WO2014084317A1 - 隅肉アーク溶接継手の形成方法及び隅肉アーク溶接継手 - Google Patents
隅肉アーク溶接継手の形成方法及び隅肉アーク溶接継手 Download PDFInfo
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- WO2014084317A1 WO2014084317A1 PCT/JP2013/082070 JP2013082070W WO2014084317A1 WO 2014084317 A1 WO2014084317 A1 WO 2014084317A1 JP 2013082070 W JP2013082070 W JP 2013082070W WO 2014084317 A1 WO2014084317 A1 WO 2014084317A1
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- welding
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K9/00—Arc welding or cutting
- B23K9/02—Seam welding; Backing means; Inserts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K9/00—Arc welding or cutting
- B23K9/0026—Arc welding or cutting specially adapted for particular articles or work
- B23K9/0043—Locally welding a thin plate to a thick piece
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K9/00—Arc welding or cutting
- B23K9/02—Seam welding; Backing means; Inserts
- B23K9/025—Seam welding; Backing means; Inserts for rectilinear seams
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K31/00—Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K9/00—Arc welding or cutting
- B23K9/02—Seam welding; Backing means; Inserts
- B23K9/028—Seam welding; Backing means; Inserts for curved planar seams
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K9/00—Arc welding or cutting
- B23K9/16—Arc welding or cutting making use of shielding gas
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K9/00—Arc welding or cutting
- B23K9/23—Arc welding or cutting taking account of the properties of the materials to be welded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2101/00—Articles made by soldering, welding or cutting
- B23K2101/006—Vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2101/00—Articles made by soldering, welding or cutting
- B23K2101/18—Sheet panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/02—Iron or ferrous alloys
- B23K2103/04—Steel or steel alloys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/02—Iron or ferrous alloys
- B23K2103/04—Steel or steel alloys
- B23K2103/05—Stainless steel
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G2206/00—Indexing codes related to the manufacturing of suspensions: constructional features, the materials used, procedures or tools
- B60G2206/01—Constructional features of suspension elements, e.g. arms, dampers, springs
- B60G2206/80—Manufacturing procedures
- B60G2206/82—Joining
- B60G2206/8201—Joining by welding
Definitions
- the present invention relates to a fillet arc welded joint forming method and fillet arc welded joint, and is particularly suitable for use in fillet arc welding of a plurality of metal members.
- High fatigue strength is also required for high-strength steel sheets that reduce the weight of vehicle bodies.
- the fatigue strength of the base material used for the welded member increases in proportion to the strength of the steel plate, but it is known that the fatigue strength of the welded joint hardly increases even when the strength of the steel plate increases. This hinders the weight reduction of the vehicle body due to the use of high-strength thin steel sheets.
- the fatigue strength of the welds is more important.
- Fillet arc welding is often used for welding these suspension members. Therefore, in order to achieve weight reduction of the suspension member, it is a problem to increase the fatigue strength of the fillet arc welded joint.
- the upper steel material 1 and the lower steel material 2 are overlapped and formed by welding only one of the corners on both sides of the contact portion between the upper steel material 1 and the lower steel material 2.
- the cross-sectional shape of a typical lap fillet welded joint is shown.
- stress concentrates on the toe end portion 4 and the root portion 5 of the fillet weld bead 3 and the fatigue crack propagates in a direction perpendicular to the load and the welded joint is destroyed. . Therefore, it is important to reduce the stress concentration at the toe portion 4 and the root portion 5 in order to improve the fatigue strength.
- the fillet weld bead is referred to as a fillet bead as necessary.
- the toes of the weld bead are finished by welding reinforcing members such as ribs in appropriate shapes and positions, or by grinder processing or face-up welding. Things are done.
- welding another member leads to an increase in cost. Also, it takes time to finish the toe. Therefore, these means are not technologies that can be applied to manufacture of mass-produced products such as automobile parts.
- Patent Document 1 discloses a method of improving fatigue strength by reducing the stress concentration on the toe portion by optimizing the chemical component of the weld metal and increasing the radius of curvature of the toe portion.
- Patent Document 2 discloses a weld bead structure in which an end face of the other steel plate is butted against one surface of the steel plate in a T-shaped cross section and fillet beads are formed on both sides of the butted portion to extend the weld bead.
- Patent Document 3 when the plate surface of the flat plate member and the square member are abutted with each other, the corners of the square member are welded when fillet welding is performed on all the ridges of the square member contacting the flat plate member. It is disclosed that linear weld portions that cross each other in a cross shape are formed on the part.
- an object of the present invention is to suppress the occurrence of cracks due to fatigue of a welded structural member formed by fillet welding a thin metal member.
- the method for forming a fillet arc welded joint includes an end region of a contact portion between at least one of a plate surface portion and a plate thickness portion of one metal member and a plate surface portion of the other metal member.
- a method of forming a fillet arc welded joint by performing fillet arc welding on at least a partial region of a corner having at least one curved portion at least in part, A fillet bead is formed by fillet arc welding with respect to a region including the curved portion at the corner, and arc welding different from the fillet arc welding is performed at one or a plurality of portions of at least one of the curved portions.
- the bead for stiffening is formed so that the welding start point or the welding end point of the stiffening bead overlaps the fillet bead, and the stiffening bead among the one metal member and the other metal member is formed.
- Other than not forming bead for When a repeated load that is assumed to be applied to the fillet arc welded joint is applied to the fillet arc welded joint formed under the same conditions as the meat arc welded joint, a larger tensile stress is generated.
- the stiffening bead is formed in the direction of the metal member, and at least one of the one metal member and the other metal member is formed from a metal plate having a plate thickness of 3.2 mm or less. It is characterized by being.
- the fillet arc welded joint of the present invention is a corner that is an end region of a contact portion between at least one of a plate surface portion and a plate thickness portion of one metal member and a plate surface portion of the other metal member.
- a fillet arc welded joint formed by performing fillet arc welding on at least a portion of a corner having at least one curved portion at least in part, wherein A fillet bead is formed by fillet arc welding on the region including the curved part, and at one or a plurality of places of at least one curved part by arc welding different from the fillet arc welding.
- a stiffening bead is formed, and the stiffening bead is formed such that a welding start point or a welding end point of the stiffening bead overlaps the fillet bead, and the one metal Member and the other gold It is assumed that the fillet arc welded joint formed under the same conditions as the fillet arc welded joint is added to the fillet arc welded joint except that the stiffening bead is not formed. It is formed in the direction of the metal member that generates a greater tensile stress when a repeated load is applied, and at least one of the one metal member and the other metal member is: It is formed from a metal plate having a plate thickness of 3.2 mm or less.
- FIG. 1 is a diagram showing a cross-sectional shape of a lap fillet welded joint.
- FIG. 2 is a view showing a test piece in which a lap fillet weld joint is formed.
- FIG. 3 is a diagram showing the fatigue life (times) when no stiffening bead is arranged and when a stiffening bead is arranged.
- FIG. 4 is a diagram showing the fatigue life (times) corresponding to the difference between the hardness of the stiffening bead and the maximum hardness of the steel member.
- FIG. 5 is a diagram illustrating a first example of a welded structure member.
- FIG. 6 is a diagram illustrating a second example of a welded structural member.
- FIG. 7 is a diagram illustrating a third example of the welded structure member.
- FIG. 8 is a diagram illustrating a fourth example of a welded structure member.
- FIG. 9 is a diagram illustrating a fifth example of the welded structure member.
- FIG. 10 is a diagram illustrating a fifth example of the welded structure member.
- Embodiments of a fillet arc welded joint and a method for forming the same according to the present invention will be described in detail with reference to the drawings.
- the fillet bead may be placed only on one side (not the front and back) of the thin steel plate from the viewpoint of productivity.
- the thickness portion of one thin steel plate when the thickness portion of one thin steel plate is brought into contact with the plate surface portion of the other thin steel plate and fillet welded, it can be formed on both sides of the contact portion of the one thin steel plate and the other thin steel plate. Normally, fillet arc welding is performed only on one of the corners (see FIGS. 5 to 8 described later).
- a corner (joining part) means the area
- the inventors of the present invention have proposed that at least one of the corners (joint portions) formed on both sides of the abutting portion of the steel member in which the steel member is a thin steel plate having a thickness of 3.2 mm or less.
- a fatigue test was conducted on a welded structural member in which only the joint (joint) was fillet welded. As a result, it has been found that in such a welded structural member, a fatigue crack may occur in the fillet bead.
- one corner (joint) of the corners (joint) formed on both sides of the contact portion of the two steel members is referred to as “one side corner (joint)” as necessary. ".
- the inventors further studied a means for suppressing the bending of the lower steel plate 2. As a result, it was confirmed that the occurrence of fatigue cracks can be suppressed as shown in FIG. That is, arc welding different from fillet arc welding is performed so that the position of the welding start point overlaps the fillet bead 3 and the position of the welding end point is the surface of the lower steel plate 2, A fillet bead 3 and another arc welding bead (stiffening bead 3A) are formed.
- 3 A of stiffening beads can function as a member which raises the rigidity of a steel plate and a weld metal with respect to the direction where the bending moment mentioned above is added, and can suppress the bending of the lower steel plate 2.
- FIG. Therefore, the occurrence of fatigue cracks can be suppressed.
- the bead shape at the start end of the weld bead is raised, whereas the beat shape at the end is flat, and the stress concentration at the end is reduced.
- the welding end point of the stiffening bead 3 ⁇ / b> A is the lower steel plate 2 because the compressive stress acts on the surface of the upper steel plate 1 and the tensile stress acts on the surface of the lower steel plate 2. Because it does. That is, among the steel plates 1 and 2, the steel plate to which a greater tensile stress acts when a repeated load assumed for the welded structural member is applied to the welded structural member that does not form the stiffening bead 3A. A stiffening bead 3A is formed in the direction. In each figure, a portion where the entire area of the ellipse is visible is shown as a welding end point.
- an actual test piece was prepared to examine the effect of the stiffening bead.
- the upper steel plate 1 having a plate thickness of 2.3 mm and a plate width of 35 mm is stacked on the lower steel plate 2 with a plate thickness of 2.3 mm and a plate width of 60 mm from above with a stacking allowance of 20 mm, and the overlapped portion is fillet arc welded.
