JP2015015211A - Bus bar and method of manufacturing the same - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a bus bar capable of being welded to an external terminal of an electronic component without being associated with weld cracking of the bus bar even without use of a filler metal.SOLUTION: In a bus bar 1, a plurality of terminal parts 12 and 13 connected to an external terminal of an electronic component are made of 1000 series aluminum; a body part 11 linking the terminal parts 12 and 13 is made of a 6000 series aluminum alloy; and the terminal parts 12 and 13 and the body part 11 are joined in a frictionally agitated manner and integrated.

Description

  The present invention relates to an aluminum bus bar used for connecting electronic components.

  In this specification and claims, the term “aluminum” is used to include both aluminum and its alloys.

  A highly conductive 1000 series aluminum is used as the material of the external terminal of the electronic component. In addition, a bus bar material for connecting electronic components is required to have strength in addition to conductivity, and therefore, a 6000 series aluminum alloy is used.

  Fastening and welding of bolts and nuts are known as means for connecting external terminals of electronic components and bus bars. However, since electrical resistance increases due to contact resistance when connecting by bolt fastening, it is desirable to connect by welding. ing. Further, laser welding capable of high-speed joining is known as a method for welding an external terminal of an electronic component and a bus bar (see Patent Document 1).

JP 2013-110283 A (Claim 3)

  However, in general, 6000 series aluminum alloys have poor weldability, and there is a problem that welding cracks are likely to occur in the bus bars when the external terminals and 6000 series aluminum alloy bus bars are welded. In order to prevent the weld crack of a bus bar, when the filler material which consists of 4043 aluminum alloy or 5356 aluminum alloy is used, the problem that electroconductivity falls because these filler materials exist in a welding part will arise. In addition, there are also operational problems such as the rate of supply of the filler metal being limited and the high speed of laser welding not being utilized, and the condition management such as setting of the supply position and supply angle of the filler material being difficult.

  The present invention provides a bus bar which can be welded to an external terminal of an electronic component without using a weld crack of the bus bar without using a filler material, and a related technique.

  That is, this invention has the structure as described in following [1]-[6].

  [1] A plurality of terminal portions connected to external terminals of the electronic component are made of 1000 series aluminum, a main body portion connecting these terminal portions is made of a 6000 series aluminum alloy, and the terminal portion and the main body portion are frictioned. A bus bar characterized by being integrally joined by stirring.

  [2] The bus bar according to item 1, wherein the terminal portion is thicker than the main body portion.

  [3] A plurality of terminal part materials made of 1000 series aluminum and connected to an external terminal of an electronic component are connected by a body part material made of a 6000 series aluminum alloy, and the terminal part material and the body part A method of manufacturing a bus bar, characterized in that the material is integrated by friction stir welding.

[4] A plurality of composite materials are obtained by friction stir welding and integrating a plurality of bus bar terminal part materials and a plurality of bus bar body part materials,
4. The method for manufacturing a bus bar according to item 3, wherein the plurality of composite materials for cutting are cut to obtain a plurality of bus bars.

  [5] The method for manufacturing a bus bar according to the above item 3 or 4, wherein the artificial aging treatment is performed after the terminal portion material and the main body portion material are integrated by friction stir welding.

  [6] By welding one connecting portion of the bus bar according to the preceding item 1 or 2 to an external terminal of the first electronic component and welding the other connecting portion of the bus bar to the external terminal of the second electronic component, A method for connecting electronic parts, comprising connecting one electronic part and a second electronic part.

  According to the invention described in [1], the strength as the connecting member is ensured by the body portion being made of a 6000 series aluminum alloy. Since the terminal part connected to the external terminal of the electronic component is made of 1000 series aluminum, the weldability is good, and welding cracks occur without using a filler material when welding the terminal part to the external terminal of the electronic component. Can be joined well. Further, since welding can be performed without using a filler material, there is no decrease in conductivity due to the filler material, and energy loss due to bus bar connection can be reduced. Furthermore, since work associated with setting and managing conditions for supplying the filler metal is not necessary, welding workability is good.

  Further, since the main body portion and the terminal portion of the bus bar are integrated by friction stir welding, thermal deformation at the time of joining is small, and defects such as blowholes and cracks caused by welding do not occur. Moreover, since it joins directly, without going through a brazing material and a filler material, the electroconductive fall in these junction parts does not arise.

