US20060174726A1 - Method for producing magnetostrictive element - Google Patents
Method for producing magnetostrictive element Download PDFInfo
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- US20060174726A1 US20060174726A1 US11/349,788 US34978806A US2006174726A1 US 20060174726 A1 US20060174726 A1 US 20060174726A1 US 34978806 A US34978806 A US 34978806A US 2006174726 A1 US2006174726 A1 US 2006174726A1
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F41/00—Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties
- H01F41/02—Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties for manufacturing cores, coils, or magnets
- H01F41/0253—Apparatus or processes specially adapted for manufacturing or assembling magnets, inductances or transformers; Apparatus or processes specially adapted for manufacturing materials characterised by their magnetic properties for manufacturing cores, coils, or magnets for manufacturing permanent magnets
- H01F41/0273—Imparting anisotropy
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- 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
- C22C1/047—Making non-ferrous alloys by powder metallurgy comprising intermetallic compounds
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- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N35/00—Magnetostrictive devices
- H10N35/80—Constructional details
- H10N35/85—Magnetostrictive active materials
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- 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
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- 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
- B22F2998/10—Processes characterised by the sequence of their steps
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01F—MAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
- H01F1/00—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
- H01F1/01—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
- H01F1/03—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity
- H01F1/032—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials
- H01F1/04—Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials characterised by their coercivity of hard-magnetic materials metals or alloys
- H01F1/047—Alloys characterised by their composition
- H01F1/053—Alloys characterised by their composition containing rare earth metals
- H01F1/055—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5
- H01F1/0555—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 pressed, sintered or bonded together
- H01F1/0557—Alloys characterised by their composition containing rare earth metals and magnetic transition metals, e.g. SmCo5 pressed, sintered or bonded together sintered
Definitions
- the present invention relates to a method for producing a magnetostrictive element, more particularly a method for producing a magnetostrictive element which contains Sm and a transition metal element.
- Magnetostriction is a phenomenon of a ferromagnetic material to undergo a dimensional change when magnetized, and a magnetostrictive material is a material which exhibits this phenomenon.
- Saturation magnetostrictive constant which represents a dimensional change at saturation by magnetostriction, is generally in a range from 10 ⁇ 5 to 10 ⁇ 6 , and a magnetostrictive material having a high saturation magnetostrictive constant is sometimes referred to as a giant-magnetostrictive material. These materials are widely used for vibrators, filters, sensors, and the like.
- a magnetostrictive material based on a laves type intermetallic compound of RFe 2 which is a compound of R (rare-earth element) and Fe, is known to have a high saturation magnetostrictive constant (refer to U.S. Pat. Nos. 3,949,351, 4,152,178, 4,308,474 and 4,375,372). These materials, however, involve problems of insufficient magnetostrictive value in an external magnetic field of low intensity, although exhibiting a high value when applied to a magnetic field of high intensity.
- magnetostrictive materials based on a laves type intermetallic compound of RFe 2 have been studied to have a higher magnetostrictive value even in an external magnetic field of low intensity, and it is proposed to orient the material along the [111] axis as an easy-magnetization axis of high magnetostrictive constant.
- Magnetostrictive materials based on a laves type intermetallic compound of RFe 2 exhibit a high magnetostrictive value at a composition of Tb 0.3 Dy 0.7 Fe 2.0 (atomic ratio), and this composition has been used exclusively.
- An Sm—Fe-based material is one of the materials which exhibit a high magnetostrictive value at normal temperature, like Tb 0.3 Dy 0.7 Fe 2.0 .
- a conventional magnetostrictive element of an Sm—Fe-based material is produced by melting a starting alloy and then solidifying the melt.
- the grains cannot be uniformly oriented by unidirectional solidification, because they pass the peritectic region of Fe 3 Sm while being solidified. Therefore, the conventional process gives only an isotropic magnetostrictive element, and cannot give an anisotropic one.
- the present invention has been developed to solve these technical problems. It is an object of the present invention to provide a method for producing a magnetostrictive element which can give an anisotropic magnetostrictive element, from a starting material containing Sm and a transition metal element such as an Sm—Fe-based material.
- a method of the present invention for producing a magnetostrictive element developed to achieve the above object, compacts a starting powder containing at least Sm and Fe into a compact in a magnetic field, and then sinters the compact to produce a sintered body having a composition of SmFe 2 .
- This can give an anisotropic magnetostrictive element.
- the composition may contain trace quantities of at least one element selected from the group consisting of Ni, Co, Mo, W, Cr, Nb, Ta, Ti, V, Ru, Rh, Pt, Ag, Gd and B.
- a powder of final composition may be directly used. It is however more preferable to use a mixed starting powder comprising a first alloy which forms the main phase for the magnetostrictive element and a second alloy which has a lower melting point than the first alloy. In the sintering process, the second alloy of lower melting point melts in advance of the first alloy to form the liquid phase. This can accelerate the sintering process. It is recommended that the starting powder contains the first alloy at 70% by weight or more but below 100% by weight.
- the first alloy has a larger mean particle size than the second one. This will improve degree of orientation of the first alloy, which forms the main phase, during the compaction in a magnetic field.
