Grain-oriented electrical steel sheet and magnetic domain refinement method therefor
11772199 · 2023-10-03
Assignee
Inventors
- Oh-Yeoul Kwon (Pohang-si, KR)
- Se-Min Park (Pohang-si, KR)
- Jong-Tae Park (Pohang-si, KR)
- Won-Gul Lee (Pohang-si, KR)
Cpc classification
B23K26/082
PERFORMING OPERATIONS; TRANSPORTING
Y02P10/20
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B23K26/18
PERFORMING OPERATIONS; TRANSPORTING
B23K26/364
PERFORMING OPERATIONS; TRANSPORTING
C21D8/1283
CHEMISTRY; METALLURGY
B23K26/40
PERFORMING OPERATIONS; TRANSPORTING
B23K26/359
PERFORMING OPERATIONS; TRANSPORTING
B23K2101/36
PERFORMING OPERATIONS; TRANSPORTING
B23K26/16
PERFORMING OPERATIONS; TRANSPORTING
C21D10/00
CHEMISTRY; METALLURGY
C21D1/18
CHEMISTRY; METALLURGY
C21D8/12
CHEMISTRY; METALLURGY
C22C2204/00
CHEMISTRY; METALLURGY
International classification
B23K26/364
PERFORMING OPERATIONS; TRANSPORTING
B23K26/16
PERFORMING OPERATIONS; TRANSPORTING
C21D1/18
CHEMISTRY; METALLURGY
Abstract
A grain-oriented electrical steel sheet incudes a groove formed on a surface and a solidified alloy layer formed under the groove, wherein the solidified alloy layer includes particles of a certain average diameter.
Claims
1. A magnetic domain refining method of a grain-oriented electrical steel sheet, comprising: preparing a grain-oriented electrical steel sheet; irradiating a laser to a surface of the grain-oriented electrical steel sheet to form a groove; and quenching a portion where the groove is formed with a cooling speed of 400 to 1500° C./s.
2. The magnetic domain refining method of the grain-oriented electrical steel sheet of claim 1, wherein the quenching is simultaneous quenching with the groove formation.
3. The magnetic domain refining method of the grain-oriented electrical steel sheet of claim 1, further comprising, after the quenching, stress relaxation annealing.
4. The magnetic domain refining method of the grain-oriented electrical steel sheet of claim 1, wherein, in the forming of the groove, the laser is a continuous wave laser having a Gaussian energy distribution and an output of 1 kW or more.
5. The magnetic domain refining method of the grain-oriented electrical steel sheet of claim 4, wherein the laser is a continuous wave laser that is a TEM.sub.00 mode and has a beam quality factor M.sup.2 of 1.0 to 1.1 and output of 1 to 10 kW.
6. The magnetic domain refining method of the grain-oriented electrical steel sheet of claim 1, further comprising removing a hill-up or a spatter formed on the electrical steel sheet surface after forming the groove.
7. The magnetic domain refining method of the grain-oriented electrical steel sheet of claim 1, wherein the preparing the grain-oriented electrical steel sheet includes: forming an oxide layer on the surface of the steel sheet by decarburization-annealing or nitriding-annealing cold-rolled steel sheet; and forming a non-metallic oxide layer on the surface of the steel sheet by coating an annealing separator on the surface of the steel sheet on which the oxidation layer is formed.
8. The magnetic domain refining method of the grain-oriented electrical steel sheet of claim 7, further comprising, after forming the non-metallic oxide layer, forming an insulating coating layer on the non-metallic oxide layer.
Description
DESCRIPTION OF THE DRAWINGS
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MODE FOR INVENTION
(5) The terms “first”, “second”, and “third” are used herein to explain various parts, components, regions, layers, and/or sections, but it should be understood that they are not limited thereto. These terms are used only to discriminate one portion, component, region, layer, or section from another portion, component, region, layer, or section. Thus, a first portion, component, region, layer, or section may be referred to as a second portion, component, region, layer, or section without departing from the scope of the present invention. The technical terms used herein are to simply mention a particular embodiment and are not meant to limit the present invention. An expression used in the singular encompasses the expression of the plural, unless it has a clearly different meaning in the context. The term ‘including’ used herein embodies concrete specific characteristics, regions, positive numbers, steps, operations, elements, and/or components, without limiting existence or addition of other specific characteristics, regions, positive numbers, steps, operations, elements, and/or components.
