CN107142389B - High-strength, the high-ductility Ni of one kind50Mn34In16-xCoxThe preparation method of Magnetic Memory alloy - Google Patents

High-strength, the high-ductility Ni of one kind50Mn34In16-xCoxThe preparation method of Magnetic Memory alloy Download PDF

Info

Publication number
CN107142389B
CN107142389B CN201710306539.3A CN201710306539A CN107142389B CN 107142389 B CN107142389 B CN 107142389B CN 201710306539 A CN201710306539 A CN 201710306539A CN 107142389 B CN107142389 B CN 107142389B
Authority
CN
China
Prior art keywords
powder
parts
alloy
memory alloy
ductility
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.)
Active
Application number
CN201710306539.3A
Other languages
Chinese (zh)
Other versions
CN107142389A (en
Inventor
董桂馥
张倩倩
陈建国
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.)
Dalian University
Original Assignee
Dalian 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 Dalian University filed Critical Dalian University
Priority to CN201711358227.3A priority Critical patent/CN108085523B/en
Priority to CN201710306539.3A priority patent/CN107142389B/en
Publication of CN107142389A publication Critical patent/CN107142389A/en
Application granted granted Critical
Publication of CN107142389B publication Critical patent/CN107142389B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0433Nickel- or cobalt-based alloys
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F1/00Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/10Metallic powder containing lubricating or binding agents; Metallic powder containing organic material
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F1/00Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/10Metallic powder containing lubricating or binding agents; Metallic powder containing organic material
    • B22F1/103Metallic powder containing lubricating or binding agents; Metallic powder containing organic material containing an organic binding agent comprising a mixture of, or obtained by reaction of, two or more components other than a solvent or a lubricating agent
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/115Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by spraying molten metal, i.e. spray sintering, spray casting

Abstract

The present invention relates to a kind of preparation method of magnetic shape memory alloy, especially a kind of high-strength, high-ductility Ni50Mn34In16‑xCoxThe preparation method of Magnetic Memory alloy.According to atomic percent feeding, mixing, molding, degreasing, sintering to get high-strength to high intensity, high-ductility Ni50Mn34In16‑xCox(x=2,3,4,5).Magnetic shape memory alloy Ni prepared by the present invention50Mn34In16‑xCox(x=2,3,4,5) has many advantages, such as that good toughness, intensity is big, fine microstructures.For the application extension thinking of high temperature high-ductility marmem.