- the first alloy powder is mainly composed of single crystalline particles rather than polycrystalline particles.
- polycrystalline particles having a larger particle size than the second alloy are heat-treated beforehand to grow them into the single crystalline particles having a larger particle size than the second alloy.
- the second alloy powder is finely crushed by an adequate means, e.g., hydrogen crushing.
- the alloy having a composition of SmFe 2 has a lower magnetic anisotropy energy than an alloy composition of Tb 0.4 Dy 0.6 Fe 2.0 , for example. Therefore, an alloy composition of Tb 0.4 Dy 0.6 Fe 2.0 is compacted in a magnetic field of 800 kA/m whereas an alloy composition of SmFe 2 needs a higher intensity of 1140 kA/m or so to have the same degree of orientation.
- a mixed starting powder of first alloy and second alloy, the former having a larger particle size can be oriented in a field of lower intensity than 800 kA/m, e.g., 760 kA/m in a compacting step.
- the method of the present invention can produce an anisotropic magnetostrictive element by use of a starting material containing Sm and a transition metal element. Moreover, use of a mixed starting material of first and second alloys, the former having a larger particle size and the latter having lower melting point, allows orientation during compaction in a magnetic field and sintering to be effected efficiently.
- FIG. 1 compares magnetic anisotropy energy of a magnetostrictive alloy material having a composition of SmFe 2 with that of a magnetostrictive alloy material having a composition of Tb 0.4 Dy 0.6 Fe 2 ;
- FIG. 2 illustrates the directions for applying a magnetic field and the directions for measurements, used to determine whether the sintered bodies prepared in Example are anisotropic or not.
- the present invention uses a magnetostrictive material containing Sm and a transition metal element to produce an anisotropic giant-magnetostrictive material by powder metallurgy.
- Sm may be partly substituted by at least one element selected from the group consisting of Y, Nd and Tb.
- a transition metal element T is at least one element preferably selected from the group consisting of Fe, Ni and Co, of which Fe is particularly preferable.
- a preferable magnetostrictive material is based on SmFe, accordingly.
- a transition metal element T may be partly substituted by at least one element M selected from the group consisting of Mo, W, Cr, Nb, Ta, Ti, V, Ru, Rh, Pt, Ag, Gd and B.
- an SmFe-based magnetostrictive material preferably has an SmFe 2 phase.
- Such a magnetostrictive material can be produced by a process comprising a crushing, compacting in a magnetic field and sintering steps.
- a starting material of final composition may be directly used, after being crushed.
- the embodiment of the present invention adopts a characteristic method for producing a giant-magnetostrictive material in which a mixed starting powder comprising different compositions is used.
- the mixed starting powder comprises a material for the main phase (hereinafter arbitrarily referred to as main phase material) and another material (hereinafter arbitrarily referred to as grain boundary phase material) having a lower melting point than the main phase material.
- main phase material a material for the main phase
- grain boundary phase material another material having a lower melting point than the main phase material.
- the grain boundary phase material melts in advance of the main phase material to form the liquid phase. This can accelerate the sintering process to have a higher sintered body density.
- One of the preferable mixed powder compositions which satisfy the above conditions comprises an SmFe 1.96 alloy (melting point: 900° C.) as the main phase material and Sm 2 Fe alloy (melting point: 725° C.) as the grain boundary phase material.
- the alloy powder of the main phase material is preferably single-crystalline, because of improved crystal orientation expected.
- the alloy powder of the main phase material preferably has a larger size than those for the grain boundary phase material, because they are difficult to be easily oriented while being compacted in a magnetic field when they are excessively small, and difficult to have a high sintered body density and hence deteriorate the reliability for the sintered body when they are excessively large.
- the alloy powder for the main phase material is mainly composed of single crystalline particles rather than polycrystalline particles. It is recommended that polycrystalline particles having a larger particle size than the alloy powder for the grain boundary phase material are heat-treated beforehand to produce single crystalline particles having a larger particle size than the alloy powder for the grain boundary phase and use them as the alloy powder for the main phase material.
- the mixed powder is heat-treated at 850 to 900° C. for 6 to 48 hours in a non-oxidative atmosphere, when alloy powder having a composition of SmFe 1.96 is used for the main phase material, to have the single crystalline particles having a mean particle size (D50) of 12 to 30 ⁇ m.
- the alloy powder for the grain boundary phase material is preferably crushed finely by being occluded with hydrogen, as required. When occluded with hydrogen, these alloy particles will be cracked and finely crushed due to internal stresses caused by strains produced as a result of formation of hydride or penetration of atomic hydrogen into the grains.
- the alloy powder having a composition of Sm 2 Fe (melting point: 725° C.) is used for the grain boundary phase material and occluded with hydrogen, the alloy powder is crushed to have a mean particle size of 5 to 20 ⁇ m decreased from around 20 ⁇ m.
- the mixing ratio of the main phase material to the grain boundary phase material may be set arbitrarily, but preferably according to the following relationship.
- the content “a” (% by weight) of the main phase material is preferably in a range of 70 ⁇ a ⁇ 100, more preferably 80 ⁇ a ⁇ 95.