  According to the invention described in [2], the strength of the terminal portion can be increased by making the thickness of the terminal portion thicker than that of the main body portion, and the strength difference between the main body portion and the terminal portion can be reduced.

  According to the invention described in [3], a bus bar having the above effects can be manufactured.

  According to the invention described in [4], a plurality of bus bars can be efficiently manufactured.

  According to invention of [5], the intensity | strength of the junction part of the main-body part and terminal part which were softened by friction stir welding is recoverable.

  According to the invention described in [6], since the terminal portion of the bus bar is made of 1000 series aluminum and has good weldability, the first electronic component does not cause a weld crack without supplying a filler material. These electronic components can be coupled by connecting to external terminals of the second electronic component. Further, by not using the filler material, there is no decrease in conductivity due to the filler material, and energy loss due to the bus bar connection can be reduced. Furthermore, since work associated with setting and managing conditions for supplying the filler metal is not necessary, welding workability is good.

It is a perspective view showing one embodiment of a bus bar of the present invention. It is sectional drawing which shows the connection method of the capacitor | condenser using the bus bar of FIG. It is a perspective view explaining a friction stir welding method. It is a perspective view which shows the manufacturing process of the 1st manufacture example of the bus-bar of FIG. It is a perspective view which shows the manufacturing process of the 2nd manufacturing example of the bus bar of FIG. It is a perspective view which shows the manufacturing process which changed a part of process of the 2nd manufacture example. It is sectional drawing which shows the friction stir welding of a lap joint.

[Bus bar structure]
FIG. 1 shows an embodiment of the bus bar of the present invention, and FIG. 2 shows an example of connecting electronic components by the bus bar of FIG.

  The bus bar (10) is a plate-like body, and semicircular connection portions (12) and (13) are integrally joined to both ends of the rectangular main body portion (11) so as to be approximately at the center of the terminal portions (12) and (13). A circular through hole (14) that is engaged with an external terminal of the electronic component is formed in the top. In the bus bar, the main body part (11) is made of a 6000 series aluminum alloy, the terminal parts (12) and (13) are made of a 1000 series alloy aluminum, and these are integrated by friction stir welding. It is a composite material.

  The 6000 series aluminum alloy that is the material of the main body (11) is an Al—Si—Mg series alloy containing Si and Mg as essential components, and has high strength. Since the bus bar (10) is a member that requires high conductivity, among 6000 series aluminum alloys, the Si concentration is 0.2 to 0.9 mass% and the Mg concentration is 0.35 to 1.2 mass%. It is preferable to use an alloy. An alloy having Si and Mg concentrations in the above ranges has good conductivity. In alloys registered in JIS, 6101 (Si concentration: 0.3 to 0.7 mass%, Mg concentration: 0.35 to 0.8 mass%) and 6063 (Si concentration: 0.2 to 0.6 mass%) %, Mg concentration: 0.45 to 0.9 mass%) corresponds to the alloy having the above composition.

  On the other hand, 1000 series aluminum constituting the terminal portion (12) is pure aluminum in which the concentration of the impurity element is regulated without adding other elements, and has good conductivity, and is widely used as an electrode material. In order to ensure good conductivity, it is preferable to use aluminum having an aluminum purity of 99.50% by mass or more. In pure aluminum registered in JIS, 1060 (aluminum purity is 99.60% by mass or more), 1070 (aluminum purity is 99.70% by mass or more) and the like are preferable.

  The plurality of terminal portions (12) and (13) need not be made of 1000 series aluminum having the same composition, and the plurality of terminal portions (12) and (13) may be made of 1000 series aluminum having different compositions. it can.

  The friction stir welding method, which is a method of joining the main body part (11) and the terminal parts (12) and (13), brings a welding tool that rotates at high speed into contact with the part to be joined and its vicinity, and is joined by frictional heat generated. In this method, the members to be joined are joined in a solid phase by softening and stirring the members. Since this friction stir welding can be performed at a lower temperature than melt welding or brazing, there is an advantage that thermal deformation at the time of bonding is small, and defects such as blow holes and cracks do not occur.

