Laminated core, and manufacturing device and method thereof
The manufacturing method and apparatus for laminated cores, which involves controlled pressurization and heating of core sheets with a thermosetting adhesive layer, effectively reduces compressive residual stress and iron loss, resulting in a more efficient laminated core.
Patent Information
- Application Number
- JP2024551647
- Authority / Receiving Office
- JP · JP
- Patent Type
- Patents
- Current Assignee / Owner
- Priority Date
- 2023-05-26
- Filing Date
- 2024-05-27
- Publication Date
- 2025-05-21
- Estimated Expiration
- 2044-05-27
Smart Images

Figure 0007680704000002 
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Abstract
Description
[Technical field]
[0001] The present invention relates to a laminated core, and an apparatus and method for manufacturing the same. [Background technology]
[0002] Conventionally, laminated cores having a configuration in which a plurality of electromagnetic steel sheets are laminated have been used as cores for rotating electrical machines, etc. As one method for manufacturing laminated cores, a method is known in which a core sheet of a predetermined shape is punched out of a steel strip to which an adhesive is applied, and the obtained plurality of core sheets are bonded to each other to manufacture the laminated core.
[0003] For example, in the manufacturing method of a laminated core disclosed in Patent Document 1, thin core sheets punched out of a strip-shaped steel sheet by a contour punching punch are forced into a contour punching die. The thin core sheets forced into the contour punching die are stacked on top of the previously punched thin core sheets, and are successively forced into a squeeze ring below the contour punching die. The thin core sheets forced into the squeeze ring are pressed against the inner peripheral surface of the squeeze ring while moving, thereby adhering to each other. At this time, the adhesive between each thin core sheet is hardened by the heat of the heater, and a laminated core is formed in which a predetermined number of thin core sheets are fixed together. [Prior art documents] [Patent documents]
[0004] [Patent Document 1] JP 2009-297758 A Summary of the Invention [Problem to be solved by the invention]
[0005] The method disclosed in Patent Document 1 allows the punching of the thin core plates by the punching die and the application of pressure and heat to the multiple thin core plates in the squeeze ring to be carried out continuously, which makes it possible to efficiently manufacture laminated cores.
[0006] However, as a result of research by the present inventors, it has been found that when pressurizing and heating a plurality of iron core thin plates simultaneously as described above, compressive residual stress may occur in the obtained laminated iron core, and the iron loss may increase.
[0007] Therefore, an object of the present invention is to provide a laminated core with low iron loss, as well as a manufacturing method and a manufacturing apparatus thereof.
Means for Solving the Problems
[0008] The laminated core according to an embodiment of the present invention is a laminated core in which a plurality of electromagnetic steel sheets are laminated via an adhesive layer, characterized in that an iron loss deterioration rate of the laminated core with respect to two layers of electromagnetic steel sheets separated from the laminated core is 10% or less.
[0009] A plurality of convex portions protruding outward in the lamination direction may be formed on the electromagnetic steel sheet at one end in the lamination direction of the laminated core.
[0010] The manufacturing method of a laminated core according to an embodiment of the present invention is In a manufacturing apparatus including a punch, a punching die disposed below the punch, a first holding portion disposed below the punching die, a second holding portion disposed below the first holding portion, and a heating portion disposed around the second holding portion, a plurality of core sheets are punched out from a steel strip having a thermosetting adhesive layer on its surface by the punch and the punching die, while laterally pressurizing the outer peripheral portions of the plurality of punched core sheets by the first holding portion, the plurality of core sheets are pressurized downward by the punch, the plurality of core sheets pressurized downward by the punch are heated by the heating portion while being held in the second holding portion, in the first holding portion, the plurality of core sheets are held at a temperature lower than the softening temperature of the adhesive layer, The heating section heats the plurality of core sheets held in the second holding section to a temperature equal to or higher than the softening temperature of the adhesive layer.
[0011] Moreover, an apparatus for manufacturing a laminated core according to an embodiment of the present invention includes: An apparatus for manufacturing a laminated core by punching out a plurality of core sheets from a steel strip having an adhesive layer on its surface and bonding the obtained plurality of core sheets to each other, comprising: punch, A punching die disposed below the punch; A first holding portion disposed below the punching die; A second holding portion disposed below the first holding portion; and A heating unit disposed around the second holding unit; Equipped with punching a plurality of core sheets from the steel strip with the punch and the punching die; The punch presses the outer periphery of the punched core sheets from the side by the first holding part, while pressing the core sheets downward by the punch; The plurality of core sheets pressed downward by the punch are heated by the heating unit while being held in the second holding unit, In the first holding section, the plurality of core sheets are held at a temperature lower than the softening temperature of the adhesive layer, The heating section heats the plurality of core sheets held in the second holding section to a temperature equal to or higher than the softening temperature of the adhesive layer.
[0012] The portion of the first holding portion that comes into contact with the core sheet may have a vertical length of 5 mm or more.
[0013] The punch may press the plurality of core sheets with a pressure of 2.0 MPa or less.
[0014] The heating section may include an infrared heating device. Effect of the Invention
[0015] According to the present invention, a laminated core with low core loss is obtained. [Brief description of the drawings]
[0016] [Figure 1] FIG. 1 is a schematic cross-sectional view showing a laminated core manufacturing apparatus according to a first embodiment of the present invention. [Diagram 2] FIG. 2 is an enlarged cross-sectional view showing the vicinity of the surface of the steel strip. [Diagram 3] FIG. 3 is a diagram for explaining a method for measuring iron loss. [Figure 4] FIG. 4 is a diagram for explaining a method for manufacturing a laminated core according to the first embodiment of the present invention. [Diagram 5] FIG. 5 is a diagram for explaining a method for manufacturing a laminated core according to the first embodiment of the present invention. [Figure 6] FIG. 6 is a diagram for explaining a method for manufacturing a laminated core according to the first embodiment of the present invention. [Figure 7] FIG. 7 is a diagram showing a modified example of the manufacturing apparatus. [Figure 8] FIG. 8 is a diagram showing another modified example of the manufacturing apparatus. [Figure 9] FIG. 9 is a diagram showing another modified example of the manufacturing apparatus. [Figure 10] FIG. 10 is a diagram showing a modified example of the laminated core. [Figure 11] FIG. 11 is a schematic cross-sectional view showing a laminated core manufacturing apparatus according to the second embodiment of the present invention. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0017] DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS A laminated core and a manufacturing apparatus and method thereof according to embodiments of the present invention will now be described with reference to the drawings.
[0018] (First embodiment) FIG. 1 is a schematic cross-sectional view showing a manufacturing apparatus for a laminated core according to a first embodiment of the present invention. The manufacturing apparatus 100 is an apparatus for manufacturing a laminated core 2 by punching out a plurality of core sheets 1a from a steel strip 1 conveyed in a predetermined direction and bonding the obtained plurality of core sheets 1a to each other. In this embodiment, the laminated core 2 has a cylindrical shape and is used as a stator core in a rotating electric machine. The laminated core 2 may be a laminated core used as a rotor core in a rotating electric machine. The laminated core 2 may be one of a plurality of divided cores constituting a stator core. The laminated core 2 may be a core of a device other than a rotating electric machine.
