CN109473247B - Preparation method of neodymium iron boron grain boundary infiltration alloy cast sheet - Google Patents

Preparation method of neodymium iron boron grain boundary infiltration alloy cast sheet Download PDF

Info

Publication number
CN109473247B
CN109473247B CN201811363765.6A CN201811363765A CN109473247B CN 109473247 B CN109473247 B CN 109473247B CN 201811363765 A CN201811363765 A CN 201811363765A CN 109473247 B CN109473247 B CN 109473247B
Authority
CN
China
Prior art keywords
alloy
vacuum
casting
sheet
heat treatment
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
CN201811363765.6A
Other languages
Chinese (zh)
Other versions
CN109473247A (en
Inventor
周慧杰
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.)
Ningbo Newland Magnet Industry Corp ltd
Original Assignee
Ningbo Newland Magnet Industry Corp ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Ningbo Newland Magnet Industry Corp ltd filed Critical Ningbo Newland Magnet Industry Corp ltd
Priority to CN201811363765.6A priority Critical patent/CN109473247B/en
Publication of CN109473247A publication Critical patent/CN109473247A/en
Application granted granted Critical
Publication of CN109473247B publication Critical patent/CN109473247B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F1/00Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
    • H01F1/01Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
    • H01F1/03Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
    • H01F1/032Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials
    • H01F1/04Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys
    • H01F1/047Alloys characterised by their composition
    • H01F1/053Alloys characterised by their composition containing rare earth metals
    • H01F1/055Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5
    • H01F1/057Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B
    • H01F1/0571Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B in the form of particles, e.g. rapid quenched powders or ribbon flakes
    • H01F1/0575Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B in the form of particles, e.g. rapid quenched powders or ribbon flakes pressed, sintered or bonded together
    • H01F1/0577Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B in the form of particles, e.g. rapid quenched powders or ribbon flakes pressed, sintered or bonded together sintered
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D11/00Continuous casting of metals, i.e. casting in indefinite lengths
    • B22D11/06Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars
    • B22D11/0611Continuous casting of metals, i.e. casting in indefinite lengths into moulds with travelling walls, e.g. with rolls, plates, belts, caterpillars formed by a single casting wheel, e.g. for casting amorphous metal strips or wires
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/14Metallic material, boron or silicon
    • C23C14/16Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
    • C23C14/165Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon by cathodic sputtering
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F41/00Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties
    • H01F41/02Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties for manufacturing cores, coils, or magnets
    • H01F41/0253Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties for manufacturing cores, coils, or magnets for manufacturing permanent magnets
    • H01F41/0293Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties for manufacturing cores, coils, or magnets for manufacturing permanent magnets diffusion of rare earth elements, e.g. Tb, Dy or Ho, into permanent magnets

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Manufacturing & Machinery (AREA)
  • Physical Vapour Deposition (AREA)
  • Hard Magnetic Materials (AREA)

Abstract

A preparation method of a neodymium iron boron grain boundary infiltration alloy cast sheet comprises the following steps: (1) vacuum smelting: adding the neodymium iron boron alloy distribution raw materials into a crucible of a vacuum smelting furnace in sequence for smelting; (2) casting: pouring the alloy solution in the crucible above a casting roller, and forming an alloy casting sheet after passing through the casting roller; (3) vacuum sputtering: carrying out vacuum sputtering coating on the alloy casting sheet; (4) cooling and discharging: after vacuum sputtering coating, the alloy cast sheet enters a water cooling device for cooling, and is discharged from the furnace after cooling; (5) vacuum heat treatment: and carrying out heat treatment twice on the alloy cast sheet after the alloy cast sheet is taken out of the furnace. The invention carries out vacuum sputtering coating on the uncooled alloy casting sheet, forms a heavy rare earth sputtering film on the side surface, carries out heat treatment after cooling, and leads the heavy rare earth to permeate into the alloy casting sheet, the permeation effect of the heavy rare earth is good, the use amount of the heavy rare earth can be reduced by 20-30%, the utilization rate of heavy rare earth elements is improved, and the production cost is greatly reduced.