  FIG. 3 is an explanatory view of the friction stir welding method and shows an example of butt joining of the materials to be joined (A) and (B). In the joining tool (30), a small-diameter pin (33) having the same rotation axis (Q) as that of the shoulder (31) is protruded from the tip surface (32) of the large-diameter shoulder (31). . Insert the pin (33) of the joining tool (30) into the joining portion (35) that is the butting portion of the materials to be joined (A) and (B), and join the portion to be joined at the front end surface (32) of the shoulder (31) (35) Hold the vicinity and move the welding tool (30) in the inserted / rotated state to perform bonding. In FIG. 3, (36) is the friction stir welding part joined by the joining tool (30).

  The friction stir welding method also allows butt joining of materials to be joined having different thicknesses. For example, the pin (33) of the joining tool (30) is relatively moved from the thin material side to the thick material side. It can be joined without any problem by inserting it at an angle. The friction stir welding method can also be applied to the production of lap joints.

  The bus bar (10) is obtained by abutting the terminal portions (12) and (13) at both ends of the main body portion (11), joining the abutting portions by the friction stir welding, and integrating them. Since the main body portion (11) and the terminal portions (12) and (13) are directly joined without the use of a brazing filler metal or a filler metal, the conductivity at the joining interface does not deteriorate.

[How to connect electronic components]
FIG. 2 shows an example of connecting electronic components by the bus bar (10). The first capacitor (21) and the second capacitor (22) shown in FIG. 2 correspond to the electronic component in the present invention, and these anode terminal (23) and cathode terminal (23) correspond to external terminals.

  The first capacitor (21) and the second capacitor (22) have the same shape, and the anode terminal (23) and the cathode terminal (24) protrude from the upper surface in a cylindrical shape. The anode terminal (23) and the cathode terminal (24) are made of 1000 series aluminum.

  The anode terminal (23) of the first capacitor (21) is inserted into the through hole (14) of one terminal portion (12) of the bus bar (10), and the peripheral surface of the through hole (14) and the anode terminal (23 ) And are welded. The cathode terminal (24) of the second capacitor (22) is inserted into the through hole (14) of the other terminal portion (13) of the bus bar (10), and the peripheral surface of the through hole (14) and the cathode terminal (24 ) Are circumferentially welded. Thus, the first capacitor (21) and the second capacitor (22) are connected in series via the bus bar (10).

  Since the terminal portions (12) and (13) of the bus bar (10) are made of 1000 series aluminum and have good weldability, the anode terminal (23) and the weld terminal are not generated without supplying a filler metal. It can be connected to the cathode terminal (24). Further, by not using the filler material, there is no decrease in conductivity due to the filler material, and energy loss due to the connection can be reduced. Furthermore, since work associated with setting and managing conditions for supplying the filler metal is not necessary, welding workability is good.

  The welding means is not limited at all, and can be appropriately selected according to the type of electronic component, the shape of the external terminal, and the like. Melt welding methods such as laser welding, electron beam welding, arc welding, and resistance welding can be exemplified, and laser welding can be recommended from the viewpoint of low thermal influence and excellent productivity.

  The material of the terminal parts (12) and (13) is 1000 series aluminum, which is lower in strength than the 6000 series aluminum alloy, but the main body part (11) that is not subjected to welding with the external terminal is made of 6000 series aluminum alloy. As a result, the bus bar (10) has a required strength as a connecting member.

  The shape of the bus bar of the present invention is not limited to those in which terminal portions are formed at both ends of the main body portion in the illustrated example, and the number of terminal portions and the positional relationship with the main body portion are different from those for series and parallel use, and the shapes of electronic components. The shape and position of the external terminal, the arrangement of electronic components to be connected, and the like can be changed as appropriate. Further, the engagement form between the terminal portion and the external terminal is not limited to the one in which the through hole is provided in the terminal portion and the external terminal is inserted, and the design can be appropriately changed according to the shape of the external terminal.

  In addition, the types of electronic components connected by the bus bar are not limited at all, and examples thereof include a battery, an LED lamp, an automobile ECU (engine control unit), and the like in addition to a capacitor.

[Bus bar manufacturing method]
The bus bar (10) is abutted with the terminal portions (12) and (13) on both side surfaces of one body portion (11) having the shape shown in FIG. 1, and the butted portions are joined using the friction stir welding method described above. It can produce by doing.

