Laser Welding Method

Abstract

To solve the problem that in a conventional member for welding different materials, round-chamfering and a complicated shape of a rivet such as an annular groove are required, which increases manufacturing costs, and productivity is low and moreover flexibility of design is restricted, and further rigidity at a desired place cannot be increased.SOLUTION: A third material which has a penetration part and which is difficult to be welded to a first material and a second material is nipped between the first material and the second material which are made of metal materials of the same kind which can be welded to each other, so as to form a second gap corresponding to a plate thickness of the first material positioned at a side to which a laser beam is emitted between the first material and the second material in an area corresponding to the penetration part; and in a state where there is the second gap not yet welded exists, the area corresponding to the penetration part is irradiated with a laser beam from the first material side, so as to melt and join the first material and the second material to each other through the penetration part, so that the third material is compressed and fixed, which fixes the third material and the first material and the second material.SELECTED DRAWING: Figure 1

Description

[Technical field]

[0001] The present disclosure relates to laser welding methods. [Background technology]

[0002] In recent years, the production volume of automobiles and other transportation equipment has increased due to globalization. Accordingly, there is an increasing demand for reducing the total cost per unit of automobiles and other products, in particular for improving productivity by shortening production time.

[0003] In addition, there is a strong demand worldwide for restrictions on CO2 emissions to prevent global warming, and efforts to improve fuel efficiency are accelerating in the transportation industry, including the automobile industry, to meet this demand. Specific efforts to improve fuel efficiency include reducing the weight of vehicles, and studies are underway to increase the proportion of lightweight materials used.

[0004] While such studies are being conducted, spot welding has become widespread as a welding method used in the production of transportation equipment such as automobiles. Spot welding, which is a type of resistance welding, requires welding by applying pressure to the welding material with upper and lower electrodes, which are spot welding guns, eliminating the gap between the welding material and passing electricity between the upper and lower electrodes. For this reason, spot welding is not suitable for one-sided welding. In addition, in order to apply pressure to the welding material, space is required for the upper and lower guns equipped with the electrodes for spot welding to enter above and below the welding material, This places restrictions on the product shape. Furthermore, the gun for spot welding itself is heavy, so it moves slowly, and even after it arrives at the welding position, it takes time to pressurize the welding material, and after welding, it is necessary to ensure that the welding material is cooled. In other words, spot welding requires a lot of time other than welding.

[0005] Furthermore, to reduce the weight of materials used in automobiles, there are ongoing studies to change some parts from steel to light metal materials such as aluminum, and there is a demand for technology and structures that can join light metal materials and steel.

[0006] In general, it is very difficult to join steel to aluminum, which is a dissimilar material to steel. Therefore, spot welding using rivets and joining using adhesives have been used as joining members for dissimilar materials. For example, Patent Document 1 describes a rivet shape, crimping, and spot welding method that pressurizes dissimilar materials sandwiched between a rivet and a joining material of the same type as the rivet material, and absorbs the plastic flow of the dissimilar materials due to welding heat during spot welding. According to this method, a space is secured in the rivet for a part of the dissimilar materials to deform and move during crimping and spot welding, and it is possible to prevent the dissimilar materials from collapsing due to the positional deviation of the electrodes during spot welding, thereby suppressing a decrease in fastening force. [Prior art documents] [Patent documents]

[0007] [Patent Document 1] JP 2015-42417 A Summary of the Invention [Problem to be solved by the invention]

[0008] A conventional joined member of dissimilar materials will be described with reference to FIG. 7. As shown in FIG. 7, a dissimilar material joined body 100 is composed of a rivet 51, a first material to be joined 200, and a second material to be joined 300. Here, the rivet 51 and the second material to be joined 300 are the same material. The first material to be joined 200 is a dissimilar material that is made of a different material from the rivet 51 and the second material to be joined 300. The rivet 51 has a shaft portion 52 and a head portion 53. Furthermore, the head portion 53 has an R (Radius)-shaped chamfer 30, an annular groove 31, and a flat portion 32. The chamfer 30, the annular groove 31, and the flat portion 32 ensure a space for a part of the first workpiece 200 to deform and move during crimping and spot welding, and prevent the first workpiece 200 from collapsing due to a positional shift of the electrode 400 (a shift between the axis Z1 of the electrode 400 and the axis Z2 of the rivet 51) during spot welding, making it possible to suppress a decrease in fastening force. However, in this case, the shape of the rivet 51 is complex and precision machining is required, so the manufacturing cost is high. In addition, since the rivet 51 and the second workpiece 300 are joined by spot welding, it takes time to apply pressure, pass electricity, cool, move, etc., so the work time is long. In addition, since the rivet 51 and the second workpiece 300 need to be sandwiched from both sides, the design freedom is limited. Furthermore, if the rivets are too close to each other, the spot welding current is diverted to the adjacent rivet, and the formation of a nugget, which is a welded solidified part that occurs in the welded part X during spot welding, becomes insufficient. For this reason, it is necessary to ensure a joining pitch that is greater than or equal to the minimum separation pitch at which the desired nugget can be formed without current shunting, which poses the problem that it is not possible to increase the rigidity of the joint in necessary locations. [Means for solving the problem]

[0009] The present disclosure provides a laser welding method that enables joining of dissimilar materials and improves productivity.

[0010] In order to solve the above problems, a laser welding method according to one aspect of the present disclosure includes a first material and a second material made of the same type of metallic material that can be welded to each other, at least one of which has a protrusion provided thereon, the first material and the second material having a through portion through which the protrusion is inserted, The method includes a step of sandwiching a third material that is difficult to weld to the first material and the second material. The method also includes a step of irradiating a region corresponding to the protrusion with a laser beam from the first material side while the third material is sandwiched between the first material and the second material, and welding the first material and the second material through the through-hole. In the step of sandwiching the third material between the first material and the second material, a first gap is provided between the inner peripheral surface of the through-hole and the protrusion, and a second gap according to the plate thickness of the first material in the region corresponding to the protrusion is provided between the first material and the second material in the region corresponding to the protrusion.