Description

High-strength, the high-ductility Ni of one kind50Mn34In16-xCoxThe preparation method of Magnetic Memory alloy
Technical field
The present invention relates to high-strength, the high-ductility Ni of one kind50Mn34In16-xCoxThe preparation method of Magnetic Memory alloy.
Background technology
1996, Ullakko et al. was for the first time in Ni2The reversible strain that about 0.2% is obtained in MnGa monocrystalline, is pulled open since then The research prelude of magnetic driven memory alloy, has become the research hotspot in marmem field.Current research is wide Magnetic driven memory alloy includes mainly:Ni-Mn-Ga (Al), Ni-Fe-Ga, Co-Ni-Ga (Al) and novel Ni-Mn-In (Sn, Sb) alloy.Ni-Mn-Ga based alloys are to find earliest and study most commonly used magnetic marmem at present, Magnetic-field-induced strain derives from martensitic twin variant under external magnetic field and resets the macro-strain generated, has such deformation mechanism Alloy to obtain the key of big magnetic-field-induced strain be to have high magnetocrystalline anisotropy energy and low twin boundary migration limit stress. At present in Ni-Mn-Ga series alloys, monocrystalline maximum reversible strain property reaches 10%, but due to defeated caused by variant rearrangement It is smaller to go out stress, only 2MPa or so, it is difficult to meet the application requirement of Practical Project.In the recent period, novel magnetic driven memory alloy system Ni-Mn-X (X=In, Sn, Sb) causes the attention of various countries researcher.Series Heulser alloys are in nonstoichiometry ratio With thermoelastic martensitic transformation, magnetic truly is realized in certain composition range or after the ferromagnetic Elements C o of doping Driving phase transformation, generates macro-strain, the essence of the series alloy magnetic-field-induced strain be martensitic phase with parent phase with larger Saturation magnetization is poor, and alloy transformation temperature significantly reduces under external magnetic field, applies external magnetic field in certain temperature range Martensite reverse transformation can then be brought it about to have shape memory effect, and export larger stress.But Ni-Mn-In is closed The defects such as that there are still brittleness is big for golden system, and the threshold value of field drives phase transformation is high, and Curie temperature is low, limit it to a certain extent Practical application.So how to improve magnetic field life strain, field drives threshold value is reduced, improves alloy mechanical performance, obtains big Magnetic entropy becomes and giant magnetoresistance effect, it has also become memorial alloy is applied and the main direction of studying of development.
Refined crystalline strengthening can significantly change alloy transformation temperature and improve its mechanical performance and physical property.Therefore pass through gold Belong to injection moulding and sintering process combines and prepares Ni50Mn34In16Magnetic Memory alloy improves alloy mechanical property and improves magnetics One of effective ways of performance.
Metal injection moulding (Metal Injection Molding, abbreviation MIM) is a kind of from injection molding of plastics industry In the novel powder metallurgy forming technique extending out, it is well known that the cheap price production of injection molding of plastics technology is various The product of complicated shape, but plastic products intensity is not high, in order to improve its performance, can add metal or ceramic powder in the plastic End is to obtain the product that intensity is higher, wearability is good.In recent years, development evolvement is to improve solid to the maximum extent to this idea The content of particle and in subsequent sintering process completely remove no-bonder and make forming base be densified.
Invention content
It is big in order to solve existing Ni-Mn-In-Co suitable shape memory alloys brittleness, the high problem of driving magnetic field threshold value, The present invention provide it is a kind of by metal injection moulding and sintering process in conjunction with preparing Ni50Mn34In16-xCox(x=2,3,4,5) The method of Magnetic Memory alloy.
The marmem of the present invention is prepared as follows:According to atomic percent take 50 parts Ni powder, 34 The Mn powder, 11-14 parts of In powder and 2-5 parts of Co powder of part are uniformly mixed by blender, and a certain amount of binder is then added and carries out It is kneaded, is then injection moulded by metallic injection machine, it is last degreasing sintered, Ni is made50Mn34In16-xCox(x=2,3,4, 5) Magnetic Memory alloy.
More specifically, Ni of the present invention50Mn34In16-xCoxThe preparation method of (x=2,3,4,5) Magnetic Memory alloy is as follows: Before sintering, the Ni powder that grain size is 300 mesh, Mn powder, In powder and Co powder is taken to mix according to atomic percent, with 200 in blender Turn/min-500 turns/min is uniformly mixed to stir metal powder, the binder of metal powder gross mass 2%-5% is then added So that it is sufficiently mixed uniformly with metal powder, be then added in metallic injection machine, makes to glue by being heated to 200 DEG C -400 DEG C Tie agent to melt, then 20-40 kilograms of pressure 10h-48h applied to mold, obtain injection embryo, finally will injection base through degreasing at Reason, uses 1500 DEG C -1700 DEG C of temperature, 200-400 kilograms of pressure, vacuum degree 10-3-10-4MPa, time are 20-40 minutes Sintering process is sintered, and finally obtains the Ni that grain size is about 50-60 microns50Mn34In16-xCox(x=2,3,4,5) Magnetic Memory closes Gold.
Preferably, the binder is epoxy resin and polyamide with 4:1 mass ratio mixes.