- ratio of the main phase material to be oriented in a magnetic field is excessively low, degree of orientation after sintering may be insufficient.
- degree of orientation after sintering may be insufficient.
- it is excessively high on the other hand, by which is meant that the main phase material composition is close to the final composition, it signifies little to use a grain boundary phase material for improved sintered body density.
- the magnetostrictive material produced by weighing and mixing the main phase material and grain boundary phase material may be then crushed.
- a crushing machine may be adequately selected from a wet ball mill, attritor, atomizer and the like. Of these machines, an atomizer is particularly preferable, because it can apply an impact and shear stress simultaneously to the particles to prevent their agglomeration and hence enhance productivity.
- the crushing is preferably conducted in a non-oxidative atmosphere, e.g., in an inert gas atmosphere of Ar gas or the like, or under vacuum.
- the mean particle size after crushing is 5 to 20 ⁇ m, preferably 10 to 20 ⁇ m. When it is excessively small, the particles tend to be oxidized in the production process to deteriorate the magnetostrictive characteristics. When it is excessively large, on the other hand, the sintered body will have an insufficient density and a number of open pores, because of insufficient sintering rate.
- the mixed magnetostrictive material is compacted into a desired shape before sintering.
- the compacting is carried out in a magnetic field to principally orient the main phase material particles in one direction. This is to orient the sintered magnetostrictive material along the [111] axis.
- the magnetic field applied has an intensity of 480 to 1760 kA/m, preferably 960 to 1760 kA/m.
- Magnetic field direction may be perpendicular to or in parallel to pressure direction.
- Compacting pressure is 50 ⁇ 10 6 Pa or more, preferably 300 ⁇ 10 6 Pa or more.
- a magnetostrictive alloy material represented by SmFe 2 (Formula (1)) has a magnetic anisotropy energy R roughly half that of a composition of Tb 0.4 Dy 0.6 Fe 2.0 , for example, as shown in FIG. 1 . This means that SmFe 2 needs a higher magnetic field intensity than Tb 0.4 Dy 0.6 Fe 2.0 to improve degree of orientation during the compacting in a magnetic field.
- the compact produced by compacting in a magnetic field is then sintered.
- the recommended sintering conditions are 800 to 900° C., preferably 850 to 890° C., and 3 to 48 hours.
- the recommended sintering atmosphere is non-oxidative, preferably in an inert gas atmosphere, e.g., in an Ar gas, or under vacuum.
- the magnetostrictive material thus prepared is polycrystalline and represented by SmFe 2 (Formula (1)). It is oriented along the [111] axis, a direction in which it exhibits the highest magnetostriction.
- the method of the present invention can produce an anisotropic giant-magnetostrictive material by powder metallurgy from a starting magnetostrictive material containing Sm and a transition metal element.
- an anisotropic giant-magnetostrictive material can be produced by powder metallurgy from a starting magnetostrictive material containing Sm and a transition metal element. The results are described below.
- a sintered body as a magnetostrictive element main body was produced by the following procedure.
- Sm and Fe as the main phase materials were weighed and molten in an inert Ar gas atmosphere to have a starting alloy having a composition of SmFe 1.96 .
- the starting alloy was heat-treated by annealing at 890° C. for 12 hours after temperature was stabilized to grow the grains.
- the obtained alloy powder was passed through a sieve (opening size: 2 mm) to remove coarse particles of 2 mm or more.
- Sm and Fe as the grain boundary phase materials were weighed and molten in an inert Ar gas atmosphere to have a starting alloy having a composition of Sm 2.0 Fe.
- the starting alloy powder was heat-treated at 150° C. for 6 hours after temperature was stabilized in a hydrogen atmosphere (hydrogen concentration: 80%) to crush the alloy occluded with hydrogen at around 18,000 ppm.
- the resulting crushed powder had a mean particle size of 5 ⁇ m.
- the crushed powder was passed through a sieve (opening size: 2 mm) to remove coarse particles of 2 mm or more.
- the alloy powder thus produced for the main phase and grain boundary phase materials were weighed and mixed with each other.
- the resulting mixture was finely crushed in an Ar gas atmosphere by an atomizer to have an alloy powder having a composition of SmFe 1.875 .
- the alloy powder was put in a mold and compacted in a magnetic field of 480 kA/m (6 kOe) at a compacting pressure of 8 tons/cm 2 to have a compact. It was transferred into the mold via a pipe filled with N 2 gas.
- the magnetic field was the so-called transverse one, in which the magnetic field was applied in a direction perpendicular to pressure direction.
- the compact (prepared in Example) was 10 mm cubic.
- the alloy powder was put in a mold and compacted under the same compacting pressure of 8 tons/cm 2 , but in the absence of a magnetic field, to have a compact having the same shape and size as the above (Comparative Example 1).
- Each of the compacts was put in a container for sintering and heated in a furnace in an Ar gas atmosphere at 890° C. for 6 hours after temperature was stabilized to have a sintered body (magnetostrictive element main body).
- the sintered body thus prepared was polycrystalline, represented by SmFe 2 , and was oriented along the [111] axis.