[0019] Below, the steel strip 1 will be briefly described, followed by a detailed description of the laminated core 2 and the manufacturing apparatus 100. Figure 2 is an enlarged cross-sectional view showing the vicinity of the surface of the steel strip 1.
[0020] As shown in FIG. 2, the steel strip 1 includes a base steel sheet 11a and an adhesive layer 11b. In this embodiment, a non-oriented electromagnetic steel sheet is used as the base steel sheet 11a, but an oriented electromagnetic steel sheet may also be used as the base steel sheet 11a. In this specification, the electromagnetic steel sheet means the base material portion (base steel sheet) excluding the insulating coating and the like. The adhesive layer 11b is formed on the surface of the base steel sheet 11a. In this embodiment, the adhesive layer 11b is formed on both sides of the base steel sheet 11a, but the adhesive layer 11b may be formed on only one surface of the base steel sheet 11a.
[0021] The chemical composition of the base steel sheet 11a contains basic elements, optional elements as necessary, and the balance being Fe and impurities. In this embodiment, the chemical composition of the base steel sheet 11a contains, for example, in mass %, as basic elements: Si: 1.0 to 4.5%, Al: 0.1 to 1.5%, and Mn: 0.2 to 4.0%.
[0022] The adhesive layer 11b is formed so as to cover the entire surface of the base steel plate 11a. A thermosetting resin is used as the adhesive layer 11b. In this embodiment, the adhesive layer 11b has an insulating performance in addition to an adhesive function. In this embodiment, the adhesive layer 11b is, for example, an insulating coating containing an epoxy resin and an epoxy resin curing agent.
[0023] As the epoxy resin, for example, an epoxy resin having two or more epoxy groups in one molecule can be used. As such epoxy resin, for example, bisphenol A type epoxy resin, bisphenol F type epoxy resin, phenol novolac type epoxy resin, cresol novolac type epoxy resin, alicyclic epoxy resin, glycidyl ester type epoxy resin, glycidyl amine type epoxy resin, hydantoin type epoxy resin, isocyanurate type epoxy resin, acrylic acid modified epoxy resin (epoxy acrylate), phosphorus-containing epoxy resin, and their halides (brominated epoxy resin, etc.) or hydrogenated products can be mentioned. As the epoxy resin, one type may be used alone, or two or more types may be used in combination.
[0024] Examples of epoxy resin curing agents include aromatic polyamines, acid anhydrides, phenolic curing agents, dicyandiamide, boron trifluoride-amine complexes, and organic acid hydrazides. Examples of aromatic polyamines include metaphenylenediamine, diaminodiphenylmethane, and diaminodiphenylsulfone. Examples of phenolic curing agents include phenol novolac resins, cresol novolac resins, bisphenol novolac resins, triazine-modified phenol novolac resins, and phenol resol resins. Examples of epoxy resin curing agents include phenolic curing agents, and more preferably phenol resol resins. Examples of epoxy resin curing agents include one type alone, and two or more types may be used in combination.
[0025] Although a detailed description is omitted, the adhesive layer 11b may be, for example, an insulating coating containing an acrylic resin and an acrylic resin curing agent.
[0026] Although detailed description is omitted, another insulating coating may be formed between the base steel sheet 11a and the adhesive layer 11b. Examples of the material constituting the insulating coating include (1) inorganic compounds, (2) organic resins, and (3) mixtures of inorganic compounds and organic resins. Examples of the inorganic compounds include (1) composites of dichromate and boric acid, (2) composites of phosphate and colloidal silica, (3) phosphates, (4) Zr compounds, and (5) Ti compounds. Examples of the organic resins include epoxy resins, acrylic resins, acrylic styrene resins, polyester resins, silicone resins, and fluororesins.
[0027] (Laminated core configuration) As described above, the laminated core 2 has a configuration in which a plurality of core sheets 1a punched out from a steel strip 1 are laminated. More specifically, the laminated core 2 has a configuration in which a plurality of base steel sheets (electromagnetic steel sheets) 11a punched out into a predetermined shape are laminated and bonded to each other with adhesive layers 11b. The laminated core is obtained, for example, by laminating a plurality of core sheets 1a each having an adhesive layer 11b formed on its surface, applying pressure, heating, etc., and adhering and fixing the core sheets 1a to each other via the adhesive layers 11b.
[0028] (Method of measuring iron loss deterioration rate) In this embodiment, the laminated core 2 is manufactured so that the iron loss deterioration rate of the laminated core 2 is 10% or less with respect to the two layers (two sheets in this embodiment) of base steel plate 11a (core sheet 1a) taken out from the laminated core 2. The iron losses of the laminated core 2 and the two layers of base steel plate 11a are measured as follows.
[0029] First, the iron loss of the laminated core 2 is measured. As described above, the laminated core 2 used for the measurement may have a configuration in which a plurality (two or more) of base steel sheets (electromagnetic steel sheets) 11a punched into a predetermined shape are laminated and bonded to each other with adhesive layers 11b. The laminated core 2 may be obtained, for example, by the method described above, and may be subjected to a predetermined heat treatment (strain relief annealing, etc.). The dimensions of the laminated core used for the measurement are not particularly limited. The number of layers of the electromagnetic steel sheets constituting the laminated core is also not particularly limited, and a laminated core made of, for example, two electromagnetic steel sheets may be used. In this embodiment, the iron loss W of the laminated core 2 is measured using a magnetic property measuring device (BST-L) manufactured by BROCKHAUS. 15 / 50 Measure (W / kg).
[0030] Next, the two-layer core sheet 1a to be measured for iron loss is taken out from the laminated core 2. The two-layer core sheet 1a to be measured is two core sheets separated from the laminated core 2 by a method described later and the adhesive layer is removed. As described above, in this embodiment, the laminated core 2 has a cylindrical shape, and each core sheet 1a has an annular shape. Therefore, in this embodiment, the two core sheets 1a on the front side of the laminated core 2 are the two-layer core sheets 1a to be measured for iron loss. Note that the two-layer core sheet 1a (two in this embodiment) to be measured for iron loss is preferably the two-layer core sheet 1a on one side in the thickness direction of the laminated core 2, or the two-layer core sheet 1a on the other side in the thickness direction of the laminated core 2. However, as shown in FIG. 10 described later, when a convex portion 3 for separating a plurality of laminated cores 2 is formed, the two-layer core sheet 1a on the side where the convex portion 3 is not formed is the object to be measured for iron loss. The dimensions of the two-layer core sheet 1a that is the subject of iron loss measurement are not particularly limited, but the core sheet 1a that is removed from the laminated core 2 by a method to be described later may be used as is.