[0011] A laser welding method according to an embodiment of the present disclosure includes a step of sandwiching a third material having a penetration portion between a first material and a second material made of the same type of metal material that can be welded to each other, the third material being difficult to weld to the first material and the second material. The method also includes a step of irradiating a region corresponding to the penetration portion from the first material side with a laser beam while the third material is sandwiched between the first material and the second material, and welding the first material and the second material through the penetration portion. In the step of sandwiching the third material between the first material and the second material, the sheet thickness of the first material in the region corresponding to the penetration portion is a thickness corresponding to the sheet thickness of the third material, or a thickness corresponding to a gap in the sheet thickness direction between the first material and the second material in the region.

[0012] In addition to the above, the laser welding method according to one aspect of the present disclosure is weaving, helical welding, circular welding, or spiral welding.

[0013] The laser welding method disclosed herein enables joining of dissimilar materials, significantly shortens production takt time, increases rigidity where necessary, and expands design freedom. Effect of the Invention

[0014] The laser welding method disclosed herein enables joining of dissimilar materials, significantly shortens production takt time, increases rigidity where necessary, and expands design freedom. [Brief description of the drawings]

[0015] [Figure 1] Fig. 1A is a cross-sectional view for explaining a joint structure before and after welding in the first embodiment of the present disclosure. Fig. 1B is a cross-sectional view for explaining a joint structure before and after welding in the first embodiment of the present disclosure. Fig. 1C is a cross-sectional view for explaining a joint structure before and after welding in the first embodiment of the present disclosure. Fig. 1D is a cross-sectional view for explaining a joint structure before and after welding in the second embodiment of the present disclosure. [Diagram 2] Fig. 2A is a perspective view for explaining a joining state during laser welding in the first embodiment of the present disclosure. Fig. 2B is a perspective view for explaining a joining state during laser welding in the first embodiment of the present disclosure. Fig. 2C is a perspective view for explaining a joining state during laser welding in the first embodiment of the present disclosure. Fig. 2D is a perspective view for explaining a joining state during laser welding in the third embodiment of the present disclosure. Fig. 2E is a perspective view for explaining a joining state during laser welding in the third embodiment of the present disclosure. [Diagram 3] FIG. 3 is a graph showing a result of measuring the relationship between the plate thickness of the first material and the second gap, which is a gap in the plate thickness direction, during circular welding in the first embodiment of the present disclosure. [Figure 4] FIG. 4 is a graph illustrating a result of measuring the relationship between the quality of the third material and the first gap according to the first embodiment of the present disclosure. [Diagram 5] Fig. 5A is a diagram showing an example of use in the first embodiment of the present disclosure. Fig. 5B is a diagram showing an example of use in the first embodiment of the present disclosure. [Figure 6] FIG. 6 is a graph illustrating measurement results of the relationship between the plate thickness of the first material and the second gap during helical welding in the third embodiment of this disclosure. [Figure 7] FIG. 7 is a diagram for explaining a conventional form of joining dissimilar materials. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0016] (Embodiment 1) First, the first embodiment will be described with reference to Figs. 1A and 2A. Fig. 1A is a cross-sectional view for explaining a state before and after welding in the first embodiment of the present disclosure. Fig. 2A is a perspective view for explaining a joining state during laser welding in the first embodiment of the present disclosure. Fig. 1A shows a joining structure between a first material 1, a second material 2, and a third material 3. Fig. 1A is also a cross-sectional view taken along line 1A-1A in Fig. 2A.

[0017] Here, the first material 1 and the second material 2 are homogeneous metal materials that can be welded to each other. The third material 3 is a dissimilar material different from the first material 1 and the second material 2, and is difficult to weld to the first material 1 and the second material 2. As shown in FIG. 1A, the third material 3, which is a dissimilar material, is sandwiched between the first material 1 and the second material 2, which are homogeneous metal materials, during joining. Here, the third material 3 is pre-machined with a through hole 12 as a through portion. The first material 1 and the second material 2 have protrusions 14, and the respective protrusions 14 are inserted and arranged in the through hole 12 so as to face each other. Since the protrusions 14 of the first material 1 and the second material 2 are inserted into the through hole 12 of the third material 3, the through hole 12 has the effect of suppressing the relative positional deviation of the first material 1 and the second material 2 with respect to the through hole 12. Furthermore, the protrusion 14 has the advantage that it allows visual confirmation of the appropriateness of the laser irradiation position and the bead formation position.

[0018] In the present disclosure, the through-portion is the through-hole 12, but it may be a through-groove.

[0019] Homogeneous metal materials are metals that can be welded to each other, and are not limited to metals of the same material, but are metals that have good weldability, such as ferrous metals and nonferrous metals. In other words, homogeneous metal materials are materials of the same type that have good welding compatibility. Specifically, the following combinations of the first material 1 and the second material 2 during welding can be given. Combinations of ferrous metal materials include mild steel and mild steel, mild steel and stainless steel, stainless steel and stainless steel, mild steel and high-tensile steel (high-tensile steel), high-tensile steel and stainless steel, high-tensile steel and high-tensile steel, etc. Combinations of nonferrous metal materials include aluminum and aluminum, aluminum and aluminum alloy, aluminum alloy and aluminum alloy, etc.

[0020] The third material 3 as a dissimilar material is a material of a different quality from the first material 1 and the second material 2 as the homogeneous metallic materials, and is a material that is difficult to weld to the first material 1 and the second material 2. For example, if the first material 1 and the second material 2 as the homogeneous metallic materials are ferrous metallic materials, the third material 3 as a dissimilar material is a non-ferrous metallic material such as copper or aluminum. In addition, resin materials such as CFRP (Carbon Fiber Reinforced Plastics) and PET (PolyEthlenTerephthalate) can also be cited as dissimilar materials to metallic materials.