- the starting alloy having a composition of SmFe 1.90 was molten at 900° C., and the melt was solidified in a mold to have a magnetostrictive element of the same shape and size as the above by casting (Comparative Example 2).
- Example and Comparative Examples 1 and 2 were measured for the magnetostrictive characteristic (magnetostrictive value). Those prepared in Example and Comparative Example 1 were measured for sintered body density.
- the magnetostrictive value was determined by measuring the elongation of the samples (sintered bodies) using a strain gauge while the samples were placed in a magnetic field of 80 kA/m (1 kOe), where a magnetic field used for measurement was applied in the direction in parallel to the magnetic field direction applied during compaction (X-direction) and also perpendicular to the magnetic field direction applied during compaction (Y-direction).
- FIG. 2 illustrates elongation in the X- or Y-direction when the samples were subjected to a magnetic field used for measurement in the X- or Y-direction. The results are given in Table 1.
- the samples prepared in Comparative Examples 1 and 2 had an elongation of ⁇ 275 and ⁇ 260, respectively, in a direction along the magnetic field direction used for measurement (X-direction), when the magnetic field was set in the X-direction. They had an elongation of ⁇ 245 and ⁇ 250, respectively, in a direction along the magnetic field direction used for measurement (Y-direction), when the magnetic field was set in the Y-direction.
- the sample prepared in Example had an elongation of ⁇ 475 in a direction along the magnetic field direction used for measurement (X-direction), when the magnetic field was set in the X-direction, and ⁇ 275 in a direction along the magnetic field direction used for measurement (Y-direction), when the magnetic field was set in the Y-direction.
- the method of the present invention can produce an anisotropic magnetostrictive element.
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Abstract
It is an object of the present invention to provide a method for producing a magnetostrictive element which can give an anisotropic magnetostrictive element from a starting material containing Sm and a transition metal element. The method produces an anisotropic magnetostrictive element by compacting the starting powder in a magnetic field to produce a compact, and sintering the compact to produce a sintered body having a composition of SmFe2. It is preferable that the starting powder is produced by mixing a first alloy for the main phase of the magnetostrictive element with a second alloy having a lower melting point than the first alloy. It is recommended that the first alloy has a larger particle size than the second alloy.
Description
- 1. Field of the Invention
- The present invention relates to a method for producing a magnetostrictive element, more particularly a method for producing a magnetostrictive element which contains Sm and a transition metal element.
- 2. Description of the Related Art
- Magnetostriction is a phenomenon of a ferromagnetic material to undergo a dimensional change when magnetized, and a magnetostrictive material is a material which exhibits this phenomenon. Saturation magnetostrictive constant, which represents a dimensional change at saturation by magnetostriction, is generally in a range from 10−5 to 10−6, and a magnetostrictive material having a high saturation magnetostrictive constant is sometimes referred to as a giant-magnetostrictive material. These materials are widely used for vibrators, filters, sensors, and the like.
- At present, a magnetostrictive material based on a laves type intermetallic compound of RFe2, which is a compound of R (rare-earth element) and Fe, is known to have a high saturation magnetostrictive constant (refer to U.S. Pat. Nos. 3,949,351, 4,152,178, 4,308,474 and 4,375,372). These materials, however, involve problems of insufficient magnetostrictive value in an external magnetic field of low intensity, although exhibiting a high value when applied to a magnetic field of high intensity. Therefore, magnetostrictive materials based on a laves type intermetallic compound of RFe2 have been studied to have a higher magnetostrictive value even in an external magnetic field of low intensity, and it is proposed to orient the material along the [111] axis as an easy-magnetization axis of high magnetostrictive constant. Magnetostrictive materials based on a laves type intermetallic compound of RFe2 exhibit a high magnetostrictive value at a composition of Tb0.3Dy0.7Fe2.0 (atomic ratio), and this composition has been used exclusively.
- An Sm—Fe-based material is one of the materials which exhibit a high magnetostrictive value at normal temperature, like Tb0.3Dy0.7Fe2.0.
- A conventional magnetostrictive element of an Sm—Fe-based material is produced by melting a starting alloy and then solidifying the melt. However, the grains cannot be uniformly oriented by unidirectional solidification, because they pass the peritectic region of Fe3Sm while being solidified. Therefore, the conventional process gives only an isotropic magnetostrictive element, and cannot give an anisotropic one.
- The present invention has been developed to solve these technical problems. It is an object of the present invention to provide a method for producing a magnetostrictive element which can give an anisotropic magnetostrictive element, from a starting material containing Sm and a transition metal element such as an Sm—Fe-based material.
- A method of the present invention for producing a magnetostrictive element, developed to achieve the above object, compacts a starting powder containing at least Sm and Fe into a compact in a magnetic field, and then sinters the compact to produce a sintered body having a composition of SmFe2. This can give an anisotropic magnetostrictive element. The composition may contain trace quantities of at least one element selected from the group consisting of Ni, Co, Mo, W, Cr, Nb, Ta, Ti, V, Ru, Rh, Pt, Ag, Gd and B.