Binder is the core of Metal Injection Molding, and binder has enhancing mobility to be suitble to injection in MIM It is molded and maintains the effect of briquet shape, it should also have the characteristics that readily removed, pollution-free, non-toxic, cost is reasonable in addition, Occur various binders thus, Recent study personnel just gradually select from rule of thumb to according to degreasing method And the requirement to binder function, the direction for targetedly designing binder system are developed.Inventor is by repeatedly Test of many times obtains most suitable Ni50Mn34In16-xCoxThe binder of (x=2,3,4,5) Magnetic Memory alloy, in the binder Under effect, make metal powder that there is good cavity filling, while there is good degreasing, keeps the consistency of alloy high, burning Good performance is obtained after knot.Ni50Mn34In12The reason of Co4 gold excellent in mechanical performance, the crystal grain of mainly alloy was more tiny, and And there is (Co, Ni) in the alloyxThe second phases of In, therefore the mechanical property of alloy is made to be greatly improved.
Advantageous effect
The marmem Ni that the method for the present invention is prepared50Mn34In16-xCox(x=2,3,4,5) different existing warps Magnetic shape memory alloy Ni prepared by arc melting method50Mn34In16-xCox(x=2,3,4,5), and by comparison have with Lower advantage:
Ni prepared by the present invention50Mn34In16-xCoxThere is (x=2,3,4,5) alloy higher fracture strength and fracture to answer Become, the magnetic shape memory alloy fine microstructures, good toughness, intensity is big, with excellent magnetic performance, is high temperature high-ductility shape The application extensions of shape memory alloys thinking.
Description of the drawings
Fig. 1 is Ni prepared by embodiment 450Mn34In11Co5Alloy carries out the test curve of fracture strength and breaking strain Figure;
Fig. 2 a are Ni prepared by the present invention50Mn34In16-xCoxThe fracture strength of (x=2,3,4,5) alloy is with Co contents Variation relation;
Fig. 2 b are Ni prepared by the present invention50Mn34In16-xCoxThe breaking strain of (x=2,3,4,5) alloy is with Co contents Variation relation;
Fig. 3 a are Ni prepared by the present invention50Mn34In14Co2Alloy optical microscope photograph at room temperature;
Fig. 3 b are Ni prepared by the present invention50Mn34In11Co5Alloy optical microscope photograph at room temperature.
Specific implementation mode
The present invention is described in further detail below by embodiment, but is not limited the scope of the invention.Such as without spy Different explanation, experimental method of the present invention is conventional method, and experiment equipment used, material, reagent etc. can be chemically Company buys.Preferably, the equipment that sintering process selects in the embodiment of the present invention is the production of Japanese Zhu You coals Co., Ltd. SPS 1050.The highest pulse current of the equipment is 5000A, and maximum sintering temperature can reach 2000 DEG C, maximum axial pressure Power is 100KN, and vacuum degree is up to 6Pa.
Embodiment 1
High-strength, high-ductility Ni50Mn34In14Co2Magnetic Memory alloy is prepared as follows:It is taken according to atomic percent Grain size is 14 parts of 34 parts of 50 parts of Ni powder, Mn powder, In powder and 2 parts of mixing of Co powder of 300 mesh, is turned with 200 turns/min in blender Speed stirring metal powder, makes it be uniformly mixed, binder (the m epoxy resin of metal powder gross mass 2wt% is then added:M is poly- Amide=4:1) so that it is sufficiently mixed uniformly, then said mixture is added in metallic injection machine, by being heated to 200 So that binder is melted drives metal powder to enter in mold cavity, is applying 20-40 kilograms of pressure/10h- to mold Then 48h obtains injection embryo, finally through ungrease treatment, finally utilize 1500 DEG C -1700 DEG C, it is 200-400 kilograms of pressure, true Reciprocal of duty cycle is 10-3-10-4MPa, time are that 20-40 minutes sintering process are sintered, and it is about 50-60 microns to finally obtain grain size Ni50Mn34In14Co2Magnetic Memory alloy.
Embodiment 2
High-strength, high-ductility Ni50Mn34In13Co3Magnetic Memory alloy is prepared as follows:It is taken according to atomic percent Grain size is 13 parts of 34 parts of 50 parts of Ni powder, Mn powder, In powder and 3 parts of mixing of Co powder of 300 mesh, is turned with 200 turns/min in blender Speed stirring metal powder, makes it be uniformly mixed, binder (the m epoxy resin of metal powder gross mass 2wt% is then added:M is poly- Amide=4:1) so that it is sufficiently mixed uniformly, then said mixture is added in metallic injection machine, by being heated to 200 So that binder is melted drives metal powder to enter in mold cavity, is applying 20-40 kilograms of pressure/10h- to mold Then 48h obtains injection embryo, finally through ungrease treatment, finally utilize 1500 DEG C -1700 DEG C, it is 200-400 kilograms of pressure, true Reciprocal of duty cycle is 10-3-10-4MPa, time are that 20-40 minutes sintering process are sintered, and it is about 50-60 microns to finally obtain grain size Ni50Mn34In13Co3Magnetic Memory alloy.
Embodiment 3
High-strength, high-ductility Ni50Mn34In12Co4Magnetic Memory alloy is prepared as follows:It is taken according to atomic percent Grain size is 12 parts of 34 parts of 50 parts of Ni powder, Mn powder, In powder and 4 parts of mixing of Co powder of 300 mesh, is turned with 200 turns/min in blender Speed stirring metal powder, makes it be uniformly mixed, binder (the m epoxy resin of metal powder gross mass 2wt% is then added:M is poly- Amide=4:1) so that it is sufficiently mixed uniformly, then said mixture is added in metallic injection machine, by being heated to 200 So that binder is melted drives metal powder to enter in mold cavity, is applying 20-40 kilograms of pressure/10h- to mold Then 48h obtains injection embryo, finally through ungrease treatment, finally utilize 1500 DEG C -1700 DEG C, it is 200-400 kilograms of pressure, true Reciprocal of duty cycle is 10-3-10-4MPa, time are that 20-40 minutes sintering process are sintered, and it is about 50-60 microns to finally obtain grain size Ni50Mn34In12Co4Magnetic Memory alloy.
