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US20210057942A1 - Thin strip component, method for manufacturing same, and motor using thin strip component - Google Patents

Thin strip component, method for manufacturing same, and motor using thin strip component Download PDF

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Publication number
US20210057942A1
US20210057942A1 US17/090,079 US202017090079A US2021057942A1 US 20210057942 A1 US20210057942 A1 US 20210057942A1 US 202017090079 A US202017090079 A US 202017090079A US 2021057942 A1 US2021057942 A1 US 2021057942A1
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US
United States
Prior art keywords
thin strip
strip component
amorphous
heat treating
shape
Prior art date
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Abandoned
Application number
US17/090,079
Inventor
Yukio Nishikawa
Hideaki Hamada
Naoki Nojiri
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Panasonic Corp
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Panasonic Corp
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Filing date
Publication date
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Priority to US17/090,079 priority Critical patent/US20210057942A1/en
Publication of US20210057942A1 publication Critical patent/US20210057942A1/en
Abandoned legal-status Critical Current

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    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K1/00—Details of the magnetic circuit
    • H02K1/02—Details of the magnetic circuit characterised by the magnetic material
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/021—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips involving a particular fabrication or treatment of ingot or slab
    • C21D8/0215—Rapid solidification; Thin strip casting
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/0247—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment
    • C21D8/0252—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips characterised by the heat treatment with application of tension
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/12—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of articles with special electromagnetic properties
    • C21D8/1205—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of articles with special electromagnetic properties involving a particular fabrication or treatment of ingot or slab
    • C21D8/1211—Rapid solidification; Thin strip casting
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/12—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of articles with special electromagnetic properties
    • C21D8/1244—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of articles with special electromagnetic properties the heat treatment(s) being of interest
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/12—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of articles with special electromagnetic properties
    • C21D8/1244—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of articles with special electromagnetic properties the heat treatment(s) being of interest
    • C21D8/125—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of articles with special electromagnetic properties the heat treatment(s) being of interest with application of tension
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
    • C21D9/0068—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for particular articles not mentioned below
    • 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
    • H01F41/0206—Manufacturing of magnetic cores by mechanical means
    • H01F41/0213—Manufacturing of magnetic circuits made from strip(s) or ribbon(s)
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K1/00—Details of the magnetic circuit
    • H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
    • H02K1/12—Stationary parts of the magnetic circuit
    • H02K1/14—Stator cores with salient poles
    • H02K1/146—Stator cores with salient poles consisting of a generally annular yoke with salient poles
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K1/00—Details of the magnetic circuit
    • H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
    • H02K1/12—Stationary parts of the magnetic circuit
    • H02K1/18—Means for mounting or fastening magnetic stationary parts on to, or to, the stator structures
    • H02K1/185—Means for mounting or fastening magnetic stationary parts on to, or to, the stator structures to outer stators
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K15/00—Processes or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines
    • H02K15/02—Processes or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines of stator or rotor bodies
    • H02K15/021—Magnetic cores
    • H02K15/022—Magnetic cores with salient poles
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D2201/00—Treatment for obtaining particular effects
    • C21D2201/03—Amorphous or microcrystalline structure
    • C—CHEMISTRY; METALLURGY
    • C21—METALLURGY OF IRON
    • C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
    • C21D8/00—Modifying the physical properties by deformation combined with, or followed by, heat treatment
    • C21D8/02—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips
    • C21D8/04—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing
    • C21D8/041—Modifying the physical properties by deformation combined with, or followed by, heat treatment during manufacturing of plates or strips to produce plates or strips for deep-drawing involving a particular fabrication or treatment of ingot or slab
    • C21D8/0415—Rapid solidification; Thin strip casting

Definitions

  • the technical field relates to a thin strip component, a method for manufacturing the same, and a motor using the thin strip component.
  • the technical field relates to a thin strip component obtained by heat treating a soft magnetic thin strip, a method for manufacturing the same, and a motor using the same.
  • a stator core used in this motor is, first, an amorphous alloy thin strip produced by a liquid quenching method such as a single roll method or a twin roll method is processed into a predetermined shape by a method such as winding, cutting, punching, and etching. Next, in order to improve the magnetic characteristics of the alloy thin strip, the amorphous alloy thin strip is heat treated and crystallized to obtain an alloy thin strip having nanocrystal grains. Next, these are laminated to form a stator core, and used for a motor.
  • a liquid quenching method such as a single roll method or a twin roll method
  • an object of the disclosure is to provide a thin strip component excellent in shape accuracy and magnetic characteristics even if the contraction occurs in the thin strip component by heat treatment, a method for manufacturing the same, and a motor using the thin strip component.
  • a method for manufacturing a thin strip component including a processing step of processing an amorphous thin strip member into a dimension shape larger than a target shape, and a heat treating step of heat treating and contracting the amorphous thin strip member processed in the processing step to form the amorphous thin strip member into a thin strip component of the target shape is used.
  • a method for manufacturing a thin strip component including a processing step of processing an amorphous thin strip into a dimension shape larger than a target shape, a laminating step of laminating the amorphous thin strips processed in the processing step, and a heat treating step of heat treating and contracting a laminate of the amorphous thin strips after the laminating step to form the amorphous thin strips into a laminated thin strip member of the target shape is used.
  • a thin strip component which is a magnetic laminate in which a plurality of plate-shaped thin strip component members of the same shape are laminated, and has a recess over an entire side surface of the magnetic laminate is used.
