KR20080102524A - Manufacturing method of complex busbar by explosion expander - Google Patents

Manufacturing method of complex busbar by explosion expander Download PDF

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Publication number
KR20080102524A
KR20080102524A KR1020070049109A KR20070049109A KR20080102524A KR 20080102524 A KR20080102524 A KR 20080102524A KR 1020070049109 A KR1020070049109 A KR 1020070049109A KR 20070049109 A KR20070049109 A KR 20070049109A KR 20080102524 A KR20080102524 A KR 20080102524A
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South Korea
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explosion
copper
core
coating material
manufacturing
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KR1020070049109A
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Korean (ko)
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김봉서
박수동
오민욱
이희웅
이병일
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한국전기연구원
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Priority to KR1020070049109A priority Critical patent/KR20080102524A/en
Publication of KR20080102524A publication Critical patent/KR20080102524A/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/06Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating by means of high energy impulses, e.g. magnetic energy
    • B23K20/08Explosive welding
    • B23K20/085Explosive welding for tubes, e.g. plugging
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24Selection of soldering or welding materials proper
    • B23K35/28Selection of soldering or welding materials proper with the principal constituent melting at less than 950 degrees C
    • B23K35/286Al as the principal constituent
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K35/00Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
    • B23K35/22Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
    • B23K35/24Selection of soldering or welding materials proper
    • B23K35/30Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
    • B23K35/302Cu as the principal constituent
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D39/00Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders
    • B21D39/04Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders of tubes with tubes; of tubes with rods
    • B21D39/042Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating; Tube expanders of tubes with tubes; of tubes with rods using explosives
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D51/00Making hollow objects
    • B21D51/02Making hollow objects characterised by the structure of the objects
    • B21D51/10Making hollow objects characterised by the structure of the objects conically or cylindrically shaped objects
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00Articles made by soldering, welding or cutting
    • B23K2101/04Tubular or hollow articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00Materials to be soldered, welded or cut
    • B23K2103/18Dissimilar materials
    • B23K2103/22Ferrous alloys and copper or alloys thereof

Abstract

A complex busbar manufacturing method by explosion-expansion is provided to reduce the manufacturing process and cost by welding a core formed inside a cladding to the inner surface of the cladding through explosion-expansion. A complex busbar manufacturing method by explosion-expansion is as follows. A core(200) having a diameter smaller than that of a cladding is inserted in the hollow cladding(100). After a fuse(300) is positioned inside the core, the fuse is ignited. As the core is expanded instantaneously upon the explosion of the fuse, the exterior of the core is welded to the interior of the cladding and a hollow busbar is completed. The fuse, which is an explosion wire where a high-energy explosive compound is filled in a fine metallic tube, has a length equal to or greater than that of the core. The cladding is made of copper and the core is made of aluminum, or otherwise. A buffer material can be put in between the fuse and the core for more uniform expansion.

Description

폭발 확관에 의한 복합 부스바 제조방법{manufacturing method of complex busbar by explosion expander}Manufacturing method of complex busbar by explosion expander

도 1 - 본 발명에 따른 폭발 확관에 의한 복합 부스바 제조방법에 대한 모식도((a)폭발 확관 전, (b)폭발 확관 후).Figure 1-Schematic diagram of a method for manufacturing a composite busbar by explosion expansion according to the present invention ((a) before explosion expansion, (b) after expansion expansion).

도 2 - 본 발명에 따른 폭발 확관에 의한 복합 부스바가 중공형으로 형성된 경우에 대한 사시도.Figure 2-a perspective view of the case where the composite busbar by explosion expansion in accordance with the present invention formed in a hollow.

도 3 - 본 발명에 따른 폭발 확관에 의한 복합 부스바가 평판형으로 형성된 경우에 대한 사시도.Figure 3-perspective view of the case where the composite busbar by explosion expansion according to the invention is formed in a flat plate type.