Embodiment 4
High-strength, high-ductility Ni50Mn34In11Co5Magnetic Memory alloy is prepared as follows:It is taken according to atomic percent Grain size is 11 parts of 34 parts of 50 parts of Ni powder, Mn powder, In powder and 5 parts of mixing of Co powder of 300 mesh, is turned with 200 turns/min in blender Speed stirring metal powder, makes it be uniformly mixed, binder (the m epoxy resin of metal powder gross mass 2wt% is then added:M is poly- Amide=4:1) so that it is sufficiently mixed uniformly, then said mixture is added in metallic injection machine, by being heated to 200 So that binder is melted drives metal powder to enter in mold cavity, is applying 20-40 kilograms of pressure/10h- to mold Then 48h obtains injection embryo, finally through ungrease treatment, finally utilize 1500 DEG C -1700 DEG C, it is 200-400 kilograms of pressure, true Reciprocal of duty cycle is 10-3-10-4MPa, time are that 20-40 minutes sintering process are sintered, and it is about 50-60 microns to finally obtain grain size Ni50Mn34In11Co5Magnetic Memory alloy.
Embodiment 5
High-strength, high-ductility Ni50Mn34In11Co5Magnetic Memory alloy is prepared as follows:It is taken according to atomic percent Grain size is 11 parts of 34 parts of 50 parts of Ni powder, Mn powder, In powder and 5 parts of mixing of Co powder of 300 mesh, is turned with 200 turns/min in blender Speed stirring metal powder, makes it be uniformly mixed, binder (the m epoxy resin of metal powder gross mass 2wt% is then added:M is poly- Amide=4:1) so that it is sufficiently mixed uniformly, then said mixture is added in metallic injection machine, by being heated to 400 So that binder is melted drives metal powder to enter in mold cavity, is applying 20-40 kilograms of pressure/10h- to mold Then 48h obtains injection embryo, finally through ungrease treatment, finally utilize 1500 DEG C -1700 DEG C, it is 200-400 kilograms of pressure, true Reciprocal of duty cycle is 10-3-10-4MPa, time are that 20-40 minutes sintering process are sintered, and it is about 50-60 microns to finally obtain grain size Ni50Mn34In11Co5Magnetic Memory alloy.
Embodiment 6
High-strength, high-ductility Ni50Mn34In14Co2Magnetic Memory alloy is prepared as follows:It is taken according to atomic percent Grain size is 14 parts of 34 parts of 50 parts of Ni powder, Mn powder, In powder and 2 parts of mixing of Co powder of 300 mesh, is turned with 400 turns/min in blender Speed stirring metal powder, makes it be uniformly mixed, binder (the m epoxy resin of metal powder gross mass 5wt% is then added:M is poly- Amide=4:1) so that it is sufficiently mixed uniformly, then said mixture is added in metallic injection machine, by being heated to 200 So that binder is melted drives metal powder to enter in mold cavity, is applying 40 kilograms of pressure 48h to mold, then To injection embryo, finally in pressure, the vacuum degree 10 for through ungrease treatment, finally utilizing 1600 DEG C, 200 kilograms-3MPa, time is Sintering process sintering in 30 minutes, finally obtains the Ni that grain size is about 50-60 microns50Mn34In14Co2Magnetic Memory alloy.
Comparative example
Ni is prepared using arc melting method50Mn34In11Co5Alloy:It is the Ni of 300 mesh to take grain size according to atomic percent 5 parts of 50 parts of powder, 34 parts of Mn powder, 11 parts of In powder and Co powder mixing are positioned over smelting furnace melting, be made after sample through cooling, cleaning, Heat preservation obtains Ni50Mn34In11Co5Alloy.
Alloy prepared by embodiment 4 and comparative example is carried out to the test of fracture strength and breaking strain, the survey of embodiment 4 Test result is as shown in Figure 1.Ni prepared by the present invention50Mn34In11Co5Alloy fracture intensity is in 8805 Mpa, arc melting method side Ni prepared by method50Mn34In16The fracture strength of alloy is about Ni prepared by the 400MPa present invention50Mn34In11Co5Alloy ratio compares Example improves about 8300Mpa;And the Ni only prepared by the method for sintering50Mn29Ga21Its fracture strength of alloy is about 1700MPA.
By obtained Ni in the present embodiment 1-450Mn34In16-xCoxThe fracture strength of (x=2,3,4,5) and fracture are answered Become as shown in Figure 2 a and 2 b with the variation test result of Co contents;Ni prepared by the present invention50Mn34In16-xCox(x=2,3, 4,5) Ni of the fracture strength of alloy than arc melting method50Mn34In16-xCoxAlloy improves about 200, and as x=5, fracture is answered Become 20, than existing Ni50Mn34In11Co5The breaking strain of alloy improves 15%, improves 4 times than Ni-Mn-Ga alloy, says Ni prepared by the bright present invention50Mn34In11Co5Alloy ductility is big.
High-strength, high-ductility Ni prepared by embodiment 1 and embodiment 450Mn34In14Co2Alloy and Ni50Mn34In11Co5 Alloy carries out structure observation analysis at room temperature, and the results are shown in Figure 3.The alloy that as seen in Figure 3 prepared by the present invention is brilliant More tiny, the Ni of grain50Mn34In11Co2The crystallite dimension of alloy significantly reduces, probably about 50 microns of diameter, and Ni50Mn34In11Co5 The fine microstructures of alloy, are dispersed with the second more tiny phase in crystal grain, and this method plays the role of crystal grain refinement.
In conclusion magnetic shape memory alloy Ni prepared by the method for the present invention50Mn34In16-xCox(x=2,3,4,5) Have many advantages, such as that good toughness, intensity is big, fine microstructures.