[0031] In this embodiment, the laminated core 2 is heated in a heating furnace at 400°C for 12 hours to carbonize the adhesive layer 11b, and the two core sheets 1a on the surface side of the laminated core 2 are separated. The surfaces of the two core sheets 1a separated from the laminated core 2 are then washed with acetone to completely remove the adhesive layer 11b from the surface of each core sheet 1a. Thereafter, the two core sheets 1a (base steel plates 11a) from which the adhesive layer 11b has been removed are overlapped, and the iron loss W is measured using a magnetic property measuring device (BST-L) manufactured by BROCKHAUS. 15 / 50 (W / kg) is measured. When the two core sheets 1a are separated from the laminated core 2 and the adhesive layer 11b is removed as described above, the compressive residual stress imparted to the core sheet 1a by the pressure and heat treatment during the laminated core manufacturing process and by the adhesive layer 11b during bonding can be removed while preventing an increase in the iron loss of the base steel plate 11a (core sheet 1a) during separation of the core sheet 1a and removal of the adhesive layer 11b. Therefore, the iron loss of the two base steel plates 11a separated from the laminated core 2 and having the adhesive layer 11b removed as described above is considered to be equivalent to the iron loss of the two core sheets 1a (base steel plates 11a) before being bonded to each other. By calculating the iron loss deterioration rate of the laminated core 2 based on the two core sheets 1a (base steel plates 11a), the influence of the pressure and heat treatment during the laminated core 2 manufacturing process and the iron loss deterioration caused by the adhesive layer 11b can be appropriately evaluated.
[0032] If the adhesive layer 11b cannot be removed by the above heating conditions, the laminated core 2 is immersed in a solvent to dissolve the adhesive layer 11b and separate the two core sheets 1a on the surface side of the laminated core 2. In this case, the compressive residual stress generated in the base steel plate 11a during the manufacturing (bonding) of the laminated core can be removed while preventing the iron loss of the base steel plate 11a from increasing. The solvent to be used may be determined according to the components of the adhesive layer 11b. For example, when an epoxy resin is used as the adhesive layer 11b, a ketone solvent (anone, methyl ethyl ketone, etc.) can be used. The components of the adhesive layer 11b can be inspected by a known method. Also, a known solvent can be used as the solvent for dissolving the adhesive layer 11b.
[0033] In the laminated core 2 according to this embodiment, the iron loss deterioration rate of the laminated core 2 relative to the iron loss of the two-layer (two sheets in this embodiment) base steel plate 11a measured as described above is 10% or less. Specifically, the iron loss deterioration rate calculated by the following formula (a) is 10% or less. Iron loss degradation rate (%) = ((iron loss of laminated core - iron loss of two-layer base steel plate) / iron loss of two-layer base steel plate) × 100 (a)
[0034] If the laminated core is one of multiple split cores that make up a stator, the iron loss of the laminated core is measured as follows. As shown in Fig. 3(a), if a closed magnetic circuit can be formed by one split core 2a and the U-shaped measuring head 5 of the magnetic property measuring device, the iron loss measured for the split core 2a alone is taken as the iron loss of the laminated core. In this case, the iron loss of the two core sheets on the surface side separated from the split core 2a is taken as the iron loss of the two-layer base steel plate.
[0035] On the other hand, as shown in Fig. 3(b), when a closed magnetic circuit cannot be formed by one split core 2b and the measuring head 5, multiple split cores 2b are connected so that a closed magnetic circuit can be formed. The iron loss measured with multiple split cores 2b connected is regarded as the iron loss of the laminated core. In this case, the two core sheets on the front side are separated from each split core 2b, and the separated multiple core sheets (six in this example) are connected in the same manner as in Fig. 3(b), and the iron loss measured is regarded as the iron loss of the two-layer base steel plate.
[0036] When the split core is assembled as a stator core of a rotating electrical machine, the stator core is first removed from the rotating electrical machine and disassembled into a plurality of split cores. Then, the iron loss is measured by the method described above with reference to FIG. 3(a) or FIG. 3(b).
[0037] (Configuration of manufacturing equipment) Next, the manufacturing apparatus 100 will be described in detail. As shown in FIG. 1, the manufacturing apparatus 100 according to this embodiment includes a base unit 10, a punch 12, a punching die 14, a first holding unit 16, a second holding unit 18, and a heating unit 20. Although not shown, in the manufacturing apparatus 100, predetermined processing (such as forming slots) is performed on the steel strip 1 by other punches and dies, etc., also upstream of the punch 12 and the punching die 14 in the conveying direction of the steel strip 1. For example, as shown in FIG. 10 described later, when a plurality of convex portions 3 are formed on the uppermost core sheet 1a (base steel plate 11a) of the laminated core 2, press processing is performed to form the convex portions on the area of the steel strip 1 that is to be punched out as the core sheet 1a having the convex portions 3.
[0038] The punch 12 is disposed above the base portion 10 so as to be movable up and down. The punching die 14 is disposed below the punch 12. The punching die 14 has a cylindrical shape corresponding to the outer shape of the laminated core 2. In this embodiment, an opening edge 14a on the upper end side of the punching die 14 functions as a cutting blade. In this embodiment, the opening edge 14a has a circular shape. In this embodiment, the punch 12 and the punching die 14 repeatedly perform outer shape punching processing on the steel strip 1 transported in a predetermined direction, and multiple core sheets 1a are punched out from the steel strip 1.
[0039] 1, an imaginary line A that passes through the center of the opening edge 14a of the punching die 14 and extends in the vertical direction is shown by a dashed line. In the following, the radial direction means a direction perpendicular to the imaginary line A. In addition, in the following, the circumferential direction means a circumferential direction of an imaginary circle centered on the center of the opening edge 14a when viewed from above.
[0040] The first holding portion 16 is disposed below the punching die 14. In this embodiment, the first holding portion 16 is fixed to the base portion 10 using an attachment member (not shown). In this embodiment, the first holding portion 16 includes a plurality of holding members 16a and a plurality of pressing devices 16b.
[0041] The multiple holding members 16a are arranged in a line in the circumferential direction. Each holding member 16a is provided so as to be movable in the radial direction. A pressing device 16b is provided for each holding member 16a. The pressing device 16b is a device that moves the holding member 16a in the radial direction. In this embodiment, the pressing device 16b includes, for example, a hydraulic device, and moves the pressing device 16b in the radial direction by hydraulic pressure.
[0042] The first holding section 16 may be configured so as to pressurize the core sheets 1a punched by the punch 12 and the punching die 14 from the side (outside in the radial direction). Therefore, for example, any one of the multiple holding members 16a may be fixed so as not to move in the radial direction. In this case, the pressing device 16b does not need to be connected to the fixed holding member 16a. The configuration of the first holding section is not limited to the above example, and the first holding section can be configured using the configuration of various known squeeze rings.