Description

Preparation method of neodymium iron boron grain boundary infiltration alloy cast sheet
Technical Field
The invention relates to a preparation method of a neodymium iron boron grain boundary infiltration alloy casting sheet.
Background
Neodymium iron boron as rare earth permanent magnetic material has the advantages of high cost performance, small volume, light weight, good mechanical property and strong magnetism, has extremely high magnetic energy and coercive force, is known as Magen in the magnetic field, is widely applied to the fields of electronics, electric machinery, medical appliances, toys, packaging, hardware machinery, aerospace and the like, and is more commonly used as a permanent magnet motor, a loudspeaker, a magnetic separator, a computer disk driver, a magnetic resonance imaging device instrument and the like.
The coercive force characteristic of the sintered neodymium iron boron is mainly realized by heavy rare earth elements dysprosium and terbium in the distribution, and researches find that the heavy rare earth elements are distributed in a neodymium-rich phase, the generated coercive force improving effect is very obvious, and the heavy rare earth elements are remained in a main phase and have little effect of improving the coercive force. If the heavy rare earth elements are directly added in the smelting stage, a large part of the heavy rare earth elements enter the main phase, and the distribution cost is increased. At present, dysprosium and terbium elements enter a neodymium-rich phase by using a heavy rare earth permeation technology in the industry, so that the use amount of the heavy rare earth elements is reduced, but the coercive force is improved.
At present, the main coating methods of penetrant are: 1. coating by adopting a powder penetrating agent which is composed of dysprosium oxide, dysprosium fluoride, terbium oxide, terbium fluoride and related mixed powder and an organic solvent, wherein the mode has the defects of large waste and nonuniform coating; 2. the mode of vacuum coating is adopted, and penetrant (in a metal state) is sputtered onto the neodymium iron boron black sheet to be permeated in a vacuum mode, so that the mode has high requirement on equipment, the use cost is high, the thickness of the black sheet is required to be within 2-10 mm, and the permeation purpose of an over-thick product cannot be achieved.
The rare earth is a general name of seventeen metal elements including lanthanide elements, scandium and yttrium in a chemical periodic table, and is divided into light rare earth and heavy rare earth, the light rare earth is cheap relative to the heavy rare earth, and terbium and dysprosium are used in vacuum coating of the neodymium iron boron magnet, and the two heavy rare earths are higher in price, so that the more the heavy rare earth is used, the higher the coating cost of the neodymium iron boron magnet is, the existing coating mode of grain boundary permeation can reduce the use amount of the heavy rare earth by 2% -8% compared with the common coating mode, but the cost is higher. Therefore, the method for reducing the use amount of heavy rare earth and improving the performance when sintering neodymium iron boron is a subject which needs to be overcome urgently in the magnetic material industry at present.
Disclosure of Invention
The invention overcomes the defects and provides the preparation method of the neodymium iron boron grain boundary infiltration alloy cast sheet, which greatly improves the utilization rate of heavy rare earth elements, reduces the use amount of heavy rare earth, and has good infiltration effect and high production efficiency.
The technical scheme adopted by the invention for solving the technical problems is as follows: the preparation method of the neodymium iron boron grain boundary infiltration alloy cast sheet comprises the following steps:
(1) vacuum smelting: adding the neodymium iron boron alloy distribution raw materials into a crucible of a vacuum smelting furnace in sequence for smelting;
(2) casting: pouring the alloy melt in the crucible above a casting roller after the temperature of the melted alloy reaches 1450-1500 ℃, and forming an alloy casting sheet after the alloy melt passes through the casting roller;
(3) vacuum sputtering: the alloy cast sheet falling from the casting roll passes through a vacuum sputtering device, and the vacuum sputtering device carries out vacuum sputtering coating operation on the alloy cast sheet;
(4) cooling and discharging: after the vacuum sputtering coating operation, cooling the alloy cast sheet in a water cooling device, and discharging the alloy cast sheet after cooling to 20-60 ℃;
(5) vacuum heat treatment: placing the alloy cast sheet discharged from the furnace into a heat treatment furnace for carrying out heat treatment twice; the first heat treatment process comprises the following steps: vacuum degree of 10-5~10-3Pa, the treatment temperature is 750-920 ℃, the heat preservation time is 5-7 h, and the temperature is cooled to be below 100 ℃; the second heat treatment process comprises the following steps: vacuum degree of 10-2~10-1Pa, the treatment temperature is 480-520 ℃, the heat preservation time is 4-5 h, and the temperature is cooled to the room temperature.
Wherein, the vacuum sputtering device is arranged below the casting roller and above the water cooling device.
Wherein, in the step (3), the time of vacuum sputtering is 9-12 minutes.
