EP0133758A2 - Iron-rare earth-boron permanent magnets by hot working - Google Patents
Iron-rare earth-boron permanent magnets by hot working Download PDFInfo
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- EP0133758A2 EP0133758A2 EP84304731A EP84304731A EP0133758A2 EP 0133758 A2 EP0133758 A2 EP 0133758A2 EP 84304731 A EP84304731 A EP 84304731A EP 84304731 A EP84304731 A EP 84304731A EP 0133758 A2 EP0133758 A2 EP 0133758A2
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- European Patent Office
- Prior art keywords
- permanent magnet
- iron
- hot
- boron
- neodymium
- Prior art date
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- 229910001102 IRON-RARE EARTH-BORON Inorganic materials 0.000 title 1
- 239000000463 material Substances 0.000 claims abstract description 52
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 50
- 229910052742 iron Inorganic materials 0.000 claims abstract description 23
- 229910052796 boron Inorganic materials 0.000 claims abstract description 21
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract description 19
- 229910052779 Neodymium Inorganic materials 0.000 claims abstract description 19
- QEFYFXOXNSNQGX-UHFFFAOYSA-N neodymium atom Chemical compound [Nd] QEFYFXOXNSNQGX-UHFFFAOYSA-N 0.000 claims abstract description 19
- 229910052777 Praseodymium Inorganic materials 0.000 claims abstract description 16
- PUDIUYLPXJFUGB-UHFFFAOYSA-N praseodymium atom Chemical compound [Pr] PUDIUYLPXJFUGB-UHFFFAOYSA-N 0.000 claims abstract description 16
- 239000000203 mixture Substances 0.000 claims description 41
- 230000005415 magnetization Effects 0.000 claims description 18
- 238000000034 method Methods 0.000 claims description 18
- 238000001816 cooling Methods 0.000 claims description 15
- 229910052761 rare earth metal Inorganic materials 0.000 claims description 14
- 230000008569 process Effects 0.000 claims description 5
- 229910045601 alloy Inorganic materials 0.000 claims description 4
- 239000000956 alloy Substances 0.000 claims description 4
- 238000007596 consolidation process Methods 0.000 claims description 4
- 239000011343 solid material Substances 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 3
- 239000002178 crystalline material Substances 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 claims 5
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 20
- 150000002910 rare earth metals Chemical class 0.000 description 11
- 229910052786 argon Inorganic materials 0.000 description 10
- 238000007731 hot pressing Methods 0.000 description 10
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 8
- 239000002245 particle Substances 0.000 description 8
- 229910052723 transition metal Inorganic materials 0.000 description 8
- 150000003624 transition metals Chemical class 0.000 description 8
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 6
- 238000002474 experimental method Methods 0.000 description 6
- 229910052804 chromium Inorganic materials 0.000 description 5
- 239000011651 chromium Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 238000001125 extrusion Methods 0.000 description 5
- 239000000155 melt Substances 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 229910017052 cobalt Inorganic materials 0.000 description 4
- 239000010941 cobalt Substances 0.000 description 4
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 4
- 230000005347 demagnetization Effects 0.000 description 4
- 230000006698 induction Effects 0.000 description 4
- 238000002074 melt spinning Methods 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 229910052759 nickel Inorganic materials 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 3
- QJVKUMXDEUEQLH-UHFFFAOYSA-N [B].[Fe].[Nd] Chemical class [B].[Fe].[Nd] QJVKUMXDEUEQLH-UHFFFAOYSA-N 0.000 description 3
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- 229910052748 manganese Inorganic materials 0.000 description 3
- 239000011572 manganese Substances 0.000 description 3
- 238000001000 micrograph Methods 0.000 description 3
- 239000010453 quartz Substances 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 3
- 239000007858 starting material Substances 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 238000005056 compaction Methods 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 229910002804 graphite Inorganic materials 0.000 description 2
- 239000010439 graphite Substances 0.000 description 2
- 230000005381 magnetic domain Effects 0.000 description 2
- 229910001172 neodymium magnet Inorganic materials 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 229910052684 Cerium Inorganic materials 0.000 description 1
- 229910052692 Dysprosium Inorganic materials 0.000 description 1
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- 229910052772 Samarium Inorganic materials 0.000 description 1
- 229910052771 Terbium Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229910001315 Tool steel Inorganic materials 0.000 description 1
- 238000002441 X-ray diffraction Methods 0.000 description 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 description 1
- 239000007767 bonding agent Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 description 1
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- KBQHZAAAGSGFKK-UHFFFAOYSA-N dysprosium atom Chemical compound [Dy] KBQHZAAAGSGFKK-UHFFFAOYSA-N 0.000 description 1
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- 229910052746 lanthanum Inorganic materials 0.000 description 1
- FZLIPJUXYLNCLC-UHFFFAOYSA-N lanthanum atom Chemical compound [La] FZLIPJUXYLNCLC-UHFFFAOYSA-N 0.000 description 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000012768 molten material Substances 0.000 description 1
- 238000000879 optical micrograph Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 238000001953 recrystallisation Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- KZUNJOHGWZRPMI-UHFFFAOYSA-N samarium atom Chemical compound [Sm] KZUNJOHGWZRPMI-UHFFFAOYSA-N 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- GZCRRIHWUXGPOV-UHFFFAOYSA-N terbium atom Chemical compound [Tb] GZCRRIHWUXGPOV-UHFFFAOYSA-N 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Images
Classifications
-
- 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
Definitions
- This invention relates to high temperature strain-anneal processing of extremely rapidly solidified compositions comprising iron, one or more rare earth metals and boron to produce useful permanent magnets. More particularly, this invention relates to the hot consolidation and hot working of overquenched compositions comprising iron, neodymium and/or praseodymium,and boron to form useful,magnetically- aligned permanent magnets.
- High energy product, high coercivity permanent magnet compositions comprising, for example, iron, neodymium and/or praseodymium, and boron,and methods of making them are disclosed in European Patent Application 0 108 474 (General Motors Corporation).
- An illustrative composition, expressed in atomic proportions, is Nd 0.13 (Fe 0.95 B 0.05 ) 0.87 . It is substantially the composition of a specific stable intermetallic phase that possesses high coercivity when formed as fine crystallites about 20 to 400 nanometers in largest dimension.
- melts of the above family of compositions can be very rapidly quenched, such as by melt-spinning, to produce a solid material, e.g., a thin ribbon.
- rate of cooling has been controlled to produce a suitable fine crystalline microstructure (20 nm to 400 nm)
- the material has excellent permanent magnet properties.
- faster cooling overquenching
- overquenched material can be annealed to form the suitable crystal size with the associated high coercivity and high energy product.
- this neodymium-iron-boron composition (for example) is that it is magnetically isotropic.
- a fine grain, melt spun ribbon can be broken up into flat particles. The particles can be pressed in a die at room temperature to form a unitary body of about 85% of the . material's density. Bonding agents can be employed before or after the compaction.
- the making of such bonded magnets is disclosed in European Patent Application 84301453.1 (General Motors Corporation), filed 6 March 1984: It was surprising to find that such bonded magnets displayed no preferred magnetic direction. Values of intrinsic coercivity or maximum energy product were not dependent upon the direction of the applied magnetic field. There . was no advantage in grinding the ribbon to very fine particles and magnetically aligning the particles before compaction.
- Such magnetically isotropic materials are very useful because they can be easily pressed (without magnetic alignment) into bonded shapes.
- the shapes can be magnetized in the most convenient direction.