- A powder of final composition may be directly used. It is however more preferable to use a mixed starting powder comprising a first alloy which forms the main phase for the magnetostrictive element and a second alloy which has a lower melting point than the first alloy. In the sintering process, the second alloy of lower melting point melts in advance of the first alloy to form the liquid phase. This can accelerate the sintering process. It is recommended that the starting powder contains the first alloy at 70% by weight or more but below 100% by weight.
- It is also recommended that the first alloy has a larger mean particle size than the second one. This will improve degree of orientation of the first alloy, which forms the main phase, during the compaction in a magnetic field. In order to improve degree of orientation, it is recommended that the first alloy powder is mainly composed of single crystalline particles rather than polycrystalline particles. For production of the single crystalline particles for the first alloy powder, it is recommended that polycrystalline particles having a larger particle size than the second alloy are heat-treated beforehand to grow them into the single crystalline particles having a larger particle size than the second alloy. It is also effective that the second alloy powder is finely crushed by an adequate means, e.g., hydrogen crushing.
- It is preferable to orient the starting powder in a magnetic field of 450 to 1760 kA/m in the compacting step.
- The alloy having a composition of SmFe2 has a lower magnetic anisotropy energy than an alloy composition of Tb0.4Dy0.6Fe2.0, for example. Therefore, an alloy composition of Tb0.4Dy0.6Fe2.0 is compacted in a magnetic field of 800 kA/m whereas an alloy composition of SmFe2 needs a higher intensity of 1140 kA/m or so to have the same degree of orientation. By contrast, a mixed starting powder of first alloy and second alloy, the former having a larger particle size, can be oriented in a field of lower intensity than 800 kA/m, e.g., 760 kA/m in a compacting step.
- The method of the present invention can produce an anisotropic magnetostrictive element by use of a starting material containing Sm and a transition metal element. Moreover, use of a mixed starting material of first and second alloys, the former having a larger particle size and the latter having lower melting point, allows orientation during compaction in a magnetic field and sintering to be effected efficiently.
-
FIG. 1 compares magnetic anisotropy energy of a magnetostrictive alloy material having a composition of SmFe2 with that of a magnetostrictive alloy material having a composition of Tb0.4Dy0.6Fe2; and -
FIG. 2 illustrates the directions for applying a magnetic field and the directions for measurements, used to determine whether the sintered bodies prepared in Example are anisotropic or not. - The present invention is described by the embodiments shown below.
- The present invention uses a magnetostrictive material containing Sm and a transition metal element to produce an anisotropic giant-magnetostrictive material by powder metallurgy. In the above magnetostrictive material, Sm may be partly substituted by at least one element selected from the group consisting of Y, Nd and Tb.
- A transition metal element T is at least one element preferably selected from the group consisting of Fe, Ni and Co, of which Fe is particularly preferable. A preferable magnetostrictive material is based on SmFe, accordingly. A transition metal element T may be partly substituted by at least one element M selected from the group consisting of Mo, W, Cr, Nb, Ta, Ti, V, Ru, Rh, Pt, Ag, Gd and B.
- Moreover, an SmFe-based magnetostrictive material preferably has an SmFe2 phase.
- Such a magnetostrictive material can be produced by a process comprising a crushing, compacting in a magnetic field and sintering steps.
- A starting material of final composition may be directly used, after being crushed. The embodiment of the present invention, however, adopts a characteristic method for producing a giant-magnetostrictive material in which a mixed starting powder comprising different compositions is used.
- More specifically, 2 or more compositions of different melting point are used for the starting powder. In the embodiment, the mixed starting powder comprises a material for the main phase (hereinafter arbitrarily referred to as main phase material) and another material (hereinafter arbitrarily referred to as grain boundary phase material) having a lower melting point than the main phase material. When the mixed starting powder is sintered, the grain boundary phase material melts in advance of the main phase material to form the liquid phase. This can accelerate the sintering process to have a higher sintered body density. One of the preferable mixed powder compositions which satisfy the above conditions comprises an SmFe1.96 alloy (melting point: 900° C.) as the main phase material and Sm2Fe alloy (melting point: 725° C.) as the grain boundary phase material.
- The alloy powder of the main phase material is preferably single-crystalline, because of improved crystal orientation expected.
- Moreover, the alloy powder of the main phase material preferably has a larger size than those for the grain boundary phase material, because they are difficult to be easily oriented while being compacted in a magnetic field when they are excessively small, and difficult to have a high sintered body density and hence deteriorate the reliability for the sintered body when they are excessively large.
- In order to improve degree of orientation, it is recommended that the alloy powder for the main phase material is mainly composed of single crystalline particles rather than polycrystalline particles. It is recommended that polycrystalline particles having a larger particle size than the alloy powder for the grain boundary phase material are heat-treated beforehand to produce single crystalline particles having a larger particle size than the alloy powder for the grain boundary phase and use them as the alloy powder for the main phase material.
- It is recommended that the mixed powder is heat-treated at 850 to 900° C. for 6 to 48 hours in a non-oxidative atmosphere, when alloy powder having a composition of SmFe1.96 is used for the main phase material, to have the single crystalline particles having a mean particle size (D50) of 12 to 30 μm.