Claims (2)

1. high-strength, the high-ductility Ni of one kind50Mn34In16-xCoxThe preparation method of Magnetic Memory alloy, which is characterized in that step is specific For:Before sintering, it is 50 parts of Ni powder, 34 parts of Mn powder, 11-14 parts of In powder and the 2-5 parts of Co of 300 mesh to take grain size according to atomic percent Powder mixes, and is uniformly mixed with 200 turns/min-500 turns/min to stir metal powder in blender, metal powder is then added The binder of gross mass 2%-5% makes it be sufficiently mixed uniformly with metal powder, is then added in metallic injection machine, passes through Being heated to 200 DEG C -400 DEG C makes binder melt, then applies 20-40 kilograms of pressure 10h-48h to mold, obtains injection embryo, Base will finally be injected through ungrease treatment, use 1500 DEG C -1700 DEG C of temperature, 200-400 kilograms of pressure, vacuum degree 10-3-10- 4MPa, time are that 20-40 minutes sintering process are sintered, and finally obtain the Ni that grain size is about 50-60 microns50Mn34In16-xCoxMagnetic Memorial alloy, the binder are epoxy resin and polyamide with 4:1 mass ratio mixes, wherein x=2, and 3,4,5.
2. high-strength, the high-ductility Ni of one kind50Mn34In16-xCoxMagnetic Memory alloy, which is characterized in that according to side described in claim 1 It is prepared by method.
CN201710306539.3A 2017-05-04 2017-05-04 High-strength, the high-ductility Ni of one kind50Mn34In16-xCoxThe preparation method of Magnetic Memory alloy Active CN107142389B (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN201711358227.3A CN108085523B (en) 2017-05-04 2017-05-04 High-strength, the high-ductility Ni of one kind50Mn34In11Co5The preparation method of Magnetic Memory alloy
CN201710306539.3A CN107142389B (en) 2017-05-04 2017-05-04 High-strength, the high-ductility Ni of one kind50Mn34In16-xCoxThe preparation method of Magnetic Memory alloy