- iron-neodymium- boron type compositions might provide still higher energy products if at least a portion of the grains or crystallites in their microstructure could be physically aligned and if such alignment produced at least partial magnetic domain alignment.
- the material would then have a preferred direction of magnetization.
- the material would be magnetically anisotropic and would have higher residual magnetization and higher energy product in the preferred direction.
- This has now been accomplished using overquenched melt-spun material by hot working the material to consolidate it to full density and to effect plastic flow that yields magnetic alignment.
- the same improvement can be accomplished on finely crystalline, high coercivity material (e.g., H ci > 1000 Oe) if the hot work is performed rapidly before excessive grain growth occurs and coercivity decreases.
- This anisotropic magnet has higher residual magnetization and energy product.than isotropic magnets of like composition.
- the treatment is by a hot working process, such as hot pressing, hot die-upsetting, extrusion, forging, or rolling, to fully consolidate pieces of the material, to effect suitable grain growth and to produce a plastic flow therein that results in a body having magnetic anisotropy. It is found that the maximum magnetic properties in such a hot worked body are oriented parallel to the direction of pressing (perpendicular to the direction of flow). In the direction of preferred magnetic alignment r: energy products are obtainable that are significantly greater than those in isotropic magnets of like composition.
- the ribbon or other thin, solid form may be broken, if necessary, into particles of convenient size for an intended hot working operation.
- the particles are heated under argon to a suitable elevated temperature, preferably 700°C or higher, and subjected to short term hot working under pressure, preferably at least 68,947.6 kPa (10,000 psi).
- Such processing nay be accomplished by any of a number of known hot working practices.
- the material may be hot pressed in a die. It may be extruded, or rolled, or die-upset, or hammered. Whatever the particular form of hot working employed, the several individual particles are pressed and flowed together until the mass achieves full density for the composition. In addition, the hot mass is caused to undergo plastic flow.
- the nonpermanent magnet microstructure is converted to a suitable fine grain crystalline material.
- the flow of the hot, fine grain material produces a body, that upon cooling below its Curie temperature, has preferred direction of magnetization and provides excellent permanent magnet properties.
- the high temperature working produces a finely crystalline or granular microstructure (for example, up to about 0.4 to 0.5 micrometers in greatest dimension). Care is taken to cool the material before excessive grain growth and loss of coercivity occurs.
- the preferred direction of magnetization of the hot worked product is typically parallel to the direction of pressing and transverse to the direction of plastic flow. A significantly higher energy product is obtained when the body is magnetized transverse to the direction of plastic flow.
- material of like composition and similar microstructure has been made without hot working. Such materials have been magnetically isotropic and had lower maximum energy product.
- the starting material may be a high coercivity (> 1000 Oe) isotropic material. Suitable hot working of the material will fully densify it and effect plastic flow to orient the fine crystallites in a magnetically anisotropic structure. However the duration of the hot working must be short so that the crystallites do not grow so large that the desirable magnetic properties are lost.
- the method of the present invention is applicable to compositions comprising a suitable transition metal component, a suitable rare earth component, and boron.
- the transition metal component is iron or iron and (one or more of) cobalt, nickel, chromium or manganese. Cobalt is interchangeable with iron up to about 40 atomic percent. Chromium, manganese and nickel are interchangeable in lower amounts, preferably less than about 10 atomic percent. Zirconium and/or titanium in small amounts (up to about 2 atomic percent of the iron) can be substituted for iron. Very small amounts of carbon and silicon can be tolerated where low carbon steel is the source of iron for the composition.
- the composition preferably comprises about 50 atomic percent to about 90 atomic percent transition metal component -- largely iron.
- the composition also comprises from about 10 atomic percent to about 50 atomic percent rare earth component.
- Neodymium and/or praseodymium are the essential rare earth constituents. As indicated,- they may be used interchangeably.
- Relatively small amounts of other rare earth elements such as samarium, lanthanum, cerium, terbium and dysprosium, may be mixed with neodymium and praseodymium without substantial loss of the desirable magnetic properties.
- they make up no more than about 40 atomic percent of the rare earth component. It is expected that there will be small amounts of impurity elements with the rare earth component.
- the overquenched composition contains about 1 to 10 atomic percent boron.
- the overall composition may be expressed by the formula RE 1-x (TM 1-y B y ) x .
- the rare earth (RE) component makes up 10 to 50 atomic percent of the composition (x - 0.5 to 0.9), with at least 60 atomic percent of the rare earth component being neodymium and/or praseodymium.
- the transition metal (TM) as used herein makes up about 50 to 90 atomic percent of the overall composition, with iron representing about 80 atomic percent of the transition metal content.
- the other constituents, such as cobalt, nickel, chromium or manganese, are called "transition metals" insofar as the above empirical formula is concerned.
- Boron is present in an amount of about 1 to 10 atomic percent (y - about 0.01 to 0.11) of the total composition.
- compositions For convenience, the compositions have been expressed in terms of atomic proportions. Obviously these specifications can be readily converted to weight proportions for preparing the composition mixtures.
- molten transition metal-rare earth-boron compositions can be solidified to have microstructures ranging from:
- Fine grain microstructures where the grains have a maximum dimension of about 20 to 400 nanometers, have useful permanent magnet properties. Amorphous materials do not. However, some of the glassy microstructure materials can be annealed to convert them to fine grain permanent magnets having isotropic magnetic properties.
- the present invention is applicable to such overquenched, glassy materials. It is also applicable to "as-quenched" high coercivity, fine grain materials provided the materials are exposed only for short times, e.g., less than five minutes, at high temperatures, over 700°C, during the hot working.
- Suitable overquenched compositions can be made by melt-spinning.
- the material is contained in a suitable vessel, such as a quartz crucible.
- the composition is melted by induction or resistance heating in the crucible under argon.
- a small, circular ejection orifice about 500 microns in diameter. Provision is made to close the top of the crucible so that the argon can be pressurized to eject the melt from the vessel in a very fine stream.
- the molten stream is directed onto a moving chill surface located about 6.35 mm (one-quarter inch) below the ejection orifice.
- the chill surface is a 25 cm diameter, 1.3 cm. thick copper wheel.
- the circumferential surface is chrome plated.
- the crucible and wheel are contained in a box that is evacuated of air and backfilled with argon. In the experiments the wheel is not cooled. Its mass is so much greater than the amount of melt impinging on it in any run that its temperature does not appreciably change. When the melt hits the turning wheel, it flattens, almost instantaneously solidifies and is thrown off as a ribbon.
- the thickness of the ribbon and the rate of cooling are largely determined by the circumferential speed of the wheel. In this work, the speed can be varied to produce an amorphous ribbon, a fine grained ribbon or a large grained ribbon.
- the cooling rate or speed of the chill wheel preferably is such that an amorphous or extremely fine crystal structure is produced.
- Such a structure will be amorphous or will have finer crystals than that which produces a permanent magnet as is, for example, less than about 20 nanometers in largest dimension.
- the distinction between an amorphous microstructure and such an extremely fine crystalline. microstructure is probably not discernible.
- an overquenched material that has-less than optimum permanent magnetic properties but that can be annealed to produce improved permanent magnet properties.
- the material is not separately annealed. It is, in effect, annealed while it is hot worked to produce a magnetic microstructure that has anistropic magnetic properties.
- An overquenched, melt spun ribbon was prepared.
- a molten mixture was prepared in accordance with the following formula: Nd 0.13 (Fe 0.95 B 0.05 ) 0.87 .