- a test piece A in which a fillet bead 3 having a width of 7 mm and a length of 40 mm was formed at the end of the upper steel plate 1 was produced.
- the bead-on welding is used to weld a stiffening bead 3 ⁇ / b> A having a length of 10 mm and a width of 6 mm so that a part of the fillet bead 3 partially overlaps the fillet bead 3.
- a test piece B formed as a point was produced (see FIG. 2).
- a fatigue test of these test pieces A and B was performed. As a result, as shown in FIG. 3, when the stiffening bead was formed in the middle of the fillet bead, it was confirmed that the fatigue strength of the joint was improved.
- a fillet arc welded joint formed by joining a plate thickness portion and a plate surface portion, such as a welded joint having a T-shaped cross section. Also in this case, depending on the shape of the steel member, only one corner may be welded. The present inventors have confirmed that even when fillet arc welding is performed only on one side corner of such a fillet arc welded joint, the fillet arc welding can be handled in the same manner.
- a bead for stiffening is provided at one or a plurality of areas (second areas) of a bent portion and a curved portion of a weld line in a fillet bead region formed in a single-stroke manner. It has been found effective to form
- the first region or the second region described above is used. It is effective to form a stiffening bead at one or more locations in the region (third region) where the maximum principal stress (tensile stress) is greater than the fillet bead welding start point. It turned out to be.
- the stress in the fillet bead can be obtained, for example, by obtaining the stress distribution when a repeated load is applied to the welded structure member by FEM stress analysis using three-dimensional CAD.
- the stress in the fillet bead can also be obtained by conducting a stress addition test using an actual welded structural member and examining the strain distribution using a strain gauge or the like.
- FIG. 5 is a diagram illustrating a first example of a welded structure member.
- the welded structural member 50 shown in FIG. 5 has one end portion of a channel material (grooved steel) 51 in contact with one side surface (surface) of a box material 52 using a square steel pipe,
- the channel material 51 is formed by fillet welding only the portion outside the plate surface.
- the fillet bead 53 when forming the fillet bead 53, the region of one end of the contact portion that is the contact portion between the channel member 51 and the box member 52 and is outside the plate surface of the channel member 51 is formed. Instead of the welding start point, after forming the extended bead 54 at a position separated from the region by a certain distance along the contact portion from the region, the fillet bead 53 is continuously formed. Similarly, without using the region at the other end of the contact portion as a welding end point, the fillet bead 53 is set at a position farther from the region by a certain distance along the contact portion than the region as a welding end point. After forming, an extended bead is continuously formed.
- the fillet bead 53 formed on the welded structural member 50 has two bent portions in the middle thereof.
- the corner of the bent portion (channel material (channel steel) 51). Part) is greater in the magnitude of the maximum principal stress than the welding start position of the fillet bead 53 (extension bead).
- the stiffening beads 55A and 55B are formed so that the two bent portions of the fillet bead 53 serve as welding start points and the surface of the box material 52 serves as a welding end point, respectively. It is sufficient to form one stiffening bead at a location.
- FIG. 6 is a diagram illustrating a second example of a welded structural member.
- a welded structural member 60 shown in FIG. 6 has a pipe-shaped box material 62 using a circular steel pipe and a surface of a pipe-shaped box material 62. Of the contacted parts, only the part outside the plate surface of the channel material 61 is formed by fillet welding.
- the region of one end of the contact portion that is the contact portion between the channel member 61 and the box member 62 and is outside the plate surface of the channel member 61 is formed.
- a portion separated from the region by a certain distance along the contact portion from the region is set as the welding start point, and after forming the extended bead 64, the fillet bead 63 is continuously formed. To do.
- the region at the other end of the contact portion is not set as the welding end point, but a place away from the region by a certain distance along the contact portion from the region is set as the welding end point, and the fillet bead 63 After forming, an extended bead is continuously formed.
- the fillet bead 63 formed on the welded structural member 60 also has two bent portions in the middle, similarly to the weld bead 53 shown in FIG. Therefore, here, the stiffening beads 65A and 65B are formed so that the positions of the two bent portions of the fillet bead 63 serve as welding start points and the surface of the box material 62 serves as a welding end point, respectively. It is sufficient to form one stiffening bead at a location.
- the fillet bead 63 has a region having the same curvature as the curvature of the box material 62 (a constant curvature exceeding 0). In the welded structural member 60, it is assumed that the maximum principal stress is larger in the bent portion than in this region, and here, no stiffening bead is formed in this region.
- FIG. 7 is a diagram illustrating a third example of the welded structure member.
- the welded structure member 70 shown in FIG. 7 is brought into contact with one side surface (surface) of a box material 72 using a square steel pipe by abutting one end portion of a pipe-shaped channel material 71 using a circular steel pipe. Of the portions, only the portion outside the plate surface of the channel material 71 is formed by fillet welding. As shown in FIG. 7, the welding start point and the welding end point of the fillet bead 73 are connected to each other, and the fillet bead 73 has no start end and no end (independently).
- the fillet beads 73 formed on the welded structural member 70 generally have the same curvature as the curvature of the channel material 71 (a constant curvature exceeding 0). Therefore, when a repeated load that is assumed to be applied to the welded structural member 70 is applied to the welded structural member 70 that does not have a stiffening bead, the point at which a fatigue crack first occurs is the welding start point.
- the stiffening bead 74 is formed so that the surface of the box material 72 becomes the welding end point. Specifically, here, a point opposite to the side to which the load is applied is set as a welding start point of the stiffening bead 74. It is sufficient to form one stiffening bead at a location.
- one stiffening bead 74 is arranged on the fillet bead 73.
- a total of two stiffening beads may be arranged on each side of the stiffening bead 74 at a certain distance from the stiffening bead 74. Good.
- FIG. 8 is a diagram illustrating a fourth example of a welded structure member.
- a welded structural member 80 shown in FIG. 8 is a channel material 81 having a hollow rectangular parallelepiped shape in which a top surface and a bottom surface are opened by forming a thin steel plate on one side surface (surface) of a box material 82 using a square steel pipe. One end part is brought into contact, and only the part outside the plate surface of the channel material 81 among the contacted parts is formed by fillet welding. As shown in FIG. 8, the welding start point and the welding end point of the fillet bead 83 are connected to each other, and the fillet bead 83 has no start end and no end (independently).
- the fillet bead 83 formed in the welded structural member 80 has four bent portions in the middle.
- the portion where a fatigue crack first occurs is the bending Shall be a part. Therefore, here, the stiffening beads 84A, 84B, and 84C are formed so that the positions of the four bent portions of the fillet bead 83 are the welding start points and the surface of the box member 82 is the welding end point. . It is sufficient to form one stiffening bead at a location.
- the present inventors determined that at least one steel member to be welded by performing fillet arc welding is a steel member.
- a welded structure member formed from a steel plate having a thickness of 3.2 mm or less if the welding start position of the stiffening bead is not the fillet bead side but the box material side, even if the stiffening bead is formed, It has been found that the fatigue life does not improve, but may decrease. That is, the present inventors form a stiffening bead when the welding start position of the stiffening bead exists alone in the region near the fillet bead without intersecting with other welding beads. However, it has been found that the fatigue life is not improved and may be lowered.
- the welding start position of the stiffening bead does not exist alone in the region near the fillet bead without intersecting with other weld beads, and the fillet bead
- the stiffening bead is formed so that the welding start point or the welding end point is located in a region (curved portion) where the corner is bent.
- this embodiment it is a region between the welding start point and the welding end point of the fillet bead formed in a single stroke in one welding operation, and the corner is bent ( A stiffening bead is formed on the curved portion.
- the fillet bead welding operation and the stiffening bead welding operation are performed separately. That is, the fillet bead and the stiffening bead are formed by separate arc welding, and the welding start point or welding end point of the stiffening bead formed so as to overlap the fillet bead is distinguished from the fillet bead. To remain in the state.
- FIGS. 5 to 8 show examples of fillet arc welded joints in which the plate thickness portion of one steel member and the plate surface portion of the other steel member are joined to each other.
- FIG. 9 is a diagram illustrating a fifth example of the welded structure member.
- the welded structural member 90 shown in FIG. 9 has a box material 92 on the back surfaces of the flange portions on both sides of a channel material (channel steel processed so that the tip portions of the flange portions on both sides are curved with a certain curvature) 91. It attaches to the mutually opposing side surface, and it forms by pile-up-welding the front-end
- the extension bead 94A is formed at a position separated from the region by a certain distance along the curvature of the curved region rather than the region, and then the fillet bead 93 is continuously formed.
- the region at the other end of the boundary between the distal end portion and the proximal end portion of the flange portion is not a welding end point, and is separated from the region by a certain distance along the curvature of the curved region rather than the region.
- the fillet bead 93 formed on the welded structural member 90 generally has the same curvature as the curvature of the tip of the flange portion of the channel material 91 (a constant curvature exceeding 0). Therefore, when a repeated load that is assumed to be applied to the welded structural member 90 is applied to the welded structural member 90 that does not have a stiffening bead, the point where a fatigue crack first occurs is the welding start point.
- the stiffening bead 95 is formed so that the surface of the box material 92 becomes the welding end point. Specifically, here, the central portion (the deepest portion) in the direction along the weld line of the fillet bead 93 is set as the welding start point of the stiffening bead 95. It is sufficient to form one stiffening bead at a location.
- one stiffening bead 95 is arranged at the deepest part of the fillet bead 93.
- two stiffening beads one each in the vicinity of the length position of 1/3 and 2/3 of the fillet bead 95, may be arranged. Good.
- the stacked fillet bead, the extension bead and the stiffening bead are provided.
- a bead is formed.
- FIG. 9 shows an example of a fillet arc welded joint (lap fillet arc welded joint) in which plate portions of one steel member and the other steel member are joined to each other.
- FIG. 10 is a diagram illustrating a sixth example of a welded structure member.
- a welded structural member 100 shown in FIG. 10 has a box material 52 using a square steel pipe, and one set of surfaces of the two opposing surfaces of the tip of the square steel pipe matches the shape of the box material 52.
- the flange material 51 cut out.
