EP0289680B1 - Permanent magnet and method of producing the same - Google Patents
Permanent magnet and method of producing the same Download PDFInfo
- Publication number
- EP0289680B1 EP0289680B1 EP87308666A EP87308666A EP0289680B1 EP 0289680 B1 EP0289680 B1 EP 0289680B1 EP 87308666 A EP87308666 A EP 87308666A EP 87308666 A EP87308666 A EP 87308666A EP 0289680 B1 EP0289680 B1 EP 0289680B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- magnet
- permanent magnet
- alloy
- cast
- ppm
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000000034 method Methods 0.000 title claims description 39
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 34
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 22
- 239000000956 alloy Substances 0.000 claims abstract description 22
- 229910052761 rare earth metal Inorganic materials 0.000 claims abstract description 19
- 239000013078 crystal Substances 0.000 claims abstract description 12
- 229910052742 iron Inorganic materials 0.000 claims abstract description 12
- 229910052796 boron Inorganic materials 0.000 claims abstract description 11
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract description 10
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 6
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims abstract description 6
- 229910052799 carbon Inorganic materials 0.000 claims abstract description 6
- 239000001301 oxygen Substances 0.000 claims abstract description 6
- 229910052760 oxygen Inorganic materials 0.000 claims abstract description 6
- 238000005266 casting Methods 0.000 claims description 11
- 238000004519 manufacturing process Methods 0.000 claims description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- 229910017052 cobalt Inorganic materials 0.000 claims description 3
- 239000010941 cobalt Substances 0.000 claims description 3
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 239000010949 copper Substances 0.000 claims description 3
- 239000012535 impurity Substances 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 claims description 2
- 229910052804 chromium Inorganic materials 0.000 claims description 2
- 229910052735 hafnium Inorganic materials 0.000 claims description 2
- 229910052750 molybdenum Inorganic materials 0.000 claims description 2
- 229910052758 niobium Inorganic materials 0.000 claims description 2
- 229910052715 tantalum Inorganic materials 0.000 claims description 2
- 229910052721 tungsten Inorganic materials 0.000 claims description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 2
- 229910052726 zirconium Inorganic materials 0.000 claims description 2
- 239000012768 molten material Substances 0.000 claims 1
- 238000007731 hot pressing Methods 0.000 description 9
- 239000012634 fragment Substances 0.000 description 7
- 238000010438 heat treatment Methods 0.000 description 6
- 239000000203 mixture Substances 0.000 description 6
- 238000002074 melt spinning Methods 0.000 description 5
- 238000005245 sintering Methods 0.000 description 5
- 239000004615 ingredient Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 239000011347 resin Substances 0.000 description 4
- 229920005989 resin Polymers 0.000 description 4
- 229910000521 B alloy Inorganic materials 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 229910052723 transition metal Inorganic materials 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- 229910052779 Neodymium Inorganic materials 0.000 description 2
- 229910052777 Praseodymium Inorganic materials 0.000 description 2
- 239000011230 binding agent Substances 0.000 description 2
- 239000011261 inert gas Substances 0.000 description 2
- 150000002910 rare earth metals Chemical class 0.000 description 2
- 229910052727 yttrium Inorganic materials 0.000 description 2
- 229910052684 Cerium Inorganic materials 0.000 description 1
- 229910052692 Dysprosium Inorganic materials 0.000 description 1
- 229910052691 Erbium Inorganic materials 0.000 description 1
- 229910052693 Europium Inorganic materials 0.000 description 1
- 229910052688 Gadolinium Inorganic materials 0.000 description 1
- 229910001047 Hard ferrite Inorganic materials 0.000 description 1
- 229910052689 Holmium Inorganic materials 0.000 description 1
- 229910052765 Lutetium Inorganic materials 0.000 description 1
- 229910052772 Samarium Inorganic materials 0.000 description 1
- 229910052771 Terbium Inorganic materials 0.000 description 1
- 229910052775 Thulium Inorganic materials 0.000 description 1
- 229910052769 Ytterbium Inorganic materials 0.000 description 1
- 229910000828 alnico Inorganic materials 0.000 description 1
- 229910000808 amorphous metal alloy Inorganic materials 0.000 description 1
- 229910052786 argon Inorganic materials 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000004663 powder metallurgy Methods 0.000 description 1