Wherein, in the step (3), the thickness of the vacuum sputtering coating is 0.02-0.2 mm.
Compared with the prior art, the invention carries out vacuum sputtering coating operation after casting the alloy casting piece and before cooling, so that a layer of heavy rare earth sputtering film is formed on the side surface of the uncooled alloy casting piece, and then the heavy rare earth is subjected to heat treatment after cooling, so that the heavy rare earth is infiltrated into the alloy casting piece, the infiltration effect of the heavy rare earth is good, the use amount of the heavy rare earth can be reduced by 20-30%, the utilization rate of heavy rare earth elements is improved, the production cost is greatly reduced, and the invention can be popularized and applied in a large scale.
Drawings
FIG. 1 is a process flow diagram of the preparation method of the NdFeB grain boundary infiltration alloy casting sheet of the invention.
Detailed Description
The invention is described in further detail below with reference to the accompanying examples.
Example 1
Referring to fig. 1, a method for preparing an ndfeb grain boundary infiltration alloy cast sheet includes the following steps:
(1) charging in a vacuum smelting furnace: adding the conventional commercial neodymium iron boron alloy distribution raw materials of N45 in the industry into a crucible of a vacuum smelting furnace in sequence;
(2) vacuum smelting: smelting the alloy, and preparing for casting after smelting;
(3) preparing vacuum sputtering: starting a vacuum sputtering device, setting parameters, and performing coating preparation according to the coating thickness of 0.05 mm;
(4) starting a casting system: after the temperature of the alloy melt subjected to vacuum melting reaches 1450 ℃, starting a casting roller, pressing down an automatic pouring device of the crucible, pouring the alloy melt in the crucible above the casting roller, and forming an alloy casting sheet after passing through the casting roller;
(5) starting vacuum sputtering: when the alloy cast sheet begins to fall from the casting roll, starting a vacuum sputtering device, and carrying out vacuum sputtering coating operation on the fallen alloy cast sheet, wherein the whole process is about 9 minutes;
(6) cooling and discharging: stopping the vacuum sputtering device after the end, cooling the alloy cast sheet in a water cooling device for about 1 hour, and discharging the alloy cast sheet after the alloy cast sheet is cooled to 60 ℃;
(7) vacuum heat treatment: placing the neodymium iron boron alloy coated with the heavy rare earth coating in a vacuum heat treatment furnace for twice heat treatment; the first heat treatment process comprises the following steps: degree of vacuum 10-5Pa, the treatment temperature is 750 ℃, the heat preservation time is 5 hours, and the temperature is cooled to be below 100 ℃; the second heat treatment process comprises the following steps: degree of vacuum 10-2Pa, the treatment temperature is 480 ℃, the heat preservation time is 5 hours, and the temperature is cooled to the room temperature;
(8) and (3) processing and forming: after the heat treatment is finished, the black sheet with the specification of 30mm multiplied by 20mm multiplied by 7mm is processed, and the obtained black sheet is subjected to performance test, so that the coercive force can be improved by 5.9kOe under the original process condition, and the residual magnetism and the magnetic energy product are basically unchanged.
Example 2
Referring to fig. 1, a method for preparing an ndfeb grain boundary infiltration alloy cast sheet includes the following steps:
(1) charging in a vacuum smelting furnace: adding the conventional commercial neodymium iron boron alloy distribution raw materials of N45 in the industry into a crucible of a smelting furnace in sequence;
(2) vacuum smelting: smelting the alloy, and preparing for casting after smelting;
(3) preparing vacuum sputtering: starting a vacuum sputtering device, setting parameters, and performing coating preparation according to the coating thickness of 0.1 mm;
(4) starting a casting system: after the temperature of the alloy melt subjected to vacuum melting reaches 1450 ℃, starting a casting roller, pressing down an automatic pouring device of the crucible, pouring the alloy melt in the crucible above the casting roller, and forming an alloy casting sheet after passing through the casting roller;
(5) starting vacuum sputtering: when the alloy cast sheet begins to separate from the casting roll and fall downwards, starting a vacuum sputtering device, and carrying out vacuum sputtering coating operation on the fallen alloy cast sheet, wherein the whole process is about 10 minutes;
(6) cooling and discharging: stopping the vacuum sputtering device after the end, cooling the alloy cast sheet in a water cooling device for about 1 hour, and discharging the alloy cast sheet after the alloy cast sheet is cooled to 60 ℃;
(7) vacuum heat treatment: placing the neodymium iron boron alloy coated with the heavy rare earth coating in a vacuum heat treatment furnace for twice heat treatment; the first heat treatment process comprises the following steps: degree of vacuum 10-5Pa, the treatment temperature is 750 ℃, the heat preservation time is 5 hours, and the temperature is cooled to be below 100 ℃; the second heat treatment process comprises the following steps: degree of vacuum 10-2Pa, the treatment temperature is 480 ℃, the heat preservation time is 5 hours, and the temperature is cooled to the room temperature;