- the back surface of the portion of the flange material 51 that is not cut is in contact with the surface of the box material 52, and the plate thickness portion of the portion of the flange material 51 that is cut off is the surface of the box material 52.
- the welded structural member 100 is formed by combining the box material 52 and the flange material 51 and performing fillet welding of the contact portion.
- the fillet bead 103 formed on the welded structural member 100 has a bent portion in the middle thereof.
- the fatigue crack first occurs at the tip of the flange member 51.
- it is a bent part in the corner part where the plate
- the stiffening beads 104A and 104B are formed so that the positions of these two bent portions of the fillet bead 103 become welding start points and the surface of the box material 102 becomes the welding end point, respectively. It is sufficient to form one stiffening bead at a location.
- FIG. 10 shows an example of a fillet arc welded joint in which both the plate surface portion and the plate thickness portion of one steel material are joined to the plate surface portion of the other steel material. Moreover, as shown in FIG. 10, it is not necessary to form a stiffening bead for all of the bent portions at the corners.
- At least one steel member to be welded by performing fillet arc welding is a welded structure member (fillet arc welded joint) formed from a steel plate having a thickness of 3.2 mm or less.
- a welded structural member (fillet arc welded joint) to which a repeated load such as a vibration load is applied is an object. This is because such a welded structural member is likely to generate a fatigue crack at the toe portion or root portion of the fillet weld bead and is required to improve the fatigue strength by simple means.
- the present invention is directed to a welded structural member having a corner portion having at least one curved portion. Furthermore, the present invention is directed to a welded structure member in which a fillet bead is formed in a single stroke manner so as to include at least one of the curved portions.
- the curved portion may be a bent portion or a curved portion. Further, the curvature of the music part may be constant or may change. Further, if there is at least one fillet bead formed in a single-stroke manner, the number of fillet beads formed in one welded structure member may be one or plural.
- welding of the stiffening bead can be easily performed by performing welding of the stiffening bead following the fillet welding using the welding machine and welding material used for forming the fillet bead.
- the fatigue strength can be improved.
- the welding start position or the welding end position of the stiffening bead it is necessary to form the welding start position or the welding end position of the stiffening bead so as to overlap the fillet bead. This is because if the stiffening bead is formed apart from the fillet bead, it does not function as a member that increases the rigidity of the steel plate.
- the position where the fillet bead overlaps is set as the welding start point, and among the steel members constituting the corner (joint portion), the surface of the steel member on which a large tensile stress acts on the surface is the welding end point.
- a stiffening bead is formed. As described above, at the welding start point, the shape of the toe portion is swelled and the swell angle is steep, so stress concentration easily occurs.
- the welding start point of the stiffening bead overlaps with one fillet bead and the welding end point is the other fillet bead. It will overlap. That is, either the welding start point or the welding end point of the stiffening bead overlaps with the fillet bead, and the welding start point of the stiffening bead does not exist independently of other welding beads. I just want to do it. This is because it is possible to prevent the bead shape at the position of the welding start point of the stiffening bead from rising.
- the welding start point of the stiffening bead exists independently without intersecting with other welding beads. This is because if such a location is used as the welding start point of the stiffening bead, the fatigue strength of the fillet arc welded joint is not greatly affected even if the bead shape of the location is raised.
- the stiffening bead may be formed on the fillet weld bead, or a weld bead corresponding to the stiffening bead is arranged in advance before fillet welding, and the fillet bead is placed thereon. It is also possible to arrange. That is, if the welding start position or welding end position of the stiffening bead overlaps with the fillet bead, the stiffening bead may be above or below the fillet bead.
- the welding end point of the stiffening bead is more when a load is repeatedly applied to the welded structure member among the steel members constituting the corner (joint portion). As a rule, the area of the steel plate is to be subjected to a large tensile stress. This is because, at the welding end point, the bead shape is flat, and stress concentration is unlikely to occur.
- the arrangement position of the stiffening bead with respect to the fillet bead is one of at least one of the second region, the third region, and the fourth region on the assumption that the first region is provided. Or multiple locations. Further, if the stiffening bead is arranged in such a region, the stiffening bead may be arranged in another region.
- the length La of the stiffening bead satisfies the following condition (A).
- the length La of the stiffening bead is the length from the contact point between the fillet bead and the stiffening bead to the melting end of the stiffening bead.
- the length La of the stiffening bead When the length La of the stiffening bead is short, the rigidity of the steel member cannot be sufficiently increased, and the function of improving the fatigue strength of the welded joint cannot be exhibited. If the length La of the stiffening bead protruding from the toe portion of the fillet bead is equal to or greater than the width W of the fillet bead, it exhibits a function to improve fatigue strength depending on the degree of load applied to the welded structure member However, in order to further increase the rigidity, it is preferable that the length of the stiffening bead is at least twice the width W of the fillet bead.
- the upper limit of the length La of the stiffening bead is restricted by the shape and structure of the steel product manufactured by welding.
- the length La of the stiffening bead can be made less than 0.5 ⁇ L.
- the height Ha from the surface of the steel member of the stiffening bead preferably satisfies the following condition (B) with respect to the thickness t (mm) of the steel member forming the stiffening bead.
- B Stiffening bead height Ha ⁇ steel member thickness t ⁇ 0.5
- the greater the height Ha of the stiffening bead the greater the effect, but there is a limit in order to avoid slipping through and melting through the steel plate. Therefore, it is realistic to set the height Ha of the stiffening bead to be equal to or less than the thickness t of the steel member on which the stiffening bead is formed.
- width Wa of the stiffening bead satisfies the following condition (C).
- C Stiffening bead width Wa ⁇ fillet bead width W ⁇ 0.5
- the width Wa of the stiffening bead is less than 0.5 times (W / 2) the width W of the fillet bead, the function as the stiffening bead is not sufficiently exhibited.
- the upper limit of the width Wa of the stiffening bead is not particularly defined, it is necessary to form the stiffening bead within a range in which it does not pass through or melt down, similarly to the height Ha of the stiffening bead. Will be determined automatically.
- the length, width, and height of the stiffening bead are preferably selected within the aforementioned range.
- the hardness of the stiffening bead that is, the hardness Hw of the weld metal of the stiffening bead is the following (D) with respect to the steel plate maximum hardness Hb of the steel member on which the stiffening bead is placed. It is preferable to satisfy the condition. (D) Hardness Hw of weld metal of stiffening bead> Maximum hardness Hb of steel plate When the hardness Hw of the weld metal of the stiffening bead is larger than the maximum hardness Hb of the steel plate, the strain concentration on the weld toe is suppressed, and the fatigue life (number of times) can be improved.
- the hardness Hw of the weld metal of the stiffening bead is measured as follows. First, the portion of the welded structural member where the stiffening bead is formed is cut perpendicular to the weld line at the center in the longitudinal direction of the stiffening bead, and the cut surface is polished. Then, the hardness is measured in the direction parallel to the surface of the steel plate (base material) at the position of the cut surface at a depth of 0.2 mm from the surface of the steel plate (base material) in the thickness direction.
- the steel sheet maximum hardness Hb is measured as follows. First, the portion of the welded structural member where the stiffening bead is formed is cut perpendicular to the weld line at the center in the longitudinal direction of the stiffening bead, and the cut surface is polished. Then, the hardness is measured in the direction parallel to the surface of the steel plate (base material) at the position of the cut surface at a depth of 0.2 mm from the surface of the steel plate (base material) in the plate thickness direction.
- the Vickers hardness is measured with a Vickers hardness meter at a distance of 10 mm from the melting boundary at a 0.2 mm interval in the base material direction starting from one point of the melting boundary at the position, and the maximum value among them Is the steel plate maximum hardness Hb.
- the hardness of a fusion boundary is excluded.
- the load applied during measurement is preferably 1 kgf.
- the starting point when measuring the hardness Hw (Vickers hardness) of the weld metal of the stiffening bead is matched with the starting point when measuring the maximum hardness Hb (Vickers hardness) of the steel plate,
- the direction in which the hardness Hw (Vickers hardness) of the weld metal of the rigid bead is measured and the direction in which the steel plate maximum hardness Hb (Vickers hardness) is measured are opposite to each other (the angle between these directions is 180 °).
- the angle ⁇ of the stiffening bead satisfies the following condition (E).
- E 45 ° ⁇ angle of stiffening bead ⁇ ⁇ 135 °
- the angle ⁇ of the stiffening bead is preferably 45 to 135 °. When the angle ⁇ is less than 45 ° or more than 135 °, the function of the stiffening bead is deteriorated.
- the stiffening bead is formed as shown in FIGS. 5 to 9 (the curved portion at the corner (joining portion) is formed on one surface of the box members 52, 62, 72, 82, and 92.
- the angle ⁇ of the stiffening bead is the angle relative to the tangent at the point where it overlaps the stiffening bead of the fillet bead.
- the stiffening bead is formed as shown in FIG. 10 (when the curved portion at the corner (joining portion) is formed on two continuous surfaces of the box material 102), the stiffening bead is formed.
- the bead angle is defined as an angle formed by the fillet bead and the stiffening bead on the surface on which the stiffening bead is formed.
- the arc welding conditions and the composition of the welding wire used at the time of construction of the fillet bead and the stiffening bead may be in accordance with ordinary methods and are not limited to specific ones. However, as described above, it is preferable in production to perform the fillet bead construction and the stiffening bead construction continuously using the same welding equipment. However, as long as the function of increasing the rigidity of the steel plate of the stiffening bead is ensured, the welding conditions of the two and the composition of the welding wire used may be different.
- a stiffening bead is placed around the welded joint at the required angle, and the required length, height, and width. It is necessary that there is a region that can be formed by.
- the fatigue strength of a steel member can be greatly improved only by providing a stiffening bead.
- a joint with improved fatigue strength can be obtained by combining the construction for reducing the stress concentration at the start and end points of welding and the construction of the stiffening bead.
- the fillet bead is extended from the corner, and the welding start point and the welding end point of the fillet bead are arranged at positions away from the corner, respectively.
- the stiffening bead can be applied on top (i.e., after forming the aforementioned extension bead).
- such an extension of the fillet bead is not always necessary.
- the present inventors have confirmed that the method of this embodiment can be applied even to a metal member other than a steel member.