- a solidified melt spun ribbon came off the wheel. It was about 30 ⁇ m thick and about one mm wide.
- This material was cooled too rapidly to have useful permanent magnet properties. In other words, it was overquenched. Had the wheel been rotated slightly slower, the ribbon could have been produced to have a microstructure affording useful hard magnetic properties.
- the ribbon was broken into short pieces and they were placed into a cylindrical cavity 12 of a round die 10 like that depicted in Figure l.
- the cavity was 9.525 mn (3/8 inch) in diameter and the material was contained by upper and lower punches 14.
- the die was made of a high temperature nickel alloy with a tool steel liner, and the punches were tungsten carbide.
- the die and the contents were rapidly heated under argon with an induction coil 16 to a maximum temperature of 750°C.
- the temperature was measured using a thermocouple (not shown) in the die adjacent the cavity.
- the upper punch was then actuated to exert a maximum pressure of 220632.32 kPa (32,000 psi) on the broken-up ribbon particles. Heating and pressure were stopped.
- the workpiece was cooled to room temperature on the die. However, the total time that the workpiece was at a temperature above 700°C was only about five minutes.
- the consolidated workpiece was removed from the die.
- the resulting cylinder was hard and strong. It had a density of about 7.5 grams per cubic centimeter, which is substantially its full density.
- the magnetic properties of the material were determined by cutting a piece from the cylinder and grinding a small sphere, about 2 mm in diameter, from the cut off piece.
- the sphere was magnetized in a known direction by subjecting it to a pulsed magnetic field having a strength of about forty kilo gauss. -
- the sphere was then placed in a vibrating sample magnetometer with the positive magnetic pole of the sphere aligned with the positive pole of the magnetometer.
- the sample was subjected to a gradually decreasing magnetic field from +lOkOe to -20kOe that produced corresponding decreasing sample magnetization (4 ⁇ M). In this manner the second quadrant demagnetization plot (4 ⁇ M versus H) was obtained for the particular direction of magnetization.
- the sample was removed from the magnetometer and magnetized in a pulsed field as before in a different direction. It was returned to the magnetometer and a new demagnetization curve determined. This process was again repeated and the respective curves compared. The sample displayed magnetic anistropy.
- Figure 2 contains four different second quadrant plots of 4 ⁇ M versus H.
- the second quadrant portion of a hysteresis loop provides useful information regarding permanent magnet properties.
- Three of these plots in Figure 2 represent good properties.
- the upper curve 18 represents a favorable direction of magnetization obtained in the spherical sample.
- the lowest curve 20 represents the data obtained from a direction relatively far removed from the aligned direction of the hot pressed compact.
- the middle line 22 is the demagnetization plot also generated in the vibrating sample magnetometer of an isotropic array of the same ribbon from which its hot compact was made.
- plot 22 is of an isotropic magnet of the same composition as the anisotropic magnet produced in this example.
- a hysteresis curve was also prepared from a sample of the original overquenched ribbon.
- the second quadrant portion is produced as curve 24 in Figure 2. It has relatively low intrinsic coercivity and residual magnetization.
- the hot pressing operation produced a fully densified body and also produced flow in the material that oriented the microstructure so that it became magnetically anisotropic.
- the preferred direction of magnetization represented by curve 181 the residual magnetization and energy product are greater than in the isotropic material.
- hot pressed body In addition to having excellent permanent properties at room temperature the hot pressed body retains its properties during exposure at high temperatures in air.
- a hot pressed body of this example was exposed at 160°C in air to a reverse field of 4kOe for 1507 hours. It suffered only minimal loss in permanent magnet properties.
- Figure 3a is a photomicrograph of a cross-section of a bonded magnet that was compacted at room temperature to 85% of full density. The platelike sections of the original ribbon are seen to line up and be preserved in the bonded magnet.
- Figure 3b is a photomicrograph at the same magnification of a hot pressed specimen fully densified in accordance with the invention. The flat ribbon fragments are still perceptible at about the same size as in the bonded magnet, but there are no voids in this fully densified specimen.
- Example 2 Another overquenched, melt spun ribbon was prepared by the method described in Example 1.
- the nominal composition of the ribbon was in accordance with the empirical formula Nd 0.13 (Fe 0.94 B 0.06 ) 0.87 .
- the ribbons were produced by quenching the melt on a chill wheel rotating at a velocity of 32 m/s.
- the thickness of the ribbon was approximately 30 ⁇ m and the width approximately one millimeter. This cooling rate produced a microstructure that could not be magnetized to form a magnet having useful permanent magnet properties.
- Ribbon pieces were compacted at room temperature in a die to form a precompacted body of about 85% full density.
- the precompact was then placed in the cavity of a high temperature alloy die similar to that described in Example 1. However, the die had a graphite liner. Carbide punches confined the precompact in the die cavity.
- the die and its contents were quickly heated under argon to 740°C and a ram pressure of 68,947.6 k Pa (10 kpsi)was applied in an attempt to extrude the preform.
- An unexpected form of backward extrusion was obtained as the precompacted material flowed out from between the punches and displaced graphite die liner to form a cup-like piece. After cooling to room temperature this piece was removed from the die and it was found that the extruded portion of the sample was of sufficient dimensions to allow density measurement as well as magnetic measurement. The extruded portion was fully densified.
- a 2 mm cube was ground from a portion of the extruded metal and it was tested in a vibrating sample magnetometer. By magnetizing and demagnetizing the sample transverse to the cube faces it was observed that the specimen displayed magnetic anisatmpy. Three orthogonal directions are displayed in Figure 4- by curves 26, 28 and 30. The separations of these second quadrant plots from different directions of magnetization results from physical alignment of magnetic domains within the sample. The greater the separation of the plots, the greater the degree of magnetic alignment. It is seen that the alignment.for the extruded sample was even more pronounced than for the sample of Figure 1.
- the demagnetization curves for the annealed ribbon 22 and the overquenched ribbon 24 are also included in this figure as in Figure 2.
- the coercivity of the extruded sample is even higher than that of the annealed ribbons pre-. sumably because a more appropriate crystallite size was achieved during the extrusion.
- the magnetization of the extruded sample in its most preferred direction is higher and results in higher energy product than that obtainable in isotropic annealed ribbons.
- Figure 3c is a photomicrograph at 600X magnification of a cross-section of the extruded sample. It is seen that greater plastic flow occurred in the extruded sample as evidenced by the reduction in thickness of the original ribbon particles. It is believed that this plastic flow is essential to alignment of the magnetic moments within the material and that this alignment is generally transverse to the plastic flow. In other words, with respect to this sample, the magnetic alignment is transverse to the long dimension of the extruded ribbons (i.e., up and down in Figure 3c).
- Figure 5 is a scanning electron microscope micrograph at nearly 44,000X magnification of a fracture surface of the extruded sample. It shows the fine grain texture.
- Example 1 Additional hot press tests, like Example 1, and modified extrusion tests, like Example 2, were carried out at various die temperatures in the range of 700 to 770°C and pressures in the range of 68,947.6 to 206,842.8 kPa (10,000 to 30,000 psi). These tests shewed that full densification could be realized even at the lower pressures and temperatures. However, the samples prepared at the lower temperatures and pressures appeared to be more brittle. Optical micrographs revealed the ribbon pieces to have cracks similar to those present in Figure 3a. Evidently, higher pressure is required at temperatures of 750°C and lower before such cracks disappear as in Figure 3b.