(8) and (3) processing and forming: after the heat treatment is finished, the black sheet with the specification of 30mm multiplied by 20mm multiplied by 7mm is processed, and the obtained black sheet is subjected to performance test, so that the coercive force can be improved by 8.5kOe under the original process condition, and the residual magnetism and the magnetic energy product are basically unchanged.
Example 3
Referring to fig. 1, a method for preparing an ndfeb grain boundary infiltration alloy cast sheet includes the following steps:
(1) charging in a vacuum smelting furnace: adding the conventional commercial neodymium iron boron alloy distribution raw materials of N45 in the industry into a crucible of a smelting furnace in sequence;
(2) vacuum smelting: smelting the alloy, and preparing for casting after smelting;
(3) preparing vacuum sputtering: starting a vacuum sputtering device, setting parameters, and performing coating preparation according to the coating thickness of 0.15 mm;
(4) starting a casting system: after the temperature of the alloy melt subjected to vacuum melting reaches 1500 ℃, starting a casting roller, pressing down an automatic pouring device of the crucible, pouring the alloy melt in the crucible above the casting roller, and forming an alloy casting sheet after passing through the casting roller;
(5) starting vacuum sputtering: when the alloy cast sheet begins to separate from the casting roll and fall downwards, starting a vacuum sputtering device, and carrying out vacuum sputtering coating operation on the fallen alloy cast sheet, wherein the whole process is about 12 minutes;
(6) cooling and discharging: and after the end, stopping the vacuum sputtering device, cooling the alloy casting sheet in a water cooling device for about 2 hours, and discharging the alloy casting sheet after the alloy casting sheet is cooled to 20 ℃.
(7) Vacuum heat treatment: placing the neodymium iron boron alloy coated with the heavy rare earth coating in a vacuum heat treatment furnace for twice heat treatment; the first heat treatment process comprises the following steps: degree of vacuum 10-3Pa, the treatment temperature is 920 ℃, the heat preservation time is 7 hours, and the temperature is cooled to be below 100 ℃; the second heat treatment process comprises the following steps: degree of vacuum 10-1Pa, the treatment temperature is 520 ℃, the heat preservation time is 4 hours, and the temperature is cooled to the room temperature.
(8) And (3) processing and forming: after the heat treatment is finished, the black sheet with the specification of 30mm multiplied by 20mm multiplied by 7mm is processed, and the obtained black sheet is subjected to performance test, so that the coercive force can be improved by 9.4kOe under the original process condition, and the residual magnetism and the magnetic energy product are basically unchanged.
In the above embodiments 1 to 3, a crucible, a casting roll, a vacuum sputtering apparatus, and a water cooling apparatus may be sequentially disposed in a vacuum melting furnace, the crucible being disposed above the casting roll, the vacuum sputtering apparatus being disposed below the casting roll, and above the water cooling apparatus; the existing vacuum rapid hardening furnace can be modified, a support frame is added above a water cooling device, a vacuum magnetron sputtering device is installed on the support frame, the center position of a nozzle is aligned to an effective area of an alloy casting sheet, and the height of the nozzle is 10-20 cm; the vacuum sputtering device adopts heavy rare earth elements dysprosium, terbium and alloys of dysprosium, terbium, aluminum and copper in a certain proportion as target materials for vacuum sputtering.
The thickness of the coating film of the sample after the coating treatment in examples 1 to 3 can be 0.02 to 0.2 mm.
The magnetic properties of the coated samples of examples 1-3 were compared with those of untreated commercial N45 dispensed black flakes in Table 1.
TABLE 1 comparison of magnetic Properties of the samples of the examples with those of the untreated samples
Sample (I) Br/kGs Hcb/kOe Hcj/kOe (BH)max/MGOe △Hcj/kOe
Commercial N45 partition 13.52 12.80 13.21 43.26 /
Example 1 sample 13.48 12.96 19.11 43.68 5.9
Example 2 sample 13.47 12.98 21.71 43.72 8.5
Example 3 sample 13.46 13.01 22.61 43.85 9.4
In the process of casting in the vacuum rapid hardening furnace, the infiltration material is sputtered onto the uncooled alloy casting sheet in vacuum, a layer of heavy rare earth sputtering film is formed on the side surface of the alloy casting sheet, and the alloy casting sheet is placed into the vacuum heat treatment furnace for heat treatment, so that the heavy rare earth element is infiltrated into the alloy casting sheet, the effect of infiltration process is achieved, the infiltration effect of the heavy rare earth is good, the use amount of the heavy rare earth can be reduced by 20-30%, the utilization rate of the heavy rare earth element is improved, the production cost is greatly reduced, and the method can be popularized and applied in a large scale.
Finally, it should be noted that: the above examples are merely illustrative of the technical solutions of the present invention, and not limitative thereof; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions of the embodiments of the present invention.

