WO2020209319A1 - ブランクおよび部品 - Google Patents
ブランクおよび部品 Download PDFInfo
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- WO2020209319A1 WO2020209319A1 PCT/JP2020/015911 JP2020015911W WO2020209319A1 WO 2020209319 A1 WO2020209319 A1 WO 2020209319A1 JP 2020015911 W JP2020015911 W JP 2020015911W WO 2020209319 A1 WO2020209319 A1 WO 2020209319A1
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- Prior art keywords
- region
- blank
- vickers hardness
- softened
- convex
- Prior art date
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Classifications
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- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C37/00—Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape
- B21C37/02—Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape of sheets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
- B21C37/00—Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape
- B21C37/06—Manufacture of metal sheets, bars, wire, tubes or like semi-manufactured products, not otherwise provided for; Manufacture of tubes of special shape of tubes or metal hoses; Combined procedures for making tubes, e.g. for making multi-wall tubes
- B21C37/15—Making tubes of special shape; Making tube fittings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D11/00—Bending not restricted to forms of material mentioned in only one of groups B21D5/00, B21D7/00, B21D9/00; Bending not provided for in groups B21D5/00 - B21D9/00; Twisting
- B21D11/20—Bending sheet metal, not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D22/00—Shaping without cutting, by stamping, spinning, or deep-drawing
- B21D22/20—Deep-drawing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/88—Making other particular articles other parts for vehicles, e.g. cowlings, mudguards
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
- B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
- B60N2/68—Seat frames
-
- 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
- C21D1/00—General methods or devices for heat treatment, e.g. annealing, hardening, quenching or tempering
- C21D1/26—Methods of annealing
-
- 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
- C21D8/005—Modifying the physical properties by deformation combined with, or followed by, heat treatment of ferrous alloys
-
- 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
- C21D2221/00—Treating localised areas of an article
-
- 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
- C21D2261/00—Machining or cutting being involved
Definitions
- the present invention relates to blanks and parts.
- the present application claims priority based on Japanese Patent Application No. 2019-074618 filed in Japan on April 10, 2019, the contents of which are incorporated herein by reference.
- the blank When processing a blank to form a molded product having a predetermined shape, the blank may be subjected to various treatments to adjust the properties and functions of the blank.
- Patent Document 1 when a welding line is arranged in a concave region that becomes an elongated flange portion after molding in a composite blank, the ductility of the elongated flange portion is ensured by partially irradiating with a laser to soften the weld line.
- the technology to be used is described.
- Patent Document 2 describes a technique for partially softening a region to be a ridgeline portion of a member having a hat-shaped cross section after molding in a blank.
- Patent Document 1 is for ensuring the ductility of the stretch flange portion formed by tensile deformation due to partial softening, and the problem in the shrink flange portion formed by compressive deformation is taken into consideration. Not.
- Patent Document 2 is also for improving the bendability of the ridgeline portion of the cross-sectional hat shape after molding by partial softening, and the problem in the shrinking flange portion is not considered. .. In particular, in the techniques described in Patent Documents 1 and 2, the influence of wrinkles on the shrinking flange portion is not considered.
- the present invention has been made in view of the above problems, and an object of the present invention is to provide a new and improved blank capable of suppressing the influence of wrinkles generated on a shrinking flange portion or the like. is there.
- the present invention is made of a steel material and has at least two convex regions whose outer edges are convex outward in the in-plane direction, and the convex regions are at least partially softened.
- the portion is formed, and the softened portion is formed at least a part of the outer edge of the convex portion region.
- the Vickers hardness of the softened portion is set lower than the Vickers hardness of the main portion region, and the softened portion is formed.
- a blank characterized by having at least two of the convex regions.
- the radius of curvature R of the outer edge of the convex region is 150 mm or less, and the opening angle of the outer edge is 120 °. It may be as follows.
- the tensile strength of the main region of the blank may be 1100 MPa or more.
- the tensile strength of the softened portion may be 1000 MPa or less.
- the Vickers hardness of the softened portion has a ratio of 0.4 or more to 0.9 of the Vickers hardness of the main region of the blank. It may be as follows.
- the first vertical wall portion and the second vertical wall portion which are made of a steel material and are erected from the bottom surface portion and the end portion of the bottom surface portion, and the above-mentioned first vertical wall portion. It is a component having at least two corner portions provided between the vertical wall portion 1 and the second vertical wall portion, and a softening portion is formed at least partially in the corner portion to soften the corner portion.
- the Vickers hardness of the portion is set lower than the Vickers hardness of the main portion region of the component, and the component is provided characterized by having at least two corner portions in which the softened portion is formed.
- the tensile strength of the main region of the component may be 1100 MPa or more.
- the tensile strength of the softened portion may be 1000 MPa or less.