[0021] In this embodiment, the shapes of the protrusions 14 of the first material 1 and the second material 2 are substantially the same. Here, as shown in FIG. 1A, a gap between the protrusion outer edge 9 of the protrusions 14 of the first material 1 and the second material 2 arranged opposite to each other and the end (inner peripheral surface) of the through hole 12 of the third material 3 in a direction perpendicular to the plate thickness direction is defined as a first gap 4. In addition, a gap between the protrusions 14 in the plate thickness direction when the protrusions 14 of the first material 1 and the protrusions 14 of the second material 2 are inserted into the through hole 12 of the third material 3 is defined as a second gap 5. In other words, a gap between the first material 1 and the second material 2 in a state where they are separated in the plate thickness direction of the through hole 12 is defined as a second gap 5. Furthermore, a region of the inner edge of the protrusion 14 is defined as a protrusion inner edge 10. As shown in FIG. 1A and FIG. 2A, in this embodiment, welding is performed using a laser 7 as a laser beam. As shown in FIG. 2A, welding is performed by irradiating the laser 7 from the upper side in the plate thickness direction of the first material 1 toward the inside of the protrusion inner edge 10 corresponding to the protrusion 14, which is an area (joinable range) that can be irradiated with the laser 7, in a circular shape. As a result, as shown in FIG. 1A, a weld bead 11, which is a part of the welded portion 8, is formed in the protrusion inner edge 10. The welded portion 8 is a portion where the first material 1 and the second material 2 are welded, and is composed of the weld bead 11 as the weld metal where the molten metal melted during welding solidifies, and the heat-affected portion affected by the heat of welding. As described above, in this embodiment, the laser 7 is irradiated from the first material 1 side to the area corresponding to the protrusion 14. In this area, the gap according to the plate thickness in the area corresponding to the protrusion 14 of the first material 1 provided between the first material 1 and the second material 2 can be said to be the second gap 5.

[0022] Next, the joining state during and after welding will be described with reference to FIG. 1A. When the laser 7 is irradiated in a circular shape within the inner edge 10 of the protrusion of the first material 1 to perform welding, a weld bead 11 is formed during welding. At this time, the molten metal in the welded portion 8 of the first material 1 and the second material 2 solidifies and shrinks, thereby reducing the second gap 5 therebetween. In this manner, the laser 7 is irradiated from the plate thickness direction in the region corresponding to the protrusion 14 irradiated with the laser 7 while the second gap 5 exists before welding, and the first material 1 and the second material 2 as homogeneous metallic materials melt and bond to each other and solidify and shrink, and the third material 3 as a dissimilar material sandwiched therebetween is compressed and fixed.

[0023] Moreover, the size of the second gap 5 is set to 4% to 38% of the plate thickness t of the first material 1 on the side irradiated with the laser 7. In this case, solidification and shrinkage of the welded portion 8 becomes a compressive force 6 that sandwiches the third material 3 between the first material 1 and the second material 2, making it possible to compress and fix the third material 3.

[0024] The setting of the size of the second gap 5 to be 4% to 38% of the plate thickness t of the first material 1 on the side irradiated with the laser 7 was derived from experimental data, and an example of the experimental data is shown in FIG. 3.

[0025] FIG. 3 is a graph showing a result of measuring the relationship between the plate thickness t of the first material 1 and the second gap 5 during circular welding in the first embodiment of the present disclosure.

[0026] In this experiment, the first material 1 and the second material 2 were both mild steel, which is a homogeneous metal material, and the third material 3 was PET, which is a different resin material. In this combination, the first material 1 was placed above the second material 2, and the third material 3 was sandwiched between the first material 1 and the second material 2. The laser 7 was irradiated in a circular shape from above in the overlapping direction (in other words, the plate thickness direction) to weld the first material 1 into the protruding inner edge portion 10. In this experiment, the output of the laser 7 was set to 3 kW.

[0027] The diameter of the protrusion inner edge 10 of the first material 1 and the second material 2 was φ10 mm, and the diameter of the through hole 12 of the third material 3 was φ12 mm. The area of ​​the laser 7 irradiated into the protrusion inner edge 10 is made smaller by a predetermined distance than the diameter or width of the protrusion inner edge 10. The area of ​​the laser 7 irradiation in this experiment was a circular area of ​​φ8 mm, which was as close as possible to the diameter of the protrusion inner edge 10 and smaller than the diameter of the protrusion inner edge 10. The above numerical values ​​are examples and are not limited to these.

[0028] Next, the experimental results of FIG. 3 will be described. In the graph shown in FIG. 3, the horizontal axis indicates the plate thickness t of the first material 1, and the vertical axis indicates the size of the second gap 5. For example, when the plate thickness t is 0.8 mm, and the size of the second gap 5 is 0.1 mm to 0.3 mm, the third material 3 can be compressed and fixed by the solidification and shrinkage of the molten metal of the welded portion 8. Also, when the second gap 5 becomes larger than 0.3 mm, a part of the weld line becomes a holed state (at least one open hole is formed in the welded portion due to insufficient filling of the molten metal during welding), resulting in poor welding. Therefore, when the plate thickness t of the first material 1 is 0.8 mm, the size of the second gap 5 is effective for compression fixing when it is 13% to 38% of the plate thickness t of the first material 1.

[0029] In addition, when the plate thickness t is 2.3 mm, if the size of the second gap 5 is 0.1 mm to 0.7 mm, the third material 3 can be compressed and fixed by the solidification and contraction of the molten metal of the welded portion 8. If the size of the second gap 5 exceeds 0.7 mm, a part of the weld line becomes a holed state (at least one open hole is formed in the welded portion due to insufficient filling of the molten metal during welding), resulting in poor welding. Therefore, when the plate thickness t of the first material 1 is 2.3 mm, the size of the second gap 5 is effective for compression and fixing when it is 4% to 30% of the plate thickness t of the first material 1. As a result, welding is possible if the size of the second gap 5 according to the plate thickness t of the first material 1 on the side irradiated with the laser 7 is within a predetermined range. Specifically, welding is possible if the size of the second gap 5 is 4% or more and 38% or less of the plate thickness t of the first material 1. In addition, if the size of the second gap 5 is within the above-mentioned predetermined range, the third material 3 can be compressed and fixed by the first material 1 and the second material 2.

[0030] This indicates that when the sheet thickness t of the first material 1 and the size of the second gap 5 satisfy the above relationship, molten metal equivalent to a maximum of 30% to 38% of the sheet thickness t of the first material 1 falls into the second gap 5 and can be joined to the second material 2 without creating a hole. When the size of the second gap 5 exceeds a maximum of 30% to 38% of the sheet thickness t of the first material 1, the amount of molten metal required to fill the second gap 5 cannot be secured, resulting in a state in which a hole is partially created.