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710306539.3A CN107142389B (en) 2017-05-04 2017-05-04 High-strength, the high-ductility Ni of one kind50Mn34In16-xCoxThe preparation method of Magnetic Memory alloy

Related Child Applications (1)

Application Number Title Priority Date Filing Date
CN201711358227.3A Division CN108085523B (en) 2017-05-04 2017-05-04 High-strength, the high-ductility Ni of one kind50Mn34In11Co5The preparation method of Magnetic Memory alloy

Publications (2)

Publication Number Publication Date
CN107142389A CN107142389A (en) 2017-09-08
CN107142389B true CN107142389B (en) 2018-11-02

Family

ID=59775257

Family Applications (2)

Application Number Title Priority Date Filing Date
CN201711358227.3A Active CN108085523B (en) 2017-05-04 2017-05-04 High-strength, the high-ductility Ni of one kind50Mn34In11Co5The preparation method of Magnetic Memory alloy
CN201710306539.3A Active CN107142389B (en) 2017-05-04 2017-05-04 High-strength, the high-ductility Ni of one kind50Mn34In16-xCoxThe preparation method of Magnetic Memory alloy

Family Applications Before (1)

Application Number Title Priority Date Filing Date
CN201711358227.3A Active CN108085523B (en) 2017-05-04 2017-05-04 High-strength, the high-ductility Ni of one kind50Mn34In11Co5The preparation method of Magnetic Memory alloy

Country Status (1)

Country Link
CN (2) CN108085523B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107626928B (en) * 2017-09-19 2020-06-16 西迪技术股份有限公司 Die and forming method for bent pipe
CN108950275B (en) * 2018-08-02 2020-09-22 大连大学 Method for synthesizing NiCoMnin magnetic memory alloy at high temperature through combustion reaction
CN108929963B (en) * 2018-08-02 2020-02-18 大连大学 High-wear-resistance Ni50Mn34In16-xCoxPreparation method of magnetic memory alloy
CN109022864B (en) * 2018-08-02 2020-04-07 大连大学 Method for synthesizing NiMnGaCo magnetic memory alloy at high temperature through combustion reaction
CN108950274B (en) * 2018-08-02 2020-05-19 大连大学 Preparation method of high-corrosion-resistance NiMnInCo magnetic shape memory alloy
CN113684390A (en) * 2021-08-16 2021-11-23 大连大学 Method for preparing hyperelastic NiMnInCo magnetic memory alloy by liquid die forging

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103243241A (en) * 2013-05-22 2013-08-14 哈尔滨工业大学 Preparation method of high-plasticity Ni-Mn-In alloy
CN105448443A (en) * 2015-11-26 2016-03-30 北京科技大学 Preparation method of bonding martensitic phase change material
CN105755346A (en) * 2016-04-15 2016-07-13 西安交通大学 Ni-Mn-In room-temperature magnetic refrigeration material and preparation method thereof

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5265259B2 (en) * 2008-07-01 2013-08-14 株式会社豊田中央研究所 Ferromagnetic shape memory alloy sintered body and method for producing the same
CN105296925B (en) * 2015-07-27 2018-07-06 大连大学 The method that laser pulse sputtering sedimentation prepares Ni-Mn-Co-In alloy firms

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103243241A (en) * 2013-05-22 2013-08-14 哈尔滨工业大学 Preparation method of high-plasticity Ni-Mn-In alloy
CN105448443A (en) * 2015-11-26 2016-03-30 北京科技大学 Preparation method of bonding martensitic phase change material
CN105755346A (en) * 2016-04-15 2016-07-13 西安交通大学 Ni-Mn-In room-temperature magnetic refrigeration material and preparation method thereof

Also Published As

Publication number Publication date
CN108085523A (en) 2018-05-29
CN108085523B (en) 2019-09-13
CN107142389A (en) 2017-09-08