- the Vickers hardness of the softened portion has a ratio of 0.4 or more to 0.9 of the Vickers hardness of the main region of the component. It may be as follows.
- the corner portion may include a shrinking flange portion.
- a new and improved blank capable of suppressing the influence of wrinkles generated on a shrinking flange portion or the like is provided.
- FIG. 1A is a perspective view showing an example of a blank 100 according to the present embodiment.
- FIG. 1B is a perspective view showing an example of a molded product 200 according to the present embodiment.
- the blank 100 according to the present embodiment is a material to be processed, which is finally processed into a molded product having a predetermined shape through various processing.
- the blank 100 is formed into a predetermined plate shape by cutting from, for example, a steel plate which is a flat plate-shaped member. Examples of the cutting process include known cutting techniques such as punching press processing and laser processing, and are not particularly limited.
- the blank 100 cut out from the steel plate is processed into a molded product having a predetermined shape by, for example, cold molding.
- the details of the shape of the blank 100 after processing will be described later, but the blank 100 is processed into a shape having a shrink flange portion (corresponding to the shrink flange portion 221 in FIG. 1B described later) by cold forming.
- the cold forming technique include known cold forming techniques such as press bending and press drawing, and are not particularly limited.
- the blank 100 has a main portion region 110 and a convex portion region 113.
- the main portion region 110 is a region mainly constituting the blank 100, and has the same properties as the steel plate from which the blank 100 is cut out.
- the main region 110 may be a steel material having a tensile strength of 1100 MPa or more. Further, the main portion region 110 may be a steel material having a tensile strength of 1100 MPa or more and 2000 MPa or less.
- the convex region 113 is a region in which a part of the outer edge 111 of the blank 100 is convex outward in a plan view substantially perpendicular to the plate surface of the blank 100, that is, in the in-plane direction of the blank 100. Further, the convex portion region 113 is a region that becomes a shrinking flange portion after molding. In other words, at least a portion of the molded convex region 113 constitutes at least a portion of the shrink flange portion.
- a softening portion 120 is formed at least partially in the convex portion region 113. Details of the softening portion 120 will be described later.
- the blank 100 may have at least two or more convex regions 113 on which the softened portions 120 are formed.
- the blank 100 having a predetermined shape is molded into a molded product 200 having a predetermined shape, for example, by cold molding.
- the molded product 200 has a box shape as an example, and has a web portion 210 as a bottom surface, a flange portion 220 erected from the bottom surface, and a shrink flange portion 221.
- the molded product 200 includes a finished product that is completed by processing the blank 100 into a predetermined shape, and a semi-finished product that requires steps such as additional processing and processing.
- the molded product 200 has a flange portion 220 formed by bending the outer peripheral side of the blank 100.
- the flange portion 220 has a contraction flange portion 221 that is deformed while receiving compressive stress in a part thereof during molding.
- a problem may occur due to its shape. That is, due to the compressive stress during molding, a part of the blank 100 (convex region 113) is deformed in a wavy shape as a result of out-of-plane deformation during molding. When the deformed portion is further crushed by a mold, wrinkles, which are minute irregularities, are generated after molding. Wrinkles formed on the molded product may cause deterioration of the appearance or dimensional accuracy of the molded product, or deterioration of welding quality.
- the yield stress of the steel material is high and the ductility is inferior, so that the formability is lowered.
- the high-strength steel sheet is often used for the purpose of weight reduction, and since it is thinned, the surface rigidity of the steel sheet is lowered. Due to these causes, when a molded product 200 having a shrink flange portion 221 is molded using a blank 100 of a high-strength steel plate, wrinkles after molding are likely to occur on the shrink flange portion 221, and the height of the wrinkles and the wrinkle portion are increased. The amount of increase in plate thickness also increases.
- the appearance or dimensional accuracy of the molded product 200 is likely to be deteriorated, or the welding quality is likely to be deteriorated.
- the base material of the blank 100 is a steel material having a tensile strength of 1100 MPa or more, the influence of the occurrence of wrinkles becomes large.
- the present inventors have come up with the idea of forming the softened portion 120 in the convex portion region 113 of the blank 100, which corresponds to the contracted flange portion 221 of the molded product 200. That is, the present inventors reduce the yield point of the region to be the contracted flange portion 221 by forming the softened portion 120 in the convex portion region 113, suppress the out-of-plane deformation during molding, and suppress the contracted flange portion 221. I came up with the idea of suppressing the occurrence of wrinkles in.
- the Vickers hardness of the shrinking flange portion differs in the ridgeline direction.
- the plate thickness differs in the ridge line direction.
- the shrinking flange portion is different from, for example, a bent portion in a molded product obtained by bending a plate material in an out-of-plane direction.
- the ridgeline direction of the flange portion can be rephrased as a direction parallel to the line of intersection of virtual planes in which the plate surfaces of the two flange portions adjacent to the contracted flange portion are expanded.