[0031] Conversely, if the second gap 5 is smaller than 0.1 mm, the gap between the protrusions 14 becomes too small, causing the first material 1 and the second material 2 to melt and bond to each other, resulting in insufficient compression force 6 to compress and fix the third material 3.

[0032] In this way, the larger the second gap 5 is within a range that ensures the amount of molten metal during welding, in other words, within a range that does not cause holes, the greater the solidification shrinkage of the welded portion 8 during welding between the protrusions 14. This increases the compressive force 6 that serves as a fixing force sandwiching the third material 3 between the first material 1 and the second material 2.

[0033] Although the above describes the case where the laser 7 is irradiated from the first material 1 side, the same effect can be obtained when the laser 7 is irradiated from the second material 2 side. In other words, when the laser 7 is irradiated from the second material 2, the first material 1 and the second material 2 can be welded together if the size of the second gap 5 is about 4% or more and 38% or less of the plate thickness of the second material 2. In addition, the third material 3 can be compressed and fixed by the first material 1 and the second material 2.

[0034] In this embodiment, the shapes of the protrusions 14 of the first material 1 and the second material 2 are the same, but they do not necessarily have to be the same. Although the laser 7 is irradiated from the first material 1 side, the present invention is not limited to this. If the second gap 5 between the protrusions 14 is set according to the thickness of the metal material of the same type on the side on which the laser 7 is irradiated from the thickness direction so that the thickness is 4% to 38% of the thickness of the material on the side on which the laser 7 is irradiated, the amount of molten metal required for the second gap 5 during melting can be secured. As a result, the third material 3 can be sandwiched and compressed and fixed between the first material 1 and the second material 2 due to solidification and shrinkage of the welded portion 8 during welding.

[0035] For this reason, in this embodiment, the protrusions 14 are provided on both sides of the first material 1 and the second material 2, but as long as the condition for the size of the second gap 5 is satisfied, the protrusions 14 may be provided on either the first material 1 or the second material 2. In addition, regarding the laser irradiation direction, the laser 7 is irradiated from the first material 1 side in this embodiment, but it may be irradiated from the second material 2 side.

[0036] In addition, the first material 1 and the second material 2 are made of the same type of metal material, and although they have been described as being made of mild steel, the materials may be different as long as they are made of the same type of metal material that can be welded to each other and provide sufficient joining strength.

[0037] For example, the following combinations are possible for the first material 1 and the second material 2 as homogeneous metal materials. Combinations of ferrous metal materials include mild steel materials, stainless steel materials, high tensile steel materials, and the like, or mild steel and high tensile steel (high tensile steel), high tensile steel and stainless steel, etc. Combinations of non-ferrous metal materials include: There are combinations of aluminum materials, aluminum alloys, or aluminum and aluminum alloys. The above-mentioned ferrous metal materials and non-ferrous metal materials are materials that can be laser-joined. The third material 3 as a dissimilar material is copper, which has a low absorption rate of laser light and is difficult to laser-join, various resin materials, and materials that are incompatible with the first material 1 and the second material 2 in terms of weldability. An example of a combination that is incompatible with weldability is when the first material 1 and the second material 2 are both mild steel materials, and the third material 3 is aluminum material as the material to be welded to them. Or the reverse combination is also possible.

[0038] Next, a case where the second gap 5 becomes relatively large due to the thickness of the third material 3 being thick, etc., will be described with reference to FIG. 1B. Explanations of parts that overlap with the above will be omitted. When the second gap 5, which is the gap between the first material 1 and the second material 2, is large, a spacer 13 made of a metal material of the same type that can be welded to the first material 1 and the second material 2 is placed inside the through hole 12 of the third material 3. With this configuration, the second gap 5 can be made relatively small. As described above, the thickness of the spacer 13 is set so that the size of the second gap 5 when the spacer 13 is placed inside the through hole 12 is 4% to 38% of the thickness of the first material 1. With this configuration, good joining is possible. The size of the second gap 5 when the spacer 13 is placed inside the through hole 12 is the gap between the spacer 13 and the first material 1 in the thickness direction when the spacer 13 is placed between the first material 1 and the second material 2.

[0039] The spacer 13 disposed between the first material 1 and the second material 2 may not only be disposed as a separate part, but may also be created directly between the first material 1 and the second material 2 using a welding material such as a consumable electrode or a filler.

[0040] In this case, too, as shown in Fig. 3, if the range of the second gap 5 is within a predetermined range according to the plate thickness on the side irradiated with the laser 7 (plate thickness t of the first material 1 in Fig. 3), keyhole-type laser welding is performed so as to penetrate to the second material 2, which is the lower plate. This causes solidification shrinkage in the welded portion 8, which becomes a compressive force 6 and compresses and fixes the third material 3.

[0041] Furthermore, if the second gap 5 exceeds a maximum of 30% to 38% of the plate thickness t of the first material 1 to which the laser 7 is irradiated, the amount of molten metal required for the second gap 5 cannot be secured, which may result in a partial hole being formed.

[0042] Conversely, if the second gap 5 is smaller than 0.1 mm, the gap between the protrusions 14 becomes too small, and the first material 1 and the second material 2, which are homogeneous metal materials, are melt-bonded to each other, resulting in insufficient compressive fixing force for compressively fixing the dissimilar third material 3.

[0043] In the above, the case where only one type of third material 3, which is a dissimilar material, is used has been described. In the following, the case where two different types of dissimilar materials are used will be described. FIG. 1C is a cross-sectional view for explaining a joining structure before and after welding in the first embodiment of the present disclosure. As shown in FIG. 1C, when joining two different types of dissimilar materials, the third material 3 and the fourth material 15, are sandwiched between the first material 1 and the second material 2, which are homogeneous metallic materials. Then, the laser 7 is irradiated from the first material 1 side with the size of the second gap 5 being 4% or more and 38% or less of the plate thickness of the first material 1, and laser welding is performed.