[0043] The second holding portion 18 is disposed below the first holding portion 16. In this embodiment, the second holding portion 18 is configured by a member separate from the first holding portion 16. In this embodiment, the second holding portion 18 is provided coaxially with the first holding portion 16. In this embodiment, the second holding portion 18 has a plurality of holding members 18a that are provided so as to be movable in the radial direction. Although not shown, a biasing device is provided for each holding member 18a. In this embodiment, the biasing device includes, for example, an elastic member such as a spring, and biases the holding member 18a toward the radial inside (the imaginary line A side). The configuration of the second holding portion is not limited to the above example, and the second holding portion can be configured by utilizing the configuration of various known squeeze rings. For example, each holding member 18a may be configured by a plurality of members that are stacked in the vertical direction and connected to each other.
[0044] The heating unit 20 is disposed around the second holding unit 18. In this embodiment, the heating unit 20 is provided below the first holding unit 16. In this embodiment, the heating unit 20 includes a plurality of heating devices 20a. For example, an infrared heating device is used as the heating device 20a. In this embodiment, a heating device 20a is provided for each holding member 18a. The configuration of the heating unit 20 is not limited to the above example, and various heating devices capable of heating the second holding unit 18 (holding member 18a) or the core sheet 1a held by the second holding unit 18 can be used as the heating unit. For example, a high-frequency induction heating device provided to surround the second holding unit 18 may be used as the heating unit.
[0045] (Manufacturing method of laminated core) Next, a description will be given of a manufacturing method of the laminated core 2 using the above-mentioned manufacturing apparatus 100. In this embodiment, a steel strip 1 is fed in a predetermined direction from a coil (hoop material) (not shown) by a feed mechanism (rollers, etc.) (not shown), while a plurality of core sheets 1a are punched out of the steel strip 1 by a punch 12 and a punching die 14 (opening edge 14a).
[0046] As shown in Fig. 4, a plurality of punched core sheets 1a are stacked in sequence in a punching die 14. Note that, although the outer periphery of the core sheet 1a punched from the steel strip 1 comes into contact with the inner peripheral surface of the punching die 14, in this embodiment, the punching die 14 does not apply a large pressure to the core sheet 1a. Therefore, the core sheet 1a punched from the steel strip 1 by the punch 12 and the punching die 14 (opening edge 14a) moves downward within the punching die 14 without being held by the inner peripheral surface of the punching die 14.
[0047] 5, by punching out more core sheets 1a from the steel strip 1, a plurality of core sheets 1a are successively pushed into the first holding portion 16. In this embodiment, each time a new core sheet 1a is punched out by the punch 12 and the punching die 14, one core sheet 1a is pushed from the punching die 14 into the first holding portion 16.
[0048] As described above, the first holding section 16 is configured to be able to pressurize the core sheet 1a from the side (radial outside). In this embodiment, the state in which the multiple core sheets 1a are pressed from the side is maintained in the first holding section 16. Therefore, the pressure generated between the vertically adjacent core sheets 1a by the punch 12 pressing the multiple core sheets 1a downward can be maintained in the first holding section 16. As a result, the multiple core sheets 1a are pressed in the vertical direction, and the vertically adjacent base steel plates 11a are pressure-bonded via the adhesive layer 11b in the first holding section 16. In this embodiment, a pressure greater than the pressure generated between the vertically adjacent core sheets 1a by the weight of the multiple core sheets 1a can be generated and maintained between the vertically adjacent core sheets 1a in the first holding section 16. In addition, the core sheets 1a adjacent to each other in the vertical direction pressurized in the first holding section 16 are fixed with a force (adhesive force) weaker than that of the core sheets 1a after being heated and pressurized in the second holding section 18 described later. That is, in the first holding section 16, the core sheets 1a adjacent to each other in the vertical direction are bonded (temporarily bonded). In addition, the pressure applied from the punch 12 to the multiple core sheets 1a is preferably set to 2.0 MPa or less, and more preferably close to the pressure required to punch the core sheets 1a (punching pressure: for example, about 0.1 MPa). The pressure may be set to, for example, 1.8 MPa or less, or 1.0 MPa or less. It may also be set to 0.1 MPa or more. In addition, the pressure applied from the first holding section 16 (in this embodiment, the holding member 16a) to the outer periphery of the core sheet 1a is set to, for example, a magnitude that can prevent the core sheet 1a from falling. In this embodiment, the pressure is set so that the static friction force generated between the core sheet 1a and the first holding portion 16 is greater than the weight of the core sheet 1a.
[0049] As described above, no large pressure is applied to the core sheet 1a from the inner peripheral surface of the punching die 14. Therefore, even if pressure is generated between adjacent core sheets 1a in the vertical direction in the punching die 14 as a result of the punch 12 applying downward pressure to the multiple core sheets 1a, this state is not maintained. Therefore, the multiple core sheets 1a are not pressure-bonded to each other in the punching die 14.
[0050] In this embodiment, the first holding section 16 holds the multiple core sheets 1a at a temperature lower than the softening temperature of the adhesive layer 11b. This prevents the adhesive layer 11b between a pair of base steel sheets 11a adjacent to each other in the vertical direction from softening before the pair of base steel sheets 11a are pressure-bonded in the first holding section 16. When the multiple core sheets 1a are held in the first holding section 16 at a temperature lower than the softening temperature of the adhesive layer 11b, even when the multiple core sheets 1a are simultaneously pressurized and heated, the compressive residual stress generated in the obtained laminated core can be reduced and an increase in iron loss can be suppressed. In addition, the holding temperature of the multiple core sheets 1a in the first holding section 16 is not limited as long as it is lower than the softening temperature of the adhesive layer 11b, but can be, for example, a temperature 10°C or more lower than the softening temperature of the adhesive layer 11b, and may be a temperature 30°C or more lower than the softening temperature of the adhesive layer 11b. The lower limit of the above-mentioned holding temperature in the first holding section 16 is not particularly limited, but may be, for example, 0°C or higher, or about room temperature (20°C) or higher, or 40°C or higher. The holding temperature (temperature of the adhesive layer 11b) of the multiple core sheets 1a in the first holding section 16 can be measured by embedding a thermocouple thermometer or a radiation thermometer in the first holding section 16. In this embodiment, based on the holding temperature (temperature of the adhesive layer 11b) measured as described above, the output of the heating section 20 is controlled so that the temperature of the core sheet 1a (adhesive layer 11b) in the first holding section 16 is lower than the softening temperature. In addition, the length of the first holding section 16 in the vertical direction may be adjusted, or a heat insulating section may be provided at the boundary between the first holding section 16 and the second holding section 18. In addition, a heating test of the heating section 20 may be performed in advance to simulate the temperature rise behavior of the adhesive layer 11b due to heating by the heating section 20. Then, based on the temperature rise behavior of the adhesive layer 11b obtained by the simulation, the output of the heating section 20 may be controlled. The temperature within the first holding portion 16 may rise due to the influence of the temperature within the second holding portion that is provided continuously from the first holding portion 16, but the above-mentioned method can be used to control the temperature within the first holding portion 16 to be below the softening temperature of the adhesive layer 11b.In this embodiment, the holding temperature in the first holding section 16 only needs to be lower than the softening temperature of the adhesive layer 11b, and the effect of this embodiment is not affected by the presence or absence of a heating section in the first holding section 16 and the presence or absence of intentional heating of the core sheet 1a. On the other hand, from the viewpoint of further reducing the compressive residual stress generated in the core sheet 1a, it is preferable that the first holding section 16 suppresses the heating of the multiple core sheets 1a. For example, in order to simplify the device and further reduce the compressive residual stress generated in the core sheet 1a, it is preferable not to provide the heating section 20 in the first holding section 16. For this reason, in this embodiment, the heating section 20 is positioned below the lower end of the first holding section 16.