- the technique of this embodiment can be applied to an aluminum member or a stainless steel member instead of a steel member.
- the present inventors have confirmed that the method of the present embodiment can be applied to different types of metal members.
- welded structural members 50, 60, 70, 80, 90, 100 having the shapes shown in FIGS. 5 to 10 were produced. Further, except that the welding start point and the welding end point of the stiffening bead are interchanged, weld structure members having the same shape as the weld structure members 50, 60, 70, 80, 90, 100 shown in FIGS. did. Further, weld structure members having the same shape as the weld structure members 50, 60, 70, 80, 90, and 100 shown in FIGS. 5 to 10 were produced except that no stiffening bead was formed. These welded structural members were subjected to a fatigue test.
- Table 1 shows steel members and welding materials used for welded structural members.
- steel material A and steel material B were used.
- steel plate A and the steel plate B two plate thicknesses (2.3 mm, 2.6 mm) were prepared.
- wire A and wire B were used as the steel plate A and the steel plate B.
- the diameter of the wire A and the wire B is 1.2 mm.
- the size of the box material 52 shown in FIG. 5 is 300 mm ⁇ 150 mm ⁇ 50 mm.
- the size of the channel material 51 is flange width 80 mm ⁇ web width 75 mm ⁇ height 80 mm.
- the size of the box member 62 shown in FIG. 6 is 150 mm in diameter ⁇ 300 mm in height (length in the axial direction).
- the size of the channel member 61 is: flange width 80 mm ⁇ corner portion (joint portion) web width 75 mm ⁇ height (maximum value) 80 mm.
- the size of the box material 72 shown in FIG. 7 is 300 mm ⁇ 100 mm ⁇ 50 mm.
- the size of the channel member 71 is 50 mm in diameter ⁇ 150 mm in height (length in the axial direction).
- the size of the box material 82 shown in FIG. 8 is 300 mm ⁇ 150 mm ⁇ 50 mm.
- the size of the channel material 81 is 180 mm ⁇ 75 mm ⁇ 56 mm.
- the size of the box material 92 shown in FIG. 9 is 300 mm ⁇ 100 mm ⁇ 50 mm.
- the size of the channel member 91 is flange width 75 mm ⁇ web width 105 mm ⁇ height 80 mm.
- the radius of curvature of the tip of the flange of the channel material 81 is 50 mm.
- the size of the box material 102 shown in FIG. 10 is 300 mm ⁇ 100 mm ⁇ 50 mm.
- the channel material 101 is obtained by cutting out a portion of a square steel pipe of 180 mm ⁇ 75 mm ⁇ 56 mm having a length of 56 mm from the tip thereof by 30 mm.
- a stiffening bead was formed for each of the case where the welding start point of the stiffening bead (the start position of the stiffening bead in Table 2) was placed on the fillet bead and the box material.
- the welding start point of the stiffening bead is set on the fillet bead, and the welding end point of the stiffening bead (end of the stiffening bead in Tables 2 to 12) is set on the box material.
- the stiffening bead is formed for each of the case where the welding start point of the stiffening bead is placed on the fillet bead and the welding end point of the stiffening bead is placed on the channel material. did.
- the stiffening bead was formed for each of the case where the stiffening bead was formed at the curved portion at the corner (joined portion) and the case where the stiffening bead was formed at the straight portion at the corner. Further, the stiffening bead was formed by changing the length La of the stiffening bead, the height Ha of the stiffening bead, and the width Wa of the stiffening bead.
- the welding conditions are as follows. ⁇ Common welding conditions> Welding method Consumable electrode welding Welding power supply DP350 (Daihen Co., Ltd.) Welding mode DC-Pulse Welding posture Downward horizontal Distance between tip steel plates (extrusion length) 15mm Shield gas type Ar + 20% CO 2 Shielding gas flow rate 20L / min ⁇ Conditions for forming fillet beads> Torch angle Raise angle from lower plate 60 °, advance angle 0 ° Target position Corner of overlapped part Welding speed 80cm / min Welding current and voltage Set values so that undercut does not occur.
- the electro-hydraulic type of one of the steel members (box material) and the other steel member (channel material) of the prepared test specimen is so arranged that the direction of load is the direction indicated by the white arrows in FIGS.
- the sample was gripped by a fatigue test apparatus and subjected to a fatigue test with a constant load range (constant stress range), a load ratio of ⁇ 1, and a repetition frequency of 5 Hz.
- the hardness Hw of the stiffening bead and the maximum steel sheet hardness Hb were measured by the methods described above. The effects of the embodiment will be described based on Tables 2 to 12.
- Specimen symbols C1, C5, C7, C9, C11, and C14 are welded structural members 50, 60, 70, 80, and 90 shown in FIGS. 5, 6, 7, 8, 9, and 10, respectively.
- , 100 is a result of a welded structural member that does not form a stiffening bead. Based on the fatigue life of these welded structural members, the effect of the stiffening bead was verified. The “fatigue life improvement rate” was calculated based on the fatigue life of the test piece symbols described in “Reference Test Piece Symbols” in Tables 2 to 12. In this example, when the “fatigue life improvement rate” exceeds 120%, it is determined that the effect of the stiffening bead is obtained.
- D1 to D9 are evaluations of the effect of the stiffening bead for the welded structural member 50 shown in FIG.
- the bead for stiffening was not formed, a crack occurred at the weld toe portion on the box material 52 side in the bent portion of the fillet bead 53 (see “crack generation position” in C1). For this reason, it is necessary to increase the fatigue life of this location with the stiffening beads 55A and 55B. Therefore, the bead for stiffening 55A, 55B was formed with the position of the bent portion of the fillet bead 53 as the welding start position and the surface of the box material 52 as the welding end position (D1 to D9, “Start of stiffening bead”). (See “Inside the box” in “Position bead angle” in “Position” and “End position of stiffening bead”).
- the length La of the stiffening bead is not more than twice the width W of the fillet bead (“La / W” of D1 does not exceed 200% and satisfies the condition (A). Absent).
- the angle ⁇ of the stiffening bead is not in the range of 45 ° to 135 ° (the “angle of stiffening bead” in D2 does not become 45 ° to 135 ° and does not satisfy the condition (E)). .
- the height Ha of the stiffening bead is not more than 0.5 times the thickness t of the steel member on which the stiffening bead is formed, and the width Wa of the stiffening bead is the fillet bead.
- the maximum hardness (steel plate maximum hardness Hb) of the box material in which the crack occurs does not exceed the hardness Hw (welding metal) of the stiffening bead (D8 “stiffening bead weld metal”).
- the “hardness Hw” does not exceed the “box material maximum hardness Hb” and does not satisfy the condition (D)).
- the fatigue life improvement rate exceeded 120%.
- D10 is an evaluation of the effect of the stiffening bead for the welded structural member 60 shown in FIG.
- the stiffening bead was not formed, a crack occurred at the weld toe portion on the box material 62 side in the bent portion of the fillet bead 63 (see “crack generation position” in C5).
- the stiffening beads 65A and 65B were formed with the bent portion of the fillet bead 63 as the welding start position and the surface of the box material 62 as the welding end position (see “Starting position of stiffening bead” in D10). (Refer to “Box top” in “Bead corner” and “End position of stiffening bead”).
- stiffening beads 65A and 65B As shown in D10, by forming the stiffening beads 65A and 65B as described above, the fatigue life is increased, and the crack is generated from the toe portion of the fillet bead 63 to the stiffening bead 65A. , 65B (refer to “Stiffening bead termination” in “Crack occurrence position” in D10). Although not shown in the table, even with the welded structure member 60 shown in FIG. 6, the fatigue life improvement allowance tends to decrease unless the conditions (A) to (E) described above are satisfied. confirmed.
- D11 is an evaluation of the effect of the stiffening bead for the welded structure member 70 shown in FIG.
- a crack occurred at the weld toe portion on the side of the box member 72 at a position opposite to the point where the load of the fillet bead 73 was applied (C7 (See Crack initiation position). Therefore, this portion of the fillet bead 73 is set as the welding start position, and the surface of the box material 62 is set as the welding end position, so that the stiffening bead 74 is formed (“fillet” of “starting position of the stiffening bead” in D11). (Refer to “On box” in “Bead end” and “End position of stiffening bead”).
- D12 is an evaluation of the effect of the stiffening bead for the welded structural member 80 shown in FIG.
- the stiffening bead was not formed, a crack occurred at the weld toe portion on the box material 82 side in the bent portion of the fillet bead 83 (see “crack generation position” in C9). For this reason, it is necessary to increase the fatigue life of this location by the stiffening beads 84A, 4B, 84C.
- stiffening beads 84A, 84B, and 84C were formed with the bent portion of fillet bead 83 as the welding start position and the surface of box member 82 as the welding end position (D12 "starting position of stiffening bead” in D12). (Refer to “Box on the box” in “Corner bead angle” and “End position of stiffening bead”). In addition, the stiffening bead was formed in the other bent portion which is hidden in FIG. 8 like the other stiffening beads.
- D13 to D20 are evaluations of the effect of the stiffening bead for the welded structural member 90 shown in FIG.
- a stiffening bead 95 is formed with the center portion of the fillet bead 93 in the direction along the weld line as the welding start position and the surface of the box material 92 as the welding end position (D13 to D20, “stiffening beads”).
- the length La of the stiffening bead is not more than twice the width W of the fillet bead (“La / W” in D13 does not exceed 200% and satisfies the condition (A). Absent).
- the angle ⁇ of the stiffening bead is not in the range of 45 ° to 135 ° (“La / W” in D14 does not exceed 200% and does not satisfy the condition (E)).
- the height Ha of the stiffening bead is not more than 0.5 times the thickness t of the steel member on which the stiffening bead is formed, and the width Wa of the stiffening bead is the fillet bead.
- the width W is not more than 0.5 times the width W (“Ha / t” of D15 does not exceed 50% and does not satisfy the condition of (B), and “Wa / W” of D15 does not exceed 50% and (C )
- the maximum hardness (steel plate maximum hardness Hb) of the box material in which a crack occurs does not exceed the hardness Hw (of the weld metal) of the stiffening bead (the “welding bead welding metal for D19”).