  Also, as shown in FIGS. 4 to 6, a plurality of body material and a plurality of terminal material are joined together to produce a plurality of bus bar composite materials. A plurality of bus bars can also be produced by cutting the composite material for individual production. By using a composite material for taking a plurality of pieces, the bus bar can be efficiently manufactured by reducing the number of friction stir welding.

  In the following description, the dimensions of each part of the bus bar (10) are as follows: width: W, overall length in the longitudinal direction: L, length of the body part (11) in the longitudinal direction: L1, terminal part in the longitudinal direction (12 ) Length: L2, the length (L3) of the terminal portion (13) in the longitudinal direction: L3, and the thickness: T.

(First production example)
FIG. 4 shows a process of producing a plurality of bus bars (10) from a multi-cavity composite material (40) whose cross section corresponds to the planar shape of the bus bar (10).

  For producing the multi-piece composite material (40), a square bar material having a cross-sectional dimension of L1 × W and a cross-sectional shape of the main body (11) as the main body (11) material. (41), a semicircular bar (42) corresponding to the planar shape of the terminal portion (12), and a terminal portion (13 ) As a material, a semicircular bar (43) having a cross-sectional dimension of L3 × W and a cross-sectional shape corresponding to the planar shape of the terminal portion (13) is used. The lengths of these rods (41), (42), and (43) are dimensions obtained by adding a cutting allowance to the thickness T of the number of bus bars (10) to be produced.

  The flat part of the semi-circular bar (42) (43) is butted against both sides of the square bar (41), and the pin (33) of the joining tool (30) is inserted into the butted part (44). These bars (41), (42), (43) are moved by moving the joining tool (30) along the longitudinal direction of (44), that is, along the length of the bars (41), (42), (43) of the material. ) Is friction stir welded. Thereby, the composite material (40) for taking a plurality of pieces in which the rods (41), (42) and (43) are integrated is produced.

  The multi-piece composite (40) is cut in a plane perpendicular to the longitudinal direction of the butting portion (44), and the cut surface is the planar shape of the bus bar (10). A plurality of bus bars (10) can be obtained by cutting the material (40) into the thickness (T) of the bus bar (10). The through hole (14) may be drilled after cutting, or a hollow material may be used as the through hole (14) by using a hollow material instead of the semicircular rods (42) and (43). In addition, bus bars having different thicknesses can be produced from one multi-cavity composite material (40).

(Second production example)
FIG. 5 shows a process of producing a plurality of bus bars (10) from a multi-cavity composite material (50) having the same thickness T as the bus bar (10).

  For the production of the multi-piece composite material (50), the cross-sectional dimension is a plate material (51) having a width L1 × thickness T as a material for the main body (11) and the cross-sectional dimension is as a material for the terminal part (12). A plate member (52) having a width (L2 + α) × thickness T and a plate member (53) having a cross-sectional dimension of width (L3 + α) × thickness T are used as the material for the terminal portion (13). The reason why the widths of the plate members (52) and (53) for the terminal portions (12) and (13) are made larger than the actual dimensions L2 and L3 of the terminal portions (12) and (13) is to anticipate the punching allowance α in the subsequent process. Because it is. The lengths of these plate members (51), (52), and (53) are dimensions obtained by adding a punching allowance to the width W corresponding to the number of bus bars (10).

  The plate members (52) and (53) are butted against both side surfaces of the plate material (51), the pins (33) of the joining tool (30) are inserted into the butted portions (54), and the longitudinal direction of the butted portions (54), that is, The plate members (51), (52), and (53) are friction stir welded by moving the joining tool (30) along the length direction. As a result, a plate-shaped multi-cavity composite material (50) in which the plate materials (51) (52) (53) are integrated is produced.

  A plurality of bus bars (10) can be obtained by punching the plate-like multi-cavity composite material (50) into a planar shape of the bus bar (10).

  FIG. 6 shows a manufacturing process in which a part of the process of the second manufacturing example of FIG. 5 is changed. The multi-ply composite material (55) in FIG. 6 is a plate-like material having a thickness T similar to the multi-ply composite material (50) in FIG. (10) is punched out. The composite material (55) for taking a plurality of sheets is a plate (51) having a cross-sectional dimension of width (L2 + L3 + α) × thickness T as a material (51) for the main body (11) and a material for both terminals (12) (13) ( 56) are alternately assembled, and further, the terminal (12) plate (52) and the terminal (13) plate (53) (not shown) outside the plate (51) for the body (11) at both ends. ) And the butted portion (57) are integrated by friction stir welding. Since the composite material (55) for taking plural pieces can be produced by assembling an arbitrary number of plate members (51) for the body portion (11) and plate members (56) for both terminal portions (12) (13), A large number of bus bars (10) can be efficiently manufactured.