- the Vickers hardness of the contraction flange portion 221 increases as the distance from the web portion 210 increases in the direction of the ridgeline of the contraction flange portion 221, and the contraction flange portion 221 further increases.
- the plate thickness increases.
- the softening portion 120 is a softening region formed at least partially in the convex region 113 of the blank 100.
- the Vickers hardness of the softened portion 120 is set lower than the Vickers hardness of the main portion region 110 of the blank 100.
- the Vickers hardness of the softened portion 120 may be set to be 0.4 or more and 0.9 or less in proportion to the Vickers hardness of the main portion region 110 of the blank 100.
- the Vickers hardness of the softened portion 120 By setting the Vickers hardness of the softened portion 120 to 0.9 or less of the Vickers hardness of the main region 110, the yield point of the convex region 113 is partially lowered, and wrinkles are generated in the shrink flange portion 221 of the molded product. The effect of suppressing is obtained. On the other hand, by setting the Vickers hardness of the softened portion 120 to 0.4 or more with respect to the Vickers hardness of the main portion region 110, the strength of the molded product can be sufficiently maintained.
- the hardness measurement conditions are as follows. A sample including the convex region 113 of the blank 100 is collected, a sample of the measurement surface is prepared, and the sample is subjected to a Vickers hardness test.
- the method for preparing the measurement surface is carried out according to JIS Z 2244: 2009. After polishing the measurement surface with # 600 to # 1500 silicon carbide paper, a mirror surface is finished using a diluted solution such as alcohol or a liquid in which diamond powder having a particle size of 1 ⁇ m to 6 ⁇ m is dispersed in pure water.
- the Vickers hardness test is carried out by the method described in JIS Z 2244: 2009.
- the Vickers hardness is measured on the sample on which the measurement surface is prepared, using a micro Vickers hardness tester with a test load of 1 kgf (9.8 N).
- the softening portion 120 may be a portion where the Vickers hardness is 0.9 or less with respect to the average value of the Vickers hardness at a plurality of locations in the central portion of the main portion region 110.
- the softening portion 120 may be set so that the tensile strength is 1000 MPa or less. As a result, the strength of the softened portion 120 is suppressed, and the occurrence of wrinkles is further suppressed.
- Examples of the method of forming the softened portion 120 include a method of softening the blank 100 by partially tempering it using a known partial heating technique such as laser heating or high frequency heating. Further, as another example, the blank 100 may be partially tempered to be softened by a hot forming technique such as partial hot forming. The method for forming the softened portion 120 may be a method other than tempering by heating, as long as the hardness can be partially reduced. For example, a method such as partially decarburizing the blank 100 may be used.
- the softening portion 120 may not be formed in all the convex portions 113 of the blank 100. Considering the shape, size, etc. of the shrinkage flange portion 221 after molding, the softening portion 120 may be formed in the convex portion region 113 where the occurrence of wrinkles is predicted.
- the softening portion 120 may be formed in a region including the outer edge 111 of the convex portion region 113. In other words, the softening portion 120 may be formed at least a part of the outer edge 111 of the convex portion region 113. Since the softening portion 120 is formed in the region including the outer edge 111 of the convex portion region 113, the vicinity of the outer edge 111 where wrinkles are likely to occur is softened, and the occurrence of wrinkles can be further suppressed.
- the softening portion 120 may extend in the in-plane direction (direction orthogonal to the plate thickness direction) of the blank 100 in the convex portion region 113.
- the softening portion 120 includes the outer edge 111 and may be formed in the in-plane direction over a distance from the outer edge 111 to 60 mm, preferably formed over a distance from the outer edge 111 to 40 mm. May be good.
- the softened portion 120 expands in the in-plane direction, a sufficiently softened region in the convex portion region 113 is sufficiently secured, and the occurrence of wrinkles in the contracted flange portion 221 is further suppressed. Further, since the softening portion 120 is formed in the in-plane direction from the outer edge 111 within a predetermined range, it is possible to maintain high strength as a molded product while securing a softening region. Further, the softening portion 120 may be formed only in the convex portion region 113, or may be formed up to the main portion region 110 as long as it is within a range of 50 mm outward from the convex portion region 113.
- the forming range of the softening portion 120 is taken into consideration in consideration of the movement of the blank 100 during molding. May be determined. Further, the depth of the softened portion 120 in the plate thickness direction is not particularly limited, and the softened portion 120 may be formed over the plate thickness direction.
- the softening portion 120 may be made of a separate member made of a different material from the main portion region 110 of the blank 100.
- the Vickers hardness of the separate member may be set lower than the Vickers hardness of the main portion region 110 of the blank 100, and the separate member may be attached to the blank 100 by welding or the like to form the softening portion 120.
- the separate member has a convex shape and becomes a contracted flange portion 221 after molding the blank 100.