- the “hardness Hw” does not exceed the “box material maximum hardness Hb” and does not satisfy the condition (D)).
- the fatigue life improvement rate exceeded 120%.
- D21 is an evaluation of the effect of the stiffening bead for the welded structural member 100 shown in FIG.
- the stiffening bead if the stiffening bead is not formed, a weld toe portion on the box material 102 side in the bent portion of the fillet bead 103 that is in contact with the plate surface portion of the channel material 101 can be formed. A crack has occurred (see “crack generation position” in C14). For this reason, it is necessary to increase the fatigue life of this location with the stiffening beads 104A and 104B.
- the bends 104A and 104B for stiffening were formed with the bent portion of the fillet bead 103 as the welding start position and the surface of the box material 102 as the welding end position (the “starting position of the stiffening bead” in D21). (Refer to “Box top” in “Corner bead angle” and “End position of stiffening bead”).
- C3 shows the result of replacing the welding start point and the welding end point of the stiffening bead with respect to the welded structural member 50 shown in FIG. C4 is the width direction of the web of the channel material 51 in the region of the fillet bead 53 without forming a stiffening bead at the bent portion of the fillet bead 53 with respect to the welded structure member 50 shown in FIG.
- the result of forming a bead for stiffening with the inside of the fillet bead 53 as the welding start position and the surface of the box material 52 as the welding end position is shown in the center region.
- the fatigue life improvement rate was less than 120%.
- C6 shows the result of replacing the welding start point and the welding end point of the stiffening bead with respect to the welded structural member 60 shown in FIG. C8 shows the result of replacing the welding start point and the welding end point of the stiffening bead with respect to the welding structural member 70 shown in FIG. C10 shows the result of replacing the welding start point and the welding end point of the stiffening bead with respect to the welding structural member 80 shown in FIG.
- the fatigue life improvement rate was less than 120%.
- C12 a crack is generated when a load is applied to the welding structural member 90 shown in FIG. 9 at the welding end point of the stiffening bead, and the welding structural member 90 not forming the stiffening bead.
- the results for the channel material 91 side instead of the box material 92 side are shown.
- C13 shows the result of replacing the welding start point and the welding end point of the stiffening bead with respect to the welded structural member 90 shown in FIG. In both cases of C12 and C13, the fatigue life improvement rate was less than 120%.
- C15 shows the result of replacing the welding start point and the welding end point of the stiffening bead with respect to the welded structural member 100 shown in FIG.
- the fatigue life improvement rate was less than 120%.
- the present invention can be used, for example, in an industrial field using welding such as machine industry.
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Abstract
Description
特許文献1には、溶接金属の化学成分を最適化して止端部の曲率半径を大きくすることにより、止端部への応力集中を低減して疲労強度を向上させる方法が開示されている。
特許文献2には、鋼板の一面に他方の鋼板の端面を断面T形に突き合わせ、突き合わせ部分の両側に隅肉ビードを形成する際、溶接ビードを延長する溶接ビード構造が開示されている。
また、特許文献2に開示された技術では、溶接ビードを延長することにより、溶接ビードの溶接開始点(始端部)と、溶接ビードの溶接終了点(終端部)の疲労強度は向上する。しかしながら、溶接ビードの中間部の疲労強度の向上に対しては効果がほとんどない。
例えば、自動車用の薄鋼板を隅肉溶接する場合、生産性の観点から、薄鋼板の(表裏ではなく)片側のみにしか、隅肉ビードを置かないことがある。
なお、隅部(接合部)とは、一方の金属部材の板面部分および板厚部分の少なくとも何れか一方と、他方の金属部材の板面部分との当接部分の端の領域をいう。このような隅部(接合部)の少なくとも一部の領域に対して隅肉アーク溶接が行われる。
その結果、図2に示すようにすれば、疲労き裂の発生を抑制することができることを確認した。すなわち、溶接開始点の位置が隅肉ビード3と重なるようにするとともに溶接終了点の位置が下側鋼板2の表面になるようにして、隅肉アーク溶接とは別のアーク溶接を行って、隅肉ビード3と別のアーク溶接ビード(補剛用ビード3A)を形成する。このようにすれば、補剛用ビード3Aが、前述した曲げモーメントが付加される方向に対する鋼板及び溶接金属の剛性を高める部材として機能して下側鋼板2の曲がりを抑制することができる。したがって、疲労き裂の発生を抑制することができる。前述したように、溶接ビードの始端部のビード形状は盛り上がる形状となるのに対し、終端部のビート形状は扁平となり、終端部の応力集中は低減するからである。
尚、各図では、楕円全体の領域が見えている箇所を溶接終了点として示している。
試験片として、板厚2.3mm、板幅60mmの下側鋼板2に、板厚2.3mm、板幅35mmの上側鋼板1を上から重ね代20mmで重ね、重ね部を隅肉アーク溶接して、上側鋼板1の端部に、幅7mm、長さ40mmの隅肉ビード3を形成した試験片Aを作製した。
次に、隅肉ビード3に加え、さらに隅肉ビード3の中央部に一部が重なるように、ビードオン溶接により長さ10mm、幅6mmの補剛用ビード3Aを、隅肉ビード3を溶接開始点として形成した試験片Bを作製した(図2参照)。
これらの試験片A、Bの疲労試験を実施した。
その結果、図3に示すように、隅肉ビードの途中に補剛用ビードを形成した場合には、継手の疲労強度が向上することが確認された。
硬さが182Hvの鋼板1、2を用いるとともに、硬さHwが150Hvの溶接金属を用いて、前述した試験片Aと同様の試験片Cを形成して疲労試験を実施した。
また、硬さが192Hvの鋼板1、2を用いるとともに、硬さHwがそれぞれ150、183、270の溶接金属を用いて、前述した試験片Bと同様の試験片D、E、Fを形成して疲労試験を実施した。
尚、図4の「-36」、「1」、及び「88」は、補剛用ビードの硬さHwから鋼部材最大硬さHbを減算した値を示す。また、鋼板最大硬さHbと補剛用ビードの硬さHwについては後述する。
また、前述した第1の領域、第2の領域、または第3の領域のうち、補剛用ビードを形成していない溶接構造部材に付加されると想定される繰り返し荷重を当該溶接構造部材に付加した際に疲労き裂が最初に発生する領域(第4の領域)に補剛用ビードを形成することが有効であることが判明した。疲労き裂が最初に発生する個所は最大主応力の大きさが最大(引張応力が最大)になる個所に対応する。
特に、隅肉ビードの溶接線の曲率が一定である場合には、このような第4の領域に補剛用ビードを形成することが有効である。
図5は、溶接構造部材の第1の例を示す図である。
図5に示す溶接構造部材50は、角型鋼管を用いたボックス材52の一つの側面(表面)に、チャンネル材(溝形鋼)51の一端部を当接させ、当接した部分のうち、チャンネル材51の板面の外側にある部分のみを隅肉溶接することにより形成される。
そこで、ここでは、隅肉ビード53の2カ所の屈曲部が溶接開始点となり、ボックス材52の表面が溶接終了点となるように、それぞれ補剛用ビード55A、55Bを形成する。補剛用ビードは一箇所に1本ずつ形成すれば十分である。
図6に示す溶接構造部材60は、円形鋼管を用いたパイプ状のボックス材62の表面に、チャンネル材(一端をパイプ材の形状に合わせて加工した溝形鋼)61の当該一端部を当接させ、当接した部分のうち、チャンネル材61の板面の外側にある部分のみを隅肉溶接することにより形成される。
図7に示す溶接構造部材70は、角型鋼管を用いたボックス材72の一つの側面(表面)に、円形鋼管を用いたパイプ状のチャンネル材71の一端部を当接させ、当接した部分のうち、チャンネル材71の板面の外側にある部分のみを隅肉溶接することにより形成される。