  • a thin strip component which is a magnetic laminate in which a plurality of plate-shaped thin strip component members of the same shape are laminated, and to which the thin strip components are bonded is used.
  • a thin strip component which is a magnetic laminate in which a plurality of plate-shaped thin strip component members of the same shape are laminated, in which one plane is formed by covering a side surface of the magnetic laminate with resin is used.
  • a thin strip component which is a magnetic laminate in which a plurality of plate-shaped thin strip component members of the same shape are laminated, in which one plane is formed on a side surface of the magnetic laminate, and resin is positioned between the thin strip components is used.
  • a motor including the above-described thin strip component, a plurality of coils disposed on the thin strip component, and a rotor disposed between the plurality of coils is used.
  • the thin strip component, the laminate, the method for manufacturing thereof, and the motor of the disclosure it is possible to improve the shape accuracy and the magnetic characteristics of the thin strip component, and the motor characteristics.
  • FIG. 1 is a top view of an iron thin strip component in an amorphous state according to Embodiment 1 of the disclosure
  • FIG. 2A is a side view of a laminate in which heat treated thin strip components are laminated according to Embodiment 1 of the disclosure
  • FIG. 2B is a top view of the laminate in which the heat treated thin strip components are laminated according to Embodiment 1 of the disclosure;
  • FIG. 3B is a top view of the motor using the laminate according to Embodiment 1 of the disclosure.
  • FIG. 4A is a cross-sectional view of a vicinity of end surface of teeth of the laminate according to Embodiment 1 of the disclosure.
  • FIG. 4B is a front view of the teeth of the laminate according to Embodiment 1 of the disclosure.
  • FIG. 5 is a cross-sectional view of a vicinity of an end surface of a laminate according to Embodiment 2 of the disclosure.
  • FIG. 6A is a cross-sectional view of a vicinity of an end surface of a laminate according to Embodiment 3 of the disclosure.
  • FIG. 6B is a front view of the vicinity of the end surface of the laminate according to Embodiment 3 of the disclosure.
  • FIG. 7 is a view showing a cross-sectional configuration of a heat treatment device for a laminate according to Embodiment 4 of the disclosure.
  • FIG. 8A is a cross-sectional view of a vicinity of an end surface of the laminate according to Embodiment 4 of the disclosure.
  • FIG. 8B is a front view of the vicinity of the end surface of the laminate according to Embodiment 4 of the disclosure.
  • FIG. 9A is a cross-sectional view of a vicinity of an end surface of a laminate according to Embodiment 5 of the disclosure.
  • FIG. 9B is a front view of the vicinity of the end surface of the laminate according Embodiment 5 of the to disclosure.
  • FIG. 1 is a plan view of amorphous thin strip member 1 according to Embodiment 1 of the disclosure.
  • Amorphous thin strip member 1 is an iron thin strip component, a magnetic member.
  • Amorphous thin strip member 1 has a plurality of T-shaped portions called teeth 1 a on an inner side.
  • rotor 10 is placed on the inner side of end surface 30 of teeth 1 a .
  • coils are wound on these teeth la. A current flows through the coils, a magnetic field is generated, rotor 10 rotates, and becomes a motor.
  • fitting holes 1 b at four positions around amorphous thin strip member 1 .
  • a fixing member such as a bolt is inserted into each fitting hole 1 b.
  • donut-like or hollow frame-shaped core back 1 c which connects a plurality of teeth 1 a and has the fitting holes 1 b on an outer periphery of amorphous thin strip member 1 .
  • Amorphous thin strip member 1 is heat treated to improve magnetic characteristics.
  • fine crystal grains of pure iron called nanocrystal grains are generated by being crystallized in the heat treatment, soft magnetic characteristics are improved.
  • Amorphous thin strip member 1 is a magnetic material, the coils are wound, and becomes a component of the motor.
  • amorphous thin strip member 1 Since amorphous thin strip member 1 is in an unstable state in which the interatomic distance is longer than the unique interatomic distance, atoms move so that the interatomic distances become unique distances for stabilization as the temperature rises due to the heat treatment . As a result, amorphous thin strip member 1 contracts. Since the heat treated thin strip becomes brittle, at the time of manufacturing, it is necessary to perform a shaping process in the amorphous state, and then move onto the heat treating step.
  • Embodiment 1 a method for manufacturing a thin strip component including a processing step of processing amorphous thin strip member 1 into a predetermined shape having a ratio of a dimension larger than a target shape, and a heat treating step of heat treating and contracting processed amorphous thin strip member 1 into a shape within a target dimension is used.
  • amorphous thin strip member 1 is processed to a large dimension in consideration of the contraction factor of amorphous thin strip member 1 due to the heat treatment .
  • Amorphous thin strip member 1 processed to be larger is heat treated, contracted, and contained within the predetermined dimensional specification.
  • the movement of atoms becomes clear from about 100° C., and nanocrystal grains having a size of several tens of nanometers begin to be generated between about 370° C. to 500° C.
  • the contraction factor is 0.6% at maximum in the uniaxial direction for a rectangular test piece, but the value varies depending on the heat treatment conditions. As the temperature of the heat treatment is higher or the heat treatment is longer, the movement amount of the atoms becomes larger, so that the contraction factor becomes larger.
  • the processing dimension is decided accordingly.
  • the contraction factor the influence of plate thickness is small.
  • the contraction factor the influence of the shape is large, and the behavior of the contraction factor depending on the location is complicated depending on the shape. Since not only the contraction factor of each material itself but also the manner of connection of the materials are mutually restrained, the contraction factor is not uniform and varies from place to place.