- 238000010298 pulverizing process Methods 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 150000003624 transition metals Chemical class 0.000 description 1
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 description 1
- 229910000859 α-Fe Inorganic materials 0.000 description 1
Images
Classifications
-
- 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
- H01F41/0293—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 diffusion of rare earth elements, e.g. Tb, Dy or Ho, into permanent magnets
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/02—Making metallic powder or suspensions thereof using physical processes
- B22F9/023—Hydrogen absorption
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F9/00—Making metallic powder or suspensions thereof
- B22F9/16—Making metallic powder or suspensions thereof using chemical processes
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
- C21D8/12—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of articles with special electromagnetic properties
- C21D8/1216—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of articles with special electromagnetic properties the working step(s) being of interest
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/0433—Nickel- or cobalt-based alloys
- C22C1/0441—Alloys based on intermetallic compounds of the type rare earth - Co, Ni
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/005—Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/10—Ferrous alloys, e.g. steel alloys containing cobalt
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/16—Ferrous alloys, e.g. steel alloys containing copper
-
- 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
- H01F1/0571—Alloys 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
- H01F1/0575—Alloys 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
- H01F1/0576—Alloys 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 pressed, e.g. hot working
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/90—Magnetic feature
Definitions
- the present invention relates to a permanent magnet which comprises a rare earth element, iron and boron, and a method of producing the same.
- rare earth element R
- Y Yttrium
- a permanent magnet is one of the major components used in the electrical and electronic field, e.g. in various household electrical appliances and in the peripheral console units of large computers.
- Typical permanent magnets now in use include an alnico hard ferrite magnet and a rare earth element -transition metal magnet.
- an R - Co permanent magnet and an R - Fe - B permanent magnet which are rare earth element - transition metal magnets, can produce a high magnetic performance, so that many researches have hitherto been made on them.
- Reference 1 Japanese Patent Laid-Open Specification No. 46008/1984.
- Reference 3 Japanese Patent Laid-Open Specification No. 211549/1984.
- Reference 5 Japanese Patent Laid-Open Specification No. 100402/1985.
- an alloy ingot is first made by melting and casting, and is pulverized to a particle diameter of about 3 »m.
- the pulverized powder is kneaded with a binder, and pressed in a magnetic field to obtain a moulded body.
- the moulded body is sintered at approximately 1,100°C in an argon gas atmosphere for 1 hour, and thereafter heat treated at approximately 600°C to improve the coercive force.
- the resin bonding method (2) which incorporates a melt spinning method, rapidly-quenched thin fragments of an R - Fe - B alloy are first produced by a melt spinning apparatus at an optimum substrate velocity.
- a thus-obtained ribbon-like thin fragment having a thickness of 30 »m is an aggregate of crystal grains having a diameter of not more than 1,000 ⁇ . Since the crystal axes of the crystal grains are distributed isotropically, the thin ribbon is magnetically isotropic. If the thin ribbon is pulverized into an appropriate grain size, kneaded with a resin, and then pressed, an isotropic magnet is obtained.
- the ribbon-like thin fragments used in the method (2) are pressed at a temperature of about 700°C and under a pressure of not more than 1.4 ton/cm2 in vacuo or in an inert gas. Then this pressed body is next pressed at 700°C and under a pressure of 7 ton/cm2 for several seconds to reduce the thickness to half the initial thickness. Thus, a dense and anisotropic R - Fe - B magnet is obtained.
- LDC liquid dynamic compaction process
- the sintering process (1) necessitates the step of powdering an alloy. Since the powder of an R - Fe - B alloy is very reactive to oxygen, it is necessary to handle the charge of the powder used in the sintering process very carefully and an expensive equipment for inert gas, etc. is required.