- the softening portion 120 in the convex portion region 113, the yield point of the region to be the shrinking flange portion 221 is lowered, and the out-of-plane deformation during molding is suppressed. That is, since the softened portion 120 is formed, the convex portion region 113 is likely to be plastically deformed, and the convex portion region 113 and the mold become familiar with each other at an early stage after the start of molding. As a result, out-of-plane deformation of the shrinking flange portion 221 is suppressed.
- the blank 300 according to the present embodiment is different from the first embodiment in that it is a blank formed on the seat cushion frame by molding. In the description of the present embodiment, the description of the configuration common to the first embodiment will be omitted.
- FIG. 2A is a plan view showing an example of the blank 300 according to the present embodiment.
- FIG. 2B is a perspective view showing an example of the seat cushion frame 400 according to the present embodiment.
- the blank 300 cut out from the steel plate is further cold-molded into a seat cushion frame 400 (side frame) which is a molded product having a predetermined shape.
- the blank 300 is processed into a shape having a shrink flange portion (corresponding to the shrink flange portion 421 in FIG. 2B described later) by cold forming such as press bending and press drawing.
- the seat cushion frame 400 is a part of the seat frame that is the internal skeleton of the vehicle seat, and is a member provided on the side of the seat cushion that supports the thighs or buttocks of the seat occupants.
- the blank 300 has a main portion region 310 and a convex portion region 313.
- the convex region 313 is a region in which a part of the outer edge 311 of the blank 300 is convex outward in a plan view substantially perpendicular to the plate surface of the blank 300, that is, in the in-plane direction of the blank 300.
- the convex portion region 313 is a region that becomes a shrinking flange portion after molding. In other words, at least a portion of the molded convex region 313 constitutes at least a portion of the shrink flange portion.
- a softening portion 320 is formed in the convex portion region 313.
- the seat cushion frame 400 has a frame main body portion 410 and a frame flange portion 420 erected from an end portion of the frame main body portion 410.
- the frame flange portion 420 has a shrink flange portion 421.
- the seat cushion frame 400 can take various shapes depending on the structure of the seat frame.
- the seat cushion frame 400 has a frame flange portion 420 formed by bending the outer peripheral side of the blank 300.
- the convex region 313 of the blank 300 is deformed while receiving compressive stress during molding, so that the frame flange portion 420 is formed with a contracted flange portion 421.
- wrinkles may also occur in the shrink flange portion 421 of the seat cushion frame 400 due to molding.
- a plurality of convex regions 313 can be formed in the blank 300. Further, the convex region 313 may have various convex shapes in consideration of the shape of the seat cushion frame 400 after molding.
- the convex region 313 according to the present embodiment will be described below with reference to FIG.
- FIG. 3 is a diagram for explaining the convex region 313 of the blank 300, and is an enlarged view of the region X in FIG. 2A.
- the convex region 313 is a region in which a part of the outer edge 311 of the blank 300 is convex outward.
- the convex region 313 is determined by setting an arc parallel to the plate surface of the blank 300 at the outer edge 311 of the blank 300 by a known calculation method, and determining the radius of curvature and the opening angle of the arc.
- the arc is an arc connecting three points separated by a pitch of 1 mm along the outer edge 311. As shown in FIG.
- the radius of curvature R of the arc for determining the convex region 313 is 150 mm or less, and the opening angle ⁇ is 60 degrees or more and 120 degrees or less.
- the convex region 313 is determined by the above method, and the softened portion 320 is formed in the convex region 313.
- the convex region 313 is specified, and the softening portion 320 is formed in the convex region 313, so that the softening portion 320 can be provided in the convex region 313 where wrinkles are expected to occur.
- the occurrence of wrinkles in the shrinking flange portion 421 of the seat cushion frame 400 can be effectively suppressed, and the high strength of the seat cushion frame 400 after molding can be maintained.
- the blank 300 may have at least two or more convex region regions 313 on which the softened portion 320 is formed. Further, the main portion region 310 of the blank 300 may be a steel material having a tensile strength of 1100 MPa or more. Further, the main region 310 of the blank 300 may be a steel material having a tensile strength of 1100 MPa or more and 2000 MPa or less.
- the softening portion 320 in the convex portion region 313, the yield point of the region to be the shrinking flange portion 421 is lowered, and the out-of-plane deformation during molding is suppressed.
- the occurrence of wrinkles in the shrinking flange portion 421 is suppressed.
- the influence of wrinkles on the seat cushion frame 400 can be reduced. In particular, deterioration of appearance or dimensional accuracy of the contracted flange portion 421 of the seat cushion frame 400 is reduced.
- the present invention is not limited to the seat cushion frame as long as it is a molded product having a shrinkable flange portion.
- it may be applied to a seat back frame.