- The alloy powder for the grain boundary phase material is preferably crushed finely by being occluded with hydrogen, as required. When occluded with hydrogen, these alloy particles will be cracked and finely crushed due to internal stresses caused by strains produced as a result of formation of hydride or penetration of atomic hydrogen into the grains. When the alloy powder having a composition of Sm2Fe (melting point: 725° C.) is used for the grain boundary phase material and occluded with hydrogen, the alloy powder is crushed to have a mean particle size of 5 to 20 μm decreased from around 20 μm.
- The mixing ratio of the main phase material to the grain boundary phase material may be set arbitrarily, but preferably according to the following relationship.
- The content “a” (% by weight) of the main phase material is preferably in a range of 70≦a<100, more preferably 80≦a≦95. When it is excessively low, i.e., ratio of the main phase material to be oriented in a magnetic field is excessively low, degree of orientation after sintering may be insufficient. When it is excessively high, on the other hand, by which is meant that the main phase material composition is close to the final composition, it signifies little to use a grain boundary phase material for improved sintered body density.
- The magnetostrictive material produced by weighing and mixing the main phase material and grain boundary phase material may be then crushed. In the crushing step, a crushing machine may be adequately selected from a wet ball mill, attritor, atomizer and the like. Of these machines, an atomizer is particularly preferable, because it can apply an impact and shear stress simultaneously to the particles to prevent their agglomeration and hence enhance productivity. The crushing is preferably conducted in a non-oxidative atmosphere, e.g., in an inert gas atmosphere of Ar gas or the like, or under vacuum. The mean particle size after crushing is 5 to 20 μm, preferably 10 to 20 μm. When it is excessively small, the particles tend to be oxidized in the production process to deteriorate the magnetostrictive characteristics. When it is excessively large, on the other hand, the sintered body will have an insufficient density and a number of open pores, because of insufficient sintering rate.
- The mixed magnetostrictive material is compacted into a desired shape before sintering. The compacting is carried out in a magnetic field to principally orient the main phase material particles in one direction. This is to orient the sintered magnetostrictive material along the [111] axis. The magnetic field applied has an intensity of 480 to 1760 kA/m, preferably 960 to 1760 kA/m. Magnetic field direction may be perpendicular to or in parallel to pressure direction. Compacting pressure is 50×106 Pa or more, preferably 300×106 Pa or more. A magnetostrictive alloy material represented by SmFe2 (Formula (1)) has a magnetic anisotropy energy R roughly half that of a composition of Tb0.4Dy0.6Fe2.0, for example, as shown in
FIG. 1 . This means that SmFe2 needs a higher magnetic field intensity than Tb0.4Dy0.6Fe2.0 to improve degree of orientation during the compacting in a magnetic field. - The compact produced by compacting in a magnetic field is then sintered. The recommended sintering conditions are 800 to 900° C., preferably 850 to 890° C., and 3 to 48 hours. The recommended sintering atmosphere is non-oxidative, preferably in an inert gas atmosphere, e.g., in an Ar gas, or under vacuum.
- The magnetostrictive material thus prepared is polycrystalline and represented by SmFe2 (Formula (1)). It is oriented along the [111] axis, a direction in which it exhibits the highest magnetostriction.
- As described above, the method of the present invention can produce an anisotropic giant-magnetostrictive material by powder metallurgy from a starting magnetostrictive material containing Sm and a transition metal element.
- It is confirmed in this example that an anisotropic giant-magnetostrictive material can be produced by powder metallurgy from a starting magnetostrictive material containing Sm and a transition metal element. The results are described below.
- First, a sintered body as a magnetostrictive element main body was produced by the following procedure.
- First, Sm and Fe as the main phase materials were weighed and molten in an inert Ar gas atmosphere to have a starting alloy having a composition of SmFe1.96. The starting alloy was heat-treated by annealing at 890° C. for 12 hours after temperature was stabilized to grow the grains. The obtained alloy powder was passed through a sieve (opening size: 2 mm) to remove coarse particles of 2 mm or more.
- Sm and Fe as the grain boundary phase materials were weighed and molten in an inert Ar gas atmosphere to have a starting alloy having a composition of Sm2.0Fe. The starting alloy powder was heat-treated at 150° C. for 6 hours after temperature was stabilized in a hydrogen atmosphere (hydrogen concentration: 80%) to crush the alloy occluded with hydrogen at around 18,000 ppm. The resulting crushed powder had a mean particle size of 5 μm. The crushed powder was passed through a sieve (opening size: 2 mm) to remove coarse particles of 2 mm or more.
- Then, the alloy powder thus produced for the main phase and grain boundary phase materials were weighed and mixed with each other. The resulting mixture was finely crushed in an Ar gas atmosphere by an atomizer to have an alloy powder having a composition of SmFe1.875.
- The alloy powder was put in a mold and compacted in a magnetic field of 480 kA/m (6 kOe) at a compacting pressure of 8 tons/cm2 to have a compact. It was transferred into the mold via a pipe filled with N2 gas. The magnetic field was the so-called transverse one, in which the magnetic field was applied in a direction perpendicular to pressure direction. The compact (prepared in Example) was 10 mm cubic.
