CN1038182C - Composite brazing filler metal and manufacturing method thereof - Google Patents
Composite brazing filler metal and manufacturing method thereof Download PDFInfo
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- CN1038182C CN1038182C CN95118810A CN95118810A CN1038182C CN 1038182 C CN1038182 C CN 1038182C CN 95118810 A CN95118810 A CN 95118810A CN 95118810 A CN95118810 A CN 95118810A CN 1038182 C CN1038182 C CN 1038182C
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- 239000002131 composite material Substances 0.000 title claims abstract description 63
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 14
- 239000002184 metal Substances 0.000 title abstract description 17
- 229910052751 metal Inorganic materials 0.000 title abstract description 17
- 238000005219 brazing Methods 0.000 title abstract description 16
- 239000000945 filler Substances 0.000 title abstract description 12
- 229910000679 solder Inorganic materials 0.000 claims abstract description 51
- 239000010410 layer Substances 0.000 claims abstract description 46
- 229910045601 alloy Inorganic materials 0.000 claims abstract description 45
- 239000000956 alloy Substances 0.000 claims abstract description 45
- 238000000034 method Methods 0.000 claims abstract description 20
- 238000005096 rolling process Methods 0.000 claims abstract description 20
- 238000010438 heat treatment Methods 0.000 claims abstract description 11
- 238000009792 diffusion process Methods 0.000 claims abstract description 9
- 238000003466 welding Methods 0.000 claims abstract description 9
- 239000012792 core layer Substances 0.000 claims abstract description 5
- 238000005476 soldering Methods 0.000 claims description 51
- 229910000906 Bronze Inorganic materials 0.000 claims description 27
- 239000002253 acid Substances 0.000 claims description 27
- 239000000203 mixture Substances 0.000 claims description 21
- 239000000463 material Substances 0.000 claims description 17
- 238000003801 milling Methods 0.000 claims description 6
- 238000004140 cleaning Methods 0.000 claims description 2
- 238000009413 insulation Methods 0.000 claims description 2
- 239000000126 substance Substances 0.000 claims description 2
- 239000010949 copper Substances 0.000 abstract description 29
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical group [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 abstract description 20
- 229910052802 copper Inorganic materials 0.000 abstract description 18
- 229910000831 Steel Inorganic materials 0.000 abstract description 8
- 239000010959 steel Substances 0.000 abstract description 8
- 229910000881 Cu alloy Inorganic materials 0.000 abstract description 3
- 238000010923 batch production Methods 0.000 abstract description 2
- 238000013329 compounding Methods 0.000 abstract 2
- 238000010276 construction Methods 0.000 abstract 1
- 238000005275 alloying Methods 0.000 description 6
- 238000010008 shearing Methods 0.000 description 6
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 4
- 230000000052 comparative effect Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 229910001316 Ag alloy Inorganic materials 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
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Abstract
The utility model provides a composite solder comprises three layer construction, and two outer strata are a silver solder alloy 1, characterized by: the core layer is a copper-based alloy 2, and comprises the following components in percentage by weight: 1.0-3.0 parts of Mn1.0, and the balance of Cu. The copper alloy can also be optionally added with Ni with the weight percentage of 0.5-1.0, Zn with one or two of the weight percentages of 0.5-1.0, and the weight percentage of the sum of the two is 1.0-1.5. The manufacturing method of the composite solder comprises the steps of three-layer rolling and compounding, diffusion welding heat treatment between compounding surfaces, and finally finish rolling to the thickness of 0.3mm to obtain a finished product. The composite brazing filler metal is mainly used for brazing hard alloy/steel workpieces, and the joint of the composite brazing filler metal has high shear strength and good impact resistance. The composite solder has simple manufacturing method, less working procedures and lower manufacturing cost, and is suitable for continuous batch production.
Description
The present invention relates to carbide alloy and drill rod and connect and use composite soldering, particularly accompany the formation and the manufacture method thereof of three layers of composite soldering band of sandwich layer between silver solder alloy.