  • T-shaped portion that is teeth 1 a which needs to consider the contraction factor in order to improve the shape accuracy.
  • a rotor which is rotor 10 , is inserted into the inner diameter portion. Therefore, when a gap between rotor 10 and end surface 30 of teeth 1 a is large, the motor efficiency is deteriorated, and when the gap is not constant, the rotation operation becomes unstable.
  • End surface 30 of a tip portion of teeth 1 a shows the most complicated contraction behavior. If the shape accuracy of teeth 1 a is poor, the motor characteristics also become unstable.
  • fitting holes 1 b at four positions around amorphous thin strip member 1 .
  • the position of each fitting hole 1 b is important because it affects the positional accuracy of the center of amorphous thin strip member 1 and the accuracy of a diameter of a space into which rotor 10 is inserted.
  • core back 1 c which connects the plurality of teeth 1 a and has fitting hole 1 b .
  • the accuracy of core back 1 c may be lower than that of teeth 1 a or fitting hole 1 b in terms of the degree of rigidity.
  • a shape close to the final shape is produced first, and heat treated.
  • the ones subjected to heat treatment are measured and the contraction factor is determined.
  • the contraction factor measured with different heat treatment conditions and the portion shape is between 0% to 0.6%.
  • the contraction amount after the heat treatment is influenced by the nonuniformity such as the amorphous state in amorphous thin strip member 1 , the plate thickness, the temperature during the heat treatment, and the like. There is a difference in the contraction amount even if the same treatment is carried out. However, if the maximum diameter is about 130 mm or less as in this embodiment, the accuracy is within ⁇ 0.01 mm.
  • FIG. 2A is a side view of thin strip component 3 in which thin strip component members 2 obtained by heat treating amorphous thin strip member 1 are laminated.
  • FIG. 2B is a top view of thin strip component 3 in which thin strip component members 2 obtained by heat treating amorphous thin strip member 1 are laminated.
  • heat treated thin strip component members 2 are laminated and fastened by nut 7 via spring washer 5 and washer 6 by bolt 4 .
  • the fixation is four positions.
  • amorphous thin strip members 1 After laminating a plurality of or more amorphous thin strip members 1 , amorphous thin strip members 1 may be heat treated and fastened by bolt 4 as shown in FIG. 2A to form laminated thin strip component 3 .
  • Laminated thin strip component 3 is a magnetic laminate in which a plurality of plate-shaped thin strip component members 2 of the same shape are laminated.
  • FIG. 3A is a side view of a motor using laminated thin strip component 3
  • FIG. 3B is a top view of the motor using laminated thin strip component 3
  • nut 7 is removed at one end, metal base 8 is inserted under laminated thin strip component 3 and fastened again by nut 7 .
  • winding 9 is applied to laminated thin strip component 3 at a portion called teeth 1 a ( FIG. 1 ) of thin strip component member 2 to make it a stator.
  • Rotor 10 is installed in the inner diameter portion of laminated thin strip component 3 . If electricity is supplied to winding 9 in this state, it can be driven as a motor.
  • FIG. 4A is a cross-sectional view of a vicinity of end surface 30 of teeth 1 a of laminated thin strip component 3
  • FIG. 4B is a front view of a vicinity of end surface 30 of teeth 1 a of laminated thin strip component 3 .
  • the dimensional accuracy of thin strip component member 2 after heat treatment is within ⁇ 0.01 mm.
  • misalignment in the plane tends to occur during the lamination.
  • unevenness occurs on end surface 30 due to the deviation of the dimensions caused by the heat treatment.
  • Dimensional variations a of the unevenness of FIG. 4A and dimensional variation of end surface 30 in dimensional variation b of the unevenness of FIG. 4B are both within ⁇ 0.1 mm. Since thin strip component member 2 is heat treated, it is possible to confirm visible oxide film 11 on end surface 30 in FIG. 4B . Oxidation does not progress and corrosion resistance improves due to the presence of oxide film 11 .
  • FIG. 5 is a cross-sectional view of a vicinity of end surface 30 of teeth 1 a of laminated thin strip component 3 according to Embodiment 2 of the disclosure. Items not described are the same as those in Embodiment 1.
  • FIG. 5 is different from FIG. 4 in Embodiment 1 in that resin coating layer 12 is formed on end surface 30 of thin strip component members 2 . Unevenness occurs on end surface 30 due to the difference in contraction amount of each thin strip component member 2 . However, it is particularly important to improve the accuracy of mutual gap distance (distance between end surface 30 and rotor 10 ) in the inner diameter portion in which rotor 10 is rotated.
  • resin coating layer 12 is formed on end surface 30 .
  • resin coating layer 12 enters deeper into the interlayer of thin strip component members 2 , the space factor becomes worse. Therefore, resin coating layer 12 is formed only on end surface 30 mainly. Since end surface 30 has unevenness, even if resin coating layer 12 is formed only in the vicinity of the surface of end surface 30 , the bonding force can be sufficiently secured. Furthermore, if the surface of resin coating layer 12 is cut to form plane 31 , the shape accuracy is further improved.
  • resin coating layer 12 only on teeth 1 a portion of thin strip component 3 .
  • FIG. 6A is a cross-sectional view of a vicinity of end surface 30 of teeth 1 a of laminated thin strip component 3 according to Embodiment 3 of the disclosure.
  • FIG. 6B is a front view of the vicinity of end surface 30 of teeth 1 a of laminated thin strip component 3 according to Embodiment 3 of the disclosure. Items not described are the same as those in Embodiments 1 and 2.