Claims (4)

1. A preparation method of a neodymium iron boron grain boundary infiltration alloy cast sheet is characterized by comprising the following steps: the method comprises the following steps:
(1) vacuum smelting: adding the neodymium iron boron alloy distribution raw materials into a crucible of a vacuum smelting furnace in sequence for smelting;
(2) casting: pouring the alloy melt in the crucible above a casting roller after the temperature of the melted alloy reaches 1450-1500 ℃, and forming an alloy casting sheet after the alloy melt passes through the casting roller;
(3) vacuum sputtering: after the alloy cast sheet is cast, carrying out vacuum sputtering coating operation before cooling to form a layer of heavy rare earth sputtering film on the side surface of the uncooled alloy cast sheet;
(4) cooling and discharging: after the vacuum sputtering coating operation, cooling the alloy cast sheet in a water cooling device, and discharging the alloy cast sheet after cooling to 20-60 ℃;
(5) vacuum heat treatment: placing the alloy cast sheet discharged from the furnace into a heat treatment furnace for carrying out heat treatment twice; the first heat treatment process comprises the following steps: vacuum degree of 10-5~10-3Pa, the treatment temperature is 750-920 ℃, the heat preservation time is 5-7 h, and the temperature is cooled to be below 100 ℃; the second heat treatment process comprises the following steps: vacuum degree of 10-2~10-1Pa, the treatment temperature is 480-520 ℃, the heat preservation time is 4-5 h, and the temperature is cooled to the room temperature.
2. The method for preparing the NdFeB grain boundary infiltration alloy casting sheet according to claim 1, wherein the vacuum sputtering device is arranged below the casting roller and above the water cooling device.
3. The method for preparing the NdFeB grain boundary infiltration alloy casting sheet according to claim 1, wherein in the step (3), the vacuum sputtering time is 9-12 minutes.
4. The method for preparing the NdFeB grain boundary infiltration alloy casting sheet according to claim 1, wherein in the step (3), the thickness of the vacuum sputtering coating is 0.02-0.2 mm.
CN201811363765.6A 2018-11-16 2018-11-16 Preparation method of neodymium iron boron grain boundary infiltration alloy cast sheet Active CN109473247B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811363765.6A CN109473247B (en) 2018-11-16 2018-11-16 Preparation method of neodymium iron boron grain boundary infiltration alloy cast sheet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811363765.6A CN109473247B (en) 2018-11-16 2018-11-16 Preparation method of neodymium iron boron grain boundary infiltration alloy cast sheet

Publications (2)

Publication Number Publication Date
CN109473247A CN109473247A (en) 2019-03-15
CN109473247B true CN109473247B (en) 2020-09-18

Family

ID=65673600

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811363765.6A Active CN109473247B (en) 2018-11-16 2018-11-16 Preparation method of neodymium iron boron grain boundary infiltration alloy cast sheet

Country Status (1)