Carbide alloy and drill rod meet area 〉=10 * 10mm
2The soldering occasion, during with common solder alloy soldering, because the linear expansion coefficient of carbide alloy and steel is widely different, in the cooling procedure, steel can produce obvious contraction behind the pricker, and that carbide alloy shrinks is very little.The result, not to be torn by the part brazing filler metal intensity is descended owing to solder layer, make carbide alloy produce be full of cracks exactly, in order to eliminate this stress rupture phenomenon that carbide alloy and drill rod postwelding are produced, in existing technology, using a kind of silver solder/copper/silver solder three shape composite soldering layer by layer, the spy opens the manufacture method that clear 63-44476 discloses a kind of like this composite soldering, promptly thick at 2mm, 130mm is wide, the long silver solder alloy plate of 500mm is electroplated last layer 5 μ m copper by middle copper coin one side, thick sandwiching a 4mm between these two blocks of silver solder plates then, 130mm, the copper coin that wide 500mm is long, after 500 ℃ of heating, with 5.0 tons/cm
2Pressure compacting, obtain the composite plate blank, and then be rolled into the composite soldering band of thickness 0.30mm, during soldering, intermediate layer copper does not melt, behind pricker in the cooling procedure, copper will behind the pricker since two kinds partially absorbed because of the stress that coefficient of expansion greatest differences is produced by brazing metal, thereby improve a brazing filler metal intensity and eliminate the carbide alloy cracking phenomena.This class composite soldering intermediate layer fine copper matter is soft, the plasticity height can absorb residual stress behind the pricker, still well, in practicality, find, be subjected to destroy all vestiges of visible copper of incision position, promptly at middle copper damage layer under high shear force and the greater impact load at pricker spare, moreover, in the mill since the resistance of deformation of sandwich layer copper well below the resistance of deformation of silver solder, manufacturing process's complexity of material, cost is higher.
The spy opens clear 56-165587 and also discloses a kind of compound silver solder, its version mainly contains two kinds, a kind of is cylindrical two-layer composite soldering, its internal layer is a silver-base alloy, its skin is an acid bronze alloy, another kind of form is a three ply board formula structure composite soldering, and its sandwich layer is a silver-base alloy, and its two skin is an acid bronze alloy.But this composite soldering core alloys and outer layer alloys when soldering melt simultaneously, form brazing filler metal alloy after the alloying, thereby are not suitable for brazing filler metal area 〉=10 * 10mm
2Carbide alloy and the brazing filler metal of steel.
Purpose of the present invention, be to overcome the shortcoming of prior art, a kind of improved composite soldering is provided, with the member of soldering carbide alloy and steel effectively, use composite soldering of the present invention, both can partially absorb effectively after the soldering because two kinds of stress that produced because of coefficient of expansion greatest differences by brazing metal, can improve the intensity of brazing filler metal head again, shearing strength particularly, the shock resistance of joint is better than fine copper core goods.
Technical scheme of the present invention is, opens the spy on the basis of clear 63-44476, changes the composition of sandwich layer, is about to sandwich layer and changes a kind of acid bronze alloy into by fine copper.
Composite soldering of the present invention is made up of three-decker, and its two skin is a kind of prior art silver solder alloy 1, and its composition and percentage by weight thereof are: Ag48～50, Cu18.0～28.0, Zn20.0～21.0, Mn2.0～8.0, Ni0.3～5.0, its fusion temperature are 670～690 ℃; Feature of the present invention is: the sandwich layer of said composite soldering is a kind of acid bronze alloy 2, its composition and percentage by weight thereof are Mn1.0～3.0, the Cu surplus, and silver solder layer and core layer thickness ratio, be the silver solder layer: sandwich layer: silver solder layer=1: (1.5～2.0): 1, composite soldering band gross thickness is 0.3 ± 0.05mm; In said acid bronze alloy, also can select to add Ni; Its percentage by weight is 0.5～1.0 and Zn; Its percentage by weight is one or both in 0.5～1.0, and the percentage by weight of sum of the two is 1.0～1.5.