Similar Documents

Publication Publication Date Title
CN107142389B (en) High-strength, the high-ductility Ni of one kind50Mn34In16-xCoxThe preparation method of Magnetic Memory alloy
CN107058848B (en) A kind of high intensity Ni50Mn34In16The preparation method of Magnetic Memory alloy
CN104835641B (en) Method for producing rare-earth magnet
CN106756579B (en) A kind of fe-Ni soft magnetic alloy and fe-Ni soft magnetic alloy part with shot-range ordered structure
US11273493B2 (en) Method of manufacturing Ni alloy part
JP5640954B2 (en) Rare earth magnet manufacturing method
CN110600254B (en) 4D printing manufacturing method suitable for magnetic composite material
JP2016032116A (en) Manganese-bismuth based magnetic material, manufacturing method thereof, manganese-bismuth based sintered magnet, and manufacturing method thereof
JP2011159981A (en) HIGHLY QUENCHABLE Fe-BASED RARE EARTH MATERIAL FOR FERRITE REPLACEMENT
CN108060341B (en) A kind of high tenacity Ni50Mn25Ga25Memorial alloy and preparation method thereof
KR102287740B1 (en) Rare earth permanent magnet material and manufacturing method thereof
JP7428791B2 (en) High-entropy alloys of rare earths and transition metals as building blocks to synthesize novel magnetic phases for permanent magnets
CN107424695A (en) A kind of dual alloy nanocrystalline rare-earth permanent magnet and preparation method thereof
JPH02288305A (en) Rare earth magnet and manufacture thereof
Strnat Rare-earth magnets in present production and development
CN105312574B (en) The manufacture method of sintered compact body
CN101241789A (en) A lanthanon permanent magnetic powder and its making method
CN105931791A (en) Fe-50% Co soft magnetic alloy prepared from powder metallurgy process and method
US20160322136A1 (en) METAL-BONDED RE-Fe-B MAGNETS
CN106252011A (en) The compound interpolation of a kind of Grain-Boundary Phase improves the coercitive method of sintered NdFeB
JP2019519941A (en) Method of manufacturing rare earth sintered magnet
CN110415908A (en) A kind of rare-earth Nd-Fe-B permanent magnetic material and preparation method thereof
CN106521245A (en) Cobalt-vanadium-silicon-gallium base high-temperature shape memory alloy
JP2016066675A (en) Rare earth isotropic bond magnet
Xi et al. Preparation and characterization of phenol formaldehyde bonded Nd–Fe–B magnets with high strength and heat resistance

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
EE01 Entry into force of recordation of patent licensing contract
EE01 Entry into force of recordation of patent licensing contract

Application publication date: 20170908

Assignee: ZYBODY CO.,LTD.

Assignor: DALIAN University

Contract record no.: X2023210000200

Denomination of invention: A preparation method for high-strength and high plasticity Ni50Mn34In16-xCoxmagnetic memory alloy

Granted publication date: 20181102

License type: Common License

Record date: 20231127

EE01 Entry into force of recordation of patent licensing contract
EE01 Entry into force of recordation of patent licensing contract

Application publication date: 20170908

Assignee: Dalian Funuo Machinery Co.,Ltd.

Assignor: DALIAN University

Contract record no.: X2023210000252

Denomination of invention: A Preparation Method for High Strength and High Plasticity Ni50Mn34In16-xCoxMagnetic Memory Alloy

Granted publication date: 20181102

License type: Common License

Record date: 20231129

Application publication date: 20170908

Assignee: Dalian Sanfengsheng Heavy Industry Machinery Co.,Ltd.

Assignor: DALIAN University

Contract record no.: X2023210000251

Denomination of invention: A Preparation Method for High Strength and High Plasticity Ni50Mn34In16-xCoxMagnetic Memory Alloy

Granted publication date: 20181102

License type: Common License

Record date: 20231129

Application publication date: 20170908

Assignee: DALIAN MENGYU MACHINERY CO.,LTD.

Assignor: DALIAN University

Contract record no.: X2023210000220

Denomination of invention: A Preparation Method for High Strength and High Plasticity Ni50Mn34In16-xCoxMagnetic Memory Alloy

Granted publication date: 20181102

License type: Common License

Record date: 20231129