- the carbon of a binder has a deleterious influence on the magnetic performance, and is difficult to handle the moulded body called a green body.
- Both methods (2) and (3) require an expensive vacuum melt spinning apparatus or hot press which has a poor productivity.
- a magnet produced by the method (2) is isotropic and, hence, it is impossible to obtain a high energy product. This magnet is therefore disadvantageous both in its temperature characteristics and in use.
- the method (3) uses a two-stage hot pressing process. Therefore, the productivity is very poor, and it cannot make the best use of an R - Fe - B magnet which, as stated above, is inexpensive in its material cost.
- the LDC process also has the problems of requiring an expensive equipment and having a poor productivity.
- the alloy contains Nd and/or Pr.
- the invention also comprises a method of making a permanent magnet as recited in Claim 9.
- the magnet is heat treated at a temperature not lower than 250°C.
- the magnet is subjected to hot processing at a temperature not lower than 500°C so as to make the magnet anisotropic.
- the method comprises hot processing the magnet at a temperature not lower than 500°C so as to make the magnet anisotropic, and heat treating the magnet at a temperature not lower than 250°C.
- a preferred composition of a permanent magnet containing at least one rare earth element, iron and boron as basic ingredients is 8 to 30 atm% of a rare earth element or elements, 2 to 28 atm% of boron, the balance being substantially iron.
- rare earth element or elements employed Y, La, Ce, Pr, Nd, Pm, Sm, Eu, Gd, Tb, Dy, Ho, Er, Tm, Yb and Lu are usable. Above all, Nd and Pr are preferable.
- Two or more of these rare earth elements may be used in combination.
- impurities inevitable in the manufacturing process may be contained in the alloy, and cobalt may be added, e.g. in an amount of up to 40 atm%, in order to raise the Curie temperature.
- cobalt may be added, e.g. in an amount of up to 40 atm%, in order to raise the Curie temperature.
- the carbon content and the oxygen content in the magnet are set at no more than 400 ppm and 1,000 ppm, respectively, because if they exceed 400 ppm and 1,000 ppm, respectively, the magnetic performance is lowered.
- the grain diameter of the crystal grains must be appropriate.
- the average grain diameter of the magnet after casting exceeds 150 »m, the coercive force does not reach that of a ferrite magnet, namely 4 KOe, even after hot processing, and such a R - Fe - B alloy cannot be said to be a practical permanent magnet alloy. Therefore, the average grain diameter must be not more than 150 »m.
- the grain diameter can be controlled by varying the cooling temperature by altering the material of a mould, the heat capacity of the mould, etc.
- a heat treatment after casting is necessary for diffusing the Fe phase which exists as the primary crystal in the cast alloy, thereby elminating a magnetically soft phase. It goes without saying that a similar heat treatment carried out after hot processing is effective for improving the magnetic properties.
- the hot processing at a temperature of not lower than 500°C is effective for orientating the crystal axes of the crystal grains to make the magnet anisotropic and for making the crystal grains finer, thereby greatly enhancing the magnetic properties.
- Table 1 shows the compositions, in atm%, of permanent magnets containing various rare earth elements, iron, boron as the basic ingredients which were produced in the following procedure.
- An alloy having a desired composition was melted in an Ar atmosphere in an induction furnace and cast into various moulds at 1,000°C. When 20 minutes had passed after casting the ingots were taken out.
- the alloy contained a rare earth metal having a purity of 95% (the impurities being mainly other rare earth metals), and the alloy contained a transition metal having a purity of not less than 99.9%.
- boron a ferroboron alloy was used.
- the cast alloy was subjected to heat treatment at a temperature of not lower than 250°C (in Example 1, at 1,000°C for 24 hours), and was then cut to obtain a permanent magnet.
- the magnetic performance and the average grain diameter of the magnet obtained by casting each composition into an iron mould is shown in Table 2 below.
- the accompanying drawing shows the relationship between the average diameter (»m) after casting and the coercive force (iHc) after hot pressing of the samples Nos. 3 and 4 having the respective compositions shown in Table 1.