<도면에 사용된 주요부호에 대한 설명><Description of Major Symbols Used in Drawings>

100 : 피복재(100) 200 : 중심재100: covering material (100) 200: core material

300 : 도폭선300: dopter line

본 발명은 부스바 제조방법에 관한 것으로서, 특히 피복재 내부에 형성된 중심재를 폭발 확관에 의해 피복재 내면에 용접함으로써 제조공정의 단순화 및 비용을 절감시키는 폭발 확관에 의한 복합 부스바 제조방법에 관한 것이다.BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a method for manufacturing a busbar, and more particularly, to a method for manufacturing a composite busbar by explosion expansion, which simplifies a manufacturing process and reduces cost by welding a core material formed inside a coating material to an inner surface of the coating material by explosion expansion.

일반적으로 부스바(busbar)는 구리로 형성되어 있으며, 표면적이 크므로 방열효과가 우수하고 표면에 흐르는 고주파 전류의 임피던스를 낮추어 줌으로써 대전류를 전달하기 위한 시스템에 널리 활용되고 있다.In general, busbars are made of copper and have a large surface area, and thus have excellent heat dissipation effect and are widely used in a system for delivering large currents by lowering the impedance of high frequency current flowing on a surface.

종래의 부스바는 전기전도도(100% IACS) 및 융점(1083℃)이 높은 관계로 거의 순수한 구리로만 제작되었으나, 순수한 구리는 가격이 높을 뿐만 아니라 비중(8.92g/cm3)이 커서, 부스바의 보관 및 설치가 어려우며, 설치 시간이 많이 소요되어, 전체적으로 생산 비용 및 설치비용을 상승시키는 요인이 되고 있다.Conventional busbars are made of almost pure copper due to their high electrical conductivity (100% IACS) and high melting point (1083 ° C), but pure copper has a high specific gravity (8.92 g / cm 3 ) and a busbar. It is difficult to store and install, and it takes a lot of installation time, which is a factor that increases the overall production cost and installation cost.

이러한 문제점을 해결하기 위해 최근에는 원가를 절감하고 무게를 줄이며, 성능을 향상시키기 위해 알루미늄 외부에 구리를 피복하여 사용하거나, 강도를 높이기 위해 철합금 외부에 구리를 피복하여 사용하는 등 복합 재질로 형성된 부스바가 나오고 있다.In order to solve these problems, in recent years, the copper material is coated on the outside of aluminum to reduce the cost, reduce the weight, and improve the performance, or the copper is coated on the outside of the iron alloy to increase the strength. Busbars are coming out.

이러한 구리 피복 복합재로 형성된 부스바는 클래드(clad) 접합방법과 정수압 압출법(Hydrostatic Extrusion) 및 간접 압출법에 의해 제조되게 되는데, 클래드 접합방법은 두 가지 이상의 금속재료를 고온에서 압연하여 접합이 이루어지도록 하는 것이고, 정수압 압출법(Hydrostatic Extrusion) 및 간접 압출법은 소정 형태의 빌렛을 압출 콘테이너에 삽입하여 층상 복합 재질로 형성된 부스바를 제조할 수 있도록 하는 것이다.The busbar formed of the copper clad composite is manufactured by clad bonding method, hydrostatic extrusion method and indirect extrusion method. Clad bonding method is formed by rolling two or more metal materials at a high temperature. Hydrostatic Extrusion and Indirect Extrusion may be performed by inserting a billet of a predetermined type into an extrusion container to manufacture a busbar formed of a layered composite material.

그러나 상기 클래드 접합에 의한 압연 방법은 일반적으로 고온에서 이루어지게 되는데, 구리, 철 등의 금속재료는 200℃ 이하의 낮은 온도에서 산화가 이루어 지거나 각각의 금속재료들 간에 열팽창률이 상이하여 접합이 제대로 이루어지지 않아 불량품을 양산하게 되며, 또한 이러한 방법은 제조공정 및 장비가 복잡하여 생산 비용이 많이 드는 문제점이 있다.However, the method of rolling by cladding is generally made at a high temperature. Metal materials such as copper and iron are oxidized at a low temperature of 200 ° C. or lower, or the thermal expansion coefficients of the metal materials are different so that the bonding is performed properly. It is not made to produce a defective product, and this method also has a problem that the production process and equipment is complicated and the production cost is high.