  • FIG. 6A is different from FIG. 5 in Embodiment 2 in that the surface of resin coating layer 12 is cut to expose thin strip component members 2 from end surface 30 to form one plane 31 .
  • thin strip component members 2 can be brittle due to the heat treatment, by leaving a state in which the interlayer is bonded by resin coating layer 12 in end surface 30 , it is possible to perform cutting without damaging thin strip component members 2 .
  • FIG. 7 is a view showing a cross-sectional configuration of a heat treatment device of laminated thin strip component 3 according to Embodiment 4 of the disclosure. Items not described are the same as those in Embodiments 1 to 3.
  • Laminate 14 of amorphous thin strip members 1 is sandwiched between pressure plates 15 , and heated by heater 16 in pressure plate 15 so as to perform heat treatment while pressing. During the heat treatment process, the surface of oxide film 32 develops between amorphous thin strip members 1 , and the entire or a portion of the members are mutually bonded to each other. As a result, since laminate 14 is integrated, the handling after heat treatment becomes easier.
  • Oxide film 32 is larger on the outside of laminate 14 than between inside amorphous thin strip member 1 .
  • FIG. 8A is a cross-sectional view of a vicinity of end surface 30 of laminate 17 after the heat treatment
  • FIG. 8B is a front view of the vicinity of end surface 30 of laminate 17 after the heat treatment.
  • amorphous thin strip member 1 Under the heat treatment conditions under which nanocrystal grains are generated, amorphous thin strip member 1 itself generates heat and the heat is accumulated on the central side of laminate 14 , so that the temperature rises, and the contraction factor on the central side also increases. Due to these influences, the contraction amount in the center becomes large and recess 18 exists sometimes on end surface 30 of laminate 17 after heat treatment.
  • Laminate 14 is a magnetic laminate in which the plurality of plate-shaped thin strip components 2 of the same shape are laminated, and is a thin strip component having recess 18 over the entire side surface of the magnetic laminate. As for the size of thin strip component member 2 , thin strip component member 2 located outside laminate 14 has a larger size.
  • FIG. 9A is a cross-sectional view of a vicinity of end surface 30 of teeth 1 a of laminate 17 according to Embodiment 5 of the disclosure.
  • FIG. 9B is a front view of the vicinity of end surface 30 of teeth 1 a of laminate 17 according to Embodiment 5 of the disclosure. Items not described are the same as those in Embodiment 4 .
  • laminate 17 of Embodiment 4 is further processed to form one plane on the side surface.
  • FIGS. 9A and 9B are different from FIGS. 8A and 8B in Embodiment 4 in that the surface of end surface 30 is cut to form one plane 31 .
  • thin strip component members 2 can be brittle due to the heat treatment, this process is possible because the entire or a portion of the interlayer of thin strip component members 2 are bonded to each other by oxide film 32 by performing the heat treatment while pressing in the device of FIG. 7 .
  • Embodiments 2 and 3 maybe applied to the laminate produced in Embodiments 4 and 5.
  • teeth 1 a have been mainly described, it can be similarly applied to other parts of thin strip component members 2 .
  • the thin strip component is an example and can be applied to other structures and shapes.
  • the thin strip component the laminate, the method for manufacturing thereof, and the motor of the disclosure, it is possible to improve the shape accuracy and the magnetic characteristics of thin strip component, and the motor characteristics.
  • the laminate according to the disclosure can also be applied to applications of electronic components such as transformers, other than motors.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Materials Engineering (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Power Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Electromagnetism (AREA)
  • Manufacture Of Motors, Generators (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)
  • Heat Treatment Of Articles (AREA)
  • Manufacturing Cores, Coils, And Magnets (AREA)

Abstract

A method for manufacturing a thin strip component, including a processing step of processing an amorphous thin strip member into a dimension shape larger than a target shape, and a heat treating step of heat treating and contracting the amorphous thin strip member processed in the processing step to form the amorphous thin strip member into a thin strip component of the target shape. A thin strip component which is a magnetic laminate in which a plurality of plate-shaped thin strip component members of the same shape are laminated, and has a recess over an entire side surface of the magnetic laminate is used. A motor including the thin strip component, a plurality of coils disposed on the thin strip component, and a rotor disposed between the plurality of coils is used.

Description

    CROSS-REFERENCE OF RELATED APPLICATIONS
  • This application is a Divisional application of U.S. patent application Ser. No. 16/268,455, filed on Feb. 5, 2019, which is a Continuation of International Patent Application No. PCT/JP2018/001498, filed on Jan. 19, 2018, which in turn claims the benefit of Japanese Application No. 2017-025234, filed on Feb. 14, 2017, the entire disclosures of which Applications are incorporated by reference herein.
    • TECHNICAL FIELD
  • The technical field relates to a thin strip component, a method for manufacturing the same, and a motor using the thin strip component. In particular, the technical field relates to a thin strip component obtained by heat treating a soft magnetic thin strip, a method for manufacturing the same, and a motor using the same.
    • BACKGROUND
  • As a laminate of magnetic plates of an iron core (stator) for a motor in the related art, pure iron or an electromagnetic steel plate is used. In motors aimed for higher efficiency, amorphous thin strips or thin strips having nanocrystal grains are used in some iron cores (for example, see Japanese Patent Unexamined Publication No. 6-145917).