Country Link
CN (1) CN109473247B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110211792A (en) * 2019-04-28 2019-09-06 深圳市吉胜华力科技有限公司 A kind of rare earth permanent-magnetic material preparation method
CN116334552B (en) * 2023-04-07 2023-09-05 宁波招宝磁业有限公司 Neodymium iron boron cast sheet sputtering processing method

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104240883A (en) * 2014-09-12 2014-12-24 沈阳中北通磁科技股份有限公司 Rare-earth permanent magnet alloy plate, double-alloy neodymium-iron-boron permanent magnet and manufacturing methods thereof
CN104733148A (en) * 2015-03-31 2015-06-24 安徽省瀚海新材料有限公司 High-performance Re-TM-B permanent magnetic material manufacturing method
CN107424825A (en) * 2017-07-21 2017-12-01 烟台首钢磁性材料股份有限公司 A kind of neodymium iron boron magnetic body coercivity improves method

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH04180554A (en) * 1990-11-13 1992-06-26 Yaskawa Electric Corp Production of rare earth magnetic thin film
US5395459A (en) * 1992-06-08 1995-03-07 General Motors Corporation Method for forming samarium-iron-nitride magnet alloys
US10256018B2 (en) * 2014-02-14 2019-04-09 Santoku Corporation Cast rare earth-containing alloy sheet, manufacturing method therefor, and sintered magnet
CN106282948B (en) * 2016-07-28 2017-12-01 北京中科三环高技术股份有限公司 A kind of preparation method of film plating process and coating system and rare-earth magnet

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104240883A (en) * 2014-09-12 2014-12-24 沈阳中北通磁科技股份有限公司 Rare-earth permanent magnet alloy plate, double-alloy neodymium-iron-boron permanent magnet and manufacturing methods thereof
CN104733148A (en) * 2015-03-31 2015-06-24 安徽省瀚海新材料有限公司 High-performance Re-TM-B permanent magnetic material manufacturing method
CN107424825A (en) * 2017-07-21 2017-12-01 烟台首钢磁性材料股份有限公司 A kind of neodymium iron boron magnetic body coercivity improves method

Also Published As

Publication number Publication date
CN109473247A (en) 2019-03-15

Similar Documents

Publication Publication Date Title
CN101707107B (en) Manufacturing method of high-residual magnetism high-coercive force rare earth permanent magnetic material
US9350203B2 (en) Rare earth sintered magnet, method for producing the same, motor, and automobile
US11114237B2 (en) Method of improving the coercivity of Nd—Fe—B magnets
CN104112580B (en) Preparation method of rare earth permanent magnet
JP6488976B2 (en) R-T-B sintered magnet
JP7220300B2 (en) Rare earth permanent magnet material, raw material composition, manufacturing method, application, motor
JP4702549B2 (en) Rare earth permanent magnet
US20150187494A1 (en) Process for preparing rare earth magnets
US20220293309A1 (en) R-t-b-based permanent magnet material, preparation method therefor and use thereof
JP2018504769A (en) Manufacturing method of RTB permanent magnet
KR20130115151A (en) Rare earth sintered magnet and making method
JP2016122862A (en) Rare earth permanent magnet material and manufacturing method therefor
US10672545B2 (en) R-T-B based permanent magnet
JP2005011973A (en) Rare earth-iron-boron based magnet and its manufacturing method
CN110428947B (en) Rare earth permanent magnetic material and raw material composition, preparation method and application thereof
WO2021098225A1 (en) Neodymium-iron-boron magnet material, raw material composition, preparation method therefor and use thereof
CN109473247B (en) Preparation method of neodymium iron boron grain boundary infiltration alloy cast sheet
EP3667685A1 (en) Heat-resistant neodymium iron boron magnet and preparation method therefor
CN110648813B (en) R-T-B series permanent magnetic material, raw material composition, preparation method and application
CN108389712A (en) A kind of method that electrophoresis reduction prepares high-performance neodymium-iron-boron magnet
KR102606749B1 (en) R-T-B series permanent magnet materials, raw material composition, manufacturing method, application
KR20190061244A (en) Method for preparing rare-earth permanent magnet
CN113936879A (en) La-containing R-T-B rare earth permanent magnet
JP2021532565A (en) R-TB permanent magnet material and its preparation method
WO2021147908A1 (en) R-fe-b sintered magnet and grain boundary diffusion treatment method therefor

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