[0044] Even in this case, the third material 3 and the fourth material 15 can be compressed and fixed by the compressive force 6 due to the solidification and shrinkage of the molten metal of the first material 1 and the second material 2. In particular, when the third material 3 and the fourth material 15, which are two different types of dissimilar materials, are resin materials such as PET materials or non-metallic materials such as CFRP, the transmittance of the laser 7 is high. In other words, the absorption rate of the laser 7 is often low, making laser welding difficult. For this reason, as in the case where there is only one type of dissimilar material, a method of compressing and fixing the third material 3 and the fourth material 15 with the first material 1 and the second material 2 is effective. Specifically, a second gap 5, which is a gap in the plate thickness direction that separates the protrusions 14, is provided, and a structure is provided in which the amount of molten metal required to fill this second gap 5 is supplied. The laser welding method is particularly effective in that it melts and bonds the protrusions 14, and compresses and fixes the third material 3 and the fourth material 15 with the first material 1 and the second material 2 using the compressive force 6 caused by solidification and shrinkage of the welded portion 8 between the protrusions 14. Of course, even if there are two or more different types of materials, they can be joined without any problems.

[0045] Moreover, the irradiation area where the laser 7 irradiates the protrusion 14 from the plate thickness direction is smaller than the diameter or width of the embossed protrusion 14. In this embodiment, the irradiation area is smaller than the protrusion inner edge 10 of the protrusion 14 by a predetermined distance, for example, about 2 mm in diameter or width.

[0046] Here, in order for the third material 3 as a dissimilar material to melt due to the welding heat input transmitted from the welded portion 8 irradiated with the laser 7 and melted, the positional relationship between the protrusion inner edge 10 and protrusion outer edge 9 of the embossed protrusion 14 extruded in a tapered shape from the first material 1 and the second material 2 and the through hole 12 of the third material 3 is important.

[0047] In the present invention, the outermost shape of the protrusion outer edge 9 of the protrusion 14 of the first material 1 and / or the second material 2 as the homogeneous metal material is referred to simply as the diameter or width of the protrusion 14.

[0048] When the projection outer edge 9, which is the diameter or width of the projection 14 to be inserted, is within an appropriate range relative to the diameter of the through hole 12 of the third material 3, the end of the through hole 12 is indirectly affected by the heat of the welding heat input to the welded portion 8 by the irradiation of the laser 7, and softens and melts. The softened and melted third material 3 (end of the through hole 12) flows into the first gap 4. As a result, the third material 3 can be fixed in a compressive manner by the solidification and shrinkage action of the welded portion 8, and can also be fixed in close contact between the first material 1 and / or the second material 2 and the third material 3 in a direction intersecting the plate thickness direction.

[0049] Here, the irradiation area where the laser 7 irradiates the protrusion 14 from the plate thickness direction is smaller than the diameter of the embossed protrusion 14. In this embodiment, the irradiation area is smaller than the protrusion inner edge 10 of the protrusion 14 by, for example, a distance of about 2 mm in diameter.

[0050] In addition, in order for the third material 3 to melt due to the welding heat input transmitted from the molten welded portion 8 irradiated with the laser 7, the positional relationship between the protrusion inner edge 10 of the protrusion 14, the protrusion outer edge 9, and the through hole 12 is important. Here, the protrusion 14 is extruded into the first material 1 and the second material 2 in a tapered shape.

[0051] If the distance from the outer edge 9 of the protrusion 14 to the end of the through hole 12 is too close at the protrusion 14 where the laser 7 is irradiated, the end will be directly or indirectly affected by the thermal effect of the welding heat input transmitted from the welded portion 8 by the irradiation of the laser 7.

[0052] As a result, the molten third material 3, which is the end of the through hole 12, passes through the first gap 4 and flows into the second gap 5. As described above, the molten metal of the first material 1, which is the upper plate irradiated with the laser 7, falls into the second gap 5. Therefore, for example, if the third material 3 is a material with a low boiling point such as resin, it may vaporize and erupt, resulting in poor welding of the welded portion 8.

[0053] Furthermore, if the first gap 4 is too large, for example, 2.0 mm or more when the third material 3 is a resin material, or 1.5 mm or more when the third material 3 is CFRP, the end of the through hole 12 in the third material 3 is not easily subjected to the welding heat input of the welded portion 8 and does not melt. As a result, the third material 3 does not flow into the first gap, and it becomes difficult to closely fix the first material 1 and / or the second material 2 to the third material 3 in a direction intersecting the plate thickness direction. Therefore, the third material 3 is only compressed and fixed by the solidification and shrinkage action of the first material 1 and the second material 2.

[0054] From the above, the heat transfer conditions from the outer edge portion 9 of the protrusion to the end of the through hole 12 and the molten state of the third material 3 due to the thermal effects during welding change depending on the size of the first gap 4 and the material of the third material 3.

[0055] In addition, the protrusion 14 of the same type of metal material to be inserted may be positioned relative to the diameter of the through hole 12 of the different material using a clamp fixing jig, positioning pin, or a support and positioning method using a robot arm (not shown).

[0056] Furthermore, the size of the protruding outer edge 9 of the protruding portion 14, which is embossed, is offset from the protruding inner edge 10 by about 1 mm to the plate thickness in the outer circumferential direction in the embossed shape by press processing of the protruding portion 14, but this explanation will be described as 1 mm for simplicity. Note that this offset amount is preferably equivalent to the plate thickness, but may be about 0.6 to 1.4 times the plate thickness as long as it does not adversely affect the strength at the time of welding joint.

[0057] The above is derived from experimental data, an example of which is shown in Fig. 4. Fig. 4 is a graph showing the results of measuring the relationship between the quality of the third material 3 and the first gap 4 in the second embodiment of the present disclosure.

[0058] 4, the horizontal axis indicates the quality of the third material 3, and the vertical axis indicates the size of the first gap 4. Specifically, PET material, CFRP material, and A5000 material were used as the quality of the third material 3. Here, the A5000 material is an aluminum alloy, which is a non-ferrous metal material.

[0059] In this experiment, mild steel was used as the first material 1 and the second material 2, and the plate thickness t was set to 1.6 mm. As the third material 3, any one of the third materials 3 shown above was used, and the plate thickness was set to 2.0 mm. In the above combination, the first material 1 was placed on the upper side of the second material 2, and the third material 3 was sandwiched between the first material 1 and the second material 2, and the laser 7 was irradiated in a circular shape onto the inside of the protrusion inner edge portion 10 of the first material 1 to perform welding. In this experiment, the output of the laser 7 was set to 3 kW. For example, the diameter of the protrusion inner edge portion 10 of the first material 1 and the second material 2 was set to φ10 mm, and the diameter of the through hole 12 of the third material 3 was set to φ12 mm, and the laser 7 was irradiated from the plate thickness direction toward the protrusion portion 14 in a circular locus of φ8 mm, which is smaller than the diameter of the protrusion inner edge portion 10, to perform welding.