  • A stator core used in this motor is, first, an amorphous alloy thin strip produced by a liquid quenching method such as a single roll method or a twin roll method is processed into a predetermined shape by a method such as winding, cutting, punching, and etching. Next, in order to improve the magnetic characteristics of the alloy thin strip, the amorphous alloy thin strip is heat treated and crystallized to obtain an alloy thin strip having nanocrystal grains. Next, these are laminated to form a stator core, and used for a motor.
    • SUMMARY
  • However, in the motor disclosed in Japanese Patent Unexamined Publication No. 6-145917, since the amorphous alloy thin strip is processed into a predetermined shape and heat treated, the distance between atoms constituting the thin strip is narrowed as the temperature rises, and contraction of the thin strip occurs.
  • As a result, the shape of the stator core after the heat treatment sometimes does not fall within a predetermined range. Therefore, troubles have occurred in assembling the stator to the motor. A gap distance between the stator core and a rotor core was not constant, and the motor characteristics were not constant.
  • Therefore, an object of the disclosure is to provide a thin strip component excellent in shape accuracy and magnetic characteristics even if the contraction occurs in the thin strip component by heat treatment, a method for manufacturing the same, and a motor using the thin strip component.
  • In order to achieve the above-described object, a method for manufacturing a thin strip component including a processing step of processing an amorphous thin strip member into a dimension shape larger than a target shape, and a heat treating step of heat treating and contracting the amorphous thin strip member processed in the processing step to form the amorphous thin strip member into a thin strip component of the target shape is used.
  • A method for manufacturing a thin strip component including a processing step of processing an amorphous thin strip into a dimension shape larger than a target shape, a laminating step of laminating the amorphous thin strips processed in the processing step, and a heat treating step of heat treating and contracting a laminate of the amorphous thin strips after the laminating step to form the amorphous thin strips into a laminated thin strip member of the target shape is used.
  • A thin strip component which is a magnetic laminate in which a plurality of plate-shaped thin strip component members of the same shape are laminated, and has a recess over an entire side surface of the magnetic laminate is used.
  • A thin strip component which is a magnetic laminate in which a plurality of plate-shaped thin strip component members of the same shape are laminated, and to which the thin strip components are bonded is used.
  • A thin strip component which is a magnetic laminate in which a plurality of plate-shaped thin strip component members of the same shape are laminated, in which one plane is formed by covering a side surface of the magnetic laminate with resin is used.
  • A thin strip component which is a magnetic laminate in which a plurality of plate-shaped thin strip component members of the same shape are laminated, in which one plane is formed on a side surface of the magnetic laminate, and resin is positioned between the thin strip components is used.
  • A motor including the above-described thin strip component, a plurality of coils disposed on the thin strip component, and a rotor disposed between the plurality of coils is used.
  • As described above, according to the thin strip component, the laminate, the method for manufacturing thereof, and the motor of the disclosure, it is possible to improve the shape accuracy and the magnetic characteristics of the thin strip component, and the motor characteristics.
    • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 is a top view of an iron thin strip component in an amorphous state according to Embodiment 1 of the disclosure;
  • FIG. 2A is a side view of a laminate in which heat treated thin strip components are laminated according to Embodiment 1 of the disclosure;
  • FIG. 2B is a top view of the laminate in which the heat treated thin strip components are laminated according to Embodiment 1 of the disclosure;
  • FIG. 3A is aside view of a motor using the laminate according to Embodiment 1 of the disclosure;
  • FIG. 3B is a top view of the motor using the laminate according to Embodiment 1 of the disclosure;
  • FIG. 4A is a cross-sectional view of a vicinity of end surface of teeth of the laminate according to Embodiment 1 of the disclosure;
  • FIG. 4B is a front view of the teeth of the laminate according to Embodiment 1 of the disclosure;
  • FIG. 5 is a cross-sectional view of a vicinity of an end surface of a laminate according to Embodiment 2 of the disclosure;
  • FIG. 6A is a cross-sectional view of a vicinity of an end surface of a laminate according to Embodiment 3 of the disclosure;
  • FIG. 6B is a front view of the vicinity of the end surface of the laminate according to Embodiment 3 of the disclosure;
  • FIG. 7 is a view showing a cross-sectional configuration of a heat treatment device for a laminate according to Embodiment 4 of the disclosure;
  • FIG. 8A is a cross-sectional view of a vicinity of an end surface of the laminate according to Embodiment 4 of the disclosure;
  • FIG. 8B is a front view of the vicinity of the end surface of the laminate according to Embodiment 4 of the disclosure;
  • FIG. 9A is a cross-sectional view of a vicinity of an end surface of a laminate according to Embodiment 5 of the disclosure;
  • and
  • FIG. 9B is a front view of the vicinity of the end surface of the laminate according Embodiment 5 of the to disclosure.
    •  DESCRIPTION OF EMBODIMENTS
  • Hereinafter, embodiments of the disclosure will be described with reference to the drawings.
    • Embodiment 1
  • FIG. 1 is a plan view of amorphous thin strip member 1 according to Embodiment 1 of the disclosure.
    • Amorphous Thin Strip Member 1
  • Amorphous thin strip member 1 is an iron thin strip component, a magnetic member.
  • Amorphous thin strip member 1 has a plurality of T-shaped portions called teeth 1 a on an inner side. In a case where amorphous thin strip member 1 is used for a motor, rotor 10 is placed on the inner side of end surface 30 of teeth 1 a. Finally, coils are wound on these teeth la. A current flows through the coils, a magnetic field is generated, rotor 10 rotates, and becomes a motor.