- FIG. 4 is a diagram showing an automobile skeleton 500 as an example to which a skeleton member formed by using the blanks 100 and 300 according to the embodiment of the present invention is applied.
- the skeleton member formed using the blanks 100, 300 can constitute the automobile skeleton 500 as a cabin skeleton or a shock absorbing skeleton. Examples of applications as a cabin skeleton include a roof side rail 501, an A-pillar lower 507, an A-pillar upper 505, a kick clean force 511, a floor cross member 513, a front header 515, and the like.
- skeleton member examples include rear side member 503, bumperine force 509 and the like.
- the skeleton member formed by using the blanks 100 and 300 according to any embodiment of the present invention suppresses the occurrence of wrinkles in the shrinking flange portion. As a result, the influence of wrinkles on the skeleton member is reduced.
- FIG. 5A is a diagram showing an example of a part molded by using the blank 100 according to the present embodiment.
- FIG. 5B is a diagram showing an example in which a part formed by using the blank 100 according to the present embodiment is applied.
- An example of a component molded using the blank 100 according to the present embodiment is a bulkhead 610.
- the bulkhead 610 is a substantially box-shaped member having an open surface.
- the bulkhead 610 forms a partition wall inside the hollow skeleton member, so that the rigidity and collision performance of the skeleton member are further improved.
- the bulkhead 610 as a component has a box shape as an example, and has a web portion 611 as a bottom surface portion and a flange portion 613 as a vertical wall portion erected from the end portion of the bottom surface portion. And a corner portion 615.
- a softening portion 620 is formed at least partially in the corner portion 615.
- the web portion 611 and the flange portion 613 are composed of a main portion region 617.
- the flange portion 613 has a first flange portion 613a as a first vertical wall portion and a second flange portion 613b as a second vertical wall portion.
- the corner portion 615 is provided between the first flange portion 613a and the second flange portion 613b so as to bend and connect the first flange portion 613a and the second flange portion 613b.
- the second flange portion 613b is provided in a direction substantially orthogonal to the first flange portion 613a from the end portion of the corner portion 615. Further, one end of the corner portion 615 in the ridgeline direction is connected to the web portion 611.
- At least two corner portions 615 are formed in the bulkhead 610. Further, the bulkhead 610 has at least two corner portions 615 on which the softening portion 620 is formed. A part of the corner part 615 is formed as a part of the shrinking flange part described above.
- the Vickers hardness of the softened portion 620 is set lower than the Vickers hardness of the main portion region 617 constituting the web portion 611 or the flange portion 613 of the bulkhead 610.
- the Vickers hardness of the softened portion 620 may be set to be 0.4 or more and 0.9 or less in proportion to the Vickers hardness of the main portion region 617 of the bulkhead 610.
- the Vickers hardness of the softened portion 620 By setting the Vickers hardness of the softened portion 620 to 0.9 or less of the Vickers hardness of the main region 617, it is possible to obtain the effect of suppressing breakage at the corner portion 615 of the molded product at the time of collision. Further, by setting the Vickers hardness of the softened portion 620 to 0.9 or less of the Vickers hardness of the main portion region 617, an effect of suppressing the occurrence of wrinkles can be obtained. On the other hand, by setting the Vickers hardness of the softened portion 620 to 0.4 or more with respect to the Vickers hardness of the main portion region, the strength of the molded product can be sufficiently maintained.
- the main region 617 of the bulkhead 610 may be a steel material having a tensile strength of 1100 MPa or more. Further, the softening portion 620 may be set so that the tensile strength is 1000 MPa or less.
- the bulkhead 610 is provided inside the square tubular skeleton member 630 along the lateral direction of the skeleton member 630.
- the skeleton member 630 is orthogonal to the pair of first wall portions 631, the corner portions 633 provided at the lateral ends of the first wall portions 631, and the corner portions 633 to the first wall portions 631. It has a pair of second wall portions 635 provided in the direction.
- the flange portion 613 of the bulkhead 610 is attached to the inner surface side of the first wall portion 631 and the second wall portion 635. Further, the corner portion 615 of the bulkhead 610 is attached to the inside of the corner portion 633 of the skeleton member 630.
- the bulkhead 610 is molded from the blank 100 according to the present embodiment, and a softening portion 620 is provided at the corner portion 615 of the bulkhead 610. Therefore, when a load is input to the skeleton member 630, it is possible to prevent the bulkhead 610 from breaking starting from the corner portion 615 which is the contracted flange portion.
- the bulkhead 610 is molded from the blank 100 according to the present embodiment, the occurrence of wrinkles is suppressed in the corner portion 615 which is the shrinking flange portion. As a result, the influence of wrinkles on the bulkhead 610 is reduced, for example, the adhesion between the bulkhead 610 and the skeleton member 630 is improved.
- FIG. 6A is a blank model used in the simulation analysis as Comparative Example 1.