(6) It will be understood that when an element such as a layer, film, region, or substrate is referred to as being “on” or “above” another element, it can be directly on or above the other element or intervening elements may also be present. In contrast, when an element is referred to as being “directly on” another element, there are no intervening elements therebetween.
(7) If not defined differently, all the terminologies including technical terminologies and scientific terminologies used herein have meanings that are the same as ones that those skilled in the art generally understand. The terms defined in dictionaries should be construed as having meanings corresponding to the related prior art documents and those stated herein, and are not to be construed as being ideal or official, if not so defined.
(8) Hereinafter, exemplary embodiments of the present invention will be described in detail so as to be easily practiced by a person skilled in the art to which the present invention pertains. As those skilled in the art would realize, the described embodiments may be modified in various different ways, all without departing from the spirit or scope of the present invention.
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(12) The solidified alloy layer 30 is formed during laser irradiation for refining the magnetic domain. The thickness of the solidified alloy layer 30 may be between 0.6 and 3.0 μm. When the thickness of the solidified alloy layer 30 is very thin, since the recrystallized particles 31 in the solidified alloy layer 30 are not grown to the base portion in which the secondary recrystallization occurs, the iron loss improvement effect by the recrystallized particles 31 does not occur, and when the thickness of solidified alloy layer 30 is too thick, the recrystallized particles 32 are formed, but the recrystallized particles 32 after stress relaxation annealing are also formed at the lower portion, the side portion, and the base portion by a heat effect, and accordingly the magnetic flux density deterioration may become remarkable.
(13) As shown in
(14) Accordingly, a laser output required for forming the groove 20 is reduced by 20% or more for the steel plate on which the non-metallic oxide layer 40 is formed compared with the steel plate on which the non-metallic oxide layer 40 is not formed, thereby increasing the efficiency in improving the iron loss.
(15) In addition, when the non-metallic oxide layer 40 is formed on the surface of the steel plate, the non-metallic oxide layer is physically and chemically solid-bonded to the steel plate surface and is not easily damaged by thermal impact by laser irradiation.
(16) Preferably, the non-metallic oxide layer 40 is formed on the surface of the steel plate with a thickness of 1 to 20 μm. If the thickness of the non-metallic oxide layer 40 is too thin, the effect of increasing the laser absorption rate is low and the non-metallic oxide layer may be destroyed by the thermal impact during the laser irradiation, and if the thickness of the non-metallic oxide layer 40 is too thick, there is drawback that it is difficult to control the process conditions for forming the non-metallic oxide layer 40 and the laser output for forming the groove 20 is increased.
(17) The non-metallic oxide layer 40 may comprise Mg.sub.2SiO.sub.4, Al.sub.2SiO.sub.4, or Mn.sub.2SiO.sub.4.
(18) An insulating coating layer 50 may be formed on the non-metallic oxide layer 40.
(19) The depth D of groove 20 may be 3% to 8% of the thickness of the electrical steel sheet. More specifically, it may be 4% to 8%. If it is less than 3%, the groove of an appropriate depth for improving the iron loss is not formed. If it exceeds 8%, a heat affected part may increase and the growth of the Goss texture may have an adverse effect.
(20) In addition, the groove 20 may be formed at 82° to 98° with respect to the rolling direction of the electrical steel sheet. By forming the groove 20 in an oblique shape not including 90 degrees, the semi-magnetic field may be weakened, thereby improving the magnetism.
(21) The grooves 20 may be formed intermittently from 2 to 10 pieces in the width direction of the steel plate.
(22) The magnetic domain refining method of the grain-oriented electrical steel sheet according to an exemplary embodiment of the present invention includes: preparing the grain-oriented electrical steel sheet; irradiating a laser to the surface of the grain-oriented electrical steel sheet to form the groove; and quenching the part where the groove is formed at a cooling speed of 400 to 1500° C./s. Hereinafter, each step is described in detail.
(23) First, the grain-oriented electrical steel sheet is prepared.
(24) The preparation of the grain-oriented electrical steel sheet may include: decarbonizing or nitriding a cold-rolled electrical steel sheet to form an oxidation layer on the surface of the steel plate; and coating an annealing separator on the surface of the steel plate on which the oxidation layer is formed and annealing at a high temperature to form a non-metallic oxide layer on the surface of the steel plate.
(25) Generally, the cold-rolled steel sheet may be produced by subjecting a slab containing 1 to 7% by weight of Si to hot rolling, hot-rolled sheet annealing, and cold rolling. Since the non-metallic oxide layer is the same as described above, repeated description is omitted.