또한, 정수압압출방법은 압력전달용매의 취급이 용이하지 않으며, 간접압출방법과 함께 압출장치가 대형이고 고가이며 유지 보수 비용이 많이 들며, 사용 방법이 복잡하여 작업의 효율성이 떨어져, 부스바의 단가를 상승시키는 요인이 되고 있다.In addition, the hydrostatic extrusion method is not easy to handle the pressure transfer solvent, and in addition to the indirect extrusion method, the extrusion apparatus is large, expensive, expensive to maintain, and complicated to use, resulting in inefficient work efficiency. It is becoming a factor to raise.

본 발명은 상기 문제점을 해결하기 위해 안출된 것으로서, 피복재 내부에 형성된 중심재를 폭발 확관에 의해 피복재 내면에 용접함으로써 제조공정의 단순화 및 비용을 절감시키는 폭발 확관에 의한 복합 부스바 제조방법의 제공을 목적으로 한다.The present invention has been made to solve the above problems, by providing a method for manufacturing a composite busbar by explosion expansion to simplify the manufacturing process and reduce the cost by welding the core material formed inside the coating material to the inner surface of the coating material by explosion expansion. The purpose.

상술한 바와 같은 목적 달성을 위해 본 발명은, 중공형의 피복재 내부에 상기 피복재보다 상대적으로 내경이 작은 중심재를 삽입시키고, 상기 중심재 내부에 도폭선을 위치시킨 후, 상기 중심재를 확관 폭발시켜 상기 피복재 내면에 상기 중심재를 용접시키는 것을 특징으로 하는 폭발 확관에 의한 복합 부스바 제조방법을 기술적 요지로 한다.In order to achieve the object as described above, the present invention, by inserting a central material having a relatively smaller inner diameter than the coating material inside the hollow coating material, by placing a dopant line inside the central material, by expanding the explosion of the center material The manufacturing method of the composite busbar by explosion expansion characterized by welding the said central material to the said inner surface of the said coating material is a technical subject matter.

또한, 상기 피복재는 구리, 상기 중심재는 알루미늄으로 형성된 구리-알루미늄 복합 부스바로 제공되거나, 상기 피복재는 알루미늄, 상기 중심재는 구리인 알 루미늄-구리 부스바로 제공되는 것이 바람직하다.In addition, it is preferable that the coating material is provided as a copper-aluminum composite busbar formed of copper, and the core material is made of aluminum, or the coating material is provided as an aluminum-copper busbar which is aluminum and the core material is copper.

여기에서, 상기 중심재는, 서로 다른 두 가지 이상의 금속이 상기 도폭선을 중심으로 동축형성될 수도 있으며, 용도 및 목적에 따라 상기 피복재에 접하는 알루미늄 및 구리, 상기 피복재에 접하는 알루미늄 합금 및 구리, 상기 피복재에 접하는 철 및 구리, 상기 피복재에 접하는 철합금 및 구리 중 어느 하나인 것이 바람직하다.Here, the central material, two or more different metals may be coaxially formed around the dopant line, and aluminum and copper in contact with the coating material, aluminum alloy and copper in contact with the coating material, and the coating material depending on the purpose and purpose. It is preferable that it is any of iron and copper which contact | connect, and an iron alloy and copper which contact | connect the said coating material.

또한, 상기 폭발 확관에 의한 복합 부스바는 중공형 또는 압연에 의해 평판형으로 가공되는 것이 바람직하다.In addition, it is preferable that the composite bus bar by the explosion expansion is processed into a flat shape by hollow or rolling.

이에 따라 피복재 내부에 형성된 중심재를 폭발 확관에 의해 피복재 내면에 용접함으로써 제조공정 및 제조장비의 단순화 및 생산비용을 절감시키며 중심재 전체에 걸쳐 균일한 힘으로 일정하게 확관시킴으로써 제품의 불량률을 최소화하여 대전류 시스템에서의 오작동없이 효율적으로 사용할 수 있는 이점이 있다.Therefore, by welding the core material formed inside the cladding to the inner surface of the cladding by explosion expansion, it simplifies the manufacturing process and manufacturing equipment and reduces the production cost. The advantage is that it can be used efficiently without malfunction in large current systems.

