CN111029128A - Rapid heat treatment method of rare earth permanent magnet - Google Patents
Rapid heat treatment method of rare earth permanent magnet Download PDFInfo
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- CN111029128A CN111029128A CN201911423935.XA CN201911423935A CN111029128A CN 111029128 A CN111029128 A CN 111029128A CN 201911423935 A CN201911423935 A CN 201911423935A CN 111029128 A CN111029128 A CN 111029128A
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- permanent magnet
- rare earth
- earth permanent
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- heat treatment
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F41/00—Apparatus 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
- H01F41/02—Apparatus 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
- H01F41/0253—Apparatus 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
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F1/00—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
- H01F1/01—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
- H01F1/03—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
- H01F1/032—Magnets 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
- H01F1/04—Magnets 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
- H01F1/047—Alloys characterised by their composition
- H01F1/053—Alloys characterised by their composition containing rare earth metals
- H01F1/055—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5
- H01F1/057—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 and IIIa elements, e.g. Nd2Fe14B
Abstract
The invention discloses a rapid heat treatment method of a rare earth permanent magnet material. The method uses an improved spark plasma sintering technology, and adds an electric insulating layer material with better heat conductivity between an SPS die and a sample and between an electrode and the sample, thereby avoiding the direct action of current and a permanent magnet and carrying out rapid and transient heat treatment on the rare earth permanent magnet. The invention aims to realize annealing, improve the organization structure, reduce the stray field at the interface, reduce the reverse magnetization nucleation area and improve the coercive force of the magnet while avoiding the growth of crystal grains in the magnet through rapid heat treatment.
Description
Technical Field
The invention relates to the field of permanent magnets, in particular to a rapid heat treatment method of a rare earth permanent magnet.
Background
The third generation rare earth permanent magnet neodymium iron boron has the advantages of high remanence, high coercivity and high magnetic energy product, and is widely applied to the fields of power electronics, communication information, transportation, medical equipment, military and the like. However, the temperature stability of the neodymium iron boron is relatively poor, and the thermal demagnetization effect is obvious. The improvement of the coercivity is an important solution to meet the application of complex service environments. To a certain extent, the smaller the neodymium iron boron crystal grain is, the higher the coercive force of the magnet is. However, along with the refinement of the crystal grains, the number of the interfaces is increased, the defect density at the interfaces is high, the relaxation and reconstruction phenomena of atoms are more likely to occur, and a high stray field is presented. The heat treatment is an effective method for optimizing a grain boundary region, reducing the defect density at an interface and improving the coercive force. However, the conventional heat treatment technology has a slow heating speed and a long heat treatment period, and is easy to cause abnormal growth of crystal grains, and the effect of improving the magnetic performance is limited. Therefore, a rapid thermal processing method is urgently needed, which can provide large driving force, improve the distribution of grain boundary phases, reduce the reverse magnetization nucleation sites and improve the coercivity while avoiding the growth of crystal grains.
Especially for the high-abundance rare earth permanent magnet which has gained wide attention in recent years, due to the difference of physicochemical properties between lanthanum cerium yttrium rare earth element and didymium, new grain boundary phase including REFE is easy to be precipitated at the grain boundary under the high lanthanum cerium yttrium substitution amount2、RE2O3And the like, the number of the grain boundaries is more, the environment of the grain boundaries is more complicated, and the requirement on heat treatment is higher. Therefore, for high-abundance rare earth permanent magnets, the interdiffusion of rare earth elements, the growth of crystal grains and the distribution and evolution of crystal boundaries need to be controlled in the heat treatment process so as to meet the commercial requirements.
The Spark Plasma Sintering (SPS) technology can realize rapid temperature rise, the whole period is relatively short, and abnormal growth of crystal grains and diffusion precipitation of elements in the magnet in the long-time temperature rise, heat preservation and temperature reduction processes can be avoided. However, rare earth permanent magnets belong to metal-based multi-phase alloys, and have strong conductivity, and in the heat treatment process, conducted current passes through the magnet and reacts with the permanent magnet material, and the generated polarization effect and the like have uncontrollable influences on element diffusion, grain boundary distribution and magnetic performance.
Disclosure of Invention
The invention aims to overcome the defects of the prior art and provide a rapid heat treatment method of rare earth permanent magnet.