(26) In an exemplary embodiment of the present invention, the magnetic domain refining may be performed directly on the surface of the steel plate, or the non-metallic oxide may be formed on the surface of the steel plate, magnetic domain refining and then the laser may be irradiated to perform the magnetic domain refining, and an insulating coating layer may be additionally formed on the surface of the steel plate by coating and heat-treating an insulating coating liquid including colloidal silica and a metal phosphate on the non-metallic oxide layer and then the laser may be irradiated to perform the magnetic domain refining. If the non-metallic oxide layer is formed on the surface of the steel plate, this layer may increase the laser absorption rate and form the groove with relatively low energy density.
(27) Next, the surface of the grain-oriented electrical steel sheet is irradiated with the laser to form the groove.
(28) At this time, the laser may be a continuous wave laser having a Gaussian energy distribution and an output of 1 kW or more. This continuous wave laser is suitable for forming the uniform groove on the electrical steel sheet surface after the secondary recrystallization is completed. More specifically, the laser is a TEM.sub.00 mode, and may be a continuous wave laser of which a beam quality factor M2 is 1.0 to 1.1 and the output is 1 to 10 kW. Since forming grooves with a gasify only by the laser irradiation does not form the solidified alloy layer, the method of forming the groove using the laser with too high an output is not preferable.
(29) A step of removing a hill-up or a spatter formed on the electrical steel sheet surface after the step of forming the groove may be further included. The hill-up means that a fusion material generated during the groove formation has risen to the both tops of the groove, and the spatter is formed by scattering of the fusion material. The hill-up and the spatter may be removed by brushing or pickling.
(30) Next, the portion where the groove is formed is quenched at a cooling speed of 400 to 1500° C./s. In an exemplary embodiment of the present invention, the size of the recrystallized particles in the solidified alloy layer may be controlled by controlling the cooling speed. Specifically, the average particle diameter of the recrystallized particles in the solidified alloy layer may be controlled from 1 to 10 μm by controlling the cooling speed from 400 to 1500° C./s. More specifically, the cooling speed may be adjusted from 500 to 1200° C./s.
(31) The quenching method is not particularly limited, and an air cooling method above the laser irradiation may be used. The quenching steps may be done simultaneously with the groove formation.
(32) After the quenching, the stress relaxation annealing may be further included. In case of the heat treatment above the recrystallization temperature such as the stress relaxation annealing in an exemplary embodiment of the present invention, the recrystallized grain grows in the solidified alloy layer and to the base portion such that recrystallized particles are formed after the stress relaxation annealing. The recrystallized particles after the stress relaxation annealing may have the average particle diameter of 1 to 20 μm.
(33) In this heat treatment condition above the recrystallization temperature after the formation of the solidified alloy layer, the recrystallized particle formation after the stress relaxation annealing may achieve an improvement effect of the iron loss of 2% or more and simultaneously a magnetic flux density degradation rate of 1.0% or less.
(34) Hereinafter, the present invention is described in more detail through an example. However, this example is merely to illustrate the present invention, and the present invention is not limited thereto.
Example
(35) The grain-oriented electrical steel sheet of the cold-rolled thickness of 0.30 mm is decarburization-annealed to form the oxidation layer, the annealing separator including MgO is coated, and the high temperature annealing is performed to form a forsterite film. Thereafter, the insulating coating liquid containing the colloidal silica and the metal phosphate is coated to form the insulating coating layer.
(36) That laser that is a TEM.sub.00 mode and has the beam quality factor of M.sup.2 of 1.0 is irradiated to the electrical steel sheet surface by controlling the output to 1.8 kW. In a case of Comparative Example 2 of Table 2, a pulse laser that is not a continuous wave laser is used. During the laser irradiation, the cooling speed is adjusted as shown in the following table through the air cooling. After the magnetic domain refinement treatment, the stress annealing is performed.
(37) The groove depth, the solidified alloy layer thickness, the average particle diameter of the recrystallized particles in the solidified alloy layer, and the recrystallized particle average particle diameter of the stress annealing are summarized in Table 1 and Table 2.
