BLANK, FORMED ARTICLE, DIE ASSEMBLY, AND METHOD FOR PRODUCING BLANK
20170320122 · 2017-11-09
Inventors
Cpc classification
B21D28/16
PERFORMING OPERATIONS; TRANSPORTING
B21D28/34
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
A sheet-shaped blank (10) for press forming is produced by shearing a metal sheet (30). The blank (10) includes a sheared edge (14), which includes a sheared surface (14b) and a fractured surface (14c) in the sheet thickness direction and has a loop shape in plan view. In plan view, an edge of the sheared edge (14) includes concavely curved portions (20). The average of lengths of the fractured surface (14c) in the sheet thickness direction in the curved portions (20) is greater than the average of lengths of the fractured surface (14c) in the sheet thickness direction over the entire perimeter of the sheared edge (14).
Claims
1. A sheet-shaped blank for press forming produced by shearing a metal sheet, the blank comprising: a sheared edge comprising, in a sheet thickness direction, a sheared surface and a fractured surface, wherein the sheared edge has a loop shape in plan view, the sheared edge has an edge comprising, in plan view, a curved portion that is concavely curved, and an average of lengths of the fractured surface in the sheet thickness direction in the curved portion is greater than an average of lengths of the fractured surface in the sheet thickness direction over an entire perimeter of the sheared edge.
2. The blank according to claim 1, wherein, provided that a reference point of the curved portion is defined as a midpoint of the curved portion in a perimeter direction of the sheared edge or a point where a curvature of the curved portion in plan view is greatest, an average of lengths of the fractured surface in the sheet thickness direction within a region, which extends a predetermined length in the perimeter direction with the reference point as a center, is greater than the average of lengths of the fractured surface in the sheet thickness direction over the entire perimeter of the sheared edge.
3. The blank according to claim 2, wherein the average of lengths of the fractured surface in the sheet thickness direction within the region of the predetermined length is greater by 10% or more of the sheet thickness than the average of lengths of the fractured surface in the sheet thickness direction over the entire perimeter of the sheared edge.
4. The blank according to claim 2, wherein the sheared edge further comprises a shear droop portion positioned opposite from the fractured surface in the sheet thickness direction with the sheared surface interposed therebetween, and wherein an average of lengths of the shear droop portion in the sheet thickness direction within the region of the predetermined length is 20% or less of the sheet thickness.
5. The blank according to claim 2, wherein the predetermined length is a length of 50% of the sheet thickness of the blank.
6. The blank according to claim 2, wherein the predetermined length is a length of 2000% of the sheet thickness.
7. The blank according to claim 2, wherein the region of the predetermined length is a region where a curvature is 5 m.sup.−1 or more.
8. The blank according to claim 1, wherein the metal sheet comprises a hole formed by punching, and the sheared edge is formed along an edge of the hole.
9. The blank according to claim 1, wherein the metal sheet has an outer perimeter edge formed by blanking, and the sheared edge is formed along the outer perimeter edge.
10. The blank according to claim 1, wherein the curved portion is configured to stretch and deform during press forming.
11. A formed article produced by subjecting the blank according to claim 1 to press forming.
12. A die assembly comprising: a columnar punch; and a hollow die configured to receive the punch, the die assembly being configured to shear a metal sheet placed on the die by moving the punch in a predetermined direction, the punch comprising a bottom surface and an outer perimeter surface, the bottom surface comprising a cutting edge constituted by an outer perimeter edge of the bottom surface, the outer perimeter surface extending from the outer perimeter edge in a direction parallel to the predetermined direction, the outer perimeter edge comprising, in plan view, a curved portion that is convexly curved or concavely curved, the bottom surface comprising a planar portion and a cutout portion recessed with respect to the planar portion in the predetermined direction and configured to comprise the curved portion in plan view.
13. A die assembly comprising: a columnar punch; and a hollow die configured to receive the punch, the die assembly being configured to shear a metal sheet placed on the die by moving the punch in a predetermined direction, the die comprising a hollow support surface and an inner perimeter surface, the support surface being configured to support the metal sheet and comprising a cutting edge constituted by an inner perimeter edge of the die, the inner perimeter surface extending from the inner perimeter edge in a direction parallel to the predetermined direction, the inner perimeter edge comprising, in plan view, a curved portion that is convexly curved or concavely curved, the support surface comprising a planar portion and a cutout portion recessed with respect to the planar portion in the predetermined direction and configured to comprise the curved portion in plan view.