- the grain diameter was controlled by using a water-cooled copper mould, an iron mould, a ceramic mould, etc, and by vibrating the mould. From this result, it is found that it is possible to obtain a permanent magnet by casting while controlling the grain diameter.
- compositions shown in Table 3 below were cast into a water cooled copper mould in the same way as in Example 1, and thereafter the ingots were hot pressed at 1,000°C to make the respective permanent magnets anisotropic.
- the average diameter and the magnetic performance after heat treatment, and the average diameter and the magnetic performance after hot pressing, of each magnet are shown in Table 4 below.
- the hot pressing makes the grain diameters smaller and greatly enhances the magnetic performance, and the heat treatment improves the magnetic performance.
- the casting method was adopted,and the carbon content and the oxygen content in the magnet obtained were not more than 400 ppm and not more than 1,000 ppm, respectively.
- the permanent magnets of the present invention can be produced in bulk with a satisfactory coercive force without the need for pulverizing a cast ingot, it is possible to greatly simplify the manufacturing steps, and a high-performance and low-cost permanent magnet can be obtained.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Materials Engineering (AREA)
- Power Engineering (AREA)
- Crystallography & Structural Chemistry (AREA)
- Physics & Mathematics (AREA)
- Inorganic Chemistry (AREA)
- Thermal Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Electromagnetism (AREA)
- Hard Magnetic Materials (AREA)
- Manufacturing Cores, Coils, And Magnets (AREA)
- Permanent Field Magnets Of Synchronous Machinery (AREA)
- Soft Magnetic Materials (AREA)
Abstract
Description
- The present invention relates to a permanent magnet which comprises a rare earth element, iron and boron, and a method of producing the same.
- The term "rare earth element" (R) is used in this specification in a wide sense as including Yttrium (Y).
- A permanent magnet is one of the major components used in the electrical and electronic field, e.g. in various household electrical appliances and in the peripheral console units of large computers.
- With a recently growing demand for smaller and higher-efficiency electrical appliances, permanent magnets have increasingly been required to have a higher and higher performance. Typical permanent magnets now in use include an alnico hard ferrite magnet and a rare earth element -transition metal magnet. In particular, an R - Co permanent magnet and an R - Fe - B permanent magnet, which are rare earth element - transition metal magnets, can produce a high magnetic performance, so that many researches have hitherto been made on them.
- For example, the following methods have been devised for manufacturing an R -Fe - B permanent magnet.
- (1) A method of sintering a material on the basis of a powder metallurgy technique (
References - (2) A resin bonding method using rapidly-quenched thin fragments obtained by a melt spinning method. A rapidly-quenched thin fragment of about 30 »m thick is produced by a melt spinning apparatus which is used for manufacturing an amorphous alloy, and a magnet is produced from the thin fragments by adopting a resin bonding method. (References 3 and 4, referred to below).
- (3) A method of mechanically aligning the rapidly-quenched thin fragments used in method (2) by a two-stage hot pressing method (
References 4 and 5, referred to below). - Reference 1: Japanese Patent Laid-Open Specification No. 46008/1984.
- Reference 2: M. Sagawa, S. Fujimura, N. Togawa, H. Yamamoto, and Y Matushita: J. Apl. Phys. Vol, 55 (6), 15th March p. 2083 (1984).
- Reference 3: Japanese Patent Laid-Open Specification No. 211549/1984.
- Reference 4: R.W. Lee: Appl. Phys. Lett. Vol. 46(8), 15th April p. 790 (1985).
- Reference 5: Japanese Patent Laid-Open Specification No. 100402/1985.
- In the sintering method (1), an alloy ingot is first made by melting and casting, and is pulverized to a particle diameter of about 3 »m. The pulverized powder is kneaded with a binder, and pressed in a magnetic field to obtain a moulded body.
- The moulded body is sintered at approximately 1,100°C in an argon gas atmosphere for 1 hour, and thereafter heat treated at approximately 600°C to improve the coercive force.