図7に示すように、隅肉ビード73の溶接開始点と溶接終了点とは連結され、隅肉ビード73には始端部と終端部が(独立して)存在しない。
図8に示す溶接構造部材80は、角型鋼管を用いたボックス材82の一つの側面(表面)に、薄鋼板を成形して上面と下面とが開口した中空直方体形状としたチャンネル材81の一端部を当接させ、当接した部分のうち、チャンネル材81の板面の外側にある部分のみを隅肉溶接することにより形成される。
図8に示すように、隅肉ビード83の溶接開始点と溶接終了点とは連結され、隅肉ビード83には始端部と終端部が(独立して)存在しない。
そこで、ここでは、隅肉ビード83の4カ所の屈曲部の位置が溶接開始点となり、ボックス材82の表面が溶接終了点となるように、それぞれ補剛用ビード84A、84B、84Cを形成する。補剛用ビードは一箇所に1本ずつ形成すれば十分である。
また、隅肉ビードの溶接作業と補剛用ビードの溶接作業とを別々に行う。すなわち、隅肉ビードと補剛用ビードとを別のアーク溶接で形成し、隅肉ビードと重なるように形成される補剛用ビードの溶接開始点または溶接終了点が、隅肉ビードと区別される状態で残るようにする。
以上のようにすることにより、補剛用ビードの溶接開始点及び溶接終了点の位置の自由度が向上する。したがって、隅肉ビードの近くの位置で、他の溶接ビードと交わらずに単独で存在してしまう溶接開始点の数が必要以上に多くなってしまうことを抑制することができる。
以上の図5~図8は、一方の鋼部材の板厚部分と他方の鋼部材の板面部分が相互に接合された隅肉アーク溶接継手の例を示すものである。
図9に示す溶接構造部材90は、チャンネル材(両側のフランジ部の先端部のそれぞれが一定の曲率で湾曲するように加工された溝形鋼)91の両側のフランジ部の裏面をボックス材92の相互に対向する側面に取り付け、フランジ部の先端部を重ね隅肉溶接することにより形成される。図9に示すように、隅肉ビード93を形成する際には、フランジ部の先端部と基端部との境界(前記湾曲した領域とその他の領域と境界)の一端の領域を溶接開始点とせずに、当該領域よりも当該湾曲した領域の曲率に沿って一定の距離だけ当該領域から離れた箇所を溶接開始点として延長ビード94Aを形成した後、隅肉ビード93を連続して形成する。同様に、フランジ部の先端部と基端部との境界の他端の領域を溶接終了点とせずに、当該領域よりも前記湾曲した領域の曲率に沿って一定の距離だけ当該領域から離れた箇所を溶接終了点として隅肉ビード93を形成した後、延長ビード94Bを連続して形成する。
前述したように、チャンネル材91のフランジ部の反対側にも、隅肉ビード93、延長ビード94A、94B、及び補剛用ビード95と同様に、重ね隅肉ビード、延長ビード、及び補剛用ビードが形成されている。
図9は、一方の鋼部材と他方の鋼部材の板面部分同士が相互に接合された隅肉アーク溶接継手(重ね隅肉アーク溶接継手)の例を示すものである。
図10に示す溶接構造部材100は、角型鋼管を用いたボックス材52と、角型鋼管の先端部の相互に対向する二組の面のうち一組の面がボックス材52の形状に合わせて切り取られたフランジ材51とを用いて構成される。フランジ材51の先端部の切り取られていない部分の裏面がボックス材52の表面と当接するとともに、フランジ材51の先端部が切り取られた部分の板厚部分がボックス材52の表面に当接するように、ボックス材52とフランジ材51とが組み合わせて、当接部を隅肉溶接することにより溶接構造部材100が形成される。
図10は、一方の鋼材の板面部分と板厚部分の双方が他方の鋼材の板面部分に接合された隅肉アーク溶接継手の例を示すものである。また、図10に示すように、隅部の屈曲部の全てに対して補剛用ビードを形成しなくてもよい。
(溶接構造部材)
本実施形態では、隅肉アーク溶接を行って溶接される鋼部材の少なくとも一方の鋼部材が、板厚3.2mm以下の鋼板から形成される溶接構造部材(隅肉アーク溶接継手)を対象とする。また、振動荷重のような繰り返し荷重が付加される溶接構造部材(隅肉アーク溶接継手)を対象とする。
そのような溶接構造部材は、隅肉溶接ビードの止端部またはルート部に疲労き裂が発生しやすく、簡単な手段により疲労強度を向上させることが求められているためである。
このような溶接構造部材であれば、隅肉ビードの形成に用いる溶接機及び溶接材料を用いて、隅肉溶接の後に続いて補剛用ビードの溶接を行うことにより、簡単に溶接構造部材の疲労強度を向上させることができる。
補剛用ビードの溶接開始位置または溶接終了位置は、隅肉ビードと重なるように形成する必要がある。補剛用ビードが隅肉ビードと離れて形成されると、鋼板の剛性を高める部材として機能しないからである。
本実施形態では、隅肉ビードと重なる位置を溶接開始点にするとともに、隅部(接合部)を構成する鋼部材のうち、表面により大きな引張の応力が作用する鋼部材の表面を溶接終了点として、補剛用ビードを形成することを原則とする。前述したように、溶接開始点では、止端部の形状が盛り上がり、且つ、盛り上がりの角度が急峻なため、容易に応力集中が生じるからである。
一方、本実施形態では、補剛用ビードの溶接終了点は、前述したように、隅部(接合部)を構成する鋼部材のうち、溶接構造部材に繰り返し荷重が付加された際に、より大きな引張の応力が作用する鋼板の領域とすることを原則とする。溶接終了点では、ビード形状が扁平となるので、応力集中が生じにくいからである。
補剛用ビードの長さLaは、下記の(A)の条件を満たすようにするのが好ましい。
(A) 補剛用ビードの長さLa≧隅肉ビードの幅W×2
ここで、補剛用ビードの長さLaは、隅肉ビードと補剛用ビードとの接点を起点として、補剛用ビードの溶融端までの長さである。
補剛用ビードの鋼部材の表面からの高さHaは、補剛用ビードを形成する鋼部材の厚さt(mm)に対して、下記の(B)の条件を満たすのが好ましい。
(B) 補剛用ビードの高さHa≧鋼部材の厚さt×0.5
補剛用ビードの高さHaが、補剛用ビードが形成される鋼部材の厚さtの0.5倍(=t/2)未満であると、補剛用ビードとしての機能を十分に発揮しない。補剛用ビードの高さHaが大きいほど、その効果は大きいが、鋼板への裏抜けや溶け落ちを避けるため自ずと限界がある。したがって、補剛用ビードの高さHaを、補剛用ビードが形成される鋼部材の厚さt以下にするのが現実的である。
また、補剛用ビードの幅Waは、下記の(C)の条件を満たすようにするのが好ましい。
(C) 補剛用ビードの幅Wa≧隅肉ビードの幅W×0.5
補剛用ビードの幅Waが隅肉ビードの幅Wの0.5倍(W/2)未満であると、補剛用ビードとしての機能を十分に発揮しない。補剛用ビードの幅Waの上限は、特に定めないが、補剛用ビードの高さHaと同様に、裏抜けや溶け落ちない範囲で補剛用ビードを形成する必要があるので、その観点から自ずと定まる。
補剛用ビードの硬さ、すなわち、補剛用ビードの溶接金属の硬さHwは、補剛用ビードが置かれる方の鋼部材の鋼板最大硬さHbに対して、下記の(D)の条件を満たすようにするのが好ましい。
(D) 補剛用ビードの溶接金属の硬さHw>鋼板最大硬さHb
補剛用ビードの溶接金属の硬さHwが、鋼板最大硬さHbより大きいと、溶接止端部へのひずみの集中が抑制され、疲労寿命(回数)を向上させることができる。
補剛用ビードの角度γは、下記(E)の条件を満たすようにするのが好ましい。
(E) 45°≦補剛用ビードの角度γ≦135°
補剛用ビードが鋼板の剛性を高め、曲がりを抑制する機能を発揮するためには、補剛用ビードの角度γは45~135°であることが好ましい。角度γが45°未満又は135°超であると、補剛用ビードの前記機能が低下する。
一方、図10に示すようにして補剛用ビードを形成する場合(隅部(接合部)における曲部が、ボックス材102の連続する二つの面において構成される場合)には、補剛用ビードの角度は、当該二つの面のうち補剛用ビードが形成される面の隅肉ビードと補剛用ビードとのなす角度とする。
隅肉ビードの施工時や補剛用ビードの施工時のアーク溶接条件や使用する溶接ワイヤの組成は、常法に従えばよく、特定のものに限定されない。ただし、前記のように、同じ溶接機器を用いて隅肉ビードの施工と補剛用ビードの施工とを連続的に行うことが生産上好ましい。しかし、補剛用ビードの鋼板の剛性を高める機能が担保される限り、両者の溶接条件や使用する溶接ワイヤの組成が異なってもよい。
そして、これらの溶接構造部材を疲労試験に供した。
本実施例において、図6に示すボックス材62の大きさは、直径150mm×高さ(軸方向の長さ)300mmである。チャンネル材61の大きさは、フランジ幅80mm×隅部(接合部)のウエブ幅75mm×高さ(最大値)80mmである。
本実施例において、図8に示すボックス材82の大きさは、300mm×150mm×50mmである。チャンネル材81の大きさは、180mm×75mm×56mmである。
本実施例において、図10に示すボックス材102の大きさは、300mm×100mm×50mmである。チャンネル材101は、180mm×75mm×56mmの角型鋼管の56mmの長さの部分を先端から30mm切り欠いたものである。
また、補剛用ビードの溶接開始点を、隅肉ビードの上にするとともに、補剛用ビードの溶接終了点(表2~表12の補剛用ビードの終了位置)を、ボックス材の上にする場合と、補剛用ビードの溶接開始点を、隅肉ビードの上にするとともに、補剛用ビードの溶接終了点を、チャンネル材上にする場合とのそれぞれについて補剛用ビードを形成した。
また、補剛用ビードの長さLa、補剛用ビードの高さHa、および補剛用ビードの幅Waを変えて補剛用ビードを形成した。
<共通する溶接条件>
溶接方式 消耗式電極溶接
溶接電源 DP350(株式会社ダイヘン製)
溶接モード DC-Pulse
溶接姿勢 下向き水平
チップ鋼板間距離(突き出し長さ) 15mm
シールドガス種 Ar+20%CO2
シールドガス流量 20L/min
<隅肉ビードの形成条件>
トーチ角度 下板からの起こし角60°、前進角0°
ねらい位置 重ね部の隅
溶接速度 80cm/min
溶接電流及び電圧 アンダーカットが出ない値を設定
一例:板厚2.3mmの隅肉アーク溶接の
場合、約220A、約24V)
<補剛用ビードの形成条件>
トーチ角度 鋼板からの起こし角90°、前進角0°
ねらい位置と溶接方向 試験片の幅方向中央で、隅肉ビードの溶接
金属表面を起点とし、隅肉ビードに直角方
向に下側鋼板へ溶接
溶接速度 50cm/min
溶接電流及び電圧 隅肉ビードの2/3程度の溶接電流を設定
一例:板厚2.3mmの鋼板に補剛用ビー
ドを配置する場合、150A、21V
補剛用ビードの硬さHwと鋼板最大硬さHbは、それぞれ前述した方法で測定した。
実施例の効果を、表2~表12に基づいて説明する。
具体的に、D1では、補剛用ビードの長さLaが隅肉ビードの幅Wの2倍以上でない(D1の「La/W」が200%以上にならず、(A)の条件を満たさない)。D2では、補剛用ビードの角度γが45°~135°の範囲にない(D2の「補剛用ビードの角度」が45°~135°にならず、(E)の条件を満たさない)。D3では、補剛用ビードの高さHaが、補剛用ビードが形成される鋼部材の厚さtの0.5倍以上でなく、且つ、補剛用ビードの幅Waが隅肉ビードの幅Wの0.5倍以上でない(D3の「Ha/t」が50%以上にならず(B)の条件を満たさないとともに、D3の「Wa/W」が50%以上ならず、(C)の条件を満たさない)。D8では、き裂の発生するボックス材の最大硬さ(鋼板最大硬さHb)が、補剛用ビードの(溶接金属の)硬さHwを上回っていない(D8の「補剛用ビード溶接金属硬さHw」が「ボックス材最大硬さHb」を上回らず、(D)の条件を満たさない)。しかし、何れの場合でも、疲労寿命向上率は120%を上回った。
尚、表には示していないが、図6に示した溶接構造部材60でも、前述した(A)~(E)の条件を満たさないと、疲労寿命の向上代は低下する傾向になることを確認した。
尚、表には示していないが、図7に示した溶接構造部材70でも、前述した(A)~(E)の条件を満たさないと、疲労寿命の向上代は低下する傾向になることを確認した。
尚、表には示していないが、図8に示した溶接構造部材80でも、前述した(A)~(E)の条件を満たさないと、疲労寿命の向上代は低下する傾向になることを確認した。