14. The die assembly according to claim 12, wherein a cutout depth of the cutout portion in a direction parallel to the predetermined direction is 0.1 times or more a sheet thickness of the metal sheet and 0.7 times or less the sheet thickness.
15. A method for producing a blank for press forming, the method using the die assembly according to claim 12, the method comprising the steps of: placing a metal sheet on the die of the die assembly, and shearing the metal sheet on the die using the punch of the die assembly.
16. A method for producing a blank comprising: a sheared edge comprising, in a sheet thickness direction, a sheared surface and a fractured surface, wherein the sheared edge has a loop shape in plan view, the sheared edge has an edge comprising, in plan view, a curved portion that is concavely curved, and an average of lengths of the fractured surface in the sheet thickness direction in the curved portion is greater than an average of lengths of the fractured surface in the sheet thickness direction over an entire perimeter of the sheared edge, the method using the die assembly according to claim 12, the method comprising the steps of: placing a metal sheet on the die of the die assembly, and shearing the metal sheet on the die using the punch of the die assembly, wherein, in the step of shearing, at least a portion of the curved portion of the blank is formed by cutting a portion of the metal sheet via the cutout portion of the punch or the cutout portion of the die.
17. The die assembly according to claim 13, wherein a cutout depth of the cutout portion in a direction parallel to the predetermined direction is 0.1 times or more a sheet thickness of the metal sheet and 0.7 times or less the sheet thickness.
18. A method for producing a blank for press forming, the method using the die assembly according to claim 13, the method comprising the steps of: placing a metal sheet on the die of the die assembly, and shearing the metal sheet on the die using the punch of the die assembly.
19. A method for producing a blank comprising: a sheared edge comprising, in a sheet thickness direction, a sheared surface and a fractured surface, wherein the sheared edge has a loop shape in plan view, the sheared edge has an edge comprising, in plan view, a curved portion that is concavely curved, and an average of lengths of the fractured surface in the sheet thickness direction in the curved portion is greater than an average of lengths of the fractured surface in the sheet thickness direction over an entire perimeter of the sheared edge, the method using the die assembly according to claim 13, the method comprising the steps of: placing a metal sheet on the die of the die assembly, and shearing the metal sheet on the die using the punch of the die assembly, wherein, in the step of shearing, at least a portion of the curved portion of the blank is formed by cutting a portion of the metal sheet via the cutout portion of the punch or the cutout portion of the die.
Description
BRIEF DESCRIPTION OF DRAWINGS
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DESCRIPTION OF EMBODIMENTS
[0076] Hereinafter, blanks, formed articles, die assemblies, and methods for producing a blank, according to the present invention, will be described with reference to the drawings. There are no particular limitations on the material for blanks according to the present invention. Examples of the material for the blanks include metal materials such as steels. When a steel is used as the material for the blanks, there are no particular limitations on the type of steel. Also, there are no particular limitations on the thickness and strength of the blanks provided that the thickness and strength are sufficient for shearing.
(Configurations of Blank and Formed Article)
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[0078] The blank 10 is subjected to, for example, press forming (e.g., burring or deep drawing) to be formed into parts for automobiles, home appliances, and others. Specifically, referring to
[0079]
[0080] Referring to
[0081] Referring to
[0082]
[0083] Referring to
[0084] The average of lengths of the fractured surface 14c in the curved portion 20 in the sheet thickness direction is determined in the following manner. Firstly, the curved portion 20 is equally divided into five areas in the perimeter direction of the sheared edge 14. Then, the lengths of the fractured surface 14c in the sheet thickness direction are measured at the boundaries between adjacent areas. That is, in the curved portion 20, the length of the fractured surface 14c in the sheet thickness direction is measured at four points different in position in the perimeter direction of the sheared edge 14. Then, the average of the measured lengths at the four points is calculated and the result is designated as the average of lengths of the fractured surface 14c in the sheet thickness direction in the curved portion 20. The averages of lengths of the shear droop portion 14a and the sheared surface 1413 in the sheet thickness direction in the curved portion 20 can be determined in the same manner.