[0051] In order to prevent the adhesive layer 11b between a pair of vertically adjacent core sheets 1a (base steel plates 11a) from softening before the pair of the base steel plates 11a is pressed against each other, the vertical length of the portion of the first holding portion 16 that contacts the core sheet 1a (the length of the holding member 16a in this embodiment) is preferably 5 mm or more, and more preferably 10 mm or more. The upper limit of the vertical length of the portion of the first holding portion 16 that contacts the core sheet 1a is not particularly limited, but may be, for example, 160 mm or less, or may be 20 mm or less. In this case, sufficient time can be secured for pressing the core sheets 1a together in the first holding portion 16, so that the core sheets 1a can be more appropriately pressed against each other before the adhesive layer 11b softens.
[0052] The softening temperature of the adhesive layer 11b can be measured by TMA (thermo-mechanical analysis). Specifically, a cut plate of 7 mm×7 mm or less is taken from the steel strip 1, and the softening temperature of the adhesive layer 11b is measured in a penetration mode using the taken cut plate. The needle load is set to 0.5 kgf to 2.0 kgf, and the heating rate is set to 15° C. / min. The needle load is adjusted appropriately based on the needle penetration depth. Specifically, first, a measurement is performed with a needle load of 0.5 kgf, and if the needle penetration depth does not match the thickness of the adhesive layer 11b, the needle load is increased so that the needle penetration depth and the thickness of the adhesive layer 11b match, and the measurement is performed again. For example, the needle load is set to 1.5 kgf and the measurement is performed again. The needle load for matching the needle penetration depth to the thickness of the adhesive layer 11b also changes depending on the hardness of the adhesive layer 11b.
[0053] 6, as more core sheets 1a are punched out from the steel strip 1, the multiple core sheets 1a are successively pushed into the second holding section 18. In this embodiment, each time a new core sheet 1a is punched out by the punch 12 and the punching die 14, one core sheet 1a is pushed from the first holding section 16 into the second holding section 18.
[0054] The core sheet 1a pressed into the second holding section 18 is heated by the heating section 20 and pressed by the punch 12 while being held from the side (radial outside) by the second holding section 18 (multiple holding members 18a). In this embodiment, the heating section 20 heats the multiple core sheets 1a held in the second holding section 18 to a temperature equal to or higher than the softening temperature of the adhesive layer 11b. As a result, the adhesive layer 11b of each core sheet 1a softens and hardens in the second holding section 18, and the multiple core sheets 1a are fixed to each other. In addition, the multiple core sheets 1a are pressed into the second holding section 18 one by one from the lower side, and are heated in order from the one pressed into the second holding section 18. Therefore, the multiple stacked core sheets 1a are heated in order from the one located on the lower side to the one located on the upper side, and are gradually heated from the lower side. In this embodiment, the heating unit 20 heats the second holding unit 18 so that the temperature of the adhesive layer 11b in the second holding unit 18 rises to a temperature equal to or higher than the softening temperature. In this embodiment, the pressure applied from the second holding unit 18 to the laminated core 2 from the side is set to a magnitude capable of preventing the laminated core 2 from falling. In this embodiment, the pressure is set so that the static friction force generated between the laminated core 2 and the second holding unit 18 is greater than the weight of the laminated core 2. The heating temperature in the second holding unit 18 may be a temperature equal to or higher than the softening temperature of the adhesive layer 11b, but may be, for example, a temperature 10°C or higher than the softening temperature of the adhesive layer 11b, or may be, for example, a temperature 40°C or higher than the softening temperature of the adhesive layer 11b. The upper limit of the heating temperature in the second holding unit 18 is not particularly limited, but may be, for example, 200°C or lower. Furthermore, when the adhesive forming the adhesive layer 11b is a thermosetting resin, the heating unit 20 heats the multiple core sheets 1a held by the second holding unit 18 to a temperature equal to or higher than the curing temperature of the adhesive layer 11b.
[0055] When an infrared heating device is used as the heating section 20, the temperature of each core sheet 1a can be gradually increased from the outer periphery toward the center. This allows the adhesive layer 11b of each core sheet 1a to be gradually cured from the outer periphery toward the center. In this case, it is possible to prevent the adhesive from leaking out from between the base steel plates 11a adjacent to each other vertically in the second holding section 18. From this viewpoint, it is preferable to use an infrared heating device as the heating section 20. In this embodiment, for example, an infrared heating device that radiates near-infrared rays having a wavelength of 750 to 1000 nm is used.
[0056] Finally, as shown in FIG. 1, the multiple core sheets 1a fixed to each other in the second holding section 18 are discharged from the second holding section 18 as the laminated core 2. In this manner, the laminated core 2 is obtained. In this embodiment, the thickness of the core sheet 1a (steel strip 1) is, for example, 0.1 mm to 0.5 mm, and the mass of the laminated core 2 is, for example, 0.1 kg to 6.0 kg. When manufacturing a larger laminated core 2, for example, a laminated core 2 with a mass exceeding 6.0 kg, it may be difficult to hold the laminated core 2 only with the force of the biasing device provided in the second holding section 18. In such a case, it is preferable to support the laminated core 2 from below by a supporting device 26, as shown in FIG. 9 described later.
[0057] (Effects of this embodiment) In the manufacturing apparatus 100 according to this embodiment, the first holding unit 16 holds the multiple core sheets 1a at a temperature lower than the softening temperature of the adhesive layer 11b. This makes it possible to prevent the adhesive layer 11b from softening before the core sheets 1a adjacent to each other in the vertical direction in the first holding unit 16 are pressed together, and makes it possible to reduce the compressive residual stress generated in the core sheets 1a by pressing and heating the multiple core sheets 1a.