- the preferred magnetization direction for the hot pressed samples is parallel to the press direction and perpendicular to the direction of plastic flow. Greater directional anisotropy develops when more plastic flow is allowed, as in the extrusion tests.
- This example illustrates a die upsetting practice.
- This cylinder was re-hot pressed in the original diameter cavity along its axis (perpendicular to the original press direction) so that it was free to deform to a shorter cylinder of 9.525 nm (3/8" ) diameter (i.e., die upsetting).
- the die upsetting operation was conducted at a naximum temperature of 770°C and a pressure of 110, 316.16 kPa (16 kpsi).
- the part was cooled in the die.
- a cubic specimen was machined from the die upset body and its magnetic properties measured parallel and transverse to the press direction in a vibrating sample magnetometer, as in the above Examples 1 and 2. Second quadrant, room temperature 4 ⁇ M versus H plots for these two directions are depicted in Figure 6.
- Example 3 illustrates a die upsetting practice similar to Example 3, except a fully dense, hot pressed sample was die-upset with pressure applied in the same direction as the original hot press pressure.
- Overquenched ribbon fragments of Example 2 were hot pressed under argon in a heated die, like that depicted in Figure 1, at a maximum temperature of 760°C and pressure of 103,421.4 kpa (15 kpsi).
- This hot pressed piece was sanded to a smaller diameter (less than about 1 cm) and die upset in the same diameter cavity in a direction parallel to the first press direction.
- the die upset operation was conducted at a maximum temperature of 750°C and a pressure of 82,737.1 kPa (12 kpsi). The sample was cooled in the die.
- This practice of high'temperature consolidation and plastic flow can be viewed as a strain-anneal process.
- This process produces magnetic alignment of the grains of the workpiece and grain growth.
- the grain growth is excessive, coercivity is decreased. Therefore, consideration (and probably trial and error testing) must be given to the grain size of the starting material in conjunction with the time that the material is at a temperature at which grain growth can occur. If, as is preferred, the starting material is overquenched, the workpiece can be held at a relatively high temperature for a longer time because some grain growth is desired. If one starts with near optimal grain size material, the hot working must be rapid and subsequent cooling prompt to retard excessive grain growth.
- Hot pressing experiments were also conducted on annealed ingot that had a homogenized, large grain microstructure. When magnetized, such ingots contained very low coercivity, less than 500 oersted.
- the present hot pressing strain-anneal practice produced a significant directional dependence of B in the ingot samples, but no coercivity increase. It had been hoped that the strain-anneal practice would induce recrystallization in the ingot which would allow for development of the optimal grain size. The failure to obtain a coercivity increase in these experiments indicates that the strain-anneal practice is not beneficially applicable to large grained materials.
- this high temperature-high pressure consolidation and hot working of suitable, transition metal, rare earth metal, boron compositions yields magnetically anisotropic product of excellent permanent magnet properties.
- the practice of the present invention has been described, using specific composition]of neodymium, ircn and boron.
- other materials may be substituted or present in suitably small amounts.
- Praseodymium may be substituted for neodymium or used in combination with it.
- Other rare earth metals may be used with neodymium and/or praseodymium.
- other metals, such as cobalt, nickel, manganese and chromium, in suitably small amounts may be used in combination with iron.
- the preferred compositional ranges are described above.
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Abstract
Description
- This invention relates to high temperature strain-anneal processing of extremely rapidly solidified compositions comprising iron, one or more rare earth metals and boron to produce useful permanent magnets. More particularly, this invention relates to the hot consolidation and hot working of overquenched compositions comprising iron, neodymium and/or praseodymium,and boron to form useful,magnetically- aligned permanent magnets.
- High energy product, high coercivity permanent magnet compositions comprising, for example, iron, neodymium and/or praseodymium, and boron,and methods of making them are disclosed in
European Patent Application 0 108 474 (General Motors Corporation). An illustrative composition, expressed in atomic proportions, is Nd0.13(Fe0.95B0.05)0.87. It is substantially the composition of a specific stable intermetallic phase that possesses high coercivity when formed as fine crystallites about 20 to 400 nanometers in largest dimension. - Melts of the above family of compositions can be very rapidly quenched, such as by melt-spinning, to produce a solid material, e.g., a thin ribbon. When the rate of cooling has been controlled to produce a suitable fine crystalline microstructure (20 nm to 400 nm), the material has excellent permanent magnet properties. On the other hand,faster cooling (overquenching) produces a material with smaller crystallites and lower coercivity. However, as disclosed, such overquenched material can be annealed to form the suitable crystal size with the associated high coercivity and high energy product.
- An interesting and useful property of this neodymium-iron-boron composition (for example) is that it is magnetically isotropic. A fine grain, melt spun ribbon can be broken up into flat particles. The particles can be pressed in a die at room temperature to form a unitary body of about 85% of the . material's density. Bonding agents can be employed before or after the compaction. The making of such bonded magnets is disclosed in European Patent Application 84301453.1 (General Motors Corporation), filed 6 March 1984: It was surprising to find that such bonded magnets displayed no preferred magnetic direction. Values of intrinsic coercivity or maximum energy product were not dependent upon the direction of the applied magnetic field. There . was no advantage in grinding the ribbon to very fine particles and magnetically aligning the particles before compaction.
- Such magnetically isotropic materials are very useful because they can be easily pressed (without magnetic alignment) into bonded shapes. The shapes can be magnetized in the most convenient direction.
- It is recognized that the iron-neodymium- boron type compositions might provide still higher energy products if at least a portion of the grains or crystallites in their microstructure could be physically aligned and if such alignment produced at least partial magnetic domain alignment. The material would then have a preferred direction of magnetization. The material would be magnetically anisotropic and would have higher residual magnetization and higher energy product in the preferred direction. This has now been accomplished using overquenched melt-spun material by hot working the material to consolidate it to full density and to effect plastic flow that yields magnetic alignment. The same improvement can be accomplished on finely crystalline, high coercivity material (e.g., Hci > 1000 Oe) if the hot work is performed rapidly before excessive grain growth occurs and coercivity decreases.
- It is an object of the invention to provide a fully densified fine grain, anisotropic, permanent magnet formed by hot working a suitable material comprising iron, neodymium and/or praseodymium, and boron. This anisotropic magnet has higher residual magnetization and energy product.than isotropic magnets of like composition.
- It is an object of the invention to provide a method of treating overquenched compositions containing suitable proportions of iron, neodymium and/or praseodymium, and boron at suitable temperatures and pressures to fully density the material into a solid mass, to effect the growth of fine, high coercivity crystallites and to cause a flow and orientation of the material sufficient to produce macroscopic magnetic anisotropy.
- It is another object of the invention to treat suitable transition metal-rare earth metal-boron compositions that do not have permanent magnet properties because their microstructure is amorphous or too finely crystalline. The treatment is by a hot working process, such as hot pressing, hot die-upsetting, extrusion, forging, or rolling, to fully consolidate pieces of the material, to effect suitable grain growth and to produce a plastic flow therein that results in a body having magnetic anisotropy. It is found that the maximum magnetic properties in such a hot worked body are oriented parallel to the direction of pressing (perpendicular to the direction of flow). In the direction of preferred magnetic alignmentr:energy products are obtainable that are significantly greater than those in isotropic magnets of like composition.