具体的に、D13では、補剛用ビードの長さLaが隅肉ビードの幅Wの2倍以上でない(D13の「La/W」が200%以上にならず、(A)の条件を満たさない)。D14では、補剛用ビードの角度γが45°~135°の範囲にない(D14の「La/W」が200%以上にならず、(E)の条件を満たさない)。D15では、補剛用ビードの高さHaが、補剛用ビードが形成される鋼部材の厚さtの0.5倍以上でなく、且つ、補剛用ビードの幅Waが隅肉ビードの幅Wの0.5倍以上でない(D15の「Ha/t」が50%以上にならず(B)の条件を満たさないとともに、D15の「Wa/W」が50%以上ならず、(C)の条件を満たさない)。D19では、き裂の発生するボックス材の最大硬(鋼板最大硬さHb)さが、補剛用ビードの(溶接金属の)硬さHwを上回っていない(D19の「補剛用ビード溶接金属硬さHw」が「ボックス材最大硬さHb」を上回らず、(D)の条件を満たさない)。しかし、何れの場合でも、疲労寿命向上率は120%を上回った。
尚、表には示していないが、図10に示した溶接構造部材100でも、前述した(A)~(E)の条件を満たさないと、疲労寿命の向上代は低下する傾向になることを確認した。
C4は、図5に示した溶接構造部材50に対し、隅肉ビード53の屈曲部に補剛用ビードを形成せずに、隅肉ビード53の領域のうち、チャンネル材51のウエブの幅方向の中央の領域に、隅肉ビード53内を溶接開始位置とし、ボックス材52の表面を溶接終了位置として、補剛用ビードを形成したものの結果を示す。
C2~C4の何れの場合でも、疲労寿命向上率は120%を下回った。
C6、C8、C10の何れの場合でも、疲労寿命向上率は120%を下回った。
C13は、図9に示した溶接構造部材90に対し、補剛用ビードの溶接開始点と溶接終了点を入れ替えたものの結果を示す。
C12、C13の何れの場合でも、疲労寿命向上率は120%を下回った。
C15の場合では、疲労寿命向上率は120%を下回った。
Claims (16)
- 一方の金属部材の板面部分および板厚部分の少なくとも何れか一方と、他方の金属部材の板面部分との当接部分の端の領域である隅部であって、少なくとも一部に少なくとも1つの曲部がある隅部の少なくとも一部の領域に対して隅肉アーク溶接をして隅肉アーク溶接継手を形成する方法であって、
前記隅部の前記曲部を含む領域に対し、前記隅肉アーク溶接により隅肉ビードを形成し、
少なくとも1つの前記曲部の一個所または複数個所に、前記隅肉アーク溶接とは別のアーク溶接によって補剛用ビードを、当該補剛用ビードの溶接開始点または溶接終了点が前記隅肉ビードと重なるように形成し、
前記一方の金属部材と前記他方の金属部材とのうち、前記補剛用ビードを形成しない他は前記隅肉アーク溶接継手と同じ条件で形成された隅肉アーク溶接継手に、前記隅肉アーク溶接継手に付加されることが想定される繰り返し荷重が付加された際に、より大きな引張応力が生じる方の前記金属部材の方向に前記補剛用ビードを形成し、
前記当接部分の両側にできる前記隅部のうち、片側の前記隅部に対して、前記隅肉ビードを形成し、
前記一方の金属部材と前記他方の金属部材とのうち、少なくとも1つの金属部材は、3.2mm以下の板厚を有する金属板から形成されていることを特徴とする隅肉アーク溶接継手の形成方法。 - 前記補剛用ビードの溶接開始点が、他の溶接ビードと重なるように、前記補剛用ビードを形成することを特徴とする請求項1に記載の隅肉アーク溶接継手の形成方法。
- 前記補剛用ビードの溶接開始点が、前記隅肉ビードと重なるように、前記補剛用ビードを形成することを特徴とする請求項2に記載の隅肉アーク溶接継手の形成方法。
- 前記曲部は、屈曲部と湾曲部とのうち少なくとも何れか一方を含むことを特徴とする請求項1~3の何れか1項に記載の隅肉アーク溶接継手の形成方法。
- 前記曲部を構成する領域であって、前記補剛用ビードを形成しない他は前記隅肉アーク溶接継手と同じ条件で形成された隅肉アーク溶接継手に前記繰り返し荷重が付加された際に、前記隅肉ビードの溶接開始位置よりも最大主応力の大きさが大きくなる領域に、前記補剛用ビードを形成することを特徴とする請求項1~4の何れか1項に記載の隅肉アーク溶接継手の形成方法。
- 前記曲部を構成する領域であって、前記補剛用ビードを形成しない他は前記隅肉アーク溶接継手と同じ条件で形成された隅肉アーク溶接継手に前記繰り返し荷重が付加された際に、最大主応力の大きさが最大になる領域に、前記補剛用ビードを形成することを特徴とする請求項1~4の何れか1項に記載の隅肉アーク溶接継手の形成方法。
- 前記補剛用ビードの硬さHwは、前記一方の金属部材と前記他方の金属部材とのうち、前記補剛用ビードが形成される前記金属部材の金属部材最大硬さHbを上回ることを特徴とする請求項1~6の何れか1項に記載の隅肉アーク溶接継手の形成方法。
- 前記補剛用ビードの長さLaは、前記隅肉ビードの幅Wの2倍以上であり、
前記補剛用ビードの高さHaは、前記一方の金属部材と前記他方の金属部材とのうち、前記補剛用ビードが形成される前記金属部材の厚さtの0.5倍以上であり、
前記補剛用ビードの幅Waは、前記隅肉ビードの幅Wの0.5倍以上であり、
前記隅肉ビードに対する前記補剛用ビードの角度γは、45°以上135°以下であることを特徴とする請求項1~7の何れか1項に記載の隅肉アーク溶接継手の形成方法。 - 一方の金属部材の板面部分および板厚部分の少なくとも何れか一方と、他方の金属部材の板面部分との当接部分の端の領域である隅部であって、少なくとも一部に少なくとも1つの曲部がある隅部の少なくとも一部の領域に対して隅肉アーク溶接をすることにより形成される隅肉アーク溶接継手であって、
前記隅部の前記曲部を含む領域に対し、前記隅肉アーク溶接により隅肉ビードが形成されており、
少なくとも1つの前記曲部の一個所または複数個所に、前記隅肉アーク溶接とは別のアーク溶接によって補剛用ビードが形成されており、
前記補剛用ビードは、当該補剛用ビードの溶接開始点または溶接終了点が前記隅肉ビードと重なるように形成されており、且つ、前記一方の金属部材と前記他方の金属部材とのうち、前記補剛用ビードを形成しない他は前記隅肉アーク溶接継手と同じ条件で形成された隅肉アーク溶接継手に、前記隅肉アーク溶接継手に付加されることが想定される繰り返し荷重が付加された際に、より大きな引張応力が生じる方の前記金属部材の方向に形成されており、
前記隅肉ビードは、前記当接部分の両側にできる前記隅部のうち、片側の前記隅部に対して形成されており、
前記一方の金属部材と前記他方の金属部材とのうち、少なくとも1つの金属部材は、3.2mm以下の板厚を有する金属板から形成されていることを特徴とする隅肉アーク溶接継手。 - 前記補剛用ビードの溶接開始点が、他の溶接ビードと重なる位置にあることを特徴とする請求項9に記載の隅肉アーク溶接継手。
- 前記補剛用ビードの溶接開始点が、前記隅肉ビードと重なる位置にあることを特徴とする請求項10に記載の隅肉アーク溶接継手。
- 前記曲部は、屈曲部と湾曲部とのうち少なくとも何れか一方を含むことを特徴とする請求項9~11の何れか1項に記載の隅肉アーク溶接継手。
- 前記補剛用ビードは、前記曲部を構成する領域であって、前記補剛用ビードを形成しない他は前記隅肉アーク溶接継手と同じ条件で形成された隅肉アーク溶接継手に前記繰り返し荷重が付加された際に、前記隅肉ビードの溶接開始位置よりも最大主応力の大きさが大きくなる領域に形成されていることを特徴とする請求項9~12の何れか1項に記載の隅肉アーク溶接継手。
- 前記補剛用ビードは、前記曲部を構成する領域であって、前記補剛用ビードを形成しない他は前記隅肉アーク溶接継手と同じ条件で形成された隅肉アーク溶接継手に前記繰り返し荷重が付加された際に、最大主応力の大きさが最大になる領域に形成されていることを特徴とする請求項9~12の何れか1項に記載の隅肉アーク溶接継手。
- 前記補剛用ビードの硬さHwは、前記一方の金属部材と前記他方の金属部材とのうち、前記補剛用ビードが形成される前記金属部材の金属部材最大硬さHbを上回ることを特徴とする請求項9~14の何れか1項に記載の隅肉アーク溶接継手。
- 前記補剛用ビードの長さLaは、前記隅肉ビードの幅Wの2倍以上であり、
前記補剛用ビードの高さHaは、前記一方の金属部材と前記他方の金属部材とのうち、前記補剛用ビードが形成される前記金属部材の厚さtの0.5倍以上であり、
前記補剛用ビードの幅Waは、前記隅肉ビードの幅Wの0.5倍以上であり、
前記隅肉ビードに対する前記補剛用ビードの角度γは、45°以上135°以下であることを特徴とする請求項9~15の何れか1項に記載の隅肉アーク溶接継手。
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EP13858775.3A EP2926939B1 (en) | 2012-11-29 | 2013-11-28 | Method for forming fillet arc welding joint and fillet arc welding joint |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2016052722A1 (ja) * | 2014-10-03 | 2016-04-07 | 新日鐵住金株式会社 | 溶接構造部材及びその製造方法 |
JP6065147B1 (ja) * | 2015-10-26 | 2017-01-25 | Jfeスチール株式会社 | 重ね隅肉アーク溶接継手、プレス成形部品の接合構造 |
US10092982B2 (en) | 2015-02-13 | 2018-10-09 | Nippon Steel & Sumitomo Metal Corporation | Fillet welded joint and method of production of same |
JP2019155386A (ja) * | 2018-03-08 | 2019-09-19 | 日本製鉄株式会社 | 溶接構造部材 |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101720087B1 (ko) * | 2016-06-01 | 2017-03-28 | 주식회사 포스코 | 피로 특성이 우수한 용접이음부 및 이의 제조 방법 |
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FR3074437B1 (fr) * | 2017-12-04 | 2019-11-15 | Renault S.A.S. | Procede de fixation d'une piece metallique sur un tube metallique obtenu par pliage et soudage de tole |
JP2020006401A (ja) * | 2018-07-06 | 2020-01-16 | 株式会社神戸製鋼所 | 接合体 |
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JP7328181B2 (ja) | 2020-07-15 | 2023-08-16 | 株式会社神戸製鋼所 | 重ねすみ肉溶接継手及びその製造方法並びに閉断面部材 |
CN112620873B (zh) * | 2020-12-16 | 2022-09-13 | 中国兵器科学研究院宁波分院 | 一种大型承插件的焊接方法 |
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5114844A (ja) | 1974-07-29 | 1976-02-05 | Mitsubishi Heavy Ind Ltd | Suminikuyosetsuho |
JPH06340947A (ja) | 1993-06-01 | 1994-12-13 | Kobe Steel Ltd | 疲労強度に優れる重ねアーク溶接継手構造物 |
JPH0724570A (ja) * | 1993-07-09 | 1995-01-27 | Mitsui Eng & Shipbuild Co Ltd | すみ肉溶接方法 |