[0085] The average of lengths of the fractured surface 14c in the sheet thickness direction over the entire perimeter of the sheared edge 14 is determined in the following manner. Firstly, the sheared edge 14 is equally divided into a plurality of areas with a predetermined width in the perimeter direction of the sheared edge 14. Then, the lengths of the fractured surface 14c in the sheet thickness direction are measured at the boundaries between adjacent areas. That is, the length of the fractured surface 14c in the sheet thickness direction is measured at a plurality of points different in position in the perimeter direction of the sheared edge 14. Then, the average of the measured lengths at the plurality of points is calculated and the result is designated as the average of lengths of the fractured surface 14c in the sheet thickness direction over the entire perimeter of the sheared edge 14. The predetermined width is set to be closest to the width of the five areas of the curved portion 20 when equally divided in the perimeter direction. The averages of lengths of the shear droop portion 14a and the sheared surface 14b in the sheet thickness direction over the entire perimeter of the sheared edge 14 can be determined in the same manner.
[0086] Referring to
[0087] In the present embodiment, the average of lengths of the fractured surface 14c in the sheet thickness direction within the region R is greater than the average of lengths of the fractured surface 14c in the sheet thickness direction over the entire perimeter of the sheared edge 14, by 10% or more of the sheet thickness of the blank 10. Furthermore, in the present embodiment, the average of lengths of the shear droop portion 14a in the sheet thickness direction within the region R is 20% or less of the sheet thickness of the blank 10. The average of lengths of the fractured surface 14c in the sheet thickness direction within the region R is determined in the following manner. Firstly, the sheared edge 14 within the region R is equally divided into five areas in the perimeter direction. Then, the lengths of the fractured surface 14c in the sheet thickness direction are measured at the boundaries between adjacent areas. That is, in the region R, the length of the fractured surface 14c in the sheet thickness direction is measured at four points different in position in the perimeter direction of the sheared edge 14. Then, the average of the measured lengths at the four points is calculated and the result is designated as the average of lengths of the fractured surface 14c in the sheet thickness direction within the region R. The averages of lengths of the shear droop portion 14a and the sheared surface 14b in the sheet thickness direction within the region R can be determined in the same manner.
(Advantageous Effects of the Blank and Formed Article)
[0088] In the blank 10, the length of the fractured surface 14c in the sheet thickness direction is greater in the curved portion 20. In other words, in the portion, which tends to stretch and deform during press forming, the sheared surface 14b occupies a smaller fraction. With this configuration, the curved portion 20 can easily stretch and deform, and therefore, the occurrence of stretch flange cracking is suppressed at the curved portion 20 when the curved portion 20 is subjected to stretch flanging. Furthermore, in the areas other than the curved portion 20, the fractured surface 14c occupies a smaller fraction than in the curved portion 20. In other words, the sheared surface 14b, which is work hardened, occupies a larger fraction. As a result, sufficient fatigue strength is exhibited in the areas other than the curved portion 20. On the other hand, the fractured surface 14c occupies a larger fraction in the curved portion 20. Thus, in its condition before press forming, the curved portion 20 has reduced fatigue strength. However, during press forming, the curved portion 20 is work hardened by stretch flanging and therefore is increased in fatigue strength. As a result, the formed article 12 after press forming exhibits sufficient fatigue strength. As a result of these, the occurrence of stretch flange cracking is suppressed in production of the formed article 12 from the blank 10 while suppressing the decrease in fatigue strength of the formed article 12.
[0089] In the blank 10, for example, the average of lengths of the fractured surface 14c in the sheet thickness direction within the region R is set to be greater than the average of lengths of the fractured surface 14c in the sheet thickness direction over the entire perimeter of the sheared edge 14. This configuration suppresses the occurrence of stretch flange cracking at a central area (a positional center or an area where the curvature is large) of the curved portion 20.
[0090] In the blank 10, the average of lengths of the fractured surface 14c in the sheet thickness direction within the region R is greater than the average of lengths of the fractured surface 14c in the sheet thickness direction over the entire perimeter of the sheared edge 14, by 10% or more of the sheet thickness of the blank 10. This sufficiently suppresses the occurrence of stretch flange cracking at a central area of the curved portion 20.
[0091] In the blank 10, the average of lengths of the shear droop portion 14a in the sheet thickness direction within the region R is 20% or less of the sheet thickness of the blank 10. This suppresses the occurrence of stretch flange cracking more reliably.
[0092] In the blank 10, the predetermined length of the region R is set to a length of 50% of the sheet thickness of the blank 10, for example. This configuration more reliably suppresses the occurrence of stretch flange cracking at a central area of the curved portion 20. The predetermined length of the region R may be set to a length of 2000% of the sheet thickness of the blank 10, for example. This configuration suppresses the occurrence of stretch flange cracking over a sufficient range within the curved portion 20. Furthermore, the region R may be a region where the curvature is 5 m.sup.−1 or more, for example. This configuration sufficiently prevents the occurrence of stretch flange cracking in the curved portion 20, where larger stretch flanging deformation occurs during press forming.