[0060] Next, the measurement results of Fig. 4 will be described. As shown in Fig. 4, when the third material 3 is a resin material, PET, if the size of the first gap 4 is 0.4 mm or more, the third material 3 can be compressed and fixed. This is because even if it is subjected to the heat effect of welding by the laser 7 irradiated to the protrusion inner edge portion 10, the molten third material 3 does not flow into the second gap 5 in a way that causes poor bonding.

[0061] However, if the size of the first gap 4 is smaller than 0.4 mm, that is, if the outer edge 9 of the protrusion and the end of the through hole 12 are too close to each other, the third material 3 melts due to the heat of the welding by the laser 7 and flows into the second gap 5. This may cause the PET material of the third material 3 to vaporize and erupt, resulting in poor welding of the welded portion 8.

[0062] Furthermore, in the case where the third material 3 is a CFRP material made of a resin material, if the first gap 4 is 0.2 mm or more, the third material 3 can be compressed and fixed by a compressive force 6 in the plate thickness direction. This is because even if it is subjected to the heat effect of welding by the laser 7, the molten third material 3 does not flow into the second gap 5 in a manner that would cause a poor joint.

[0063] However, when the first gap 4 is smaller than 0.2 mm, that is, when the outer edge 9 of the protrusion and the end of the through hole 12 are too close to each other, the third material 3 melts due to the heat of welding by the laser 7 irradiated to the inner edge 10 of the protrusion and flows into the second gap 5. As a result, the CFRP material of the third material 3 vaporizes and erupts, which may result in a good weld at the welded portion 8. As described above, the size of the first gap 4 permissible during welding varies to some extent depending on the characteristics such as the melting point and boiling point of the resin material of the third material 3.

[0064] Furthermore, when the third material 3 is an A5000 series aluminum alloy material, which is a non-ferrous metal material, regardless of the size of the first gap 4, even if it is subjected to the heat effect of welding by the laser 7 irradiated to the protrusion inner edge portion 10, the molten third material 3 does not flow into the second gap 5 to cause a joining failure. Therefore, stable compression fixing is possible.

[0065] In addition, in order to insert the protrusion outer edge portion 9 of the protrusion portion 14 into the through hole 12, the first gap 4 should be, for example, larger than 0 mm and at least the size necessary to insert the protrusion outer edge portion 9 into the through hole 12.

[0066] The above is experimental data showing an example of the difference depending on the material of the third material 3, but if the third material 3 is a resin material, the tendency is almost the same as when the PET material in FIG. 4 is used. If the third material 3 is a non-ferrous metal material, the tendency is almost the same as when the A5000 material, which is an aluminum alloy material in FIG. 4, is used. This is because even if other non-ferrous metal materials are used as the third material 3, the welding heat input during welding by irradiating the protrusion 14 of the first material 1 with the laser 7 does not cause the inner wall side of the through hole 12 to vaporize and erupt, resulting in poor welding of the welded portion 8, and the like, is not affected by heat. From the above, it can be said that other non-ferrous metal materials also have almost the same tendency.

[0067] Therefore, when the third material 3 is a non-ferrous metal material, it can be said that the third material 3 will not be affected by heat to such an extent that it melts and flows into the second gap 5, which is the gap between the mating surfaces of the protrusions 14 of the first material 1 and the second material 2.

[0068] Examples other than the circular welding by irradiation of the laser 7 shown in FIG. 2A are shown in, for example, FIG. 2B and FIG. 2C. FIG. 2B and FIG. 2C are perspective views for explaining the joining state during laser welding in the first embodiment of the present disclosure. As shown in FIG. 2B, in a joining structure between a first material 1 and a second material 2 of the same metal material and a third material 3 of a different material, the weld shape of the first material 1 as the upper plate in the plate thickness direction is elliptical. Also, as shown in FIG. 2C, the weld shape of the first material 1 is linear. When the strength required for the welded portion 8, which is the welding portion during welding by irradiation of the laser 7, has directionality, in other words, when it has a required joint strength distribution, the first material 1 is arranged so that it faces the direction in which the required joint strength is high. Specifically, by arranging the shape of the joint portion of the protrusion 14 between the first material 1 and the second material 2 of the same metal material, for example, on the long side of an ellipse, the area of ​​the scanning locus of the laser 7 can be reduced compared to the case of using a large circular protrusion 14.

[0069] Furthermore, by making the trajectory of the laser 7 irradiation linear as shown in FIG. 2C, welding can be performed in a shorter time than when welding is performed at multiple locations using a circular or elliptical trajectory of the laser 7 irradiation.

[0070] 5A and 5B show examples for further increasing the strength and facilitating the positioning. FIG. 5A and FIG. 5B are diagrams showing examples of use in the first embodiment of the present disclosure. FIG. 5A shows a structure in which a third material 3 is sandwiched between a second material 2, which is a metal material of the same kind, and a first material 1 folded in a stepped shape so as to increase the tensile strength during joining. The first material 1 is a joining structure having a positioning function when joining the second material 2 and the third material 3, and a function for increasing the tensile function. As shown in FIG. 5A, the first material 1 is joined to the second material 2 at the following two points. First, as the first point, the first material 1 is joined to the second material 2 via the third material 3 at a point having a protrusion 14. Next, as the second point, the first material 1 is directly joined to the second material 2 at a different location 10A from the first point. This makes it possible to prevent stress from being concentrated on one portion of the welded portion 8 when the second material 2 is pulled and twisted relative to the third material 3, thereby increasing the strength.

[0071] 5B shows a structure in which the second material 2 includes the protrusion 14 of the first material 1, and the second material 2 is folded back to allow the third material 3 to be joined to the second material 2 without using the first material 1. With this structure, a fixture for fixing the second material 2 is not required. In addition, by providing the protrusion 14 on at least one of the first material 1 or the second material 2, the third material 3 can be slid in and inserted from the side, making it easy to position the through hole 12 of the third material 3.