- In accordance with a preferred embodiment of the invention, these and other objects and advantages are accomplished as follows:
- A molten composition comprising iron, neodymium and/or praseodymium, and boron is prepared. Other constituents may be present, as will be disclosed below. An example of a preferred composition, expressed in terms of atomic proportions, is Nd0.13(Fe0.95B0.05)0.87. The molten material is cooled extremely rapidly, as by melt spinning, to form a thin ribbon of solid material that does not have permanent magnet properties. Typically, the material is amorphous in microstructure. It will not produce an x-ray pattern containing many discrete diffraction maxima like that obtained from diffraction in crystalline substances. When highly magnified, as in a scanning electron microscope micrograph, no discrete grains (or crystallites) will be apparent.
- The ribbon or other thin, solid form may be broken, if necessary, into particles of convenient size for an intended hot working operation. The particles are heated under argon to a suitable elevated temperature, preferably 700°C or higher, and subjected to short term hot working under pressure, preferably at least 68,947.6 kPa (10,000 psi). Such processing nay be accomplished by any of a number of known hot working practices. The material may be hot pressed in a die. It may be extruded, or rolled, or die-upset, or hammered. Whatever the particular form of hot working employed, the several individual particles are pressed and flowed together until the mass achieves full density for the composition. In addition, the hot mass is caused to undergo plastic flow. During the exposure at high.temperature the nonpermanent magnet microstructure is converted to a suitable fine grain crystalline material. The flow of the hot, fine grain material produces a body, that upon cooling below its Curie temperature, has preferred direction of magnetization and provides excellent permanent magnet properties.
- As suitably practiced, the high temperature working produces a finely crystalline or granular microstructure (for example, up to about 0.4 to 0.5 micrometers in greatest dimension). Care is taken to cool the material before excessive grain growth and loss of coercivity occurs. The preferred direction of magnetization of the hot worked product is typically parallel to the direction of pressing and transverse to the direction of plastic flow. A significantly higher energy product is obtained when the body is magnetized transverse to the direction of plastic flow.
- As previously stated, material of like composition and similar microstructure has been made without hot working. Such materials have been magnetically isotropic and had lower maximum energy product.
- In another embodiment of the invention the starting material may be a high coercivity (> 1000 Oe) isotropic material. Suitable hot working of the material will fully densify it and effect plastic flow to orient the fine crystallites in a magnetically anisotropic structure. However the duration of the hot working must be short so that the crystallites do not grow so large that the desirable magnetic properties are lost.
- These and other objects and advantages of the invention will become more apparent from a detailed description thereof, which follows. Reference will be made to the drawings, in which:
- Figure 1 is a cross-sectional view of a hot pressing die for practicing one embodiment of the invention;
- Figure 2 is a second quadrant, room temperature, 4wM versus H plot of a sample produced by hot pressing;
- Figure 3a is a photomicrograph at 6QOX magnification of a sample compacted to 85% of theoretical density in accordance with earlier work;
- Figure 3b is a photomicrograph at 600X magnification of a sample hot pressed in accordance with the method of the invention;
- Figure 3c is a photomicrograph at 600X magnification of a sample extruded in accordance with the method of the invention;
- Figure 4 is a second quadrant, room temperature, 4wM versus H plot of a sample produced by extrusion;
- Figure 5 is a Scanning Electron Microscope micrograph at 43,600X magnification, illustrating the texture of the fracture surface of an extruded smple prepared in accordance with the method of the invention;
- Figure 6 is a second quadrant, room temperature, 4πM versus H plot of a sanple produced by die upsetting in accordance with the method of the invention and
- Figure 7 is a second quadrant, room temperature, 4πM versus H plot of a sample produced by a different die upsetting practice in accordance with the method of the invention.
- The method of the present invention is applicable to compositions comprising a suitable transition metal component, a suitable rare earth component, and boron.
- The transition metal component is iron or iron and (one or more of) cobalt, nickel, chromium or manganese. Cobalt is interchangeable with iron up to about 40 atomic percent. Chromium, manganese and nickel are interchangeable in lower amounts, preferably less than about 10 atomic percent. Zirconium and/or titanium in small amounts (up to about 2 atomic percent of the iron) can be substituted for iron. Very small amounts of carbon and silicon can be tolerated where low carbon steel is the source of iron for the composition. The composition preferably comprises about 50 atomic percent to about 90 atomic percent transition metal component -- largely iron.
- The composition also comprises from about 10 atomic percent to about 50 atomic percent rare earth component. Neodymium and/or praseodymium are the essential rare earth constituents. As indicated,- they may be used interchangeably. Relatively small amounts of other rare earth elements, such as samarium, lanthanum, cerium, terbium and dysprosium, may be mixed with neodymium and praseodymium without substantial loss of the desirable magnetic properties. Preferably, they make up no more than about 40 atomic percent of the rare earth component. It is expected that there will be small amounts of impurity elements with the rare earth component.
- The overquenched composition contains about 1 to 10 atomic percent boron.
- The overall composition may be expressed by the formula RE1-x(TM1-yBy)x. The rare earth (RE) component makes up 10 to 50 atomic percent of the composition (x - 0.5 to 0.9), with at least 60 atomic percent of the rare earth component being neodymium and/or praseodymium. The transition metal (TM) as used herein makes up about 50 to 90 atomic percent of the overall composition, with iron representing about 80 atomic percent of the transition metal content. The other constituents, such as cobalt, nickel, chromium or manganese, are called "transition metals" insofar as the above empirical formula is concerned.
- Boron is present in an amount of about 1 to 10 atomic percent (y - about 0.01 to 0.11) of the total composition.
- For convenience, the compositions have been expressed in terms of atomic proportions. Obviously these specifications can be readily converted to weight proportions for preparing the composition mixtures.
-
- However, it is to be understood that the method of the invention is applicable to a family of compositions as described above.
- Depending on the rate of cooling, molten transition metal-rare earth-boron compositions can be solidified to have microstructures ranging from:
- (a) amorphous (glassy) and extremely fine grained microstructures (e.g., less than 20 nanometers in largest dimension) through
- (b) very fine (micro) grained microstructures (e.g, 20 nm to about 400 nm) to
- (c) larger grained microstructures.
- Thus far, large grained microstructure materials have not been produced with useful permanent magnet properties. Fine grain microstructures, where the grains have a maximum dimension of about 20 to 400 nanometers, have useful permanent magnet properties. Amorphous materials do not. However, some of the glassy microstructure materials can be annealed to convert them to fine grain permanent magnets having isotropic magnetic properties. The present invention is applicable to such overquenched, glassy materials. It is also applicable to "as-quenched" high coercivity, fine grain materials provided the materials are exposed only for short times, e.g., less than five minutes, at high temperatures, over 700°C, during the hot working.
- Suitable overquenched compositions can be made by melt-spinning. In melt-spinning experiments the material is contained in a suitable vessel, such as a quartz crucible. The composition is melted by induction or resistance heating in the crucible under argon. At the bottom of the crucible is provided a small, circular ejection orifice about 500 microns in diameter. Provision is made to close the top of the crucible so that the argon can be pressurized to eject the melt from the vessel in a very fine stream.
- The molten stream is directed onto a moving chill surface located about 6.35 mm (one-quarter inch) below the ejection orifice. In examples described herein the chill surface is a 25 cm diameter, 1.3 cm. thick copper wheel. The circumferential surface is chrome plated. The crucible and wheel are contained in a box that is evacuated of air and backfilled with argon. In the experiments the wheel is not cooled. Its mass is so much greater than the amount of melt impinging on it in any run that its temperature does not appreciably change. When the melt hits the turning wheel, it flattens, almost instantaneously solidifies and is thrown off as a ribbon. The thickness of the ribbon and the rate of cooling are largely determined by the circumferential speed of the wheel. In this work, the speed can be varied to produce an amorphous ribbon, a fine grained ribbon or a large grained ribbon.