[0058] Here, the inventors conducted detailed studies and found that when multiple core sheets 1a are simultaneously heated and pressurized at a temperature equal to or higher than the softening temperature of the adhesive layer 11b, residual stress in the compressive direction (residual stress in the radial inward direction) may occur in the core sheets 1a. Specifically, when multiple core sheets 1a are pressurized while being heated to a temperature equal to or higher than the softening temperature of the adhesive layer 11b, softening of the adhesive layer 11b between a pair of core sheets 1a adjacent in the vertical direction progresses before the pair of core sheets 1a is pressurized. In this case, residual stress in the compressive direction is likely to occur in the base steel plate 11a due to the difference in the amount of thermal expansion between the adhesive layer 11b and the base steel plate 11a above or below it, and the contraction of the adhesive layer 11b.
[0059] On the other hand, it was found that when adjacent core sheets 1a are first pressed while being held at a temperature below the softening temperature of the adhesive layer 11b, and then adjacent core sheets 1a are heated and pressed at a temperature equal to or higher than the softening temperature of the adhesive layer 11b to bond them together, the compressive residual stress generated in the core sheets 1a due to pressurization and heating can be reduced. In addition, when multiple core sheets 1a pressed in the vertical direction are heated in order from the lower core sheet 1a, the adhesive layer 11b and the base steel plates 11a above and below expand and contract so as to follow each other. In this case, the generation of compressive residual stress in the base steel plate 11a is further suppressed. Therefore, in the manufacturing apparatus 100 according to this embodiment, as described above, the first holding unit 16 pressurizes the multiple core sheets 1a while holding them at a temperature below the softening temperature of the adhesive layer 11b. After that, the second holding unit 18 heats and presses the multiple core sheets 1a at a temperature equal to or higher than the softening temperature of the adhesive layer 11b to bond and fix the multiple core sheets 1a together. This can prevent the adhesive layer 11b from softening before the core sheets 1a adjacent in the vertical direction are pressed together in the first holding section 16. As a result, the occurrence of compressive residual stress in each base steel plate 11a in the first holding section 16 can be suppressed, and the iron loss of the laminated core 2 can be reduced. In addition, in the manufacturing apparatus 100 according to this embodiment, the punching die 14, the first holding section 16, and the second holding section 18 are continuously arranged in the vertical direction. In this configuration, the multiple core sheets 1a pressed downward by the punch 12 are heated one by one from the lower side in the second holding section 18 to a temperature equal to or higher than the softening temperature of the adhesive layer 11b. In the second holding section 18, the multiple core sheets 1a are gradually heated from the lower side to a temperature equal to or higher than the softening temperature of the adhesive layer 11b, thereby reducing the compressive residual stress occurring in each base steel plate 11a, and further reducing the iron loss of the laminated core 2.
[0060] In addition, in order to obtain a laminated core of an appropriate shape, it is usually necessary to harden the adhesive layer while applying a large pressure of more than 2.0 MPa from the punch to the multiple core sheets. However, in this case, the frictional force between the adhesive layer and the base steel plate becomes large, and compressive residual stress occurs in the base steel plate, so that iron loss increases. In contrast, in this embodiment, the multiple core sheets 1a are heated while the outer peripheries of the multiple core sheets 1a are held (pressurized in this embodiment) from the sides in the second holding section 18. This makes it possible to harden the adhesive layer 11b between the multiple core sheets 1a (base steel plate 11a) without applying a large pressure to the multiple core sheets 1a in the stacking direction. In this case, it is possible to prevent the frictional force between the adhesive layer 11b and the base steel plate 11a from increasing, and it is possible to sufficiently suppress the generation of compressive residual stress in the base steel plate 11a. As a result, even if the pressure applied from the punch 12 to the multiple core sheets 1a is as low as 2.0 MPa or less, the multiple core sheets 1a can be properly bonded to obtain a laminated core 2 of an appropriate shape.
[0061] In the manufacturing apparatus 100 according to this embodiment, the first holding section 16 and the second holding section 18 are configured with different members. More specifically, a portion of the first holding section 16 that contacts the core sheet 1a (in this embodiment, the holding member 16a) and a portion of the second holding section 18 that contacts the core sheet 1a (in this embodiment, the holding member 18a) are configured with different members. This suppresses heat transfer from the second holding section 18 to the first holding section 16, suppressing a temperature rise in the first holding section 16. As a result, a temperature rise in the multiple core sheets 1a in the holding member 16a can be easily suppressed.
[0062] (Modification) In the above embodiment, a case where one adhesive layer 11b is provided on the surface of the base steel plate 11a has been described, but multiple layers (multiple types) of adhesive layers may be provided on the surface of the base steel plate. In this case, the first holding section holds multiple core sheets so that all of the adhesive layers have a temperature below the softening temperature. The heating section heats the multiple core sheets held in the second holding section so that all of the adhesive layers have a temperature equal to or higher than the softening temperature. The same applies to the embodiments described below.
[0063] In the above embodiment, the first holding portion 16 and the second holding portion 18 are provided independently of each other. However, as shown in FIG. 7, the first holding portion 16 and the second holding portion 18 may be connected to each other by a plurality of connecting portions 22. In this case, the first holding portion 16 and the second holding portion 18 can be interlocked, so that the configuration of the first holding portion 16 and the second holding portion 18 (the configuration for pressing the holding member 16a and the holding member 18a) can be simplified. The connecting portions 22 may be recesses and protrusions formed on the holding member 16a and the holding member 18a. In this case, for example, the holding member 16a and the holding member 18a can be fixed by crimping the recesses and the protrusions. The connecting portions 22 may be fastening members such as bolts and nuts.
[0064] In the above-described embodiment, the second holding portion 18 is disposed directly below the first holding portion 16, but as shown in FIG. 8, the first holding portion 16 and the second holding portion 18 may be connected via a heat insulating member 24 having a lower thermal conductivity than the holding member 18a (the portion of the second holding portion 18 that contacts the core sheet 1a). In this case, the transfer of heat from the second holding portion 18 to the first holding portion 16 can be sufficiently suppressed, and a rise in temperature of the first holding portion 16 can be sufficiently prevented. In this embodiment, the heat insulating member 24 constitutes a connecting portion that connects the first holding portion 16 and the second holding portion 18.
[0065] In the above embodiment, the multiple core sheets 1a are supported by applying pressure to the multiple core sheets 1a from the sides in the first holding section 16 and the second holding section 18, but as shown in Fig. 9, the multiple core sheets 1a may be further supported from below by a support device 26. This allows the multiple core sheets 1a to be supported more stably. The support device 26 is a device that supports the multiple core sheets 1a from below by, for example, hydraulic pressure or the elastic force of an elastic member such as a spring.