[0072] 5B corresponds to the first material 1 in this embodiment. That is, in this embodiment, the first material 1 and the second material 2 may be integrated together before being welded.

[0073] (Embodiment 2) Next, the present embodiment 2 will be described with reference to Fig. 1D and Fig. 2A. The parts overlapping with the embodiment 1 will be omitted. In Fig. 1D, the third material 3 is processed to have a through hole 12, and the first material 1 and the second material 2 are not processed to have a protrusion 14 such as an embossed shape to be inserted into the through hole 12 of the third material 3. Therefore, the thickness of the third material 3 corresponds to the gap in the thickness direction between the first material 1 and the second material 2. In other words, in this embodiment, the thickness of the third material 3 becomes the second gap 5.

[0074] As shown in Fig. 2A, the welding is performed by irradiating a region corresponding to through hole 12 from above first material 1 with laser 7, and the resulting bead has the shape of welded portion 8 as shown in Fig. 1D. Next, the joining state during and after welding will be described with reference to Fig. 1D. Welding is performed by irradiating laser 7 in a circular pattern from the plate thickness direction (first material 1 side) toward a region corresponding to through hole 12 of third material 3 serving as second gap 5 sandwiched between first material 1 and second material 2. When a weld 8 is formed during welding, the weld 8 (molten metal) of the first material 1 solidifies and shrinks, thereby reducing the second gap 5. If the size of the second gap 5, which is the plate thickness of the third material 3, is set to be 4% to 38% of the plate thickness t of the first material 1, which is the upper plate, as shown in Fig. 3, the solidification and shrinkage of the weld 8 becomes a compressive force 6 that sandwiches the third material 3 between the first material 1 and the second material 2.

[0075] Using this compression force 6, the third material 3 can be compressed and fixed by the first material 1 and the second material 2. The setting of 6% to 38% of the thickness of the first material 1 was derived from data obtained from an experiment similar to that described in the first embodiment (the experimental results are not shown). If the size of the second gap 5 is set as above, molten metal equivalent to a maximum of 30% to 38% of the thickness t of the first material 1 falls into the inside of the through hole 12, and it is shown that joining can be performed without creating a hole. Note that if the size of the second gap 5 exceeds a maximum of 30% to 38% of the thickness t of the first material 1, the amount of molten metal required to fill the inside of the through hole 12 as the thickness equivalent to the second gap 5 cannot be secured, resulting in a state in which a hole is partially created.

[0076] Conversely, if the second gap 5, which is the gap in the plate thickness direction, is smaller than 0.1 mm, the gap becomes too small, and the first material 1 and the second material 2, which are homogeneous metal materials, are melt-bonded to each other, resulting in insufficient compressive fixing force to compress and fix the dissimilar third material 3.

[0077] (Embodiment 3) Next, the third embodiment will be described with reference to FIGS. 1B, 2D, and 2E.

[0078] In the first embodiment, as described above, when the second gap 5 is large, the spacer 13 as shown in Fig. 1B is inserted into the through hole 12. In the present embodiment, a laser welding method that enables good joining even when the second gap 5 is large without inserting the spacer 13 will be described.

[0079] 2D and 2E are perspective views for explaining the state of welding during laser welding in the third embodiment of the present disclosure. FIG. 2D shows a weaving-shaped trajectory of the laser 7. FIG. 2E shows a spiral trajectory of the laser 7. As shown in FIG. 2D and FIG. 2E, the bead width of the weld can be widened by irradiating the laser 7 in a weaving or spiral shape. This can increase the amount of molten metal. This increased amount of molten metal falls into the inside of the through hole 12, and welding can be performed without creating a hole.

[0080] As an example, by changing the trajectory of the laser 7 irradiation from a circular shape to a spiral shape, the effective range of compression fixing of the plate thickness t of the first material 1 relative to the size of the second gap 5 increases. Specifically, it is possible to increase the effective range of compression fixing of the plate thickness t of the first material 1 from 4% to 38% to 4% to 63%. This was derived from experimental data, and an example of the experimental data is shown in Figure 6. The difference from Figure 3 is that the laser output has been increased to 3.5 kW because the welding heat input is dispersed by welding in a spiral shape. FIG. 6 is a graph showing the results of measuring the relationship between the sheet thickness t of the first material 1 and the second gap 5 during spiral welding in embodiment 3 of the present disclosure. In the graph shown in FIG. 6, the horizontal axis indicates the sheet thickness t of the first material 1, and the vertical axis indicates the size of the second gap 5.

[0081] As shown in FIG. 6, when the plate thickness t of the first material 1 is 0.8 mm and the size of the second gap 5 is between 0.1 mm and 0.5 mm, the third material 3 can be compressed and fixed by the solidification and contraction action of the molten metal in the welded portion 8. Also, if the size of the second gap 5 exceeds 0.5 mm, a part of the weld line will have a hole, resulting in poor welding. Therefore, when the plate thickness t of the first material 1 is 0.8 mm, the size of the second gap 5 is within the effective range of compression fixing, from 13% to 63% of the plate thickness t of the first material 1. Also, when the plate thickness t is 2.3 mm, the size of the second gap 5 is within the range of 0.1 mm to 1.2 mm, and the third material 3 can be compressed and fixed by the solidification and shrinkage of the molten metal of the welded portion 8. If the size of the second gap 5 exceeds 1.2 mm, a part of the weld line will have a hole, resulting in poor welding. Therefore, when the plate thickness t of the first material 1 is 2.3 mm, the size of the second gap 5 is within the effective range of compression fixing welding, from 4% to 52% of the plate thickness t of the first material 1.

[0082] This indicates that when the plate thickness t of the first material 1 and the size of the second gap 5 satisfy the above relationship, molten metal equivalent to 52% or less of the plate thickness t of the first material 1 falls into the second gap 5 and can be joined to the second material 2 without creating a hole. When the size of the second gap 5 exceeds 52% of the plate thickness t of the first material 1, the amount of molten metal required to fill the second gap 5 cannot be secured, resulting in a state in which a hole is partially created.