이하에서는 본 발명의 바람직한 실시예를 첨부된 도면을 참조하여 상세히 설명하고자 한다. 도 1은 본 발명에 따른 폭발 확관에 의한 복합 부스바 제조방법에 대한 모식도((a)폭발 확관 전, (b)폭발 확관 후), 도 2는 본 발명에 따른 폭발 확관에 의한 복합 부스바가 중공형으로 형성된 경우에 대한 사시도이며, 도 3은 본 발명에 따른 폭발 확관에 의한 복합 부스바가 평판형으로 형성된 경우에 대한 사시도이다.Hereinafter, with reference to the accompanying drawings, preferred embodiments of the present invention will be described in detail. 1 is a schematic diagram of a method for manufacturing a composite busbar by explosion expansion according to the present invention ((a) before explosion expansion, (b) after expansion expansion), Figure 2 is a composite busbar hollow by explosion expansion according to the present invention 3 is a perspective view of a case formed in a mold, and FIG. 3 is a perspective view of a case in which a composite bus bar is formed in a flat form by explosion expansion according to the present invention.

도 1에 도시된 바와 같이 본 발명에 따른 폭발 확관에 의한 복합 부스바 제 조방법은 중공형의 피복재(100) 내부에 상기 피복재(100)보다 상대적으로 내경이 작은 중심재(200)를 삽입시키고, 상기 중심재(200) 내부에 도폭선(300)을 위치시킨 후 상기 도폭선(300)을 점화시킴으로써(도 1(a)), 상기 도폭선(300)의 폭발에 의해 중심재(200)가 순간적으로 확관됨으로써 상기 피복재(100) 내면에 중심재(200) 외면이 고온 용접(도 1(b))되면서 중공형의 부스바가 완성되게 되는 것이다. 상기 중심재(200)의 폭발 확관에 사용되는 도폭선(300)은 고 에너지 폭약을 아주 가느다란 금속관에 넣은 와이어(explosion wire)로 중심재(200)의 길이와 동일하거나 좀 더 길게 형성되며, 중심재(200)의 중앙에 놓여지게 된다. 여기에서 더욱 균일한 확관을 위해 상기 도폭선(300)과 중심재(200) 사이에 완충재를 더 넣을 수도 있다.As shown in FIG. 1, the method for manufacturing a composite busbar by explosion expansion according to the present invention inserts a central material 200 having a smaller inner diameter than the coating material 100 into a hollow covering material 100. By placing the dopant line 300 in the center member 200 and igniting the dopant line 300 (FIG. 1 (a)), the center member 200 is instantaneously caused by the explosion of the dopant line 300. By expanding the outer surface of the core material 200 to the inner surface of the coating material 100 is a high-temperature welding (Fig. 1 (b)) is to complete the hollow busbar. The explosive wire 300 used to expand the explosion of the central material 200 is a wire (explosion wire) in a very thin metal tube with a high energy explosive is formed the same or longer than the length of the central material 200, the center It is placed in the center of the ash (200). Here, the buffer member may be further inserted between the dopant line 300 and the center member 200 for a more uniform expansion.

상기 도폭선(300)의 점화에 의해 도폭선이 터지면서 그 충격파에 의한 충격력에 의해 고온을 발생시키면서 상기 중심재(200)가 순간적으로 확관되어 상기 피복재(100) 내면에 용접되게 되며, 양단부의 가공 및 절단에 의해 중공형의 복합 부스바가 완성되는 것이다.The core material 200 is instantaneously expanded and welded to the inner surface of the coating material 100 while generating the high temperature by the impact force caused by the shock wave while the dopant wire is burst by the ignition of the dopant wire 300. Hollow composite busbars are completed by cutting.