- In the practice of the method of the present invention, the cooling rate or speed of the chill wheel preferably is such that an amorphous or extremely fine crystal structure is produced. Such a structure will be amorphous or will have finer crystals than that which produces a permanent magnet as is, for example, less than about 20 nanometers in largest dimension. As a practical matter, the distinction between an amorphous microstructure and such an extremely fine crystalline. microstructure is probably not discernible. What is desired is an overquenched material that has-less than optimum permanent magnetic properties but that can be annealed to produce improved permanent magnet properties. However, in accordance with the method of the invention, the material is not separately annealed. It is, in effect, annealed while it is hot worked to produce a magnetic microstructure that has anistropic magnetic properties.
- A few examples will further illustrate the practice of the present invention.
- An overquenched, melt spun ribbon was prepared. A molten mixture was prepared in accordance with the following formula: Nd0.13(Fe0.95B0.05)0.87.
- About 40 grams of the mixture was melted in a quartz tube that was about 10 cm long and 2.54 cm in diameter. The quartz tube had an ejection orifice in the bottom, which was round and about 600 µm in diameter. The top of the tube was sealed and adapted to supply pressurized argon gas to the tube above the molten alloy. The alloy was actually melted in the tube using induction heating. When the melt was at 1400°C, an argon ejection pressure of about 20.68 kPa (3 psig)was applied.
- An extremely fine stream of the molten metal was ejected down onto the rim of the above described wheel. The wheel was made of copper and the perimeter surface was plated with chromium. The wheel was initially at room temperature and was neither heated nor cooled during the experiment, except from contact with the molten metal ejected onto it. The wheel was rotated at a rim velocity of about 35 meters per second (m/s).
- A solidified melt spun ribbon came off the wheel. It was about 30 µm thick and about one mm wide.
- This material was cooled too rapidly to have useful permanent magnet properties. In other words, it was overquenched. Had the wheel been rotated slightly slower, the ribbon could have been produced to have a microstructure affording useful hard magnetic properties.
- The ribbon was broken into short pieces and they were placed into a
cylindrical cavity 12 of around die 10 like that depicted in Figure l. The cavity was 9.525 mn (3/8 inch) in diameter and the material was contained by upper andlower punches 14. The die was made of a high temperature nickel alloy with a tool steel liner, and the punches were tungsten carbide. - The die and the contents were rapidly heated under argon with an
induction coil 16 to a maximum temperature of 750°C. The temperature was measured using a thermocouple (not shown) in the die adjacent the cavity. The upper punch was then actuated to exert a maximum pressure of 220632.32 kPa (32,000 psi) on the broken-up ribbon particles. Heating and pressure were stopped. The workpiece was cooled to room temperature on the die. However, the total time that the workpiece was at a temperature above 700°C was only about five minutes. The consolidated workpiece was removed from the die. The resulting cylinder was hard and strong. It had a density of about 7.5 grams per cubic centimeter, which is substantially its full density. - The magnetic properties of the material were determined by cutting a piece from the cylinder and grinding a small sphere, about 2 mm in diameter, from the cut off piece. The sphere was magnetized in a known direction by subjecting it to a pulsed magnetic field having a strength of about forty kilo gauss. - The sphere was then placed in a vibrating sample magnetometer with the positive magnetic pole of the sphere aligned with the positive pole of the magnetometer. The sample was subjected to a gradually decreasing magnetic field from +lOkOe to -20kOe that produced corresponding decreasing sample magnetization (4πM). In this manner the second quadrant demagnetization plot (4πM versus H) was obtained for the particular direction of magnetization.
- The sample was removed from the magnetometer and magnetized in a pulsed field as before in a different direction. It was returned to the magnetometer and a new demagnetization curve determined. This process was again repeated and the respective curves compared. The sample displayed magnetic anistropy.
- Figure 2 contains four different second quadrant plots of 4πM versus H. The second quadrant portion of a hysteresis loop provides useful information regarding permanent magnet properties. Three of these plots in Figure 2 represent good properties. The residual magnetization at zero field (H=0) is high and the intrinsic coercivity, i.e., the reverse field to demagnetize the sample (4πM = 0) is high. The
upper curve 18 represents a favorable direction of magnetization obtained in the spherical sample. Thelowest curve 20 represents the data obtained from a direction relatively far removed from the aligned direction of the hot pressed compact. Themiddle line 22 is the demagnetization plot also generated in the vibrating sample magnetometer of an isotropic array of the same ribbon from which its hot compact was made. These ribbon samples were heated (annealed) at a rate of 160°C per minute to a temperature of 727°C, and then cooled at the same rate to room temperature. The data obtained was normalized to a sample density of 100%. Thusplot 22 is of an isotropic magnet of the same composition as the anisotropic magnet produced in this example. - A hysteresis curve was also prepared from a sample of the original overquenched ribbon. The second quadrant portion is produced as
curve 24 in Figure 2. It has relatively low intrinsic coercivity and residual magnetization. - Thus, the hot pressing operation produced a fully densified body and also produced flow in the material that oriented the microstructure so that it became magnetically anisotropic. In the preferred direction of magnetization (represented by curve 181 the residual magnetization and energy product are greater than in the isotropic material.
- In addition to having excellent permanent properties at room temperature the hot pressed body retains its properties during exposure at high temperatures in air. A hot pressed body of this example was exposed at 160°C in air to a reverse field of 4kOe for 1507 hours. It suffered only minimal loss in permanent magnet properties.
- Figure 3a is a photomicrograph of a cross-section of a bonded magnet that was compacted at room temperature to 85% of full density. The platelike sections of the original ribbon are seen to line up and be preserved in the bonded magnet. Figure 3b is a photomicrograph at the same magnification of a hot pressed specimen fully densified in accordance with the invention. The flat ribbon fragments are still perceptible at about the same size as in the bonded magnet, but there are no voids in this fully densified specimen.
- Another overquenched, melt spun ribbon was prepared by the method described in Example 1. The nominal composition of the ribbon was in accordance with the empirical formula Nd0.13(Fe0.94B0.06)0.87. The ribbons were produced by quenching the melt on a chill wheel rotating at a velocity of 32 m/s. The thickness of the ribbon was approximately 30µm and the width approximately one millimeter. This cooling rate produced a microstructure that could not be magnetized to form a magnet having useful permanent magnet properties.
- Ribbon pieces were compacted at room temperature in a die to form a precompacted body of about 85% full density. The precompact was then placed in the cavity of a high temperature alloy die similar to that described in Example 1. However, the die had a graphite liner. Carbide punches confined the precompact in the die cavity. The die and its contents were quickly heated under argon to 740°C and a ram pressure of 68,947.6 kPa (10 kpsi)was applied in an attempt to extrude the preform. An unexpected form of backward extrusion was obtained as the precompacted material flowed out from between the punches and displaced graphite die liner to form a cup-like piece. After cooling to room temperature this piece was removed from the die and it was found that the extruded portion of the sample was of sufficient dimensions to allow density measurement as well as magnetic measurement. The extruded portion was fully densified.