- For comparison, the alloy powder was put in a mold and compacted under the same compacting pressure of 8 tons/cm2, but in the absence of a magnetic field, to have a compact having the same shape and size as the above (Comparative Example 1).
- Each of the compacts was put in a container for sintering and heated in a furnace in an Ar gas atmosphere at 890° C. for 6 hours after temperature was stabilized to have a sintered body (magnetostrictive element main body). The sintered body thus prepared was polycrystalline, represented by SmFe2, and was oriented along the [111] axis.
- For comparison, the starting alloy having a composition of SmFe1.90 was molten at 900° C., and the melt was solidified in a mold to have a magnetostrictive element of the same shape and size as the above by casting (Comparative Example 2).
- Each of the sintered bodies prepared in Example and Comparative Examples 1 and 2 was measured for the magnetostrictive characteristic (magnetostrictive value). Those prepared in Example and Comparative Example 1 were measured for sintered body density.
- The magnetostrictive value was determined by measuring the elongation of the samples (sintered bodies) using a strain gauge while the samples were placed in a magnetic field of 80 kA/m (1 kOe), where a magnetic field used for measurement was applied in the direction in parallel to the magnetic field direction applied during compaction (X-direction) and also perpendicular to the magnetic field direction applied during compaction (Y-direction).
FIG. 2 illustrates elongation in the X- or Y-direction when the samples were subjected to a magnetic field used for measurement in the X- or Y-direction. The results are given in Table 1.TABLE 1 Magnetostrictive value Magnetic field direction used for measurement X Y Elongation Elongation Sintered measurement measurement body direction direction density (%) X Y Y X Example 96.34 −475 250 −275 145 Comparative 96.30 −275 65 −245 135 Example 1 Comparative — −260 90 −250 85 Example 2 - As shown in Table 1, the samples prepared in Comparative Examples 1 and 2 had an elongation of −275 and −260, respectively, in a direction along the magnetic field direction used for measurement (X-direction), when the magnetic field was set in the X-direction. They had an elongation of −245 and −250, respectively, in a direction along the magnetic field direction used for measurement (Y-direction), when the magnetic field was set in the Y-direction. By contrast, the sample prepared in Example had an elongation of −475 in a direction along the magnetic field direction used for measurement (X-direction), when the magnetic field was set in the X-direction, and −275 in a direction along the magnetic field direction used for measurement (Y-direction), when the magnetic field was set in the Y-direction. These results indicate that the sample prepared in Example had a magnetrostrictive value widely varying depending on direction of magnetic field applied thereto, i.e., it was anisotropic.
- It is therefore confirmed that the method of the present invention can produce an anisotropic magnetostrictive element.
Claims (17)
1. A method for producing an anisotropic magnetostrictive element, comprising the steps of:
compacting a starting powder containing at least Sm and Fe into a compact in a magnetic field, and
sintering the compact to produce a sintered body having a composition of SmFe2.
2. The method for producing a magnetostrictive element according to claim 1 , wherein the starting powder is produced by mixing a first alloy which forms the main phase of the magnetostrictive element with a second alloy which has a lower melting point than the first alloy.
3. The method for producing a magnetostrictive element according to claim 2 , wherein the first alloy has a composition of SmFe1.96.
4. The method for producing a magnetostrictive element according to claim 2 or 3 , wherein the second alloy has a composition of Sm2.0Fe.
5. The method for producing a magnetostrictive element according to claim 2 , wherein the starting powder contains the first alloy at 70% by weight or more but below 100% by weight.
6. The method for producing a magnetostrictive element according to claim 2 , wherein the starting powder contains the first alloy between 80 and 95% by weight.
7. The method for producing a magnetostrictive element according to claim 2 , wherein the first alloy powder has a larger particle size than the second alloy powder.
8. The method for producing a magnetostrictive element according to claim 7 , wherein the first alloy powder has a mean particle size of 12 to 30 μm.
9. The method for producing a magnetostrictive element according to claim 7 , wherein the first alloy powder is mainly composed of single crystalline particles and heat-treated beforehand to have a larger particle size than the second alloy powder.
10. The method for producing a magnetostrictive element according to claim 9 , wherein the first alloy powder is heat-treated at 850 to 900° C. for 6 to 48 hours, in a non-oxidative atmosphere.
11. The method for producing a magnetostrictive element according to claim 1 , wherein the compact is sintered at 800 to 900° C. for 3 to 48 hours, in a non-oxidative atmosphere.
12. The method for producing a magnetostrictive element according to any of claim 1 , wherein the starting powder is oriented in a magnetic field of 450 to 1760 kA/m in the step of producing a compact.
13. A method for producing an anisotropic magnetostrictive element, comprising the steps of:
mixing a first alloy powder which has a composition of SmFe1.69 with a second alloy powder which has a composition of Sm2.0Fe to prepare a starting powder,
compacting the starting powder into a compact in a magnetic field, and
sintering the compact to produce a sintered body having a composition of SmFe2.
14. The method for producing a magnetostrictive element according to claim 13 , wherein the starting powder contains the first alloy between 80 and 95% by weight.