이에 의해 중공형의 피복재(100) 및 그 내부에 삽입된 중공형의 중심재(200) 그리고 그 내부에 위치되는 도폭선(300)의 점화에 의해 단시간의 균일한 폭발 확관에 의해 중심재(200)의 피복재(100)에의 용접이 이루어져 부스바의 비용절감 및 공정의 획기적인 단순화를 가져오게 된다.As a result, the core member 200 is formed by uniform explosion expansion in a short time by ignition of the hollow covering member 100, the hollow central member 200 inserted therein, and the dopant line 300 positioned therein. Welding to the cladding material 100 is brought to reduce the cost of the busbar and significantly simplify the process.

여기에서 상기 피복재(100)는 전기전도도 및 기계적 특성이 우수한 구리가 사용되며, 상기 중심재(200)는 비용절감 및 가공의 편이를 위해 알루미늄을 사용하여 중공형의 구리-알루미늄 복합 부스바를 제조하거나, 또한 상기 피복재로써 알루 미늄, 중심재(200)로써 구리를 사용하여 중공형의 알루미늄-구리 복합 부스바를 제조하게 된다.In this case, the coating material 100 is made of copper having excellent electrical conductivity and mechanical properties, and the core material 200 may be manufactured of a hollow copper-aluminum composite bus bar using aluminum for cost reduction and easy processing. In addition, a hollow aluminum-copper composite busbar is manufactured using aluminum as the coating material and copper as the center material 200.

일반적으로 구리의 산화가 공기 중에서 쉽게 일어나므로 지하실 등의 습한 장소에서 부스바를 사용할 경우에는 피복재(100)가 알루미늄으로 형성된 알루미늄-구리 복합 부스바의 사용이 바람직하다. 이는 알루미늄을 피복재(100)로 사용함으로써 알루미늄 산화막에 의해 구리의 산화를 방지할 수 있어 내식성이 우수한 부스바를 공급할 수 있게 되는 것이다.In general, since the oxidation of copper easily occurs in the air, when the bus bar is used in a humid place such as a basement, it is preferable to use an aluminum-copper composite bus bar in which the coating material 100 is made of aluminum. This can prevent the oxidation of copper by the aluminum oxide film by using aluminum as a coating material 100, it is possible to supply a bus bar excellent in corrosion resistance.

또한 부스바 사용 시스템의 전류 용량 및 사용하는 동안에 견뎌야 하는 기계적 강도 등을 고려하여 상기 중심재(200)를 둘 이상의 금속재로 형성시킬 수 있다. 바람직하게는 상기 중심재(200)가 상기 피복재(100)에서부터 순서대로 알루미늄 및 구리, 또는 알루미늄 합금 및 구리, 또는 철 및 구리, 또는 철합금 및 구리 중 어느 하나를 선택하여 사용할 수 있으며, 용도 및 목적에 따라 이러한 순서대로 또는 혼합하여 중심재(200)를 다수개 형성시켜도 무방하다.In addition, the core material 200 may be formed of two or more metal materials in consideration of the current capacity of the bus bar using system and the mechanical strength to withstand during use. Preferably, the core member 200 may be used to select any one of aluminum and copper, aluminum alloy and copper, or iron and copper, or iron alloy and copper in order from the coating member 100. Depending on the purpose, a plurality of the center material 200 may be formed in this order or mixed.

상기 폭발 확관법에 의해 제조된 부스바는 도 2에 도시된 바와 같이 두 가지 이상의 복합재료를 가지게 되며, 그 형상은 원통의 중공형을 띄게 된다. 사용처 및 목적에 따라 도 3에 도시된 바와 같이 이러한 중공형의 부스바에 압연 공정을 수행함으로써 평판형의 부스바의 형상으로도 가공이 가능하게 된다.The busbar manufactured by the explosion expanding method has two or more composite materials as shown in FIG. 2, and the shape of the busbar is cylindrical. According to the purpose and purpose of use, as shown in FIG. 3, the hollow bus bar may be subjected to a rolling process to form a flat bus bar.