[0066] In the above embodiment, all the core sheets 1a (base steel plate 11a) constituting the laminated core 2 have the same shape, but the shape of the laminated core 2 is not limited to the above example, and the shape of some of the core sheets 1a of the laminated core 2 may be different from the shape of the other core sheets 1a. For example, as in the laminated core 2 shown in FIG. 10, a plurality of protrusions 3 protruding outward in the lamination direction may be formed on the core sheet 1a (base steel plate 11a) at one end in the lamination direction (the upper end in this embodiment). When a plurality of laminated cores 2 are continuously manufactured, the plurality of laminated cores 2 can be easily separated by forming a plurality of protrusions 3 on the core sheet 1a at the upper end of each laminated core 2 as described above. As a result, a plurality of laminated cores 2 can be efficiently manufactured.
[0067] Second embodiment Fig. 11 is a schematic cross-sectional view showing a laminated core manufacturing apparatus according to a second embodiment of the present invention. The manufacturing apparatus 100a according to this embodiment differs from the manufacturing apparatus 100 shown in Fig. 1 in that a first holding part 60 is provided instead of the first holding part 16, and a second holding part 80 is provided instead of the second holding part 18.
[0068] In this embodiment, the first holding section 60 has a plurality of holding members 16a and a plurality of pressing devices 16b, similar to the above-mentioned first holding section 16, and the second holding section 80 has a plurality of holding members 18a, similar to the above-mentioned second holding section 18. However, in this embodiment, the portion of the first holding section 60 that contacts the core sheet 1a and the portion of the second holding section 80 that contacts the core sheet 1a are made of the same material. Specifically, each holding member 16a and the holding member 18a located below it are made of the same material. In this embodiment, the holding member 16a is a portion that holds the plurality of core sheets 1a at a temperature lower than the softening temperature of the adhesive layer 11b. In addition, in this embodiment, the upper end of the holding member 18a is a portion that contacts the core sheet 1a when the temperature of the core sheet 1a reaches the softening temperature of the adhesive layer 11b.
[0069] In this embodiment, the vertical length of the portion of the first holding part 60 that contacts the core sheet 1a (the length of the holding member 16a in this embodiment) is preferably 5 mm or more, and preferably 10 mm or more. The vertical distance between the upper end of the portion of the first holding part 60 that contacts the core sheet 1a (the upper end of the holding member 16a in this embodiment) and the upper end of the heating part 20 is preferably 5 mm or more, and preferably 10 mm or more. In this embodiment, the pressure applied from the punch 12 to the multiple core sheets 1a is preferably set to 2.0 MPa or less, and may be set to 1.8 MPa or less, and is more preferably set to the pressure required to punch the core sheet 1a (punching pressure: for example, about 0.1 MPa). Therefore, the pressure applied from the punch 12 to the multiple core sheets 1a may be, for example, 0.1 MPa or more. Moreover, the pressure applied from the first holding part 60 (holding member 16a in this embodiment) to the outer periphery of the core sheet 1a is set to a magnitude that can prevent the core sheet 1a from falling. In this embodiment, the pressure is set so that the static friction force generated between the core sheet 1a and the first holding part 60 is larger than the weight of the core sheet 1a.
[0070] In the manufacturing apparatus 100a according to this embodiment, similarly to the manufacturing apparatus 100 according to the first embodiment described above, a plurality of core sheets 1a are punched out from a steel strip 1 by a punch 12 and a punching die 14. The punched-out plurality of core sheets 1a are pressed downward by the punch 12 while the outer periphery of the punched-out plurality of core sheets 1a is pressed from the side in the first holding section 60, thereby crimping the plurality of core sheets 1a. The plurality of core sheets 1a crimped in the first holding section 60 are heated in the second holding section 80 by the heating section 20 to a temperature equal to or higher than the softening temperature of the adhesive layer 11b. As a result, the adhesive layer 11b of each core sheet 1a is softened and hardened in the second holding section 80, and the plurality of core sheets 1a are fixed to each other. Thereafter, the plurality of core sheets 1a fixed to each other are discharged from the second holding section 80 as a laminated core 2.
[0071] In the manufacturing apparatus 100a according to this embodiment, the multiple core sheets 1a are also held at a temperature below the softening temperature of the adhesive layer 11b in the first holding unit 60. This makes it possible to prevent the adhesive layer 11b from softening before the core sheets 1a adjacent in the vertical direction are pressed together in the first holding unit 60. As a result, it is possible to suppress the occurrence of compressive residual stress in each base steel plate 11a, and to reduce the iron loss of the laminated core 2.
[0072] In addition, in the manufacturing apparatus 100a according to this embodiment, the first holding unit 60 and the second holding unit 80 can be interlocked, so that the configurations of the first holding unit 60 and the second holding unit 80 (configurations for pressing the holding member 16a and the holding member 18a) can be simplified. In the manufacturing apparatus 100a shown in FIG. 11, the pressing device 16b is attached to the holding member 16a, but the pressing device 16b may be attached to the holding member 18a. In this case, the pressing device 16b can move the holding member 16a in the radial direction via the holding member 18a.
[0073] In this embodiment, the multiple core sheets 1a are heated while the outer peripheries of the multiple core sheets 1a are held (pressurized in this embodiment) from the side in the second holding section 80. This allows the adhesive layer 11b between the multiple core sheets 1a (base steel plate 11a) to harden without applying a large pressure to the multiple core sheets 1a in the stacking direction. In this case, it is possible to prevent the friction force between the adhesive layer 11b and the base steel plate 11a from increasing, and to sufficiently suppress the occurrence of compressive residual stress in the base steel plate 11a. This allows the multiple core sheets 1a to be properly bonded together to obtain a laminated core 2 with an appropriate shape, even when the pressure applied from the punch 12 to the multiple core sheets 1a is as low as 2.0 MPa or less.
[0074] Although a detailed description is omitted, another holding portion (for example, a known squeeze ring) may be further provided below second holding portion 80.
[0075] The present invention will be described in more detail below with reference to examples, but the present invention is not limited to these examples. EXAMPLES
[0076] The laminated cores of Examples 1 to 7 and Comparative Examples 1 to 4 were manufactured using a manufacturing apparatus having a similar configuration to the manufacturing apparatus 100 shown in FIG. 1. The position of the heating unit 20 was adjusted appropriately. The laminated cores of Comparative Examples 5 and 6 were manufactured using a manufacturing apparatus having a similar configuration to the manufacturing apparatus 100 shown in FIG. 1 except that the first holding unit 16 was not provided. In both the examples and the comparative examples, the laminated cores were made of two annular core sheets. The holding temperature in the first holding unit 16 was a temperature that was increased due to the influence of the heating temperature of the adjacent second holding unit 18. A non-oriented electromagnetic steel sheet was used as the base steel sheet. The adhesive layer of the laminated cores of Examples 1 to 3 and 6 and Comparative Examples 1, 2 and 5 was formed of an epoxy resin and an amine-based hardener, and the adhesive layer of the laminated cores of Examples 4, 5 and 7 and Comparative Examples 3, 4 and 6 was formed of an acrylic resin and an amine-based hardener.