  • There are fitting holes 1 b at four positions around amorphous thin strip member 1. A fixing member such as a bolt is inserted into each fitting hole 1 b.
  • There is donut-like or hollow frame-shaped core back 1 c which connects a plurality of teeth 1 a and has the fitting holes 1 b on an outer periphery of amorphous thin strip member 1.
    • Heat Treatment
  • Amorphous thin strip member 1 is heat treated to improve magnetic characteristics. In particular, when fine crystal grains of pure iron called nanocrystal grains are generated by being crystallized in the heat treatment, soft magnetic characteristics are improved. Amorphous thin strip member 1 is a magnetic material, the coils are wound, and becomes a component of the motor.
  • Since amorphous thin strip member 1 is in an unstable state in which the interatomic distance is longer than the unique interatomic distance, atoms move so that the interatomic distances become unique distances for stabilization as the temperature rises due to the heat treatment . As a result, amorphous thin strip member 1 contracts. Since the heat treated thin strip becomes brittle, at the time of manufacturing, it is necessary to perform a shaping process in the amorphous state, and then move onto the heat treating step.
    • Process
  • In Embodiment 1, a method for manufacturing a thin strip component including a processing step of processing amorphous thin strip member 1 into a predetermined shape having a ratio of a dimension larger than a target shape, and a heat treating step of heat treating and contracting processed amorphous thin strip member 1 into a shape within a target dimension is used.
  • That is, amorphous thin strip member 1 is processed to a large dimension in consideration of the contraction factor of amorphous thin strip member 1 due to the heat treatment . Amorphous thin strip member 1 processed to be larger is heat treated, contracted, and contained within the predetermined dimensional specification. In amorphous thin strip member 1, the movement of atoms becomes clear from about 100° C., and nanocrystal grains having a size of several tens of nanometers begin to be generated between about 370° C. to 500° C.
  • It takes several seconds or more for the treatment time to improve the magnetic characteristics, so the lower the temperature the longer it takes. The contraction factor is 0.6% at maximum in the uniaxial direction for a rectangular test piece, but the value varies depending on the heat treatment conditions. As the temperature of the heat treatment is higher or the heat treatment is longer, the movement amount of the atoms becomes larger, so that the contraction factor becomes larger.
  • The processing dimension is decided accordingly. Regarding the contraction factor, the influence of plate thickness is small. On the other hand, regarding the contraction factor, the influence of the shape is large, and the behavior of the contraction factor depending on the location is complicated depending on the shape. Since not only the contraction factor of each material itself but also the manner of connection of the materials are mutually restrained, the contraction factor is not uniform and varies from place to place.
  • It is the T-shaped portion that is teeth 1 a which needs to consider the contraction factor in order to improve the shape accuracy. A rotor, which is rotor 10, is inserted into the inner diameter portion. Therefore, when a gap between rotor 10 and end surface 30 of teeth 1 a is large, the motor efficiency is deteriorated, and when the gap is not constant, the rotation operation becomes unstable.
  • End surface 30 of a tip portion of teeth 1 a shows the most complicated contraction behavior. If the shape accuracy of teeth 1 a is poor, the motor characteristics also become unstable.
  • There are fitting holes 1 b at four positions around amorphous thin strip member 1. The position of each fitting hole 1 b is important because it affects the positional accuracy of the center of amorphous thin strip member 1 and the accuracy of a diameter of a space into which rotor 10 is inserted.
  • There is donut-like or hollow frame-shaped core back 1 c which connects the plurality of teeth 1 a and has fitting hole 1 b. The accuracy of core back 1 c may be lower than that of teeth 1 a or fitting hole 1 b in terms of the degree of rigidity. Process
  • Therefore, a shape close to the final shape is produced first, and heat treated. The ones subjected to heat treatment are measured and the contraction factor is determined. The contraction factor measured with different heat treatment conditions and the portion shape is between 0% to 0.6%. The contraction amount after the heat treatment is influenced by the nonuniformity such as the amorphous state in amorphous thin strip member 1, the plate thickness, the temperature during the heat treatment, and the like. There is a difference in the contraction amount even if the same treatment is carried out. However, if the maximum diameter is about 130 mm or less as in this embodiment, the accuracy is within ±0.01 mm. Laminate
  • FIG. 2A is a side view of thin strip component 3 in which thin strip component members 2 obtained by heat treating amorphous thin strip member 1 are laminated. FIG. 2B is a top view of thin strip component 3 in which thin strip component members 2 obtained by heat treating amorphous thin strip member 1 are laminated. In laminated thin strip component 3, heat treated thin strip component members 2 are laminated and fastened by nut 7 via spring washer 5 and washer 6 by bolt 4. Here, the fixation is four positions.
  • After laminating a plurality of or more amorphous thin strip members 1, amorphous thin strip members 1 may be heat treated and fastened by bolt 4 as shown in FIG. 2A to form laminated thin strip component 3.
  • Laminated thin strip component 3 is a magnetic laminate in which a plurality of plate-shaped thin strip component members 2 of the same shape are laminated.
    • Motor
  • FIG. 3A is a side view of a motor using laminated thin strip component 3, and FIG. 3B is a top view of the motor using laminated thin strip component 3. In laminated thin strip component 3 of FIGS. . 2A and 2B, nut 7 is removed at one end, metal base 8 is inserted under laminated thin strip component 3 and fastened again by nut 7.