상기 구성에 의한 본 발명은, 피복재 내부에 형성된 중심재를 폭발 확관에 의해 피복재 내면에 용접함으로써 제조공정 및 제조장비의 단순화 및 생산비용을 절감시키며 중심재 전체에 걸쳐 균일한 힘으로 일정하게 확관시킴으로써 제품의 불량률을 최소화하여 대전류 시스템에서의 오작동없이 효율적으로 사용할 수 있는 효과가 있다.The present invention by the above configuration, by welding the core material formed inside the coating material to the inner surface of the coating material by explosion expansion, simplifying the manufacturing process and manufacturing equipment and reducing the production cost and by uniformly expanding the uniform material throughout the core material By minimizing the defective rate of the product, there is an effect that can be used efficiently without malfunction in the high current system.

Claims (6)

중공형의 피복재 내부에 상기 피복재보다 상대적으로 내경이 작은 중심재를 삽입시키고, 상기 중심재 내부에 도폭선을 위치시킨 후, 상기 중심재를 확관 폭발시켜 상기 피복재 내면에 상기 중심재를 용접시키는 것을 특징으로 하는 폭발 확관에 의한 복합 부스바 제조방법.Inserting a central material having a smaller inner diameter than the coating material inside the hollow coating material, placing a dopant line in the interior of the core material, and expanding the explosion of the central material to weld the central material to the inner surface of the coating material. Composite busbar manufacturing method by explosion expansion. 제 1항에 있어서, 상기 피복재는 구리, 상기 중심재는 알루미늄인 것을 특징으로 하는 폭발 확관에 의한 복합 부스바 제조방법.The method of claim 1, wherein the coating material is copper, and the center material is aluminum. 제 1항에 있어서, 상기 피복재는 알루미늄, 상기 중심재는 구리인 것을 특징으로 하는 폭발 확관에 의한 복합 부스바 제조방법.The method of claim 1, wherein the coating material is aluminum, and the core material is copper. 제 1항에 있어서, 상기 중심재는,The method of claim 1, wherein the central material, 서로 다른 두 가지 이상의 금속이 상기 도폭선을 중심으로 동축형성된 것을 특징으로 하는 폭발 확관에 의한 복합 부스바 제조방법.The method for manufacturing a composite busbar by explosion expansion, characterized in that two or more different metals are coaxially formed about the dopant line. 제 4항에 있어서, 상기 중심재는,The method of claim 4, wherein the center material, 상기 피복재에 접하는 알루미늄 및 구리, 상기 피복재에 접하는 알루미늄 합금 및 구리, 상기 피복재에 접하는 철 및 구리, 상기 피복재에 접하는 철합금 및 구리 중 어느 하나인 것을 특징으로 하는 폭발 확관에 의한 복합 부스바 제조방법.Aluminum and copper in contact with the coating material, aluminum alloy and copper in contact with the coating material, iron and copper in contact with the coating material, iron alloy and copper in contact with the coating material, characterized in that any one of the bus bar manufacturing method by explosion expansion. . 제 1항 내지 제 5항 중 어느 한 항에 있어서, 상기 폭발 확관에 의한 복합 부스바는 중공형 또는 압연에 의해 평판형으로 가공되는 것을 특징으로 하는 폭발 확관에 의한 복합 부스바 제조방법.The method for manufacturing a composite busbar by explosion expansion according to any one of claims 1 to 5, wherein the composite busbar by explosion expansion is processed into a flat plate by hollow or rolling.
KR1020070049109A 2007-05-21 2007-05-21 Manufacturing method of complex busbar by explosion expander KR20080102524A (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102268599B1 (en) 2021-03-26 2021-06-24 추태호 Explosive wedling system
KR102538817B1 (en) * 2022-11-08 2023-05-31 국방과학연구소 Manufacturing method of refractory metal lining tube using explosive welding

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102268599B1 (en) 2021-03-26 2021-06-24 추태호 Explosive wedling system
KR102538817B1 (en) * 2022-11-08 2023-05-31 국방과학연구소 Manufacturing method of refractory metal lining tube using explosive welding

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