- In the resin bonding method (2) which incorporates a melt spinning method, rapidly-quenched thin fragments of an R - Fe - B alloy are first produced by a melt spinning apparatus at an optimum substrate velocity. A thus-obtained ribbon-like thin fragment having a thickness of 30 »m is an aggregate of crystal grains having a diameter of not more than 1,000Å. Since the crystal axes of the crystal grains are distributed isotropically, the thin ribbon is magnetically isotropic. If the thin ribbon is pulverized into an appropriate grain size, kneaded with a resin, and then pressed, an isotropic magnet is obtained.
- In the manufacturing method (3) which utilises a two-stage hot pressing process, the ribbon-like thin fragments used in the method (2) are pressed at a temperature of about 700°C and under a pressure of not more than 1.4 ton/cm² in vacuo or in an inert gas. Then this pressed body is next pressed at 700°C and under a pressure of 7 ton/cm² for several seconds to reduce the thickness to half the initial thickness. Thus, a dense and anisotropic R - Fe - B magnet is obtained.
- Furthermore, a liquid dynamic compaction process (hereinunder referred to as "LDC" process) is also used for producing an alloy having a coercive force in a bulk state (Reference 6, referred to below).
- Reference 6: T.S. Chin et al: J. Appl. Phys. 59 (4), 15th February, p. 1297 (1986).
- Although a permanent magnet containing a rare earth element, iron and boron as the basic ingredients can be made by the methods of the prior art, these methods have the defects referred to below.
- The sintering process (1) necessitates the step of powdering an alloy. Since the powder of an R - Fe - B alloy is very reactive to oxygen, it is necessary to handle the charge of the powder used in the sintering process very carefully and an expensive equipment for inert gas, etc. is required.
- In addition, in the sintering process,the carbon of a binder has a deleterious influence on the magnetic performance, and is difficult to handle the moulded body called a green body. These problems lower the productivity, and it cannot therefore be said that the method (1) is capable of making the best use of an R - Fe - B magnet whose main advantage is that it is inexpensive in the material cost.
- Both methods (2) and (3) require an expensive vacuum melt spinning apparatus or hot press which has a poor productivity.
- A magnet produced by the method (2) is isotropic and, hence, it is impossible to obtain a high energy product. This magnet is therefore disadvantageous both in its temperature characteristics and in use.
- The method (3) uses a two-stage hot pressing process. Therefore, the productivity is very poor, and it cannot make the best use of an R - Fe - B magnet which, as stated above, is inexpensive in its material cost.
- The LDC process also has the problems of requiring an expensive equipment and having a poor productivity.
- Accordingly, it is an object of the present invention to eliminate the above-described problems in the prior art and to provide a high-performance and low-cost rare earth-iron-boron permanent magnet and a method of manufacturing the same.
- According, therefore, to the present invention, there is provided a permanent magnet as recited in
Claim 1. - Preferably, the alloy contains Nd and/or Pr.
- The invention also comprises a method of making a permanent magnet as recited in Claim 9.
- In a first embodiment of the said method, the magnet is heat treated at a temperature not lower than 250°C.
- In a second embodiment of the said method, the magnet is subjected to hot processing at a temperature not lower than 500°C so as to make the magnet anisotropic.
- In a third embodiment of the said method, the method comprises hot processing the magnet at a temperature not lower than 500°C so as to make the magnet anisotropic, and heat treating the magnet at a temperature not lower than 250°C.
- A preferred composition of a permanent magnet containing at least one rare earth element, iron and boron as basic ingredients is 8 to 30 atm% of a rare earth element or elements, 2 to 28 atm% of boron, the balance being substantially iron.
- As the rare earth element or elements employed Y, La, Ce, Pr, Nd, Pm, Sm, Eu, Gd, Tb, Dy, Ho, Er, Tm, Yb and Lu are usable. Above all, Nd and Pr are preferable.