- FIG. 6B is a blank model used in the simulation analysis as an example.
- FIG. 6C is a diagram showing an example of a press working die assumed in the simulation analysis.
- FIG. 6D is a simple mold model in which the corner portion forming the shrinking flange portion is extracted from the mold shown in FIG. 6C. This analysis was performed using the simple mold model shown in FIG. 6D.
- a blank model 700A having a quadrant shape (corresponding to a convex region) was used.
- the comparative example has a region 710 corresponding to a steel material having a tensile strength of 1180 MPa as a base material, and the radius of curvature R of the outer edge 713 in a top view is 120 mm.
- the blank model 700B having a quadrant shape was used as in the comparative example.
- a region 720 serving as a softening portion is provided on the outer peripheral side of the quadrant, and a region 710 corresponding to a steel material having a tensile strength of 1180 MPa as a base material is further provided on the center side of the quadrant.
- the simulation was performed by changing the Vickers hardness of the region 720.
- the Vickers hardness of the region 720 corresponding to the softened portion was set to 0.83 with respect to the Vickers hardness of the region 710. This corresponds to the case where the softened portion is a steel material having a tensile strength of 980 MPa.
- the Vickers hardness of the region 720 was set to 0.66 with respect to the region 710. This corresponds to the case where the softened portion is a steel material having a tensile strength of 780 MPa.
- the Vickers hardness of the region 720 was set to 0.5 with respect to the Vickers hardness of the region 710.
- the softened portion is a steel material having a tensile strength of 590 MPa.
- the radius of curvature R of the outer edge 713 of the model of the example in top view is 120 mm as in Comparative Example 1, and the region 720 corresponding to the softened portion includes the outer edge 713 of the model and is separated from the outer edge 713 of the model by 60 mm. It exists up to the position. Therefore, the entire vertical wall is composed of the area 720.
- the plate thickness of the model is the same in Example and Comparative Example 1.
- a blank press working simulation was performed using the mold models A', B', and C'.
- the mold models A', B', and C' are simple models corresponding to a part of the die A, the pad B, and the punch C in FIG. 6C, respectively.
- the present inventors hold the center side of the blank model described above by the mold model C'(punch) and the mold model B'(pad), and move the model toward the mold model A'(die).
- the blank model was transformed. That is, simulation analysis was performed to form a flange by compressing and deforming the outer peripheral side of the quadrant shape shown in FIGS. 6A and 6B while bending it to form a molded product shape having a contracted flange portion.
- the plate thickness reduction rate generated in the shrinkage flange portion of each model after molding was compared.
- the plate thickness reduction rate indicates the reduction rate of the plate thickness after molding with respect to the plate thickness before molding in the contracted flange portion.
- the maximum value of the plate thickness reduction rate in the molded product was defined as the plate thickness reduction rate.
- FIG. 7 is a graph showing the plate thickness reduction rate in the shrinkage flange portion of the model after press forming, which was obtained as a result of simulation analysis.
- the plate thickness reduction rate in Examples 1 to 3 was about 16 to 18% as compared with the plate thickness reduction rate in Comparative Example.
- the plate thickness reduction rate in the shrinking flange portion can be reduced by using the blank according to any embodiment of the present invention.
- the ratio of the Vickers hardness of the softened portion to the Vickers hardness of the main portion region is 0.9 or less, the plate thickness reduction rate can be significantly reduced.
- the reduction in the plate thickness reduction rate suppressed the change in the plate thickness after molding in the shrinking flange portion, and as a result, the occurrence of wrinkles due to the change in the plate thickness was suppressed. That is, the blank according to any one of the embodiments of the present invention was able to suppress the occurrence of wrinkles in the molded product having the shrinkable flange portion.
- the plate thickness reduction rate does not change significantly between Examples 1 to 3, even if the ratio of the Vickers hardness of the softened portion is reduced from 0.9, the plate thickness reduction rate It was found that the reduction allowance of was not significantly changed. That is, it was shown that the ratio of the Vickers hardness of the softened portion to the Vickers hardness of the main region is preferably 0.9 or less from the viewpoint of suppressing wrinkles. Further, from the viewpoint of the effect of suppressing wrinkles and the strength of parts, it is desirable that the ratio of the Vickers hardness of the softened portion to the Vickers hardness of the main portion region is 0.4 or more. (Example 2)
- FIG. 8 is a diagram for explaining the three-point bending crush test conditions.
- the impactor I is made to collide with the skeleton member 630 provided with the bulkhead 610 according to the present invention in the direction of the arrow in FIG. 8, and the presence or absence of breakage of the corner portion 615 of the bulkhead 610 is evaluated. did.
- the collision position was approximately the center position in the longitudinal direction of the skeleton member 630, which is the position where the bulkhead 610 was provided.