The invention is characterized in that the rapid heat treatment is carried out on the rare earth permanent magnet by using discharge plasma sintering, and the magnet comprises the following components (A) in percentage by mass1-xRx)yQbalMzBwWherein A is one or more elements of Nd, Pr, Dy, Tb, Gd, Ho and Sm, R is one or more elements of La, Ce and Y, Q is one or more elements of Co, Fe and Ni, M is one or more elements of Al, Co, Cr, Cu, Ga, Mn, Mo, Nb, Ni, Si, Ta, Ti, V and Zr, x is more than or equal to 0 and less than or equal to 0.8, Y is more than or equal to 26 and less than or equal to 36, z is more than or equal to 0 and less than or equal to 3, and w is more than or equal to 0.8 and less than or equal to 1.3.
Electric insulation layers with good heat conduction performance are added between the SPS die and the rare earth permanent magnet and between the electrode and the rare earth permanent magnet, the die conducts electricity and generates heat, heat is conducted into a sample through the heat conduction insulation layers, rapid temperature rise is achieved, and the rare earth permanent magnet is subjected to heat treatment.
In a preferred embodiment of the present invention, the material of the electrical insulation layer with good thermal conductivity is alumina Al2O3Zirconium oxide ZrO2Silicon carbide SiC and silicon nitride Si3N4Or aluminum nitride AlN.
As a preferred scheme of the invention, the pressure applied to the rare earth permanent magnet in the rapid heat treatment is 2-50 MPa. More preferably, the pressure is 5 to 20 MPa.
As a preferred scheme of the invention, the temperature rise speed in the rapid heat treatment is 20-400 ℃/min, and the heat preservation time is 5-180 min. More preferably, the temperature rising speed is 50-300 ℃/min, and the heat preservation time is 20-120 min.
As a preferred scheme of the invention, the temperature in the rapid heat treatment is 400-1000 ℃. More preferably, the temperature in the rapid heat treatment is 500-800 ℃.
Compared with the prior art, the invention has the following beneficial effects: the invention adopts the rapid heat treatment of the spark plasma sintering equipment, although the rare earth permanent magnetic alloy is a conductor, the influence of current on the performance of the magnet is avoided while the rapid temperature rise is realized by adding the heat conduction and electric insulation material in the middle, so that the relatively rapid heat treatment is realized, the abnormal growth of crystal grains is avoided, the residual stress in the magnet is released, the defect at the crystal boundary is consumed, and the coercive force of the magnet is improved.
Detailed Description
The present invention is further illustrated by the following examples, but is not limited to the following examples:
example 1:
the magnet comprises (by mass percent) Nd0.5Ce0.5]30.5FebalAl1B1. Placing the magnet into SPS mold, and adding aluminum oxide Al between SPS mold and sample and between electrode and sample2O3And the thin layer realizes rapid heating treatment. The pressure applied in the rapid heat treatment process is 2MPa, the temperature rise speed is 100 ℃/min, the heat preservation time is 15min, and the heat treatment temperature is 600 ℃. The magnetic property of the magnet is Br=13.0kGs,Hcj=11.5kOe,(BH)max=40.1MGOe
Example 2:
the magnet comprises the following components in percentage by mass [ Pr%0.1Nd0.4Ce0.5]30.5FebalAl0.5Cu0.2Co0.5Nb0.15B1. Placing the magnet into SPS mold, and adding aluminum oxide Al between SPS mold and sample and between electrode and sample2O3And the thin layer realizes rapid heating treatment. The pressure applied in the rapid heat treatment process is 5MPa, the temperature rise speed is 100 ℃/min, the heat preservation time is 40min, and the heat treatment temperature is 600 ℃. The magnetic property of the magnet is Br=13.1kGs,Hcj=12.5kOe,(BH)max=41.1MGOe
Example 3:
the magnet comprises (by mass percent) Nd0.7Ce0.3]31.2FebalAl0.5Zr0.15Ga0.3B0.95. And (3) placing the magnet into an SPS (semi-spherical surface sintering) mold, and adding an aluminum nitride (AlN) thin layer between the SPS mold and the sample and between the electrode and the sample to realize rapid heating treatment. The pressure applied in the rapid heat treatment process is 20MPa, the temperature rise speed is 200 ℃/min, the heat preservation time is 60min, and the heat treatment temperature is 680 ℃. The magnetic property of the magnet is Br=13.5kGs,Hcj=13.5kOe,(BH)max=44.3MGOe。
Example 4:
the magnet comprises the following components in percentage by mass [ Pr%0.17Nd0.68Ce0.1La0.05]30.8FebalCo0.2Cu0.2Zr0.15B1. And (3) putting the magnet into an SPS (semi-spherical permanent magnet) mold, and adding a silicon carbide SiC thin layer between the SPS mold and the sample and between the electrode and the sample to realize rapid heating treatment. The pressure applied in the rapid heat treatment process is 15MPa, the temperature rise speed is 300 ℃/min, the heat preservation time is 60min, and the heat treatment temperature is 800 ℃. The magnetic property of the magnet is Br=13.7kGs,Hcj=14.6kOe,(BH)max=46.0MGOe。
Claims (6)
1. A rapid thermal processing method of a rare earth permanent magnet, characterized in that the rapid thermal processing of the rare earth permanent magnet is carried out by using discharge plasma sintering, the rapid thermal processing is carried out by the following method: and electric insulating layers with better heat conduction performance are added between the SPS die and the rare earth permanent magnet and between the electrode and the rare earth permanent magnet, heat is conducted into the sample through the heat conduction insulating layers, rapid temperature rise is realized, and the rare earth permanent magnet is subjected to heat treatment.