- Two or more of these rare earth elements may be used in combination. In addition to these basic ingredients, impurities inevitable in the manufacturing process may be contained in the alloy, and cobalt may be added, e.g. in an amount of up to 40 atm%, in order to raise the Curie temperature. Moreover, Aℓ, Cr, Mo, W, Nb, Ta, Zr, Hf, Ti, etc. e.g. in an amount of up to10 atm%, may be added in order to enhance the coercive force.
- As indicated above, the carbon content and the oxygen content in the magnet are set at no more than 400 ppm and 1,000 ppm, respectively, because if they exceed 400 ppm and 1,000 ppm, respectively, the magnetic performance is lowered.
- In order to obtain a desired coercive force in a bulk state in an R - Fe - B magnet, the grain diameter of the crystal grains must be appropriate.
- If the average grain diameter of the magnet after casting exceeds 150 »m, the coercive force does not reach that of a ferrite magnet, namely 4 KOe, even after hot processing, and such a R - Fe - B alloy cannot be said to be a practical permanent magnet alloy. Therefore, the average grain diameter must be not more than 150 »m. The grain diameter can be controlled by varying the cooling temperature by altering the material of a mould, the heat capacity of the mould, etc.
- A heat treatment after casting is necessary for diffusing the Fe phase which exists as the primary crystal in the cast alloy, thereby elminating a magnetically soft phase. It goes without saying that a similar heat treatment carried out after hot processing is effective for improving the magnetic properties.
- The hot processing at a temperature of not lower than 500°C is effective for orientating the crystal axes of the crystal grains to make the magnet anisotropic and for making the crystal grains finer, thereby greatly enhancing the magnetic properties.
- The invention is illustrated, merely by way of example, in the accompanying drawing which is a graph showing the relationship between the average grain diameter (»m) of the crystals after casting and the coercive force (iHc) after hot pressing in an embodiment of the present invention.
- Table 1 below shows the compositions, in atm%, of permanent magnets containing various rare earth elements, iron, boron as the basic ingredients which were produced in the following procedure.
- An alloy having a desired composition was melted in an Ar atmosphere in an induction furnace and cast into various moulds at 1,000°C. When 20 minutes had passed after casting the ingots were taken out. The alloy contained a rare earth metal having a purity of 95% (the impurities being mainly other rare earth metals), and the alloy contained a transition metal having a purity of not less than 99.9%. As boron, a ferroboron alloy was used.
- The cast alloy was subjected to heat treatment at a temperature of not lower than 250°C (in Example 1, at 1,000°C for 24 hours), and was then cut to obtain a permanent magnet.
- The magnetic performance and the average grain diameter of the magnet obtained by casting each composition into an iron mould is shown in Table 2 below.
- The accompanying drawing shows the relationship between the average diameter (»m) after casting and the coercive force (iHc) after hot pressing of the samples Nos. 3 and 4 having the respective compositions shown in Table 1. The grain diameter was controlled by using a water-cooled copper mould, an iron mould, a ceramic mould, etc, and by vibrating the mould. From this result, it is found that it is possible to obtain a permanent magnet by casting while controlling the grain diameter.
- The compositions shown in Table 3 below were cast into a water cooled copper mould in the same way as in Example 1, and thereafter the ingots were hot pressed at 1,000°C to make the respective permanent magnets anisotropic.
- The average diameter and the magnetic performance after heat treatment, and the average diameter and the magnetic performance after hot pressing, of each magnet are shown in Table 4 below.
-
- As is obvious from the above results, the hot pressing makes the grain diameters smaller and greatly enhances the magnetic performance, and the heat treatment improves the magnetic performance.
- In the embodiments of the present invention described above, the casting method was adopted,and the carbon content and the oxygen content in the magnet obtained were not more than 400 ppm and not more than 1,000 ppm, respectively.
- As described above, since the permanent magnets of the present invention can be produced in bulk with a satisfactory coercive force without the need for pulverizing a cast ingot, it is possible to greatly simplify the manufacturing steps, and a high-performance and low-cost permanent magnet can be obtained.