- the collision speed was 64 km / h, and the presence or absence of breakage was examined when the amount of impactor I invading the skeleton member 630 was 10 mm.
- Example 4 the main region 617 of the bulkhead 610 was made of a steel material having a tensile strength of 1180 MPa. Further, the strength of the softened portion 620 provided in the corner portion 615 was controlled so that the tensile strength was 980 MPa, that is, the Vickers hardness of the main portion region 617 was 0.83. In Comparative Example 2, no softening portion was provided at the corner portion, and the entire bulkhead was made of a steel material having a tensile strength of 1180 MPa.
- the dimensions of the skeleton member 630 were a square cylinder shape of 100 mm in the vertical direction and 100 mm in the horizontal direction in a cross-sectional view along the lateral direction, and the plate thickness was 0.8 mm. The thickness of the bulkhead was also set to 0.8 mm. Table 1 shows the evaluation results.
- Example 4 As shown in Table 1, in Comparative Example 2 in which the softening portion was not provided in the corner portion, breakage occurred in the corner portion of the bulkhead when the impactor I penetrated 10 mm. On the other hand, in Example 4, the bulkhead 610 did not break even when the impactor I penetrated 10 mm. In this way, the corner portion 615 is provided with the softened portion 620 softened more than the main portion region 617, and the strength of the softened portion 620 is set to 0.9 or less of the Vickers hardness of the main portion region 617, whereby the bulkhead 610 It was shown that breakage at the corner portion 615 can be suppressed.
- the present invention is industrially useful because it can provide a blank capable of suppressing the influence of wrinkles generated on a shrinking flange portion or the like.
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Abstract
Description
本願は、2019年4月10日に、日本に出願された特願2019-074618号に基づき優先権を主張し、その内容をここに援用する。
[鋼板の概略構成]
まず、図1Aおよび図1Bを参照して、本発明の第1の実施形態に係るブランク100の概略構成について説明する。図1Aは、本実施形態に係るブランク100の一例を示す斜視図である。図1Bは、本実施形態に係る成形品200の一例を示す斜視図である。本実施形態に係るブランク100は、種々の加工を経て、最終的に所定の形状を有する成形品へ加工される被加工材である。ブランク100は、例えば、平板状の部材である鋼板から切断加工により所定の板形状に形成される。切断加工の一例としては、打ち抜きプレス加工、レーザ加工等の公知の切断加工技術が挙げられ、特に限定されない。
続いて、図1Bを参照しながら、成形品200の形状および成形時の課題について説明する。所定の形状を有するブランク100は、例えば冷間成形により、所定の形状を有する成形品200に成形される。図1Bに示すように、成形品200は、一例として、箱型形状を有し、底面としてのウェブ部210と、底面から立設したフランジ部220と、縮みフランジ部221とを有する。ここで、成形品200には、ブランク100に対する加工により所定の形状とされて完成する完成品と、追加の加工、処理等の工程が必要な半製品とが含まれる。
軟化部120は、ブランク100の凸部領域113において、少なくとも部分的に形成された軟化領域である。軟化部120のビッカース硬度は、ブランク100の主部領域110のビッカース硬度よりも低く設定されている。特に、軟化部120のビッカース硬度は、ブランク100の主部領域110のビッカース硬度に対する比率で0.4以上0.9以下となるように設定されてもよい。
続いて、本発明の第2の実施形態に係るブランク300について説明する。本実施形態に係るブランク300は、成形によりシートクッションフレームに形成されるブランクである点で、第1の実施形態と相違する。なお、本実施形態の説明において、第1の実施形態と共通する構成については、説明を省略する。
以上、本発明の好適な実施の形態について詳細に説明した。ここから、図4を参照して本発明のいずれかの実施形態に係るブランク100、300を用いて成形される骨格部材の適用例について説明する。図4は、本発明の実施形態に係るブランク100、300を用いて成形される骨格部材が適用される一例としての自動車骨格500を示す図である。ブランク100、300を用いて成形される骨格部材は、キャビン骨格または衝撃吸収骨格として自動車骨格500を構成し得る。キャビン骨格としての適用例は、ルーフサイドレール501、Aピラーロア507、Aピラーアッパー505、キックリーンフォース511、フロアクロスメンバ513、フロントヘッダ515等が挙げられる。