- A 2 mm cube was ground from a portion of the extruded metal and it was tested in a vibrating sample magnetometer. By magnetizing and demagnetizing the sample transverse to the cube faces it was observed that the specimen displayed magnetic anisatmpy. Three orthogonal directions are displayed in Figure 4- by
curves ribbon 22 and theoverquenched ribbon 24 are also included in this figure as in Figure 2. It is seen that the coercivity of the extruded sample is even higher than that of the annealed ribbons pre-. sumably because a more appropriate crystallite size was achieved during the extrusion. The magnetization of the extruded sample in its most preferred direction is higher and results in higher energy product than that obtainable in isotropic annealed ribbons. - Figure 3c is a photomicrograph at 600X magnification of a cross-section of the extruded sample. It is seen that greater plastic flow occurred in the extruded sample as evidenced by the reduction in thickness of the original ribbon particles. It is believed that this plastic flow is essential to alignment of the magnetic moments within the material and that this alignment is generally transverse to the plastic flow. In other words, with respect to this sample, the magnetic alignment is transverse to the long dimension of the extruded ribbons (i.e., up and down in Figure 3c).
- Figure 5 is a scanning electron microscope micrograph at nearly 44,000X magnification of a fracture surface of the extruded sample. It shows the fine grain texture.
- Additional hot press tests, like Example 1, and modified extrusion tests, like Example 2, were carried out at various die temperatures in the range of 700 to 770°C and pressures in the range of 68,947.6 to 206,842.8 kPa (10,000 to 30,000 psi). These tests shewed that full densification could be realized even at the lower pressures and temperatures. However, the samples prepared at the lower temperatures and pressures appeared to be more brittle. Optical micrographs revealed the ribbon pieces to have cracks similar to those present in Figure 3a. Evidently, higher pressure is required at temperatures of 750°C and lower before such cracks disappear as in Figure 3b. The preferred magnetization direction for the hot pressed samples is parallel to the press direction and perpendicular to the direction of plastic flow. Greater directional anisotropy develops when more plastic flow is allowed, as in the extrusion tests.
- This example illustrates a die upsetting practice.
- Overquenched ribbon fragments of Example 2 were hot pressed under argon in a heated die, like that in Figure 1, at a maximum die temperature of 770°C and pressure of 103,421.4 kPa (15 kpsi). A 9.525 mm (3/8") cylindrical body, 100% density, was formed. This hot pressed cylinder was sanded to a snaller cylinder (diameter less than 1 cm) with its cylindrical axis transverse to the axis of the original cylinder. This cylinder was re-hot pressed in the original diameter cavity along its axis (perpendicular to the original press direction) so that it was free to deform to a shorter cylinder of 9.525 nm (3/8" ) diameter (i.e., die upsetting). The die upsetting operation was conducted at a naximum temperature of 770°C and a pressure of 110, 316.16 kPa (16 kpsi). As in previous examples the part was cooled in the die. A cubic specimen was machined from the die upset body and its magnetic properties measured parallel and transverse to the press direction in a vibrating sample magnetometer, as in the above Examples 1 and 2. Second quadrant, room temperature 4πM versus H plots for these two directions are depicted in Figure 6.
Curve 32 was obtained in the direction parallel to the die upset press direction andcurve 34 in the direction transverse thereto and thus parallel to the direction of material flow. It is seen that this die upset practice produced greater anisotropy than the single hot pressing operation or the extrusion test. This translates to a Br of 9.2 kG and an energy produced of 18 MGOe compared with isotropic ribbon values of Br = 8kG and energy product of about 12 MGOe. - This example illustrates a die upsetting practice similar to Example 3, except a fully dense, hot pressed sample was die-upset with pressure applied in the same direction as the original hot press pressure.
- Overquenched ribbon fragments of Example 2 were hot pressed under argon in a heated die, like that depicted in Figure 1, at a maximum temperature of 760°C and pressure of 103,421.4 kpa (15 kpsi). A 9.525 mm (3/8 indl) cylindrical body, 100% density, was formed. This hot pressed piece was sanded to a smaller diameter (less than about 1 cm) and die upset in the same diameter cavity in a direction parallel to the first press direction. The die upset operation was conducted at a maximum temperature of 750°C and a pressure of 82,737.1 kPa (12 kpsi). The sample was cooled in the die.
- A cubic specimen was machined from the die upset body and its magnetic properties measured in a vibrating sample magnetometer parallel and transverse to the die upset press direction as in the above example. Second quadrant, room temperature, 4πM versus H plots for these two directions are depicted in Figure 7.
Curve 36 was obtained in the direction parallel to the die upset press directions andcurve 38 in the direction transverse thereto. It is seen that this practice of hot pressing followed by die upsetting in the same direction produced greater anisotropy than was obtained in any of the previous samples. It is seen in Figure 7 that in the preferred direction of magnetization (curve 361 the remnant magnetization was greater than 11 kG, while the intrinsic coercivity was still greater than 7 kOe. The maximum energy product of this sample was 27 MGOe. - It is believed that still greater alignment can be obtained by a practice that provides greater plastic flow.at elevated temperature. One may define an alignment factor by (Br)parallel/(Br)perpendicular, where B is residual induction (at H = 0) measured parallel to and perpendicular to, respectively, the press direction. An alignment factor of 2.46 was obtained in Example 4. An alignment factor of 1.32 has been achieved by die upsetting (like in Example 3). An alignment factor of 1.18 has been achieved for extrusion (like in Example 2).
- This practice of high'temperature consolidation and plastic flow can be viewed as a strain-anneal process. This process produces magnetic alignment of the grains of the workpiece and grain growth. However, if the grain growth is excessive, coercivity is decreased. Therefore, consideration (and probably trial and error testing) must be given to the grain size of the starting material in conjunction with the time that the material is at a temperature at which grain growth can occur. If, as is preferred, the starting material is overquenched, the workpiece can be held at a relatively high temperature for a longer time because some grain growth is desired. If one starts with near optimal grain size material, the hot working must be rapid and subsequent cooling prompt to retard excessive grain growth. For example, hot pressing experiments have been carried out on neodymium-iron-boron melt-spun compositions that have been optimally quenched to produce optimal grain size for achieving the highest magnetic product. During such hot pressing the material was over 700°C for more than five minutes. The material was held too long at such temperature because the coercivity was always reduced although not completely eliminated. Therefore, optimal benefits were not obtained.
- Hot pressing experiments were also conducted on annealed ingot that had a homogenized, large grain microstructure. When magnetized, such ingots contained very low coercivity, less than 500 oersted. The present hot pressing strain-anneal practice produced a significant directional dependence of B in the ingot samples, but no coercivity increase. It had been hoped that the strain-anneal practice would induce recrystallization in the ingot which would allow for development of the optimal grain size. The failure to obtain a coercivity increase in these experiments indicates that the strain-anneal practice is not beneficially applicable to large grained materials.
- Thus, this high temperature-high pressure consolidation and hot working of suitable, transition metal, rare earth metal, boron compositions yields magnetically anisotropic product of excellent permanent magnet properties. For purposes of illustration, the practice of the present invention has been described, using specific composition]of neodymium, ircn and boron. However, other materials may be substituted or present in suitably small amounts. Praseodymium may be substituted for neodymium or used in combination with it. Other rare earth metals may be used with neodymium and/or praseodymium. Likewise, other metals, such as cobalt, nickel, manganese and chromium, in suitably small amounts, may be used in combination with iron. The preferred compositional ranges are described above.
- While the invention has been described in terms of preferred embodiments thereof, it will be appreciated that other embodiments could readily be , adapted by those skilled in the art. Accordingly, the scope of the invention is to be considered limited only by the following claims.