JPH09253843A (ja) | 1996-03-21 | 1997-09-30 | Kawasaki Heavy Ind Ltd | 応力緩和溶接ビード構造 |
JP2012110950A (ja) * | 2010-11-26 | 2012-06-14 | Komatsu Ltd | 溶接構造体及びその製造方法 |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4129974A (en) * | 1974-06-18 | 1978-12-19 | Morris Ojalvo | Warp-restraining device and improvement to beams, girders, arch ribs, columns and struts |
US4280541A (en) * | 1980-01-10 | 1981-07-28 | Reimler Associates, Inc. | Debarking tool for log debarking machines |
JPS62259676A (ja) * | 1986-04-30 | 1987-11-12 | Daihatsu Motor Co Ltd | 部材の溶接方法 |
SU1698021A1 (ru) * | 1990-01-29 | 1991-12-15 | Ворошиловградский машиностроительный институт | Способ уменьшени сварочных напр жений и деформаций |
US5084119A (en) * | 1990-10-17 | 1992-01-28 | Bridgestone/Firestone, Inc. | Lap seam and method forming same |
US5233149A (en) * | 1991-08-02 | 1993-08-03 | Eaton Corporation | Reprocessing weld and method |
JPH08155635A (ja) * | 1994-12-06 | 1996-06-18 | Nippon Steel Corp | 疲労特性に優れた構造用鋼回し溶接継手およびその溶接方法 |
JPH08174211A (ja) * | 1994-12-27 | 1996-07-09 | Nkk Corp | 鋼製部材の隅肉溶接方法 |
JPH0939829A (ja) | 1995-07-28 | 1997-02-10 | Toyota Motor Corp | 溶接部の応力緩和構造 |
US6099194A (en) * | 1997-08-20 | 2000-08-08 | Dana Corporation | Splice joint for connecting adjacent side rail sections in a vehicle body and frame assembly |
KR100427613B1 (ko) * | 2001-05-02 | 2004-04-28 | 주식회사 뉴웰엔터프라이스 | 유연성 있는 필렛용접용 이당재 |
US6696174B2 (en) * | 2002-03-22 | 2004-02-24 | Air Logistics Corporation | Method of repairing multiple tube structures and repaired multiple tube structures |
CN2533341Y (zh) * | 2002-04-16 | 2003-01-29 | 梁荣顺 | 一种接头采用双焊缝密封结构的压力容器 |
US7225966B2 (en) * | 2002-08-07 | 2007-06-05 | Eclipse Aviation Corporation | Welded joints with polymer sealant |
CN100418689C (zh) * | 2002-09-09 | 2008-09-17 | 独立行政法人物质·材料研究机构 | 使用低相变温度焊接材料的焊接方法 |
US7732733B2 (en) * | 2005-01-26 | 2010-06-08 | Nippon Welding Rod Co., Ltd. | Ferritic stainless steel welding wire and manufacturing method thereof |
CN102151954A (zh) * | 2011-02-23 | 2011-08-17 | 格菱动力设备(中国)有限公司 | 集箱管座角焊缝焊接的操作方法 |
CN102770227B (zh) * | 2011-02-23 | 2015-07-15 | 新日铁住金株式会社 | 焊接接头的制造方法以及焊接接头 |
JP6005367B2 (ja) * | 2011-06-22 | 2016-10-12 | デルタ工業株式会社 | 溶接ビードを用いた板構造体の補強方法 |
JP5881055B2 (ja) * | 2011-11-09 | 2016-03-09 | 国立大学法人大阪大学 | 溶接方法および溶接継手 |
IN2014DN08181A (ja) | 2012-04-17 | 2015-05-01 | Nippon Steel & Sumitomo Metal Corp |
-
2013
- 2013-11-28 WO PCT/JP2013/082070 patent/WO2014084317A1/ja active Application Filing
- 2013-11-28 MX MX2015002240A patent/MX352721B/es active IP Right Grant
- 2013-11-28 BR BR112015003868-9A patent/BR112015003868B1/pt not_active IP Right Cessation
- 2013-11-28 IN IN11167DEN2014 patent/IN2014DN11167A/en unknown
- 2013-11-28 ES ES13858775.3T patent/ES2658222T3/es active Active
- 2013-11-28 US US14/408,509 patent/US10035208B2/en active Active
- 2013-11-28 RU RU2015105793A patent/RU2617307C2/ru not_active IP Right Cessation
- 2013-11-28 CA CA2877237A patent/CA2877237C/en not_active Expired - Fee Related
- 2013-11-28 EP EP13858775.3A patent/EP2926939B1/en active Active
- 2013-11-28 JP JP2014526312A patent/JP5843015B2/ja active Active
- 2013-11-28 CN CN201380041508.XA patent/CN104520059B/zh active Active
- 2013-11-28 KR KR1020157007098A patent/KR101649837B1/ko active IP Right Grant
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5114844A (ja) | 1974-07-29 | 1976-02-05 | Mitsubishi Heavy Ind Ltd | Suminikuyosetsuho |
JPH06340947A (ja) | 1993-06-01 | 1994-12-13 | Kobe Steel Ltd | 疲労強度に優れる重ねアーク溶接継手構造物 |
JPH0724570A (ja) * | 1993-07-09 | 1995-01-27 | Mitsui Eng & Shipbuild Co Ltd | すみ肉溶接方法 |
JPH09253843A (ja) | 1996-03-21 | 1997-09-30 | Kawasaki Heavy Ind Ltd | 応力緩和溶接ビード構造 |
JP2012110950A (ja) * | 2010-11-26 | 2012-06-14 | Komatsu Ltd | 溶接構造体及びその製造方法 |
Non-Patent Citations (1)
Title |
---|
See also references of EP2926939A4 |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101941385B1 (ko) * | 2014-10-03 | 2019-01-22 | 신닛테츠스미킨 카부시키카이샤 | 용접 구조 부재 및 그 제조 방법 |
US10688580B2 (en) | 2014-10-03 | 2020-06-23 | Nippon Steel Corporation | Welded structure member and manufacturing method thereof |
KR20170045357A (ko) * | 2014-10-03 | 2017-04-26 | 신닛테츠스미킨 카부시키카이샤 | 용접 구조 부재 및 그 제조 방법 |
WO2016052722A1 (ja) * | 2014-10-03 | 2016-04-07 | 新日鐵住金株式会社 | 溶接構造部材及びその製造方法 |
CN106794554A (zh) * | 2014-10-03 | 2017-05-31 | 新日铁住金株式会社 | 焊接结构构件以及其制造方法 |
JPWO2016052722A1 (ja) * | 2014-10-03 | 2017-06-29 | 新日鐵住金株式会社 | 溶接構造部材及びその製造方法 |
CN106794554B (zh) * | 2014-10-03 | 2019-08-27 | 日本制铁株式会社 | 焊接结构构件以及其制造方法 |
RU2665657C1 (ru) * | 2014-10-03 | 2018-09-03 | Ниппон Стил Энд Сумитомо Метал Корпорейшн | Сварной конструктивный элемент и способ его изготовления |
US10092982B2 (en) | 2015-02-13 | 2018-10-09 | Nippon Steel & Sumitomo Metal Corporation | Fillet welded joint and method of production of same |
WO2017073129A1 (ja) * | 2015-10-26 | 2017-05-04 | Jfeスチール株式会社 | 重ね隅肉アーク溶接継手及びプレス成形部品の接合構造 |
CN108349037A (zh) * | 2015-10-26 | 2018-07-31 | 杰富意钢铁株式会社 | 搭接角焊电弧焊接头和压制成型部件的接合结构 |
JP6065147B1 (ja) * | 2015-10-26 | 2017-01-25 | Jfeスチール株式会社 | 重ね隅肉アーク溶接継手、プレス成形部品の接合構造 |
CN108349037B (zh) * | 2015-10-26 | 2020-06-30 | 杰富意钢铁株式会社 | 搭接角焊电弧焊接头和压制成型部件的接合结构 |
US10933494B2 (en) | 2015-10-26 | 2021-03-02 | Jfe Steel Corporation | Lap-fillet arc welding joint and joint structure for press forming parts |
JP2019155386A (ja) * | 2018-03-08 | 2019-09-19 | 日本製鉄株式会社 | 溶接構造部材 |
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