Claims (13)
- A permanet magnet cosisting of a body cast from an alloy having at least one rare earth element, iron and boron characterised in that the average grain diameter of the crystals of the magnet is not more than 150 »m and the carbon and oxygen content of the magnet are not more than 400 ppm and 1,000 ppm, respectively.
- A permanent magnet as claimed in claim 1 characterised in that the alloy contains Nd and/or Pr.
- A permanent magnet as claimed in claim 1 or 2 characterised in that the alloy contains 8 to 30 at% of a rare earth element or elements and 2 to 28 at% of boron, the balance being at least mainly iron.
- A permanent magnet as claimed in claim 3 characterised in that the said balance is made up wholly of iron and impurities.
- A permanent magnet as claimed in claim 3 characterised in that the said balance contains cobalt.
- A permanent magnet as claimed in claim 5 characterised in that the cobalt content of the alloy does not exceed 40 at%.
- A permanent magnet as claimed in any of claims 3, 5 or 6 characterised in that the said balance contains one or more of the elements Aℓ, Cr, Mo, W, Nb, Ta, Zr, Hf andTi.
- A permanent magnet as claimed in claim 7 characterised in that the said balance contains not more than 10 at% of the said one or more elements.
- A method of making a permanent magnet comprising the steps of:-
casting a molten alloy comprising at least one rare earth element, iron and boron to produce a cast body and further processing the cast body to produce the permanent magnet characterised in that the average grain diameter of the crystals of the magnet is not more than 150 »m and the carbon and oxygen content of the magnet are not more than 400 ppm and 1,000 ppm respectively. - A method as claimed in claim 9 characterised in that, after the alloy has been cast, it is heat treated at a temperature not lower than 250°C.
- A method as claimed in claim 9 or 10, characterised in that the cast alloy is subjected to hot processing at a temperature not lower than 500°C so as to make the magnet anisotropic.
- A method as claimed in any of Claims 9 to 11, characterised in that the said casting is conducted in an Ar atmosphere.
- A method as claimed in any of Claims 9 to 12, characterised in that said molten material is cast into a water cooled copper mould.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62104623A JP2725004B2 (en) | 1986-04-30 | 1987-04-30 | Manufacturing method of permanent magnet |
JP104623/87 | 1987-04-30 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0289680A2 EP0289680A2 (en) | 1988-11-09 |
EP0289680A3 EP0289680A3 (en) | 1990-06-06 |
EP0289680B1 true EP0289680B1 (en) | 1994-06-22 |
Family
ID=14385570
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP87308666A Expired - Lifetime EP0289680B1 (en) | 1987-04-30 | 1987-09-30 | Permanent magnet and method of producing the same |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0289680B1 (en) |
KR (1) | KR930002559B1 (en) |
AT (1) | ATE107795T1 (en) |
DE (1) | DE3750136T2 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6790296B2 (en) * | 2000-11-13 | 2004-09-14 | Neomax Co., Ltd. | Nanocomposite magnet and method for producing same |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3577618D1 (en) * | 1984-09-14 | 1990-06-13 | Toshiba Kawasaki Kk | PERMANENT MAGNETIC ALLOY AND METHOD FOR THEIR PRODUCTION. |
FR2586323B1 (en) * | 1985-08-13 | 1992-11-13 | Seiko Epson Corp | RARE EARTH-IRON PERMANENT MAGNET |
JPS6247455A (en) * | 1985-08-28 | 1987-03-02 | Sumitomo Special Metals Co Ltd | Permanent magnet material having high performance |
-
1987
- 1987-08-31 KR KR1019870009551A patent/KR930002559B1/en not_active IP Right Cessation
- 1987-09-30 EP EP87308666A patent/EP0289680B1/en not_active Expired - Lifetime
- 1987-09-30 DE DE3750136T patent/DE3750136T2/en not_active Expired - Lifetime
- 1987-09-30 AT AT87308666T patent/ATE107795T1/en not_active IP Right Cessation
Non-Patent Citations (1)
Title |
---|
JOURNAL DE PHYSIQUE, COLLOQUE C8, Supplément au n° 12, Tome 49, décembre 1988, pages 631-632 * |