[0083] The application range of the laser 7 to the second gap 5 can be increased not only by weaving or by a spiral trajectory, but also by a spiral trajectory from the inside to the outside or from the outside to the inside.

[0084] Conventionally, the rivet 51 used as a joining member for dissimilar materials had to secure space for parts of the dissimilar materials to deform and move during crimping and spot welding, and to prevent the dissimilar materials from collapsing due to misalignment of the electrodes during spot welding, thereby suppressing a decrease in fastening force. For this reason, the rivet 51 needed to have a complex and highly accurate shape, such as an R (Radius)-shaped chamfer 30 or an annular groove 31. In this case, the shape of the rivet 51 needs to be precise and complex, so precision machining is required, and the manufacturing cost is high.

[0085] In addition, because it is spot welding, it takes time to apply pressure, pass current, cool, move, etc., so productivity is low, and the need to clamp from both sides limits the freedom of design. Also, if it is too close to the adjacent rivet, the current of the spot welding is shunted, and there are cases where the formation of a nugget, which is a welded solidified part that occurs in the resistance welded weld, is insufficient. Therefore, a joining pitch greater than the minimum separation pitch that can form the desired nugget is required, and there was a problem that it was not possible to increase rigidity where it was needed, but the present disclosure can solve the conventional problem.

[0086] As shown in the examples so far, the laser welding method of the present disclosure includes a step of sandwiching a third material 3, which has a penetration part into which the protrusion 14 is inserted and is difficult to weld to the first material 1 and the second material 2, between a first material 1 and a second material 2 made of the same kind of metallic material that can be welded to each other and at least one of which is provided with a protrusion 14. The method also includes a step of irradiating a region corresponding to the protrusion 14 from the first material 1 side with laser light while the third material is sandwiched between the first material 1 and the second material 2, to weld the first material 1 and the second material 2 through the penetration part. Furthermore, in the process of sandwiching the third material 3 between the first material 1 and the second material 2, a first gap 4 is provided between the inner peripheral surface of the penetration portion and the protrusion 14, and a second gap 5 according to the plate thickness of the first material in the region corresponding to the protrusion 14 is provided between the first material 1 and the second material 2 in the region corresponding to the protrusion 14 in the plate thickness direction. With this configuration, by using a laser welding method for fixing dissimilar materials to homogeneous metal materials so that the dissimilar materials are compressed and fixed by melting and bonding the homogeneous metal materials to each other, complex structural parts that require precision are not required.

[0087] Furthermore, in the laser welding method according to the present disclosure, by setting the size of the first gap 4 and the size of the second gap 5 within a predetermined range, the first material 1 and the second material 2 can be melt-bonded to each other by laser welding alone, and the third material 3 can be compressed and fixed by the first material 1 and the second material 2.

[0088] In addition, because laser welding is used instead of spot welding, the work time including welding can be reduced to about 25% compared to spot welding, significantly improving productivity. It also makes it possible to increase rigidity where necessary and expand design freedom. [Industrial Applicability]

[0089] INDUSTRIAL APPLICABILITY The present disclosure is industrially useful as a joining structure for laser welding that has a simple structure, significantly shortens production takt time, increases rigidity in necessary locations, and expands design freedom when joining dissimilar materials. [Explanation of symbols]

[0090] 1. First Ingredient 2. Second Ingredient 3. The third ingredient 4. The First Gap 5. The Second Gap 6 Compression Force 7 Laser 8 Welding 9. Outer edge of protrusion 10. Inner edge of protrusion 11 Weld Bead 12 Through hole 13 Spacer 14 Protrusion 15 The Fourth Ingredient

Claims

1. Between a first material and a second material made of the same metallic material that can be welded to each other, A third material having a penetration portion and difficult to weld to the first material and the second material, a step of sandwiching the first material and the second material in a region corresponding to the through-hole so as to provide a second gap corresponding to a plate thickness of the first material on a side irradiated with laser light; the third material is sandwiched between the first material and the second material, and the first material and the second material are physically separated from each other by the second gap before welding between the first material and the second material in a region corresponding to the penetration portion, the region corresponding to the penetration portion is irradiated with the laser light from the first material side; The first material and the second material are melt-bonded to each other through the through-hole, and the third material is compressed and fixed, thereby fixing the third material, the first material, and the second material, A laser welding method in which, when the scanning trajectory of the welding laser light is a weaving trajectory, a spiral trajectory, a spiral trajectory from the inside to the outside, or a trajectory from the outside to the inside, the size of the second gap is set to be 0.1 mm or more and 52% or less of the plate thickness of the first material.

2. Between a first material and a second material made of the same metallic material that can be welded to each other, A third material having a penetration portion and difficult to weld to the first material and the second material, a step of sandwiching the first material and the second material in a region corresponding to the through-hole so as to provide a second gap corresponding to a plate thickness of the first material on a side irradiated with laser light; the third material is sandwiched between the first material and the second material, and the first material and the second material are physically separated from each other by the second gap before welding between the first material and the second material in a region corresponding to the penetration portion, the region corresponding to the penetration portion is irradiated with the laser light from the first material side; The first material and the second material are melt-bonded to each other through the through-hole, and the third material is compressed and fixed, thereby fixing the third material, the first material, and the second material, When the scanning trajectory of the welding laser light is a weaving trajectory, a spiral trajectory, a spiral trajectory from the inside to the outside, or a trajectory from the outside to the inside, A laser welding method in which the size of the second gap is set to be 0.1 mm or more, and 63% or less of the thickness of the first material when the thickness of the first material is 0.8 mm, 58% or less of the thickness of the first material when the thickness of the first material is 1.2 mm, 56% or less of the thickness of the first material when the thickness of the first material is 1.6 mm, or 52% or less of the thickness of the first material when the thickness of the first material is 2.3 mm.

3. At least one of the first material and the second material is provided with a protrusion, the protrusion is inserted into the through-hole of the third material, and the second gap is The laser welding method according to claim 1 or 2, wherein a laser beam is irradiated onto an area corresponding to the protrusion from the first material side.

4. 4. The laser welding method according to claim 1, wherein the second gap, which is a gap between the first material and the second material, is set by placing a spacer between the first material and the second material or by forming the second gap using a welding material.

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