15. The method for producing a magnetostrictive element according to claim 13 , wherein the first alloy powder has a mean particle size of 12 to 30 μm, and the second alloy powder has a smaller particle size than the first alloy powder.
16. The method for producing a magnetostrictive element according to claim 15 , wherein the first alloy powder is mainly composed of single crystalline particles.
17. The method for producing a magnetostrictive element according to claim 13 , wherein the sintered body is polycrystalline and the grains of the sintered body are oriented along the [111] axis.
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| JP2005030012A JP2006213985A (en) | 2005-02-07 | 2005-02-07 | Method for manufacturing magnetostrictive element |
| JP2005-030012 | 2005-02-07 |
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| US (1) | US20060174726A1 (en) |
| JP (1) | JP2006213985A (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109273182A (en) * | 2018-10-19 | 2019-01-25 | 广东省稀有金属研究所 | Single crystal magnetic powder and preparation method and application thereof |
| US20240145146A1 (en) * | 2022-11-02 | 2024-05-02 | Tdk Corporation | Magnetostrictive film and electronic device |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4900113B2 (en) * | 2007-07-24 | 2012-03-21 | Tdk株式会社 | Method for producing rare earth permanent sintered magnet |
| CN102282279B (en) * | 2009-01-16 | 2013-10-02 | 日立金属株式会社 | Method for producing R-T-B sintered magnet |
| CN103489561B (en) * | 2013-09-30 | 2016-08-17 | 华南理工大学 | A kind of permanent magnet systems providing neodymium iron boron casting magnetic field-aided |
| CN104201279A (en) * | 2014-07-25 | 2014-12-10 | 深圳市清研华创新材料有限公司 | Preparation method for magnetostrictive material and magnetostrictive material |
| CN105632673B (en) * | 2014-11-20 | 2017-11-10 | 有研稀土新材料股份有限公司 | The preparation method and permanent-magnet material of permanent-magnet material |
| CN111326303A (en) * | 2020-03-04 | 2020-06-23 | 南京大学 | Method for manufacturing rare earth alloy spherical single crystal magnetic powder and <111> oriented rare earth giant magnetostrictive material |
| JP7529969B2 (en) * | 2020-03-24 | 2024-08-07 | 愛知製鋼株式会社 | Magnetosensitive wire and its manufacturing method |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3949351A (en) * | 1974-06-03 | 1976-04-06 | The United States Of America As Represented By The Secretary Of The Navy | Variable delay line |
| US4152178A (en) * | 1978-01-24 | 1979-05-01 | The United States Of America As Represented By The United States Department Of Energy | Sintered rare earth-iron Laves phase magnetostrictive alloy product and preparation thereof |
| US4308474A (en) * | 1979-11-14 | 1981-12-29 | The United States Of America As Represented By The Secretary Of The Navy | Rare earth-iron magnetostrictive materials and devices using these materials |
| US4375372A (en) * | 1972-03-16 | 1983-03-01 | The United States Of America As Represented By The Secretary Of The Navy | Use of cubic rare earth-iron laves phase intermetallic compounds as magnetostrictive transducer materials |
| US5529745A (en) * | 1994-04-19 | 1996-06-25 | Tdk Corporation | Preparation of magnetostrictive material |
| US6991686B2 (en) * | 2004-01-26 | 2006-01-31 | Tdk Corporation | Method for producing magnetostrictive material |
-
2005
- 2005-02-07 JP JP2005030012A patent/JP2006213985A/en not_active Withdrawn
-
2006
- 2006-02-07 CN CNA2006100068071A patent/CN1818121A/en active Pending
- 2006-02-07 US US11/349,788 patent/US20060174726A1/en not_active Abandoned
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4375372A (en) * | 1972-03-16 | 1983-03-01 | The United States Of America As Represented By The Secretary Of The Navy | Use of cubic rare earth-iron laves phase intermetallic compounds as magnetostrictive transducer materials |
| US3949351A (en) * | 1974-06-03 | 1976-04-06 | The United States Of America As Represented By The Secretary Of The Navy | Variable delay line |
| US4152178A (en) * | 1978-01-24 | 1979-05-01 | The United States Of America As Represented By The United States Department Of Energy | Sintered rare earth-iron Laves phase magnetostrictive alloy product and preparation thereof |
| US4308474A (en) * | 1979-11-14 | 1981-12-29 | The United States Of America As Represented By The Secretary Of The Navy | Rare earth-iron magnetostrictive materials and devices using these materials |
| US5529745A (en) * | 1994-04-19 | 1996-06-25 | Tdk Corporation | Preparation of magnetostrictive material |
| US6991686B2 (en) * | 2004-01-26 | 2006-01-31 | Tdk Corporation | Method for producing magnetostrictive material |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109273182A (en) * | 2018-10-19 | 2019-01-25 | 广东省稀有金属研究所 | Single crystal magnetic powder and preparation method and application thereof |
| US20240145146A1 (en) * | 2022-11-02 | 2024-05-02 | Tdk Corporation | Magnetostrictive film and electronic device |
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| CN1818121A (en) | 2006-08-16 |
| JP2006213985A (en) | 2006-08-17 |
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