  FIG. 5 and FIG. 6 show an example of manufacturing a bus bar (10) in which the main body (11) and the terminal portions (12) and (13) have the same thickness, but the main body forming plate member (51) and the terminal portion forming The plate materials (52) and (53) are not limited to the same thickness, and a multi-piece composite material can be produced using plate materials having different thicknesses. A bus bar in which the main body portion and the terminal portion are different in thickness can also be produced from such a multi-cavity composite material.

  The bus bar of the present invention has a strength difference between the 6000 series aluminum alloy that is the material of the main body and the 1000 series aluminum that is the material of the terminal portion. The strength of the terminal portion can be increased and the strength of the main body portion and the terminal portion can be made uniform. Alternatively, at least the difference in strength between the main body portion and the terminal portion can be reduced. The same applies to the case where the material is made of one bus bar without using a multi-cavity composite material.

  When the thickness of the terminal portions (12) and (13) is greater than that of the main body portion (11), the thickness of the terminal portions (12) and (13) when the thickness of the main body portion (11) is 100 is set to It is preferable to set to the range of 150-300, and the range of 200-250 is more preferable. Further, the plurality of terminal portions (12) and (13) need not have the same thickness and may have different thicknesses.

  In all of the manufacturing examples in FIGS. 4 to 6, the joint shape of the main body portion and the terminal portion is abutted, but the shape of the joint is not limited to the butting and may be a lap joint. FIG. 7 shows a friction stir welding example of a joint in which steps (61a) and (62a) are formed at the ends of the main body portion (61) and the terminal portion (62), and these steps (61a) and (62a) are engaged and overlapped. Is shown. Moreover, the lap joint which does not provide a level | step difference may be sufficient.

  Since the joint portion of the bus bar joined by the friction stir welding method is softened, it is preferable to recover the strength of the base material by performing an artificial aging treatment after joining. For the multi-cavity composite material, an artificial aging treatment may be applied to the multi-cavity composite material before cutting, or an artificial aging treatment may be applied to each individual bus bar after cutting. Preferable conditions for the artificial aging treatment are 150 to 230 ° C. × 1 to 12 hours, and particularly preferable conditions are 180 to 220 ° C. × 3 to 8 hours.

  The present invention can be suitably used as a bus bar that is connected to an external terminal of an electronic component by welding.

10 ... Bus bar
11 ... Main body
12, 13… Terminal part
14 ... through hole
21 ... 1st capacitor (electronic component)
22 ... Second capacitor (electronic component)
23… Anode terminal (external terminal)
24 ... Cathode terminal (external terminal)
30 ... Joining tools
40… Composite material for taking multiple pieces
50, 55… Composite material for taking multiple pieces

Claims (6)

  A plurality of terminal portions connected to external terminals of the electronic component are made of 1000 series aluminum, a main body portion connecting these terminal portions is made of a 6000 series aluminum alloy, and the terminal portion and the main body portion are friction stir welded. A bus bar characterized by being integrated.   The bus bar according to claim 1, wherein the terminal portion is thicker than the main body portion.   A plurality of terminal part materials made of 1000 series aluminum and connected to external terminals of an electronic component are connected by a body part material made of 6000 series aluminum alloy, and the terminal part material and the body part material are A method for manufacturing a bus bar, characterized by integrating by friction stir welding. A plurality of bus bar terminal material and a plurality of bus bar body material are integrated by friction stir welding to produce a composite material
The bus bar manufacturing method according to claim 3, wherein a plurality of bus bars are obtained by cutting the plurality of composite materials.   The method for manufacturing a bus bar according to claim 3 or 4, wherein the artificial aging treatment is performed after the terminal portion material and the main body portion material are integrated by friction stir welding. By welding one connection portion of the bus bar according to claim 1 or 2 to an external terminal of the first electronic component and welding the other connection portion of the bus bar to the external terminal of the second electronic component, A method for connecting an electronic component, comprising connecting the component and a second electronic component.

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