The manufacture method of composite soldering of the present invention comprises the three-decker composite rolling, and Diffusion Welding heat treatment subsequently and last finish rolling, it is characterized in that having following operation:
A, by the design sandwich layer acid bronze alloy 2 compositions make sheet material a slice that 1.0～4.0mm is thick, 100～150mm is wide in advance;
B, make two of the sheet materials that 0.5～2.0mm is thick, 100～150mm is wide in advance by two outer silver solder alloy 1 compositions of design;
C, usefulness machinery or chemical method cleaning process A and the prepared sheet material of B, and under 400～600 ℃ of temperature, annealed 2～4 hours;
D, will be stacked together through pretreated silver solder alloy and acid bronze alloy sheet material, the acid bronze alloy sheet is clipped between the two silver solder alloy sheets, three's same length, the milling train of then it being sent into gross pressure and be 300～350 tons carries out composite rolling, obtains the composite soldering base band of three-decker;
E, with the prepared composite soldering base of step D band 300～550 ℃ of down insulations 4～12 hours, carry out Diffusion Welding heat treatment between composite surface, composite surface is combined into one securely;
F, finish rolling will be arrived needed thickness 0.3mm through the composite soldering base band finish rolling of operation E;
G, adopt above-mentioned manufacture method, can obtain different silver solder layers and core layer thickness ratio, i.e. the silver solder layer: sandwich layer: silver solder layer=1: (1.5～2.0) in design in advance: 1, and composite soldering band gross thickness is 0.3 ± 0.05mm.
Compare with prior art, composite soldering of the present invention and manufacture method thereof have following advantage:
1. copper alloy sandwich layer in pricker joint is because soft relatively, HB≤85, and there is the stress 50～65% between carbide alloy and steel faying face in absorption of residual effectively, and its effect is suitable with fine copper;
2. use composite soldering of the present invention, when soldering YG8 carbide alloy and 65Mn steel, its joint shearing strength can reach 200～250MPa, improves 5～32% than the similar product of fine copper core structure is brilliant, and the capacity of resisting impact load of joint has also had obvious improvement;
3. manufacture method is simple, and operation is few, and manufacturing cost is lower, is particularly suitable for continuous batch production.
Description of drawings:
Fig. 1 is the structural representation of composite soldering of the present invention, and wherein 1 is the silver solder alloy, the 2nd, and the sandwich layer acid bronze alloy.
Prepare two of the silver solder sheet alloys of thick 1.0mm, wide 120mm by the known technology method with the alloying element of purity 〉=99.9%, acid bronze alloy sheet material a slice of thick 2.0mm, wide 120mm, silver solder alloying component and percentage by weight thereof are: Ag49, Cu27.0, Zn20.0, Mn3.0, Ni1.0; Acid bronze alloy composition and percentage by weight thereof are: Mn2.0, Ni0.5, the Cu surplus, with the above-mentioned sheet material of alcohol wash, and under 550 ℃, annealed 2 hours, to stack through the sheet metal layer of above-mentioned processing, copper base alloy plate is clipped between the two silver solder alloy sheets, three's length is identical, then it is sent into milling train and carry out composite rolling under 300 tons of pressure, obtains the composite soldering base band of three-decker, solder base band is incubated 5 hours down at 400 ℃, carry out Diffusion Welding heat treatment, and then finish rolling is thick to 0.3mm, composite soldering gets product.
Prepare two of the silver solder sheet alloys of thick 1.5mm, wide 120mm with the alloying element of purity 〉=99.9% by the known technology method, acid bronze alloy sheet material a slice of thick 3.0mm, wide 120mm, the composition of silver solder alloy and percentage by weight are identical with embodiment 1; Acid bronze alloy composition and percentage by weight thereof are: Mn3.0, Zn0.5, the Cu surplus, with the above-mentioned sheet material of alcohol wash, and under 600 ℃, annealed 3 hours, to stack through the sheet metal layer of above-mentioned processing, copper alloy plate is clipped between the two silver alloy plates, three's length is identical, then it is sent into milling train and carry out composite rolling under 350 tons of pressure, obtains the composite soldering base band of three-decker, solder base band is incubated 5 hours down at 450 ℃, carry out Diffusion Welding heat treatment, and then finish rolling is thick to 0.3mm, composite soldering gets product.
Embodiment 3
Prepare two of the silver solder sheet alloys of thick 0.5mm, wide 150mm with the alloying element of purity 〉=99.9% by the known technology method, acid bronze alloy sheet material a slice of thick 1.0mm, wide 150mm, the composition of silver solder alloy and percentage by weight are identical with embodiment 1; The percentage by weight of acid bronze alloy composition is: Mn1.0, Ni0.5, Zn0.5, the Cu surplus, with the above-mentioned sheet material of alcohol wash, and under 400 ℃, annealed 3 hours, to stack through the sheet metal layer of above-mentioned processing, copper base alloy plate is clipped between the two silver solder alloy sheets, and three's length is identical, then it is sent into milling train and under 350 tons of pressure, carry out composite rolling, obtain the composite soldering base band of three-decker, solder base band is incubated 6 hours down at 500 ℃, carry out Diffusion Welding heat treatment, and then finish rolling is thick to 0.3mm, and composite soldering gets product.
Embodiment 4
Prepare two of the silver solder sheet alloys of thick 2.0mm, wide 100mm by the known technology method with the alloying element of purity 〉=99.9%, acid bronze alloy sheet material a slice of thick 4.0mm, wide 100mm, the composition of silver solder alloy and percentage by weight thereof are identical with embodiment 1; Acid bronze alloy composition and percentage by weight thereof are: Mn2.0, Zn0.7, the Cu surplus, with the above-mentioned sheet material of alcohol wash, and under 600 ℃, annealed 4 hours, to stack through the sheet metal layer of above-mentioned processing, copper base alloy plate is clipped between the two silver solder alloy sheets, three's length is identical, then it is sent into milling train and carry out composite rolling under 350 tons of pressure, obtains the composite soldering base band of three-decker, solder base band is incubated 6 hours down at 550 ℃, carry out Diffusion Welding heat treatment, and then finish rolling is thick to 0.3mm, composite soldering gets product.
Embodiment 5
Substantially the same manner as Example 1, just the percentage by weight of acid bronze alloy composition is Mn1.0, Ni1.0, Cu surplus.
Embodiment 6
Substantially the same manner as Example 2, just the percentage by weight of acid bronze alloy composition is Mn1.0, Zn1.0, Cu surplus.
Embodiment 7
Substantially the same manner as Example 3, just the percentage by weight of acid bronze alloy composition is Mn1.5, Ni1.0, Zn0.5, Cu surplus.
Embodiment 8
Substantially the same manner as Example 4, just the percentage by weight of acid bronze alloy composition is Mn1.5, Ni0.5, Zn0.5, Cu surplus.
Embodiment 9
Substantially the same manner as Example 1, just the percentage by weight of acid bronze alloy composition is Mn3.0, the Cu surplus.
Composite soldering (Comparative Examples 1) with above-mentioned composite soldering of the present invention and silver solder/copper/silver solder structure adopts high-frequency induction heating soldering YB8 carbide alloy/65Mn steel workpiece down at 730 ℃, on workpiece, survey the shearing strength of its brazing filler metal head then, and compare, its result is as shown in table 1, as seen from Table 1, the shearing strength of the brazing filler metal head of composite soldering of the present invention on average improves 5～32% than the shearing strength of fine copper sandwich layer composite soldering brazing filler metal head.
Table 1
Specimen coding shearing strength (MPa)
Embodiment 3 250
Embodiment 4 240
Embodiment 5 230
Embodiment 6 200
Embodiment 7 235
Embodiment 8 250
Embodiment 9 245
Comparative Examples 1 190
Claims (3)
1. composite soldering, form by three-decker, its two skin is a kind of prior art silver solder alloy (1), its composition and percentage by weight thereof are: Ag48～50, Cu18.0～28.0, Zn20.0～21.0, Mn2.0～8.0, Ni0.3～5.0, feature of the present invention is: the sandwich layer of said composite soldering is a kind of acid bronze alloy (2), and its composition and percentage by weight thereof are: Mn1.0～3.0, the Cu surplus, and silver solder layer and core layer thickness ratio, i.e. silver solder layer: sandwich layer: silver solder layer=1: (1.5～2.0): 1, composite soldering band gross thickness is 0.3 ± 0.05mm.
2. according to the composite soldering of claim 1, it is characterized in that also selecting to add Ni in the said sandwich layer acid bronze alloy: its percentage by weight is 0.5～1.0 and Zn: its percentage by weight is one or both in 0.5～1.0, and the percentage by weight of sum of the two is 1.0～1.5.
3. the manufacture method of a composite soldering comprises the three-decker composite rolling, and Diffusion Welding heat treatment subsequently and last finish rolling, it is characterized in that having following operation:
A, by the design sandwich layer acid bronze alloy (2) composition make sheet material a slice that 1.0～4.0mm is thick, 100～150mm is wide in advance;
B, make two of the sheet materials that 0.5～2.0mm is thick, 100～150mm is wide in advance by two outer silver solder alloy (1) compositions of design;
C, usefulness machinery or chemical method cleaning process A and the prepared sheet material of B, and under 400～600 ℃ of temperature, annealed 2～4 hours;
D, will be stacked together through pretreated silver solder alloy and acid bronze alloy sheet material, the acid bronze alloy sheet is clipped between the two silver solder alloy sheets, three's same length, the milling train of then it being sent into gross pressure and be 300～350 tons carries out composite rolling, obtains the composite soldering base band of three-decker;
E, with the prepared composite soldering base of step D band 300～550 ℃ of down insulations 4～12 hours, carry out Diffusion Welding heat treatment between composite surface, composite surface is combined into one securely;
F, finish rolling will be arrived needed thickness 0.3mm through the composite soldering base band finish rolling of operation E;
G, adopt above-mentioned manufacture method, can obtain different solder layers and core layer thickness ratio, i.e. solder layer: sandwich layer: solder layer=1: (1.5～2.0) in design in advance: 1, and composite soldering band gross thickness is 0.3 ± 0.05mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN95118810A CN1038182C (en) | 1995-12-27 | 1995-12-27 | Composite brazing filler metal and manufacturing method thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN95118810A CN1038182C (en) | 1995-12-27 | 1995-12-27 | Composite brazing filler metal and manufacturing method thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1136488A CN1136488A (en) | 1996-11-27 |
| CN1038182C true CN1038182C (en) | 1998-04-29 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN95118810A Expired - Fee Related CN1038182C (en) | 1995-12-27 | 1995-12-27 | Composite brazing filler metal and manufacturing method thereof |
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| Country | Link |
|---|---|
| CN (1) | CN1038182C (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100513038C (en) * | 2000-05-02 | 2009-07-15 | 约翰斯霍普金斯大学 | Composite reactive multilayer foil |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106271202B (en) * | 2016-08-30 | 2018-12-11 | 北京有色金属与稀土应用研究所 | A kind of composite brazing material and preparation method thereof |
| JP6852784B2 (en) * | 2017-03-16 | 2021-03-31 | 三菱電機株式会社 | Plate-shaped solder manufacturing equipment and its manufacturing method |
| KR102335720B1 (en) * | 2017-03-27 | 2021-12-07 | 삼성전자주식회사 | Metal unit for smd and electric device with the same |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2362893A (en) * | 1942-04-04 | 1944-11-14 | Metals & Controls Corp | Solder |
| JP4210869B2 (en) * | 2007-08-28 | 2009-01-21 | アイシン・エィ・ダブリュ株式会社 | NAVIGATION DEVICE, PROGRAM FOR THE DEVICE, AND RECORDING MEDIUM |
-
1995
- 1995-12-27 CN CN95118810A patent/CN1038182C/en not_active Expired - Fee Related
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2362893A (en) * | 1942-04-04 | 1944-11-14 | Metals & Controls Corp | Solder |
| JP4210869B2 (en) * | 2007-08-28 | 2009-01-21 | アイシン・エィ・ダブリュ株式会社 | NAVIGATION DEVICE, PROGRAM FOR THE DEVICE, AND RECORDING MEDIUM |
Non-Patent Citations (1)
| Title |
|---|
| 焊接方法及设备第四分册，北京第一版 1981.7.1 邹僖，魏月贞 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100513038C (en) * | 2000-05-02 | 2009-07-15 | 约翰斯霍普金斯大学 | Composite reactive multilayer foil |
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| Publication number | Publication date |
|---|---|
| CN1136488A (en) | 1996-11-27 |
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