Also Published As
Publication number | Publication date |
---|---|
EP0289680A3 (en) | 1990-06-06 |
DE3750136T2 (en) | 1994-10-06 |
KR880013195A (en) | 1988-11-30 |
ATE107795T1 (en) | 1994-07-15 |
DE3750136D1 (en) | 1994-07-28 |
KR930002559B1 (en) | 1993-04-03 |
EP0289680A2 (en) | 1988-11-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5538565A (en) | Rare earth cast alloy permanent magnets and methods of preparation | |
JPH04245403A (en) | Rare earth-fe-co-b-based anisotropic magnet | |
JP2558095B2 (en) | Rare earth ferrous iron permanent magnet manufacturing method | |
JPH06207203A (en) | Production of rare earth permanent magnet | |
CN1024968C (en) | Preparation method of rare earth-iron-boron permanent-magnetic powder | |
US5186761A (en) | Magnetic alloy and method of production | |
EP0288637B1 (en) | Permanent magnet and method of making the same | |
EP0289680B1 (en) | Permanent magnet and method of producing the same | |
US5460662A (en) | Permanent magnet and method of production | |
JP2725004B2 (en) | Manufacturing method of permanent magnet | |
JP2530185B2 (en) | Manufacturing method of permanent magnet | |
JP3178848B2 (en) | Manufacturing method of permanent magnet | |
JP2857824B2 (en) | Rare earth-iron permanent magnet manufacturing method | |
EP0599815B1 (en) | Magnetic alloy and method of making the same | |
JP4133315B2 (en) | Rare earth magnet manufacturing method, rare earth magnet raw material alloy and powder | |
JPH07123083B2 (en) | Cast rare earth-method for manufacturing iron-based permanent magnets | |
JPH0521219A (en) | Production of rare-earth permanent magnet | |
JP2730441B2 (en) | Manufacturing method of alloy powder for permanent magnet | |
JPH04143221A (en) | Production of permanent magnet | |
JP2992808B2 (en) | permanent magnet | |
JPH01175211A (en) | Manufacture of rare-earth elements-iron-based permanent magnet | |
JPH08250312A (en) | Rare earth-fe permanent magnet and manufacture thereof | |
JPH02118054A (en) | Permanent magnet material | |
JPS5848607A (en) | Production of rare earth cobalt magnet | |
JP2003243211A (en) | Method for manufacturing rare earth magnet powder superior in magnetic anisotropy |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AT CH DE FR GB IT LI NL |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): AT CH DE FR GB IT LI NL |
|
17P | Request for examination filed |
Effective date: 19901120 |
|
17Q | First examination report despatched |
Effective date: 19920311 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT CH DE FR GB IT LI NL |
|
REF | Corresponds to: |
Ref document number: 107795 Country of ref document: AT Date of ref document: 19940715 Kind code of ref document: T |
|
ITF | It: translation for a ep patent filed | ||
REF | Corresponds to: |
Ref document number: 3750136 Country of ref document: DE Date of ref document: 19940728 |
|
ET | Fr: translation filed | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: AT Payment date: 20000913 Year of fee payment: 14 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20010930 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: IF02 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES;WARNING: LAPSES OF ITALIAN PATENTS WITH EFFECTIVE DATE BEFORE 2007 MAY HAVE OCCURRED AT ANY TIME BEFORE 2007. THE CORRECT EFFECTIVE DATE MAY BE DIFFERENT FROM THE ONE RECORDED. Effective date: 20050930 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20060908 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: NL Payment date: 20060917 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20060927 Year of fee payment: 20 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20060928 Year of fee payment: 20 Ref country code: CH Payment date: 20060928 Year of fee payment: 20 |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: PE20 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20070929 |
|
NLV7 | Nl: ceased due to reaching the maximum lifetime of a patent |
Effective date: 20070930 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION Effective date: 20070930 |