of high-ductility and can depth clod wash tubing preparation facilities and method
CN109504884A (en) * 2019-01-10 2019-03-22 吉林大学 Polynary a small amount of high-strength plasticity magnesium alloy and its heavy reduction short flow process
CN109943758A (en) * 2019-03-29 2019-06-28 凤阳爱尔思轻合金精密成型有限公司 High-toughness heat-resistant die casting Mg-Er alloy and preparation method thereof
CN112048686A (en) * 2020-08-26 2020-12-08 中南大学 Magnesium alloy sheet with high bulging property and high impact resistance and preparation method thereof
CN112746210A (en) * 2021-02-01 2021-05-04 太原理工大学 Multi-element microalloyed magnesium alloy, preparation method thereof and plate extrusion forming process
CN112899506A (en) * 2021-01-18 2021-06-04 陕西科技大学 Mg-Zn-Ca alloy and processing method thereof
CN113215461A (en) * 2021-04-27 2021-08-06 中南大学 Magnesium alloy with high bulging property and high heat resistance and preparation method thereof
CN113755772A (en) * 2021-09-26 2021-12-07 南京理工大学 High-strength high-toughness isomeric magnesium alloy and preparation method thereof
CN114574745A (en) * 2022-03-08 2022-06-03 哈尔滨工程大学 Low-cost high-performance magnesium rare earth alloy capable of adapting to various extrusion conditions and preparation method thereof
CN114921700A (en) * 2022-05-25 2022-08-19 中南大学 Biodegradable Mg-Zn-Ca-Re alloy
CN115478199A (en) * 2022-09-21 2022-12-16 西安交通大学 High-toughness magnesium alloy deformed material and preparation method thereof
CN115781100A (en) * 2023-01-29 2023-03-14 河北钢研德凯科技有限公司 Magnesium alloy welding wire and preparation method and application thereof

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09256099A (en) * 1996-03-21 1997-09-30 Toyota Central Res & Dev Lab Inc Heat resistant magnesium alloy
US20080031765A1 (en) * 2006-03-31 2008-02-07 Biotronik Vi Patent Ag Magnesium alloy and the respective manufacturing method
CN103038379A (en) * 2010-05-24 2013-04-10 联邦科学与工业研究组织 Magnesium-based alloy for wrought applications

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH09256099A (en) * 1996-03-21 1997-09-30 Toyota Central Res & Dev Lab Inc Heat resistant magnesium alloy
US20080031765A1 (en) * 2006-03-31 2008-02-07 Biotronik Vi Patent Ag Magnesium alloy and the respective manufacturing method
CN103038379A (en) * 2010-05-24 2013-04-10 联邦科学与工业研究组织 Magnesium-based alloy for wrought applications

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
JH JUN等: "Microstructures and Mechanical Properties of Mg-Zn-RE-Ca Casting Alloys", 《MATERIALS SCIENCE FORUM》 *
东野生栓等: "Mg-x(x=2,3,4)Zn-1Gd-1Ca-0.5Mn合金显微组织和时效硬度研究", 《热加工工艺》 *

Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105886866A (en) * 2016-06-22 2016-08-24 重庆大学 High-formability magnesium alloy
CN107541627A (en) * 2016-06-24 2018-01-05 北京科技大学 A kind of wrought magnesium alloy sheet material with good room temperature formability and preparation method thereof
CN107541627B (en) * 2016-06-24 2019-09-06 北京科技大学 A kind of wrought magnesium alloy plate and preparation method thereof with good room temperature formability
CN106987747A (en) * 2017-03-23 2017-07-28 济南大学 A kind of even corrosion resistant Biological magnesium alloy and preparation method thereof
CN106987747B (en) * 2017-03-23 2019-01-22 济南大学 A kind of even corrosion resistant Biological magnesium alloy and preparation method thereof
CN107201471B (en) * 2017-07-28 2019-03-29 山东省科学院新材料研究所 A kind of wrought magnesium alloy and preparation method thereof
CN107201471A (en) * 2017-07-28 2017-09-26 山东省科学院新材料研究所 A kind of wrought magnesium alloy and preparation method thereof
CN107475590A (en) * 2017-08-21 2017-12-15 中北大学 A kind of High-strength high-plasticity cast magnesium alloy and preparation method thereof
CN107475590B (en) * 2017-08-21 2019-08-13 中北大学 A kind of High-strength high-plasticity cast magnesium alloy and preparation method thereof
CN108425054B (en) * 2018-04-13 2019-10-01 东北大学 The high energy-absorbing magnesium alloy of high-ductility and can depth clod wash tubing preparation facilities and method
CN108425054A (en) * 2018-04-13 2018-08-21 东北大学 The high energy-absorbing magnesium alloy of high-ductility and can depth clod wash tubing preparation facilities and method
CN108385008A (en) * 2018-04-13 2018-08-10 东北大学 The high energy-absorbing magnesium alloy of middle intensity and can depth clod wash tubing preparation facilities and method
CN108359870A (en) * 2018-04-13 2018-08-03 东北大学 The high energy-absorbing magnesium alloy of middle plasticity and can depth clod wash tubing preparation facilities and method
CN109504884B (en) * 2019-01-10 2020-07-28 吉林大学 Multi-element small-quantity high-strength plastic magnesium alloy and large-reduction-quantity short-flow preparation method thereof
CN109504884A (en) * 2019-01-10 2019-03-22 吉林大学 Polynary a small amount of high-strength plasticity magnesium alloy and its heavy reduction short flow process
CN109943758B (en) * 2019-03-29 2021-09-17 凤阳爱尔思轻合金精密成型有限公司 High-strength high-toughness heat-resistant die-casting Mg-Er alloy and preparation method thereof
CN109943758A (en) * 2019-03-29 2019-06-28 凤阳爱尔思轻合金精密成型有限公司 High-toughness heat-resistant die casting Mg-Er alloy and preparation method thereof
CN112048686B (en) * 2020-08-26 2022-04-05 中南大学 Magnesium alloy sheet with high bulging property and high impact resistance and preparation method thereof
CN112048686A (en) * 2020-08-26 2020-12-08 中南大学 Magnesium alloy sheet with high bulging property and high impact resistance and preparation method thereof
CN112899506A (en) * 2021-01-18 2021-06-04 陕西科技大学 Mg-Zn-Ca alloy and processing method thereof
CN112746210A (en) * 2021-02-01 2021-05-04 太原理工大学 Multi-element microalloyed magnesium alloy, preparation method thereof and plate extrusion forming process
CN113215461A (en) * 2021-04-27 2021-08-06 中南大学 Magnesium alloy with high bulging property and high heat resistance and preparation method thereof
CN113755772A (en) * 2021-09-26 2021-12-07 南京理工大学 High-strength high-toughness isomeric magnesium alloy and preparation method thereof
CN114574745A (en) * 2022-03-08 2022-06-03 哈尔滨工程大学 Low-cost high-performance magnesium rare earth alloy capable of adapting to various extrusion conditions and preparation method thereof
CN114921700A (en) * 2022-05-25 2022-08-19 中南大学 Biodegradable Mg-Zn-Ca-Re alloy
CN114921700B (en) * 2022-05-25 2023-09-26 中南大学 Biodegradable Mg-Zn-Ca-Re alloy
CN115478199A (en) * 2022-09-21 2022-12-16 西安交通大学 High-toughness magnesium alloy deformed material and preparation method thereof
CN115478199B (en) * 2022-09-21 2024-04-12 西安交通大学 High-strength and high-toughness magnesium alloy deformed material and preparation method thereof
CN115781100A (en) * 2023-01-29 2023-03-14 河北钢研德凯科技有限公司 Magnesium alloy welding wire and preparation method and application thereof
CN115781100B (en) * 2023-01-29 2023-05-02 河北钢研德凯科技有限公司 Magnesium alloy welding wire and preparation method and application thereof

Also Published As

Publication number Publication date
CN105220041B (en) 2018-06-19

Similar Documents

Publication Publication Date Title
CN105220041A (en) A kind of high-strength wrought magnesium alloys and preparation method thereof
CN103667842B (en) A kind of low Gd content, high ductibility magnesium alloy sheet material and hot rolling process thereof
CN102051509A (en) High-toughness heat-resistant Mg-Al-RE-Mn wrought magnesium alloy and preparation method of plate made of same
CN109182857B (en) High-strength and high-toughness deformed magnesium alloy and preparation method thereof
CN110129644B (en) Heat-resistant soluble magnesium alloy and preparation method and application thereof
Luo et al. Magnesium alloy development for automotive applications
CN101037753A (en) High-strength heat-proof compression casting magnesium alloy and preparation method thereof
CN101200784A (en) Magnesium-zinc-lanthanon-zirconium magnesium alloy and method for preparing same
CN108998711B (en) High-strength-toughness deformed magnesium-lithium alloy and preparation method thereof
CN103031474A (en) Magnesium lithium alloy
CN105525179A (en) Preparation method for rare-earth magnesium alloy large-size high-strength forged piece
CA2909202C (en) Aluminum-free magnesium wrought alloy
CN103841999A (en) Magnesium alloys for bioabsorbable stent
CN105543605B (en) A kind of high intensity Mg Y Ni Mn alloys and preparation method thereof
CN103305738B (en) Siliceous heat resisting magnesium-rare earth alloy and preparation method thereof
CN103938045A (en) Calcium-containing deforming magnesium alloy and preparation method of calcium-containing deforming magnesium alloy bar
CN101381832A (en) Heat resisting magnesium alloy and compound material containing heat resisting magnesium alloy and preparation method thereof
CN106521278A (en) High-strength magnesium-zinc-manganese-yttrium-cerium magnesium alloy and preparation method thereof
CN102634711A (en) High-temperature high-toughness deformation magnesium alloy material and preparation method thereof
CN105568105A (en) High-strength high-plasticity Mg-Gd-Y-Ni-Mn alloy and preparing method thereof
CN104498797A (en) High-strength casting magnesium alloy with low hot cracking tendency and preparation method for high-strength casting magnesium alloy
CN114855043B (en) Superfine crystal high-strength plastic magnesium alloy and preparation method thereof
CN103290286A (en) As-cast high-strength-and-toughness ma.gnesium-lithium alloy and preparation method thereof
CN109234592B (en) Low-temperature rolled high-strength-toughness wrought magnesium alloy and preparation method thereof
CN109930045B (en) High-strength-toughness heat-resistant Mg-Gd alloy suitable for gravity casting and preparation method thereof

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant