CN114083240A - Welding method for two-body conductive block - Google Patents
Welding method for two-body conductive block Download PDFInfo
- Publication number
- CN114083240A CN114083240A CN202111427679.9A CN202111427679A CN114083240A CN 114083240 A CN114083240 A CN 114083240A CN 202111427679 A CN202111427679 A CN 202111427679A CN 114083240 A CN114083240 A CN 114083240A
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- CN
- China
- Prior art keywords
- connecting end
- welding
- conductive block
- beryllium bronze
- phi
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 238000003466 welding Methods 0.000 title claims abstract description 32
- 238000000034 method Methods 0.000 title claims abstract description 13
- 239000000463 material Substances 0.000 claims abstract description 25
- 229910000906 Bronze Inorganic materials 0.000 claims abstract description 18
- 229910052790 beryllium Inorganic materials 0.000 claims abstract description 18
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 claims abstract description 18
- 239000010974 bronze Substances 0.000 claims abstract description 18
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 claims abstract description 18
- 238000005553 drilling Methods 0.000 claims abstract description 13
- 230000004907 flux Effects 0.000 claims abstract description 10
- 238000005219 brazing Methods 0.000 claims abstract description 9
- 238000003801 milling Methods 0.000 claims abstract description 8
- 230000007935 neutral effect Effects 0.000 claims abstract description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 abstract description 6
- 239000010949 copper Substances 0.000 abstract description 6
- 229910052802 copper Inorganic materials 0.000 abstract description 6
- 238000005516 engineering process Methods 0.000 description 3
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Arc Welding In General (AREA)
Abstract
A method for welding two conductive blocks comprises the following steps: firstly, selecting a beryllium bronze material with phi 11, then processing the beryllium bronze material into a thread with the size of M8, selecting a material with enough allowance, and milling a connecting end with the size of 1.5 flat to obtain the connecting end; secondly, selecting a beryllium bronze material with phi 24, and drilling an M8 threaded hole with the depth of 8mm in the center of the beryllium bronze material to obtain a main body of the conductive block; thirdly, screwing the connecting end into the main body of the conductive block to obtain a conductive block combination; fourthly, drilling an exhaust hole with the diameter of phi 2mm at one end of the conductive block combination, wherein the drilling depth is 12mm to the neutral size of the connecting end; then brazing is carried out through the welding flux, and the welding flux flows in from the milling flat side of the connecting end and is fully fused with the two conductive blocks; fifthly, removing the allowance and the welding beading of the connecting end by using a lathe, and turning M8 threads. The invention effectively solves the problem that the red copper generates air holes during brazing and has good reliability. In addition, welding marks can hardly be seen after removing the welding beading, and the smoothness is good. Meanwhile, the concentricity and the verticality of the two-body welding are improved, and the product performance is guaranteed.
Description
Technical Field
The invention relates to a welding method, in particular to a welding method of two conductive blocks.
Background
A novel high-voltage contactor product is applied to the field of aviation. Therefore, strict requirements are imposed on the dimensions and performance of the parts. The conductive block is one of the core devices of the high-voltage contactor product, so that the conductive block has critical factors in the aspects of embodying the functions and the performances of the product. The conducting block adopts two kinds of materials of red copper and beryllium bronze to constitute, on the technique of traditional pure red copper conducting block, because the better ductility characteristic of red copper leads to conducting block link torque value to be not enough to satisfy the requirement of novel high voltage contactor product, so adopt beryllium bronze QBe 2's material to make the link, satisfy the new maximum torque value of development needs. Because red copper has good thermal conductivity, pores are easily caused during flame brazing, and the product performance is directly influenced. In the traditional welding technology, the stability and concentricity of two-body welding are poor, and the method is not suitable for the aviation field. In order to solve the above problems, the present invention relates to a design and application of two-body conductive block welding technology.
Disclosure of Invention
The invention aims to solve the technical problems that hydrogen embrittlement phenomenon is generated during welding of two conductive blocks to cause air leakage at the welding position, and meanwhile, the high temperature generated by brazing causes deformation of the conductive blocks, so that the concentricity and the verticality of the two conductive blocks cannot meet the product requirements.
In order to solve the technical problems, the invention adopts the following technical scheme:
a method for welding two conductive blocks comprises the following steps:
the method comprises the following steps: selecting a beryllium bronze material with phi 11, then processing the beryllium bronze material into a thread with the size of M8, selecting a material with enough allowance, and milling a flat material with the size of 1.5 to obtain a connecting end;
step two: selecting a beryllium bronze material with phi 24, and drilling an M8 threaded hole with the depth of 8mm in the center of the beryllium bronze material to obtain a main body of the conductive block;
step three: screwing the connecting end obtained in the first step into the conductive block main body obtained in the second step to obtain a conductive block combination;
step four: drilling an exhaust hole with the diameter of phi 2mm at one end of the conductive block combination obtained in the step three, wherein the drilling depth is 12mm to the neutral size of the connecting end; then brazing is carried out through the welding flux, the welding flux flows in from the milling flat side of the connecting end and is fully fused with the two conductive blocks to form a fixing pin;
step five: and (5) removing connecting end allowance and welding beading by using a lathe for secondary processing, and turning M8 threads.
The beneficial effect of adopting above-mentioned technical scheme is:
1. the invention adopts the modes of anti-loosening and anti-skid double locking and secondary finish machining to solve the problem of complaint, thereby meeting the design requirement of products.
2. The invention effectively solves the problem of hydrogen embrittlement of red copper during brazing, improves the concentricity and stability of the two bodies by at least 5% in the two-body welding technology, and has good reliability in the aviation field because the two bodies are direct factors influencing the product performance and the service life. In addition, on the appearance of the component, welding marks can not be seen after the welding beading is removed, and the component has good smoothness and good performance.
Drawings
Fig. 1 is a schematic view of the connecting end structure of the present invention.
Fig. 2 is a bottom view of fig. 1.
FIG. 3 is a schematic diagram of a main structure of the conductive block of the present invention.
Fig. 4 is a schematic diagram of the connection end and the conductive block main body after being combined.
Fig. 5 is a schematic view of welding the connecting end and the conductive block main body.
FIG. 6 is a schematic view of the connection end welded to the conductive block main body.
Detailed Description
The invention is described in further detail below with reference to the accompanying drawings:
the method comprises the following steps: selecting a beryllium bronze material with phi 11, and then processing the beryllium bronze material into a thread with the size of M8, wherein the reason is that the concentricity is easy to deviate when two bodies are welded, the material with enough margin is selected to ensure the concentricity of the two bodies in the post-welding process, and in addition, a flat material with the size of 1.5 is milled to ensure that the connecting end is not loosened after being screwed into the conductive block main body, so that the connecting end is obtained;
step two: selecting a beryllium bronze material with phi 24, and drilling an M8 threaded hole with the depth of 8mm in the center of the beryllium bronze material to obtain a main body of the conductive block;
step three: screwing the connecting end obtained in the first step into the conductive block main body obtained in the second step to obtain a conductive block combination;
step four: drilling an exhaust hole with the diameter of phi 2mm at one end of the conductive block combination obtained in the step three, wherein the drilling depth is 12mm to the neutral size of the connecting end, and the drilling function is to timely remove redundant bubbles during brazing so as to avoid the phenomenon of air leakage of the conductive block; in addition, after the welding flux enters the exhaust hole, a fixing pin can be formed on the main body part of the conductive block and the connecting end to play a role in fixing, and a double-loosening anti-falling connecting structure is formed by milling the fixing pin and the connecting end flatly, so that the welding flux has good reliability; then brazing is carried out through the welding flux, and the welding flux flows in from the milling flat side of the connecting end and is fully fused with the two conductive blocks;
step five: the end allowance and the flash are connected by using a lathe, and M8 threads are lathed.
Claims (1)
1. A two-body conductive block welding method is characterized in that: it comprises the following steps:
the method comprises the following steps: selecting a beryllium bronze material with phi 11, then processing the beryllium bronze material into a thread with the size of M8, selecting a material with enough allowance, and milling a flat material with the size of 1.5 to obtain a connecting end;
step two: selecting a beryllium bronze material with phi 24, and drilling an M8 threaded hole with the depth of 8mm in the center of the beryllium bronze material to obtain a main body of the conductive block;
step three: screwing the connecting end obtained in the first step into the conductive block main body obtained in the second step to obtain a conductive block combination;
step four: drilling an exhaust hole with the diameter of phi 2mm at one end of the conductive block combination obtained in the step three, wherein the drilling depth is 12mm to the neutral size of the connecting end; then brazing is carried out through the welding flux, the welding flux flows in from the milling flat side of the connecting end and is fully fused with the two conductive blocks to form a fixing pin;
step five: the end allowance and the flash are connected by using a lathe, and M8 threads are lathed.
Priority Applications (1)
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CN202111427679.9A CN114083240B (en) | 2021-11-29 | 2021-11-29 | Welding method for two-body conductive block |
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CN202111427679.9A CN114083240B (en) | 2021-11-29 | 2021-11-29 | Welding method for two-body conductive block |
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CN114083240A true CN114083240A (en) | 2022-02-25 |
CN114083240B CN114083240B (en) | 2024-03-01 |
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CN111037212A (en) * | 2019-11-26 | 2020-04-21 | 北京卫星制造厂有限公司 | Preparation method of high-volume-fraction aluminum-based silicon carbide composite material small-hole thread |
CN112170996A (en) * | 2020-09-01 | 2021-01-05 | 合肥通用机械研究院有限公司 | Welding method for butt joint of T2 red copper and S32168 stainless steel tube |
CN214350372U (en) * | 2021-02-02 | 2021-10-08 | 杭州祥博传热科技股份有限公司 | Brazed red copper radiator |
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JPH1085917A (en) * | 1996-09-09 | 1998-04-07 | Honda Motor Co Ltd | Pin as cast |
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JP2005353529A (en) * | 2004-06-14 | 2005-12-22 | Fuji Electric Holdings Co Ltd | Manufacturing method for movable contact of electromagnetic contactor |
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