  • Next, winding 9 is applied to laminated thin strip component 3 at a portion called teeth 1 a (FIG. 1) of thin strip component member 2 to make it a stator. Rotor 10 is installed in the inner diameter portion of laminated thin strip component 3. If electricity is supplied to winding 9 in this state, it can be driven as a motor.
    • Teeth 1 a
  • FIG. 4A is a cross-sectional view of a vicinity of end surface 30 of teeth 1 a of laminated thin strip component 3, and FIG. 4B is a front view of a vicinity of end surface 30 of teeth 1 a of laminated thin strip component 3.
  • As described in FIG. 1, the dimensional accuracy of thin strip component member 2 after heat treatment is within ±0.01 mm. In addition, misalignment in the plane tends to occur during the lamination. Even if the accuracy of the alignment is increased, unevenness occurs on end surface 30 due to the deviation of the dimensions caused by the heat treatment.
  • Dimensional variations a of the unevenness of FIG. 4A and dimensional variation of end surface 30 in dimensional variation b of the unevenness of FIG. 4B are both within ±0.1 mm. Since thin strip component member 2 is heat treated, it is possible to confirm visible oxide film 11 on end surface 30 in FIG. 4B. Oxidation does not progress and corrosion resistance improves due to the presence of oxide film 11.
    • Embodiment 2
  • FIG. 5 is a cross-sectional view of a vicinity of end surface 30 of teeth 1 a of laminated thin strip component 3 according to Embodiment 2 of the disclosure. Items not described are the same as those in Embodiment 1.
  • FIG. 5 is different from FIG. 4 in Embodiment 1 in that resin coating layer 12 is formed on end surface 30 of thin strip component members 2. Unevenness occurs on end surface 30 due to the difference in contraction amount of each thin strip component member 2. However, it is particularly important to improve the accuracy of mutual gap distance (distance between end surface 30 and rotor 10) in the inner diameter portion in which rotor 10 is rotated.
  • In order to solve the dimensional difference, resin coating layer 12 is formed on end surface 30. When resin coating layer 12 enters deeper into the interlayer of thin strip component members 2, the space factor becomes worse. Therefore, resin coating layer 12 is formed only on end surface 30 mainly. Since end surface 30 has unevenness, even if resin coating layer 12 is formed only in the vicinity of the surface of end surface 30, the bonding force can be sufficiently secured. Furthermore, if the surface of resin coating layer 12 is cut to form plane 31, the shape accuracy is further improved.
  • It is preferable to form resin coating layer 12 only on teeth 1 a portion of thin strip component 3.
    • Embodiment 3
  • FIG. 6A is a cross-sectional view of a vicinity of end surface 30 of teeth 1 a of laminated thin strip component 3 according to Embodiment 3 of the disclosure. FIG. 6B is a front view of the vicinity of end surface 30 of teeth 1 a of laminated thin strip component 3 according to Embodiment 3 of the disclosure. Items not described are the same as those in Embodiments 1 and 2.
  • FIG. 6A is different from FIG. 5 in Embodiment 2 in that the surface of resin coating layer 12 is cut to expose thin strip component members 2 from end surface 30 to form one plane 31. Although thin strip component members 2 can be brittle due to the heat treatment, by leaving a state in which the interlayer is bonded by resin coating layer 12 in end surface 30, it is possible to perform cutting without damaging thin strip component members 2.
  • By the cutting process, the unevenness amount of the cross section decreases, and cutting trace 13 having metallic luster remains as seen from the front.
  • This not only improves the accuracy of the gap distance between rotor 10 and end surface 30 in particular, but also makes it possible to reduce the gap distance with thin strip component members 2. As a result, the motor efficiency is further improved.
  • It is preferable to perform the above-described treatment only on teeth 1 a portion of thin strip component 3.
    • Embodiment 4
  • FIG. 7 is a view showing a cross-sectional configuration of a heat treatment device of laminated thin strip component 3 according to Embodiment 4 of the disclosure. Items not described are the same as those in Embodiments 1 to 3.
  • Laminate 14 of amorphous thin strip members 1 is sandwiched between pressure plates 15, and heated by heater 16 in pressure plate 15 so as to perform heat treatment while pressing. During the heat treatment process, the surface of oxide film 32 develops between amorphous thin strip members 1, and the entire or a portion of the members are mutually bonded to each other. As a result, since laminate 14 is integrated, the handling after heat treatment becomes easier.
  • Oxide film 32 is larger on the outside of laminate 14 than between inside amorphous thin strip member 1.
  • FIG. 8A is a cross-sectional view of a vicinity of end surface 30 of laminate 17 after the heat treatment, and FIG. 8B is a front view of the vicinity of end surface 30 of laminate 17 after the heat treatment. When the heat treatment is performed while pressing laminate 14 the above and below, there is frictional resistance against contraction at the boundary between pressure plate 15 and laminate 14.
  • Under the heat treatment conditions under which nanocrystal grains are generated, amorphous thin strip member 1 itself generates heat and the heat is accumulated on the central side of laminate 14, so that the temperature rises, and the contraction factor on the central side also increases. Due to these influences, the contraction amount in the center becomes large and recess 18 exists sometimes on end surface 30 of laminate 17 after heat treatment.
  • In the motor shown in FIGS. 3A and 3B, operation failure occurs when end surface 30 and rotor 10 come into contact with each other. Therefore, as shown in FIG. 8A, if the shape has recess 18, thin strip component members 2 at both upper and lower ends of laminate 17 serve as a reference, and the shape is regulated. As a result, there is an advantage that the accuracy can be easily secured.