Claims (8)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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US52017083A | 1983-08-04 | 1983-08-04 | |
US520170 | 1983-08-04 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0133758A2 true EP0133758A2 (en) | 1985-03-06 |
EP0133758A3 EP0133758A3 (en) | 1987-05-20 |
EP0133758B1 EP0133758B1 (en) | 1990-09-19 |
Family
ID=24071457
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP84304731A Expired - Lifetime EP0133758B1 (en) | 1983-08-04 | 1984-07-11 | Iron-rare earth-boron permanent magnets by hot working |
Country Status (8)
Country | Link |
---|---|
EP (1) | EP0133758B1 (en) |
JP (1) | JPS60100402A (en) |
AU (1) | AU574697B2 (en) |
BR (1) | BR8403875A (en) |
CA (1) | CA1236381A (en) |
DE (1) | DE3483226D1 (en) |
ES (1) | ES8507289A1 (en) |
MX (1) | MX167658B (en) |
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- 1984-07-11 EP EP84304731A patent/EP0133758B1/en not_active Expired - Lifetime
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DE3514516A1 (en) * | 1984-04-24 | 1985-10-24 | Nippon Gakki Seizo K.K., Hamamatsu, Shizuoka | Rare-earth magnet, and method for producing it |
US5100741A (en) * | 1984-09-12 | 1992-03-31 | Seiko Epson Corporation | Magneto-optic recording systems |
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EP0231620A3 (en) * | 1986-01-29 | 1988-01-27 | General Motors Corporation | Permanent magnet manufacture from very low coercivity crystalline rare earth-transition metal-boron alloy |
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US4952239A (en) * | 1986-03-20 | 1990-08-28 | Hitachi Metals, Ltd. | Magnetically anisotropic bond magnet, magnetic powder for the magnet and manufacturing method of the powder |
US4921553A (en) * | 1986-03-20 | 1990-05-01 | Hitachi Metals, Ltd. | Magnetically anisotropic bond magnet, magnetic powder for the magnet and manufacturing method of the powder |
US5085715A (en) * | 1986-03-20 | 1992-02-04 | Hitachi Metals, Ltd. | Magnetically anisotropic bond magnet, magnetic powder for the magnet and manufacturing method of the powder |
EP0239031A1 (en) * | 1986-03-20 | 1987-09-30 | Hitachi Metals, Ltd. | Method of manufacturing magnetic powder for a magnetically anisotropic bond magnet |
WO1987007425A1 (en) * | 1986-05-23 | 1987-12-03 | Centre National De La Recherche Scientifique (Cnrs | Method for the preparation of permanent magnets by division of crystals |
US5055142A (en) * | 1986-05-23 | 1991-10-08 | Centre National De La Recherche Scientifique | Process for preparing permanent magnets by division of crystals |
FR2598949A1 (en) * | 1986-05-23 | 1987-11-27 | Centre Nat Rech Scient | PROCESS FOR THE PREPARATION OF FINALLY DIVIDED CRYSTALS FROM A METAL ALLOY, IN PARTICULAR FOR THE PREPARATION OF PERMANENT MAGNETS |
NL8701452A (en) * | 1986-06-20 | 1988-01-18 | Seiko Epson Corp | PERMANENT MAGNETS IN THE RARE NATURAL IRON SERIES. |
EP0253521A3 (en) * | 1986-07-15 | 1990-02-07 | General Motors Corporation | High energy ball-milling method for making rare earth-transition metal-boron permanent magnets |
EP0253521A2 (en) * | 1986-07-15 | 1988-01-20 | General Motors Corporation | High energy ball-milling method for making rare earth-transition metal-boron permanent magnets |
US4881984A (en) * | 1986-07-28 | 1989-11-21 | Crucible Materials Corporation | Consolidation of magnet alloy powders by extrusion and product therefrom |
EP0261292A3 (en) * | 1986-07-28 | 1988-07-27 | Crucible Materials Corporation | Method of producing fully dense permanent magnet alloy article and article produced thereby |
EP0261292A2 (en) * | 1986-07-28 | 1988-03-30 | Crucible Materials Corporation | Method of producing fully dense permanent magnet alloy article |
EP0274034A3 (en) * | 1987-01-06 | 1989-03-08 | Hitachi Metals, Ltd. | Anisotropic magnetic powder, magnet thereof and method of producing same |
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US5460662A (en) * | 1987-04-30 | 1995-10-24 | Seiko Epson Corporation | Permanent magnet and method of production |
US5076861A (en) * | 1987-04-30 | 1991-12-31 | Seiko Epson Corporation | Permanent magnet and method of production |
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US4842656A (en) * | 1987-06-12 | 1989-06-27 | General Motors Corporation | Anisotropic neodymium-iron-boron powder with high coercivity |
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US4985086A (en) * | 1987-09-10 | 1991-01-15 | Hitachi Metals, Ltd. | Method and apparatus for producing magnetically anisotropic Nd-Fe-B magnet material |
EP0306599A2 (en) * | 1987-09-10 | 1989-03-15 | Hitachi Metals, Ltd. | Method and apparatus for producing magnetically anisotropic Nd-Fe-B magnet material |
EP0306599A3 (en) * | 1987-09-10 | 1990-07-25 | Hitachi Metals, Ltd. | Method and apparatus for producing magnetically anisotropic nd-fe-b magnet material |
EP0306981A1 (en) * | 1987-09-11 | 1989-03-15 | Hitachi Metals, Ltd. | Permanent magnet for accelerating corpuscular beam |
US5292380A (en) * | 1987-09-11 | 1994-03-08 | Hitachi Metals, Ltd. | Permanent magnet for accelerating corpuscular beam |
DE3839545A1 (en) * | 1987-11-27 | 1989-06-08 | Hitachi Metals Ltd | METHOD AND DEVICE FOR PRODUCING A MAGNETICALLY ANISOTROPIC MATERIAL |
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US4892596A (en) * | 1988-02-23 | 1990-01-09 | Eastman Kodak Company | Method of making fully dense anisotropic high energy magnets |
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US4985085A (en) * | 1988-02-23 | 1991-01-15 | Eastman Kodak Company | Method of making anisotropic magnets |
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EP0334478A3 (en) * | 1988-03-24 | 1990-12-19 | General Motors Corporation | Die-upset manufacture to produce high volume fractions of re-fe-b type magnetically-aligned material |
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CN103403815B (en) * | 2011-02-23 | 2016-10-12 | 丰田自动车株式会社 | The method manufacturing rare-earth magnet |
CN105312575A (en) * | 2014-07-25 | 2016-02-10 | 丰田自动车株式会社 | Method of manufacturing rare earth magnet |
US10460871B2 (en) | 2015-10-30 | 2019-10-29 | GM Global Technology Operations LLC | Method for fabricating non-planar magnet |
Also Published As
Publication number | Publication date |
---|---|
JPH0420242B2 (en) | 1992-04-02 |
BR8403875A (en) | 1985-07-09 |
JPS60100402A (en) | 1985-06-04 |
ES534879A0 (en) | 1985-08-16 |
DE3483226D1 (en) | 1990-10-25 |
MX167658B (en) | 1993-04-01 |
EP0133758A3 (en) | 1987-05-20 |
ES8507289A1 (en) | 1985-08-16 |
AU574697B2 (en) | 1988-07-14 |
EP0133758B1 (en) | 1990-09-19 |
CA1236381A (en) | 1988-05-10 |
AU3096284A (en) | 1985-02-07 |
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