[0093] Although the blank 10 includes the plurality of curved portions 20, it suffices if one of the curved portions 20 satisfies the requirements of the present invention. Accordingly, there may be a curved portion(s) 20 that does not satisfy the requirements of the present invention among the plurality of curved portions 20.
(Die Assembly for Producing Blank and Method for Producing Blank)
[0094] In the following, a die assembly for producing the above blank 10 and a method for producing the blank 10 using the die assembly will be described.
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[0097] Referring to
[0098] Referring to
[0099] Referring to
[0100] Referring to
[0101] Referring to
[0102] In the following, a method for producing the blank 10 using the above die assembly 24 will be described specifically with reference to the drawings.
[0103] Referring to
[0104] As illustrated in
[0105] When the punch 26 is further forced inward, the cracks 52, 56 propagate in the sheet thickness direction of the metal sheet 30, so that fractured surfaces 58, 60 are formed on the front side and the back side of the metal sheet 30 as illustrated in
(Advantageous Effects of Die Assembly and Production Method Using Die Assembly)
[0106] When the blank 10 is produced by the production method described above using the die assembly 24, the sufficiently large fractured surface 14c is formed in the areas located below the cutout portions 40 in the metal sheet 30 before the cutout portions 40 are forced deeply into the metal sheet 30. As a result, the lengths of the fractured surface 14c in the sheet thickness direction in the areas below the cutout portions 40 are greater than the lengths of the fractured surface 14c in the sheet thickness direction in the other areas. Thus, by cutting the areas that will undergo stretch flanging deformation during press forming via the cutout portions 40, stretch flange cracking is prevented. In addition, in the areas cut by the planar portion 38, the lengths of the fractured surface 14c in the sheet thickness direction are shorter, and therefore the decrease in fatigue strength is suppressed.
[0107] In the die assembly 24, the cutout depth of the cutout portions 40 is set to 0.1 times or more the sheet thickness of the metal sheet 30 and 0.7 times or less the sheet thickness, for example. This configuration makes it possible to appropriately delay the time at which the cutout portions 40 begin pressing the metal sheet 30 relative to the time at which the planar portion 38 begin pressing the metal sheet 30. As a result, in the areas cut by the cutout portions 40, the fractured surface 14c has appropriate lengths in the sheet thickness direction.
[0108] The die assembly 24 of the present invention can be produced merely by partially modifying the shape of the cutting edge (a portion corresponding to the outer perimeter edge 32a of the bottom surface 32) of conventional punches. As a result, the cost of die assembly production is reduced compared with the case in which a projection is provided in the punch (see for example Patent Document 1, described above). In addition, there is no need to consider the overall tool shape for shearing tools, which are of a variety of shapes, and therefore the die assembly is readily applicable to mass production facilities. Furthermore, when stretch flange cracking has occurred during press forming, a new cutout portion 40 can be added to the punch at a location corresponding to the location where the cracking occurred in the blank, by means such as an end mill. Thus, stretch flange cracking can be addressed on-site. In this regard as well, the die assembly is readily applicable to mass production facilities. The same applies to other punches to be described later and other dies including cutout portions to be described later.
[0109] It is preferred that sites that are prone to stretch flange cracking in the sheared edge of the blank be identified in advance by performing computation or conducting a stretch flanging test. Then, the die assembly may be configured to cut the identified sites by the cutout portions. This results in reduced costs of producing the die assembly and of processing the blank.
(Other Exemplary Die Assemblies)
[0110] Although, in the embodiment described above, the description refers to a case in which the punch 26 includes rectangular cutout portions 40 in side view, the shape of the cutout portions is not limited to the example described above. For example, the punch may include cutout portions 62, which have a trapezoidal shape in side view as illustrated in
[0111] Alternatively, for example, the punch may include cutout portions 64, which have a semi-circular shape in side view as illustrated in
[0112] In the embodiment described above, the description refers to the punch 26, which includes the plurality of cutout portions 40, but it is also possible to provide the cutout portions in the die instead of providing the cutout portions in the punch.