[0077] The iron loss deterioration rate was measured by the above-mentioned method for the laminated cores of Examples 1 to 7 and Comparative Examples 1 to 6. Specifically, first, the iron loss W 15 / 50 The laminated core was then heated in a heating furnace at 400°C for 12 hours to carbonize the adhesive layer, and the two core sheets of the laminated core were separated. The surfaces of the separated two core sheets were then washed with acetone to completely remove the adhesive layer from the surface of each core sheet, after which the two core sheets (base steel sheets) were stacked together, and the core loss W was measured using a magnetic property measuring device (BST-L) manufactured by BROCKHAUS. 15 / 50 (W / kg) was measured. The iron loss degradation rate of each laminated core of the examples and comparative examples was calculated by the above formula (a). When the iron loss of a laminated core with three or more layers manufactured under the same conditions is compared with that of a laminated core with two layers, the iron loss of the laminated core with two layers is usually larger. For this reason, the iron loss degradation rate of the laminated core with two layers was evaluated in the examples and comparative examples. When the iron loss degradation rate of a laminated core with two layers obtained by the above formula (a) is 10% or less, it is considered that the iron loss degradation rate of a laminated core with three or more layers manufactured under the same conditions as the laminated core is also 10% or less. The magnetic flux density during the iron loss measurement was set to 1.5T, and the frequency was set to 50Hz. The type of resin of the adhesive layer, the softening temperature of the adhesive layer, the manufacturing conditions of the laminated core, the measurement results of the iron loss, and the calculation results of the iron loss degradation rate are shown in Table 1 below.
[0078] [Table 1]
[0079] The softening temperature of the adhesive layer in Table 1 was measured by TMA (thermo-mechanical analysis) using a cut sheet taken from the steel strip that is the material of the core sheet. The holding temperature of the first holding section in Table 1 means the maximum temperature of the core sheet in the first holding section 16. The heating temperature of the second holding section in Table 1 means the maximum temperature of the core sheet in the second holding section 18. However, for Comparative Examples 5 and 6, the heating temperature of the second holding section means the temperature of the core sheet at the upper end in the second holding section 18. In Comparative Examples 1 to 4, the minimum temperatures of the core sheet in the first holding section 16 were all equal to or higher than the softening temperature. The temperature of the core sheet in the first holding section 16 was measured by arranging a plurality of thermocouple thermometers in the first holding section 16 so as to be aligned vertically. Similarly, a plurality of thermocouple thermometers were arranged in the second holding section 18 so as to be aligned vertically, and the temperature of the core sheet in the second holding section 18 was measured.
[0080] As shown in Table 1, in Examples 1 to 7 in which the core sheet was held in the first holding portion 16 at a temperature below the softening temperature of the adhesive layer, the iron loss degradation rate of the laminated core was 10% or less, and iron loss degradation was suppressed. In particular, in Examples 1 to 5 in which the pressure applied from the punch 12 to the core sheet was set to 2.0 MPa or less, the iron loss degradation rate of the laminated core was 7% or less, and iron loss degradation was sufficiently suppressed.
[0081] On the other hand, in Comparative Examples 1 to 4, in which the core sheet was held in the first holding portion 16 at a temperature equal to or higher than the softening temperature of the adhesive layer, the iron loss degradation rate of the laminated core was 14% or more. Also, in Comparative Examples 5 and 6, in which the first holding portion 16 was not provided and the core sheet was held in the upper end portion of the second holding portion 18 at a temperature equal to or higher than the softening temperature of the adhesive layer, the iron loss degradation rate of the laminated core was 18% or more. Thus, in Comparative Examples 1 to 6, the iron loss degradation of the laminated core was greater than in Examples 1 to 7. [Industrial Applicability]
[0082] According to the present invention, a laminated core with small core loss can be manufactured. [Explanation of symbols]
[0083] 1 Steel strip 2 Laminated core 3 Convex 10 Base 12 Punch 14 Punching die 16,60 1st holding part 18,80 2nd holding part 20 Heating section 22 Connecting part 24 Thermal insulation materials 26 Support device 100,100a manufacturing equipment
Claims
1. A laminated core in which a plurality of electromagnetic steel sheets are laminated with adhesive layers interposed therebetween, A laminated core, wherein the iron loss degradation rate of the laminated core with respect to two layers of electromagnetic steel sheets separated from the laminated core is 10% or less.
2. The laminated core according to claim 1 , wherein the electromagnetic steel sheets at one end in the lamination direction have a plurality of protrusions formed thereon that protrude outward in the lamination direction.
3. A manufacturing apparatus including a punch, a punching die disposed below the punch, a first holding section disposed below the punching die, a second holding section disposed below the first holding section, and a heating section disposed around the second holding section, punching a plurality of core sheets from a steel strip having a thermosetting adhesive layer on a surface thereof by the punch and the punching die; The punch presses the outer periphery of the punched core sheets from the side by the first holding part, while pressing the core sheets downward by the punch; The plurality of core sheets pressed downward by the punch are held laterally in the second holding section while being heated by the heating section; In the first holding section, the plurality of core sheets are held at a temperature lower than the softening temperature of the adhesive layer, A method for manufacturing a laminated core, wherein the heating section heats the multiple core sheets held in the second holding section to a temperature equal to or higher than the softening temperature of the adhesive layer.
4. The method for manufacturing a laminated core according to claim 3 , wherein a length in a vertical direction of the portion of the first holding portion that contacts the core sheet is 5 mm or more.
5. The method for manufacturing a laminated core according to claim 3 or 4, wherein the punch presses the plurality of core sheets with a pressure of 2.0 MPa or less.
6. The method for manufacturing a laminated core according to claim 3 or 4, wherein the heating unit includes an infrared heating device.
7. An apparatus for manufacturing a laminated core by punching out a plurality of core sheets from a steel strip having an adhesive layer on its surface and bonding the obtained plurality of core sheets to each other, comprising: punch, A punching die disposed below the punch; A first holding portion disposed below the punching die; A second holding portion disposed below the first holding portion; and A heating unit disposed around the second holding unit; Equipped with punching a plurality of core sheets from the steel strip with the punch and the punching die; The punch presses the outer periphery of the punched core sheets from the side by the first holding part, while pressing the core sheets downward by the punch; The plurality of core sheets pressed downward by the punch are held laterally in the second holding section while being heated by the heating section; In the first holding section, the plurality of core sheets are held at a temperature lower than the softening temperature of the adhesive layer, The heating section heats the plurality of core sheets held in the second holding section to a temperature equal to or higher than the softening temperature of the adhesive layer.
8. 8. The laminated core manufacturing device according to claim 7, wherein a length in a vertical direction of the portion of the first holding portion that contacts the core sheet is 5 mm or more.
9. 9. The laminated core manufacturing apparatus according to claim 7, wherein the punch presses the plurality of core sheets with a pressure of 2.0 MPa or less.
10. The laminated core manufacturing apparatus according to claim 7 or 8, wherein the heating section includes an infrared heating device.
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