上述した実施形態に係るブランクのしわの発生への影響を確認するため、プレス成形のシミュレーション解析を行った。図6A、図6B、図6Cおよび図6Dを参照して、当該シミュレーション解析結果について説明する。図6Aは、比較例1として、シミュレーション解析に用いたブランクのモデルである。図6Bは、実施例として、シミュレーション解析に用いたブランクのモデルである。図6Cは、シミュレーション解析にて想定したプレス加工の金型の一例を示す図である。図6Dは、図6Cに示した金型において、縮みフランジ部を形成する角部分を抜き出した簡易金型モデルである。本解析は、図6Dの簡易金型モデルを用いて行った。
(実施例2)
110、310 主部領域
111、311 外縁
113、313 凸部領域
120、320 軟化部
200 成形品
210 ウェブ部
220 フランジ部
221、421 縮みフランジ部
400 シートクッションフレーム
610 バルクヘッド(部品)
611 ウェブ部(底面部)
613 フランジ部
613a 第1のフランジ部(第1の縦壁部)
613b 第2のフランジ部(第2の縦壁部)
615 コーナ部(縮みフランジ部)
617 主部領域
620 軟化部
Claims (10)
- 鋼材からなり、
外縁が面内方向において外側へ凸状となる凸部領域を少なくとも2つ有し、
前記凸部領域には、少なくとも部分的に軟化部が形成されかつ、前記凸部領域の外縁の少なくとも一部に前記軟化部が形成され、
前記軟化部のビッカース硬度は、主部領域のビッカース硬度よりも低く設定され、
前記軟化部の形成された前記凸部領域を少なくとも2つ有する
ことを特徴とするブランク。 - 前記軟化部の形成された前記凸部領域は、
当該凸部領域の外縁の曲率半径Rが150mm以下とされ、
前記外縁の開き角度が120°以下である
ことを特徴とする請求項1に記載のブランク。 - 前記ブランクの前記主部領域の引張強度が1100MPa以上である
ことを特徴とする請求項1または2に記載のブランク。 - 前記軟化部の引張強度が1000MPa以下である
ことを特徴とする請求項1~3のいずれか1項に記載のブランク。 - 前記軟化部のビッカース硬度は、前記ブランクの前記主部領域のビッカース硬度に対する比率が0.4以上0.9以下である
ことを特徴とする請求項1~4のいずれか1項に記載のブランク。 - 鋼材からなり、
底面部と、
前記底面部の端部から立設された、第1の縦壁部および第2の縦壁部と、
前記第1の縦壁部と前記第2の縦壁部との間に設けられたコーナ部を少なくとも2つ有する部品であって、
前記コーナ部には、少なくとも部分的に軟化部が形成され、
前記軟化部のビッカース硬度は、前記部品の主部領域のビッカース硬度よりも低く設定され、
前記軟化部の形成された前記コーナ部を少なくとも2つ有する
ことを特徴とする部品。 - 前記部品の前記主部領域の引張強度が1100MPa以上である
ことを特徴とする請求項6に記載の部品。 - 前記軟化部の引張強度が1000MPa以下である
ことを特徴とする請求項6または7に記載の部品。 - 前記軟化部のビッカース硬度は、前記部品の前記主部領域のビッカース硬度に対する比率が0.4以上0.9以下である
ことを特徴とする請求項6~8のいずれか1項に記載の部品。 - 前記コーナ部は、縮みフランジ部を含む
ことを特徴とする請求項6~9のいずれか1項に記載の部品。
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US17/601,626 US11951520B2 (en) | 2019-04-10 | 2020-04-09 | Blank and component |
KR1020217034696A KR102656971B1 (ko) | 2019-04-10 | 2020-04-09 | 블랭크 및 부품 |
CN202080024820.8A CN113631288B (zh) | 2019-04-10 | 2020-04-09 | 坯料以及构件 |
EP20787502.2A EP3954475A4 (en) | 2019-04-10 | 2020-04-09 | Blank and component |
JP2021513693A JP7188567B2 (ja) | 2019-04-10 | 2020-04-09 | ブランクおよび部品 |
MX2021012210A MX2021012210A (es) | 2019-04-10 | 2020-04-09 | Pieza en bruto y componente. |
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EP (1) | EP3954475A4 (ja) |
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US20130316187A1 (en) | 2010-11-03 | 2013-11-28 | Johnson Controls Gmbh | Method for the roll-forming of profiles and a structural part produced thereby |
JP5888168B2 (ja) | 2012-07-25 | 2016-03-16 | 新日鐵住金株式会社 | 低強度部を有する熱間プレス成形品及びその製造方法 |
DE102014216225A1 (de) * | 2014-08-14 | 2016-02-18 | Muhr Und Bender Kg | Strukturbauteil und Verfahren zur Herstellung eines Strukturbauteils |
JP6330930B1 (ja) * | 2017-01-27 | 2018-05-30 | Jfeスチール株式会社 | プレス成形方法 |
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US20220193742A1 (en) | 2022-06-23 |
KR20210143283A (ko) | 2021-11-26 |
JP7188567B2 (ja) | 2022-12-13 |
CN113631288A (zh) | 2021-11-09 |
EP3954475A4 (en) | 2023-01-11 |
US11951520B2 (en) | 2024-04-09 |
EP3954475A1 (en) | 2022-02-16 |
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