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[0114] The punch 70 is different from the punch 26 in that the plurality of cutout portions 40 (see
(Other Exemplary Blanks)
[0115] In the embodiment described above, the description refers to the blank 10, which has the hole 10a formed by punching, but the shape of the blank is not limited to the example described above. The present invention is also applicable to a blank in which a sheared edge is formed along the outer perimeter edge, e.g., a blank having a sheared edge formed by blanking along the outer perimeter edge.
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[0117] Next, a die assembly for producing the above blank 76 will be described.
[0118] Referring to
[0119] The outer perimeter edge 88a of the bottom surface 88 includes a plurality of (two in the present embodiment: only one curved portion 92 is illustrated in
[0120] The die 86 includes a hollow support surface 98 for supporting the metal sheet (not illustrated) and an inner perimeter surface 100, which extends downwardly from an inner perimeter edge 98a of the support surface 98. In the die 86, the inner perimeter edge 98a of the support surface 98 serves as the cutting edge. The inner perimeter edge 98a of the support surface 98 has a shape similar to the shape of the outer perimeter edge 88a of the bottom surface 88, and includes a plurality of curved portions 102, which correspond to the plurality of curved portions 92 of the outer perimeter edge 88a. The curved portions 102 have a convexly curved shape corresponding to the shape of the curved portions 92. The clearance between the punch 84 and the die 86 is set to, for example, a size of approximately 10% of the sheet thickness of the metal sheet.
[0121] In the die assembly 82 as well, the punch 84 includes the cutout portions 96 as with the above punch 26. As a result, with the die assembly 82, advantageous effects similar to those of the above die assembly 24 are achieved. As with the die assembly 24a in
EXAMPLE
[0122] In the following, the present invention will be described in more detail by way of examples, but the present invention is not limited to the examples described below.
First Example
[0123] Blanks for Examples 1 to 12 were produced by forming a hole in a 780 MPa class cold-roiled steel sheet of 1.6 mm sheet thickness (workpiece). The hole had a shape (30 mm×30 mm; the radius of curvature of the curved portions (radius corners) was 5 mm) similar to the shape of the hole 10a illustrated in
[0124] The blanks produced in the above manner were subjected to burring using a truncated pyramid-shaped burring punch having a curved edge (not illustrated) to form a flange portion (burring portion) such as illustrated in
[0125] To investigate the fatigue strength of the sheared portions, test specimens such as illustrated in
[0126] Table 1 shows the configurations of the cutout portions of the punches used for punching and the results of the burring test. Table 2 shows the shear droop fraction, sheared surface fraction, and fractured surface fraction in the sheared edge at locations corresponding to stretch flanged areas and at locations not corresponding to the stretch flanged areas. It was assumed that portions (four corner portions) corresponding to the curved portions 20, which were described with reference to
TABLE-US-00001 TABLE 1 Configuration of cutout portion Width/Sheet Depth/Sheet Length/Sheet Burring height Fatigue limit thickness (%) thickness (%) thickness (%) (mm) (MPa) Example 1 75 9.4 44 6 310 Example 2 313 12.5 Entire length 12 305 Example 3 313 31.3 Entire length 16 305 Example 4 313 50 Entire length 15 310 Example 5 313 62.5 Entire length 17 315 Example 6 625 62.5 Entire length 17 305 Example 7 938 62.5 Entire length 16 310 Example 8 313 62.5 62.5 15 310 Example 9 313 62.5 187.5 16 310 Example 10 313 62.5 625 16 310 Example 11 1875 62.5 Entire length 13 305 Example 12 313 62.5 18.8 14 310 Comparative — — — 9 310 Example 1 Comparative — — — 12 270 Example 2
TABLE-US-00002 TABLE 2 Sheared edge shape of Sheared edge shape of stretch flanged area non-stretch flanged area Difference Shear Sheared Fractured Shear Sheared Fractured in fractured droop surface surface droop surface surface surface fraction fraction fraction fraction fraction fraction fraction (%) (%) (%) (%) (%) (%) (%) Example 1 7.2 33.6 59.2 6.4 36.8 56.8 2.4 Example 2 7.36 25.6 67.04 6.4 36.8 56.8 10.24 Example 3 7.44 24 68.56 6.4 36.8 56.8 11.76 Example 4 7.6 14.4 78 6.4 36.8 56.8 21.2 Example 5 7.68 12.8 79.52 6.4 36.8 56.8 22.72 Example 6 7.68 16.8 75.52 6.56 35.2 58.24 17.28 Example 7 7.84 18.4 73.76 6.56 35.2 58.24 15.52 Example 8 7.6 17.6 74.8 6.56 36 57.44 17.36 Example 9 7.68 17.6 74.72 6.56 36 57.44 17.28 Example 10 7.68 17.6 74.72 6.56 36 57.44 17.28 Example 11 8 20 72 6.56 36 57.44 14.56 Example 12 7.52 22.4 70.08 6.56 36 57.44 12.64 Comparative 6.56 36 57.44 6.56 36 57.44 0 Example 1 Comparative 72 28 64.8 7.2 28 64.8 0 Example 2
[0127] The results of the burring test indicate that the blanks of Examples 2 to 12, in which the cutout depths of the cutout portions constitute a fraction (%) within a range of 10 to 70% of the sheet thickness of the blank, achieved larger burring heights than the blank of Comparative Example 1. Furthermore, the blank of Comparative Example 2, in which the fractured surface fraction was increased over the entire perimeter of the sheared edge, had cracks in the sheared edge at areas other than the stretch flanged areas and therefore exhibited a decreased fatigue strength. On the other hand, the blanks of Examples 1 to 12 did not have cracks also at areas other than the stretch flanged areas and therefore did not have a decrease in fatigue strength.