  • Laminate 14 is a magnetic laminate in which the plurality of plate-shaped thin strip components 2 of the same shape are laminated, and is a thin strip component having recess 18 over the entire side surface of the magnetic laminate. As for the size of thin strip component member 2, thin strip component member 2 located outside laminate 14 has a larger size.
    • Embodiment 5
  • FIG. 9A is a cross-sectional view of a vicinity of end surface 30 of teeth 1 a of laminate 17 according to Embodiment 5 of the disclosure. FIG. 9B is a front view of the vicinity of end surface 30 of teeth 1 a of laminate 17 according to Embodiment 5 of the disclosure. Items not described are the same as those in Embodiment 4. In Embodiment 5, laminate 17 of Embodiment 4 is further processed to form one plane on the side surface.
  • FIGS. 9A and 9B are different from FIGS. 8A and 8B in Embodiment 4 in that the surface of end surface 30 is cut to form one plane 31. Although thin strip component members 2 can be brittle due to the heat treatment, this process is possible because the entire or a portion of the interlayer of thin strip component members 2 are bonded to each other by oxide film 32 by performing the heat treatment while pressing in the device of FIG. 7.
  • Accordingly, thin strip component members 2 in the vicinity of end surface 30 are fixed and can be cut without being damaged. By the cutting process, the unevenness amount of end surface 30 decreases, and cutting trace 13 having metallic luster remains as seen from the front. Cutting trace 13 is a line-shaped unevenness. Accordingly, the accuracy of the gap distance between rotor 10 and end surface 30 is particularly improved, so that the motor efficiency is improved.
    • As a Whole
  • The above-described embodiments can be combined. For example, Embodiments 2 and 3 maybe applied to the laminate produced in Embodiments 4 and 5.
  • Although teeth 1 a have been mainly described, it can be similarly applied to other parts of thin strip component members 2.
  • The thin strip component is an example and can be applied to other structures and shapes.
  • According to the thin strip component, the laminate, the method for manufacturing thereof, and the motor of the disclosure, it is possible to improve the shape accuracy and the magnetic characteristics of thin strip component, and the motor characteristics. Furthermore, the laminate according to the disclosure can also be applied to applications of electronic components such as transformers, other than motors.
    • REFERENCE SIGNS LIST
    • 1 AMORPHOUS THIN STRIP MEMBER
    • 1 a TEETH
    • 1 b FITTING HOLE
    • 1 c CORE BACK
    • 2 THIN STRIP COMPONENT MEMBER
    • 3 THIN STRIP COMPONENT
    • 4 BOLT
    • 5 SPRING WASHER
    • 6 WASHER
    • 7 NUT
    • 8 METAL BASE
    • 9 WINDING
    • a DIMENSIONAL VARIATION
    • b DIMENSIONAL VARIATION
    • 10 ROTOR
    • 11 OXIDE FILM
    • 12 RESIN COATING LAYER
    • 13 CUTTING TRACE
    • 14 LAMINATE
    • 15 PRESSURE PLATE
    • 16 HEATER
    • 17 LAMINATE
    • 18 RECESS
    • 30 END SURFACE
    • 31 PLANE

Claims (10)

What is claimed is:
1. A method for manufacturing a thin strip component, comprising:
a processing step of processing an amorphous thin strip member into a dimension shape larger than a target shape; and
a heat treating step of heat treating and contracting the amorphous thin strip member processed in the processing step to form the amorphous thin strip member into a thin strip component member of the target shape.
2. The method for manufacturing a thin strip component of claim 1, further comprising:
a laminating step of laminating a plurality of the thin strip component members after the heat treating step.
3. A method for manufacturing a thin strip component of claim 1, comprising:
a processing step of processing an amorphous thin strip into a dimension shape larger than a target shape;
a laminating step of laminating the amorphous thin strips processed in the processing step; and
a heat treating step of heat treating and contracting a laminate of the amorphous thin strips after the laminating step to form the amorphous thin strips into a laminated thin strip component members of the target shape.
4. The method for manufacturing a thin strip component of claim 3,
wherein, in the heat treating step, the heat treatment is performed while pressing the laminated amorphous thin strip in a lamination direction.
5. The method for manufacturing a thin strip component of claim 3,
wherein, in the heat treating step, the laminated thin strip component members are bonded to each other.
6. The method for manufacturing a thin strip component of claim 3,
wherein, in the heat treating step, a side surface of the laminated thin strip component members is recessed.
7. The method for manufacturing a thin strip component of claim 1,
wherein the amorphous thin strip member having a dimension larger than the target shape is larger than 0% of the target shape and 0.6% or less than the target shape.
8. The method for manufacturing a thin strip component of claim 1,
wherein the processing of the amorphous thin strip into the dimension shape larger than the target shape further includes the dimension shape depending on a location of the amorphous thin strip member.
9. The method for manufacturing a thin strip component of claim 1,
wherein the processing of the amorphous thin strip into the dimension shape larger than the target shape further includes the dimension shape depending on a condition of the heat treating step.
10. The method for manufacturing a thin strip component of claim 9,
wherein the amorphous thin strip member having a dimension larger than the target shape is increased in dimension as a temperature in the heat treating step is higher or a time in the heat treating step is longer.
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EP3584332A4 (en) 2019-12-25
CN109642265A (en) 2019-04-16
WO2018150807A1 (en) 2018-08-23
EP3584332B1 (en) 2023-05-10
CN109642265B (en) 2021-06-18
US20190173329A1 (en) 2019-06-06
US10862354B2 (en) 2020-12-08

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