(38) TABLE-US-00001 TABLE 1 Recrystal- lized particles Recrystal- average lized particle After Iron Magnetic Solidified particles diameter heat loss flux alloy average after Before After treatment improve- density Groove layer particle stress laser laser stress ment degradation depth thickness diameter annealing irradiation irradiation annealing rate rate (μm) (μm) (μm) (μm) W.sub.17/50/B.sub.8 (%) (%) Example 9 0.6 6 8 0.96/ 0.86/ 0.83/ 3.5 0.0 (continuous 1.92 1.91 1.91 wave/ 9 0.97/ 0.86/ 0.84/ 2.3 0.0 cooling 1.92 1.91 1.91 speed 3.0 9 13 0.97/ 0.87/ 0.82/ 5.7 −0.5 500° C./s) 1.92 1.91 1.90 15 0.96/ 0.86/ 0.81/ 5.8 −0.5 1.92 1.91 1.90 18 0.6 5 9 0.96/ 0.85/ 0.81/ 2.4 −0.5 1.92 1.91 1.90 10 0.96/ 0.86/ 0.82/ 2.3 0.0 1.92 1.91 1.91 3.0 7 14 0.97/ 0.85/ 0.82/ 3.5 −0.5 1.92 1.90 1.89 16 0.96/ 0.87/ 0.83/ 4.6 −0.5 1.92 1.91 1.90
(39) TABLE-US-00002 TABLE 2 Recrystal- lized particle Recrystal- average lized particle After Iron Magnetic Solidified particle diameter stress loss flux alloy average after Before After annealing improve- density Occupy- Groove layer particle stress laser laser heat ment degradation ing depth thickness diameter annealing irradiation irradiation treatment rate rate ratio (μm) (μm) (μm) (μm) W.sub.17/50/B.sub.8 (%) (%) (%) Example 15 3.0 7.0 11 0.97/ 0.85/ 0.82/ 3.5 0.0 97.2 (continuous 1.92 1.90 1.90 wave/ 12 0.97/ 0.85/ 0.82/ 2.4 0.0 97.1 cooling 1.92 1.90 1.90 speed. 500° C./s) Example 15 0.6 2.0 9 0.97/ 0.85/ 0.81/ 4.7 0.0 97.3 (continuous 1.92 1.90 1.90 wave/ 9 0.97/ 0.84/ 0.80/ 5.9 0.0 97.4 cooling 1.92 1.90 1.90 speed. 1200° C./s) Comparative 15 3.5 8.7 21 0.97/ 0.93/ 0.93/ 0.0 −1.05 95.1 Example 1 1.92 1.89 1.87 (continuous 22 0.96/ 0.92/ 0.92/ 0.0 −1.05 95.2 wave/ 1.92 1.89 1.87 cooling speed. 300° C./s) Comparative 15 0.3 No — 0.97/ 1.01/ 1.01/ 0.0 −1.06 94.8 Example 2 formation 1.92 1.87 1.85 (Pulse Laser/ — 0.96/ 0.99/ 0.99/ 0.0 −0.53 94.7 cooling 1.92 1.86 1.85 speed 500° C./s)
(40) In Table 1 and Table 2, the iron loss improvement rate is calculated by (W.sub.1−W.sub.2)/W.sub.1 by measuring the iron loss W.sub.1 of the electrical steel sheet before the groove is formed by the laser irradiation and the iron loss W.sub.2 after forming the groove by the laser irradiation. The magnetic flux density degradation rate is calculated by (B.sub.2−B.sub.1)/B.sub.1 by measuring the magnetic flux density B.sub.1 of the electrical steel sheet before the groove is formed by the laser irradiation and the magnetic flux density B.sub.2 after forming the groove by the laser irradiation. The occupying ratio as a weight ratio of the steel plate corresponding to an actual volume for a theoretical volume under a 5 MPa pressure is measured by a method of JIS C 2550-2000.
(41) As shown in Table 1 and Table 2, in an example in which the continuous wave laser is used and the cooling speed is appropriately adjusted, it may be confirmed that the recrystallized particles are formed with the appropriate size in the solidified alloy layer, the iron loss improvement rate and the magnetic flux density degradation rate are excellent, and the iron loss and the magnetic flux density are excellent even after the stress annealing heat treatment.
(42) Although exemplary embodiments of the present invention were described with reference to the accompanying drawings, the present invention is not limited to the exemplary embodiments and may be modified in various ways. Further, it would be understood that the present invention may be implemented in other detailed ways by those skilled in the art without the scope and necessary components of the present invention being changed. Therefore, the embodiments described above are only examples and should not be construed as being limitative in all respects.
DESCRIPTION OF SYMBOLS
(43) TABLE-US-00003 10: electrical steel sheet 20: groove 30: solidified alloy layer 31: recrystallized particles 32: recrystallized particles after 40: non-metallic oxide stress annealing layer 50: insulating coating layer