[0128] Although, in First Example, a 780 MPa class cold-rolled steel sheet of 1.6 mm sheet thickness was used, the present inventors empirically have found that other steel sheets having different thicknesses or strengths, when used, can achieve similar advantageous effects.
Second Example
[0129] Blanks for Examples 1 to 12 having a shape similar to that of the blank 76 illustrated in
[0130]
[0131] The stretch flanging test was conducted under various conditions including different stretch flange heights hl (5 mm, 10 mm, 15 mm, 20 mm, and 25 mm), i.e., under five conditions that are different from each other in the amount of plastic deformation in the sheared edge resulting from the stretch flanging test.
[0132] Table 3 shows the configurations of the cutout portions of the punches used for shearing and the results of the stretch flanging test. Table 4 shows the shear droop fraction, sheared surface fraction, and fractured surface fraction in the sheared edge at locations corresponding to the stretch flanged areas and at locations not corresponding to the stretch flanged areas.
TABLE-US-00003 TABLE 3 Stretch Configuration of cutout portion flange Width/Sheet Depth/Sheet Length/Sheet height thickness (%) thickness (%) thickness (%) (mm) Example 1 75 9.4 44 10 Example 2 313 12.5 Entire length 15 Example 3 313 31.3 Entire length 20 Example 4 313 50 Entire length 20 Example 5 313 62.5 Entire length 25 Example 6 625 62.5 Entire length 20 Example 7 938 62.5 Entire length 25 Example 8 313 62.5 62.5 20 Example 9 313 62.5 187.5 25 Example 10 313 62.5 625 25 Example 11 1875 62.5 Entire length 15 Example 12 313 62.5 18.8 15 Comparative — — — 10 Example 1
TABLE-US-00004 TABLE 4 Sheared edge shape of Sheared edge shape of stretch flanged area non-stretch flanged area Difference Shear Sheared Fractured Shear Sheared Fractured in fractured droop surface surface droop surface surface surface fraction fraction fraction fraction fraction fraction fraction (%) (%) (%) (%) (%) (%) (%) Example 1 12 38 SO 14 42 44 6 Example 2 13 30 57 14 42 44 13 Example 3 13 27 60 14 42 44 16 Example 4 14 26 60 14 42 44 16 Example 5 15 18 67 14 42 44 23 Example 6 15 22 63 14 42 44 19 Example 7 15 17 68 14 42 44 24 Example 8 14 20 66 14 42 44 22 Example 9 15 18 67 14 42 44 23 Example 10 15 18 67 14 42 44 23 Example 11 15 27 58 14 42 44 14 Example 12 12 28 60 14 42 44 16 Comparative 14 42 44 14 42 44 0 Example 1
[0133] The results of the stretch flanging test indicate that the blanks of Examples 1 to 12 did not have stretch flange cracking in the sheared edges. In contrast, the blank of Comparative Example 1 had stretch flange cracking.
INDUSTRIAL APPLICABILITY
[0134] The present invention provides a shearing method which achieves a reduction in the cost of producing the tool, which is readily applicable to mass production facilities, and which suppresses stretch flange cracking in the sheared edge. Thus, the present invention finds high applicability in the steel processing industry.