2. The rapid thermal processing method for rare earth permanent magnet according to claim 1, wherein the composition of the rare earth permanent magnet is (A) in mass percent1-xRx)yQbalMzBwWherein A is one or more elements of Nd, Pr, Dy, Tb, Gd, Ho and Sm, R is one or more elements of La, Ce and Y, and Q is Co,Fe. One or more elements in Ni, M is one or more elements in Al, Co, Cr, Cu, Ga, Mn, Mo, Nb, Ni, Si, Ta, Ti, V and Zr, x is more than or equal to 0 and less than or equal to 0.8, y is more than or equal to 26 and less than or equal to 36, z is more than or equal to 0 and less than or equal to 3, and w is more than or equal to 0.8 and less than or equal to 1.3.
3. The rapid thermal processing method of rare-earth permanent magnet according to claim 1, wherein the electrically insulating layer having a good thermal conductivity is made of alumina Al2O3Zirconium oxide ZrO2Silicon carbide SiC and silicon nitride Si3N4Or aluminum nitride AlN.
4. The method according to claim 1, wherein the pressure applied to the rare earth permanent magnet in the rapid thermal treatment is 2 to 50 MPa.
5. The method according to claim 1, wherein the temperature rise rate in the rapid thermal treatment is 20 to 400 ℃/min, and the holding time is 5 to 180 min.
6. The method according to claim 1, wherein the temperature in the rapid thermal treatment is 400 to 1000 ℃.
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112927920A (en) * | 2021-03-05 | 2021-06-08 | 西安交通大学 | Pressurizing heat treatment method for improving magnetic property of 2:17 type Sm-Co sintered magnet |
CN113130200A (en) * | 2021-04-26 | 2021-07-16 | 浙江大学 | Method for improving magnetic property of Ce-Y-rich rare earth permanent magnet |
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EP2869311A1 (en) * | 2013-10-29 | 2015-05-06 | Institute Jozef Stefan | Method of manufacturing fully dense Nd-Fe-B magnets with enhanced coercivity and gradient microstructure |
US20160322136A1 (en) * | 2015-04-30 | 2016-11-03 | Jozef Stefan Institute | METAL-BONDED RE-Fe-B MAGNETS |
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CN101266859A (en) * | 2008-01-08 | 2008-09-17 | 上海大学 | Method for quick sintering of micro-crystal ferrite magnetic core part |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
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CN112927920A (en) * | 2021-03-05 | 2021-06-08 | 西安交通大学 | Pressurizing heat treatment method for improving magnetic property of 2:17 type Sm-Co sintered magnet |
CN112927920B (en) * | 2021-03-05 | 2022-05-06 | 西安交通大学 | Pressurizing heat treatment method for improving magnetic property of 2:17 type Sm-Co sintered magnet |
CN113130200A (en) * | 2021-04-26 | 2021-07-16 | 浙江大学 | Method for improving magnetic property of Ce-Y-rich rare earth permanent magnet |
CN113130200B (en) * | 2021-04-26 | 2022-06-17 | 浙江大学 | Method for improving magnetic property of Ce-Y-rich rare earth permanent magnet |
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Application publication date: 20200417 |